GFD Flight Maneuvers Manual

i
JEPPESEN. A BOEING COMPANY
SUIDED FLIGHT DISCOV
PRIVATE
PILOT
Soe
MANEUVERS
Jeppesen® is a registered trademark of Jeppesen Sanderson, Inc. All other trademarks,
registered trademarks, product names, and company names or logos mentioned herein are
the property of their respective owners.
———
a
LT
All rights reserved. No part of this publication may be reproduced, storedin a retrieval system,
or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, or
otherwise, without the prior permission of the publisher.
The charts, tables, and graphs usedin this publication are for illustration purposes only and
cannot be used for navigation or to determine actual aircraft performance.
ISBN-13: 978-0-88487-435-5
ISBN-10: 0-88487-435-4
Jeppesen
55 Inverness Drive East
Englewood, CO 80112-5498
Website: www.jeppesen.com
Email: Captain @jeppesen.com
Copyright © Jeppesen
All Rights Reserved.
Published 1997-2007, 2011, 2012
10001361-002 Printed in the United States of America
PREFACE
All of the individual components of Jeppesen Sanderson’s Guided Flight Discovery Pilot Training
System concentrate on an application-oriented approachto pilot training. Nothing exemplifies this
philosophy more than Private Pilot Maneuvers. When usedin conjunction with the other compo-
nents of the Private Pilot Program, this manual provides an effective, practical approach to your
training. As you examine this manual, you will discover that the maneuvers are numberedfor ease
of reference and are groupedinto categories based on similar operational characteristics. While the
categories are organized to present the maneuversin the chronological orderin whichtheyare typi-
cally introduced, this does notlimit the flexibility and usability of the manual: you can study and
review the maneuversin any orderyoudesire.
Each maneuveris presented using colorful graphics, step-by-step procedure descriptions, help-
ful hints, and the associated FAApractical test standards. In addition, Private Pilot Maneuversis
designedto lay flat for ease of study and instruction, whether you are on the ground orin flight.
These, and other unique features of the manual, are explainedin further detail in the section titled
“How the Manual Works”starting on pagevi.
To help you integrate the content of this manual with the associated Private Pilot Maneuvers
Videos and CD-ROMs, a cross-reference is included at the beginning of each maneuvercate-
gory. The video and CD-ROM programsare available for your use at participating schools and
are designed to enhance and complement your study. You also can purchasethe Private Pilot
Maneuvers CD-ROMsfor self-paced homestudy. These revolutionary CD-ROMs combine video,
animation, arid interactivity to create a dynamic learning experience. When used together, the
components of the Guided Flight Discovery Private Pilot Program provide thefinest pilot training
available.
TABLE OF CONTENTS
GROUND OPERATIONS
MANEUVER 1
PREFLIGHT INSPECTION POPP PSPC PSEC O SOC e reer rrr rrerrrrrrr rrr rrr rT TTT reer ree ae
MANEUVER 2
ENGINE STARTING eccccccccccunnsenccceunccs Ceeceseceneesesseeseuccesseeseesssesss 1"O
MANEUVER 3
TAXIING ecucccesunas Seaaeeen SSeseGeGeeeeeeaeaeaaeeeeeeaeauaanane
aen Seana eaane Seseeauuannauanauna Seneenueeaeeasn 1-8
MANEUVER 4
BEFORE TAKEOFF CHECK SSR SRS REESRSREERREReeeeee eee eee eee ee Seeseeeneaes
1 - 1 Zz
MANEUVER 5
POSTFLIGHT PROCEDURES SSSS SSS SRE REE RREEE ERR RRR
eee eee eee eee 1 - ] 6
EXERCISES
GROUND OPERATIONS BESS SSR EES EBB RBRBBR BRB eeees SSeseepeeeeueeeeeaaeeaaunan
Seeaeaanaane 1-21
BASIC MANEUVERS
MANEUVER 6
STRAIGHT-AND-LEVEL PF LMT vancetecccncnsscansdcandeccecceusées
ecéscacncucue 2-2
MANEUVER 7
CLIMBS Seseeueaeeeeeaeeanauaa Seeeepepneanaaanaeaesn Saeageeeauueuaeeauaas SSSeeeee
eaaeeeaeaeneaanueun Seeenpaeaeeaeaeas 2-4
MANEUVER 8&8
DESCENTS Seeeeeeeaeeeeeneeaeauepeaanunuanesn Seeaeeeeeepeepeeeaaeeeneeaees
SSeeeeeeueeeaeaeunuuanaaa Seeaeen 2-6
MANEUVER 9
TURNS Sesaeeeeeaeeaaauan SSSeeeeeeeeeeeeeeeeepaeaeaaeunuana SSeeeeee
aeeueeeeneaeneaeeeaeeaees Sanseenea Seana aaan 2-83
EXERCISES
BASIC MANEUVERS Seaeaeageeunueean SSeseeeeeeeeeeeeeeeaa
aeaanaaua SSe@eeaeeeeeeeeecaauaan Seaseaan 2-1 3
AIRPORT OPERATIONS
MANEUVER 10
NORMAL TAKEOFF AND CLIMB aseeccccccccccccccnane pucnncccoccocccccccese ese oO"
MANEUVER 11
CROSSWIND TAKEOFF AND GLIMB oscesesess sunneucccecscsccocece sosneccess ca"
MANEUVER 12
TRAFFIC PATTERN Suceussccuncuunnccuusess secucccce eccenauccoscccus eccccscessscses o"O
MANEUVER 13
NORMAL APPROAGH AND LANDING ccceeccecccacas suanecccccucccecccucse 3-12
MANEUVER 14
CROSSWIND APPROACH AND LANDING... eeeneccnce een eeeescennesees 3-20
EXERCISES
AIRPORT OPERATIONS Sees eeeaeeeaeaaaun Seaeeeaanaana Seseeeeaeeaeueueaaeeaen sanunuscccsesa
sas"Z2a
EMERGENCY LANDING PROCEDURES

MANEUVER 15
EMERGENCY DESCENT SS SSSSSRSEREESERERSRESHERSRRERERHEKRRRRESEeeeeeeeeeee eee
eee 4-2
MANEUVER 16
EMERGENCY APPROACH AND LAN DING cocccccccccccaccccccccececccececes 4-3
EXERCISES
EMERGENCY LANDING PROCEDURES SSS SSS SSRBRRRRESSeEeeeeeeeeeeee eee ee eee 4-9
FLIGHT MANEUVERS
MANEUVER 1°77
Slow FLIGHT ecucccuuces Seana PSS SRSSSSRERERSSR EERE
e eee eee eee 5-2
MANEUVER 18
POWER-OFF STALLS SRS SSRSK RRS ee
e eee eee eee 5-4
MANEUVER 19
POWER-ON STALLS Seeeeepaeeaeunaeeeeanaan SPSSSSSSRSRR ESSERE
eee eee eee eee eee 5-8
MANEUVER 20
DEMONSTRATED STALLS SSSSHSR SSSR RESET
ee eee ee 5-1 1
MANEUVER 21
STEEP TURNS SSSSSSSSSS STEERER RST HREKERE ER
E eRe eee 5-14
EXERCISES
FLIGHT MANELVERS Seseseeeceaueenaaan BSS SERRE REESE ee
eeee eee eee 5-1 7
GROUND REFERENGE MANEUVERS

MANEUVER 22
RECTANGULAR COURSE SSSR RSE EHRHRREHEREEEEHR ERE EER eee
eee eee 6-2
MANEUVER 23
S-TURNS. Seaeeaeaunaanea SSeseaeepeeeeaeueeeeaenaanaunaueae SS
SSS BSRSSRERSERRERRERREEEHERRREeeeeeeeee eee eee
6-4
MANEUVER 24
TURNS AROUND A POINT assess BSS SSRSRSSSSRR SERRE eeeeee eee eee eee eee eee eee 6-6
EXERCISES
GROUND REFERENCE MANEUVERS esses eueeeeueee eeeeeuesennees esecessess O-F
PERFORMANGE TAKEOFFS
AND LANDINGS
MANEUVER 25
SHORT-FIELD TAKEOFF AND CLIMB SSeS SSSR eee eee eee eee 7-2
MANEUVER 26
SHORT-FIELD APPROACH AND LANDING SSeBeSeeeepeeeaeeeeaeeeaeeaaneeaeeneeeceaneaaea 7-4
MANEUVER 2'7
SOFT-FIiELD TAKEOFF AND CLIMB SSeeeeaeeeeeeeeaeeaeaeaeeeeeeeeaepnaaeeeeauaeae Seeencaan 7-6
MANEUVER 28
SOFT-FIELD APPROACH AND LAN DIN Giseccnccnccccccuscessecesuuecususane 7-3
EXERCISES
PERFORMANGE TAKEOFFS AND LANDINGS. occuusucncccanunecucenusess 271 7
SPECIAL FLIGHT OPERATIONS

MANEUVER 29
ATTITUDE INSTRUMENT iL WEE bcoukscakeuasdusecudsrsceusuesdecbababecénnia S-2
MANEUVER SO
NIGHT OPERATIONS SO Re ee een eer eceneeBcuseseeUeceEsananeeencenaubeceuceceseces ea” I C)
EXERCISES
SPECIAL FLIGHT OPERATIONS... Seeeanaana Saeaenepeaanaeeaeaanan suscdununeaeeuasnenee” | 5
AN SWER So... iiccccccccccceseeeseeeeeeecseeeeeeeseceeeeeeesecceseeeseeeseceessas ATT

How the Manual Works
Private Pilot Maneuversuses colorful graphics and step-by-step procedure descriptions to help you
visualize and understand each maneuver you will perform in the airplane. Additional guidance
is provided through insets which contain helpful hints, common errors, and FAA practical test
standards. To get the most out of this manual, as well as the entire Guided Flight Discovery Pilot
Training System, you mayfind it beneficial to review the major design elementsin this text.
[2 CROSSWIND APPROACH AND LANDING
\s
14 — CROSSWIND
APPROACH AND LANDING
There are two basic techniques used to accomplish a crosswind approach and landing — the crab
method and the wing-low,or sideslip, method. The crab method requires youto establish a heading
(crab) into the wind on final approach with the wings level so that the airplane's ground track
remains aligned with the extended centerlineof the runway. The crab angle is maintained until just
prior to touchdown, when the longitudinal axis of the airplane must be quickly aligned with the
runway to avoid imposing any side loads on the main lending gear.
Since the crab method requires a high degree of judgment and timing, the wing-low method is nor-
mally preferred for executing crosswind landings. The wing-low method of crosswind approach
and landing is described here. Since the same general procedures used to execute a normal
approach and landing apply to a crosswind approach and landing, only the additional techniques
required for windcorrection are explained in this discussion. The wing-low method enables you to
simultaneously keep the airplane's ground track and the longitudinal axis aligned with the runway
centerline throughout the final approach,flare, touchdown, and roll-out. This technique prevents
the airplane from touching down sideways, imposing damaging side loads on the landing gear.
The degree to which flaps should be extended in a crosswind varies with the airplane's handling
charectaciatice, aswell as the wind velocity. Full flaps may be used if the croeswind companant is
plane's capab ¥ ce unless theHesfagcturer rece otherwise.
= 5
APPROACH
If the crosswindexists attraffic pattern altitude as well as near the surface, you must apply the proper
S‘| DESCENTS
wind correction (crab) in the traffic pattern so your ground track remains rectangular. Since the wind
direction is perpendicular to the runway, you must crab into the wind on the downwindleg to remain S — DESCENTS
parallel to the runway. On base leg, you will either encounter a tailwind or headwind. Your groundspeed The descentis a basic flight maneuver whichresults in a loss of altitude without gaining excessive
3-20 increases with a tailwind component and you may need to start your turn to final sooner than normal airspeed, controlling the rate of descent with pitch attitude and,in somecases, power. Initially, you
will practice descentsat the airspeed used for approaches to landings. After you learn this type of
descent, you will practice the cruise descent which is flown at cruise airspeed and results in a
higher groundspeed.
To find the specific airspeed corresponding to the type of descent you wantto perform, you should
refer to the POH for your airplane. When you perform a descent, you should develop the practice of
_ establishingthe proper flight attitudes Pane eu inne first, then cross-check your parame-
s using flight instruments. zs
J
a = a
e Whenyou reach the descent airspeed, lower the nose slightly to set the descentpitch attitude
and maintain airspeed. Trim to relieve control pressures.
J
f o r m t h e a n e v e r "
.Sen per oO Maintain descent airspeed and heading. Cross-check your airspeed andrate of descent using
“aM first time. In addition, «

the airplane nose position in relation to the horizon, the airspeed indicator, the vertical
=
speed indicator, and the pitch attitude on the attitude indicator.
* Ina power-off glide, pitch attitude controls airspeed; raise the nose to decrease airspeed,
and lowerthe noseto increase airspeed. Alwaystrim after any adjustmentis madeto pitch
attitude.
26
Vi
I
TAXIING
QHUARTERING TAILWINDS
A quartering tailwind is the mostcritical wind condition for taxiing a tricycle gear, high-wingair-
plane. Since quartering tailwinds have a tendency to flow beneaththe elevator(or stabilator) andlift
thetail, the airplane maytip over on the nosewheel and one main wheel.
ww Fully turn the yoke in the direction away from the wind.In a right quartering tailwind tum
the yoke fully to theleft, or left aileron up. Reverse the position of the aileron control when
taxiing with a left quartering tailwind.
@ Hold the yoke full forward to maintain the elevator(or stabilator) in a down position which
will counteract the airplane's tipping tendency.
in aquartering tailwind. The increasing tailwind
EXERCISES — GROUND OPERATIONS
1
EXERCISES —
GROUND
OPERATIONS
1 — PREFLIGHT INSPECTION
1. Whatshould you use to ensure thatall steps are completed when performing a preflight inspection?
2. What documents are required on board the airplane?
3. How can you tell when wateris presentin a fuel sample?
4. True/False. Nicks on the propeller can cause excessive stress and should be checked by a cer
tificated mechanic.
5. What documents are not required to be on board the airplane?

A. Airworthiness certificate, aircraft logbooks
B. Airworthiness directives (ADs), maintenance records
Cc Airworthiness directives (ADs), approved flight manual
2 — ENGINE STARTING
1. True/False. Before you start the engine, a thorough look around the propeller eliminates the
Exercises
need for opening a window or door and shouting “CLEAR!”
2. The primer pumpsfuel into what part of the engine?
a follow each oftU 3. Where would you find procedural information on starting the airplane with an external power source?
4. After you start the engine in cold weather, the oil pressure should register properly within
howmany seconds?
5. After starting the engine, what action should you take in the eventtheoil pressure does not
register within the green arc in the recommended time?
3 — TAXIING
The following questions pertain to a tricycle gear airplane.
1. True/False. Taxi speed is primarily controlled by using the brakes.
2. Does the effectiveness of the aileron , rudder, and elevator (or stabilator) controls increase or
decreaseas the airplane's speed decreases?
Vil
r
Po ft of - | | ft | | | ff
vill
GROUND
OPERATIONS
MANEUVER 1 BEEBSBSBRBRBRBRBRBRBRBRBRBRBEBRRBBERBEReBeeBeeeeeeeee) 1-2
PREFLIGHT INSPECTION
MANEUVER intdupunesnecttaceuuaccseeacneas 1-6
ENGINE STARTING
MANEUVER bape DEeeneaniescueenneseesereoeuct 1-8
TAXIING
MANELVER Ge ecccucencennnceuseepecnsusacen 1-1 A
BEFORE TAKEOFF GHECK
MANELVER Lee SEES OE SSESEEPDEbeEbeeseEE 1-1 6
POSTFLIGHT PROCEDURES
EXE RSS ES coscctewnwocceussanessecncasnsscn 1 -2 1
Video Volume I — Ground Operations, Basic Maneuvers, Airport

Operations, and Emergency Landing Procedures
Computer Training — Ground Operations
Since there can be vast differences in ground operations from one airplane
to another, the procedures in this section are intentionally general in nature.
Therefore, it is imperative that you use an appropriate printed checklist which
providesa logical step-by-step sequence for each task you will perform.
1 — PREFLIGHT _
INSPECTION -
As a pilot, you are the final authority regarding the airworthiness and safe operation of youraircraft.
Your flight instructor will point out the various components to be inspected and explain how to
determine the airworthinessof the airplane. In addition, the pilot’s operating handbook (POH) nor-
mally contains a checklist and other information regarding the preflight inspection.If a discrepancy
is discovered during yourpreflight inspection, it should be evaluated and, if required, corrected
prior to the flight. You may needto enlist the assistance of an aviation maintenance technician to
answer questions or resolve problems that you find while inspecting the airplane.
Prior to performing a visual inspection of the airplane, you should check theaircraft logbooks and
records to ensure that the appropriate airworthiness directives have been complied with, maintenance —
requirements have been met, andaircraft inspections have been performed. Airworthinessdirectives
(ADs) require correction of unsafe conditions found in engines, propellers, and other equipment. —
ADsalso prescribe the conditions under whichthe affected equipment may continue to be operated.
Records of AD compliance andtheaircraft logbooks are not required to be on boardtheaircraft. J
@™ Your preflight inspection should begin as you walk towardthe airplane. This provides you
a with an overall look at the airplane that may indicate items you will want to inspect more
closely during your walkaround. During the winter months, you should removeall frost,
snow, and ice accumulations from the airplane surfaces.
@ IN CABIN
e In the cabin, verify that all the required paperworkis on boardthe airplane. Use the acro- |
nym ARROWto help you rememberthe required documents.
Airworthinesscertificate (required by FAA)
Registration certificate (required by FAA) 4]

Radio station class license (required by the Federal Communications Commission when
transmitting to groundstations outside the United States)
Operating instructions, pilot’s operating handbook,or approvedaircraft flight manual (required |
by FAA)
1-2 Weight and Balance data, as well as equipmentlist (required by FAA)
PREFLIGHT INSPECTION |
liter msec ae not CS
Be er thatmay legally be inoperativ

e. If your airplane has an
ant ‘required, howto operatethe airplane with inopera-
wasOa
e Next, remove the control lock and check the controls for freedom of movement.
e Clear the propeller area, and then turn the master switch ON.
e Verify proper operation of fuel gauges and note the fuel quantity in each tank.
— e Lowerthe flaps and turn the master switch OFF.
a ¢ Inspect the instrumentpanelfor any irregularities, such as cracked glass or any equipment
which may have been removedfor maintenance.
— e Ensure the windscreen and windows are clean and in good condition.
—_ ¢ Before continuingto the exterior inspection, verify that the magneto switch, master switch,
mixture control, and throttle are in the OFFposition.
© FUSELAGE (LEFT SIDE)

e Moving toward thetail, visually inspect the left side of the fuselage for skin wrinkles,
dents, and looserivets.
_ ¢ Checkthe lower surface of the fuselage for evidence of engineoil leakage, dents, and gen-
eral condition.
@ EMPENNAGE
e Removethe external rudder lock(if installed).
e Inspectthe tail surfaces for general condition, looking closely for skin wrinkles, dents, and
loose rivets.
e Examine the rudder for damage, loose hinge bolts, and freedom of movement.
° Closely inspect the control cables and stops for damage.
—~— e Visually inspect the flashing beacon,tail light, and VOR navigation antenna on thevertical
stabilizer for damage.
e Examinetheelevator(or stabilator) trim tab, checking for security and general condition.
sr ¢ For tailwheel airplanes, check the steering arms, cables, and springs for wear. Additionally,
inspect the tire for wear, cuts, abrasions, and properinflation.
e Lastly, removethetail tiedown chain orrope.
@ FUSELAGE (RIGHT SIDE)

e Inspect the right side fuselage, as before, looking for skin wrinkles, dents, and looserivets.
— @ RIGHT WING
_ ¢ Thoroughly inspect the wingflap for general condition andthe flap hinges for security.
B]
If the flap track is visible, check to ensure it is in good condition and does not show
unusual wear.
Inspect the aileron surfaces for dents and skin wrinkles and the hinges for security, dam-
age, and freedom of movement.
Check the aileron pushrod or cables for security, damage, and tension.
Check the right wingtip for damage and secure attachment, and inspect the right naviga-
tion light.
Examine the leading edge of the wingfor dents or other damage.
Inspect the upper surface of the wing for wrinkles or dents which may indicate internal
structural damage.
Next, remove the fuel cap andvisually check the fuel quantity. In addition to ensuring that
the fuel quantity is sufficient for the proposedflight, you should verify that the fuel level
agrees with the fuel quantity gauge indication observed earlier.
Before replacing the fuel cap, inspect the rubbergasket for cracks or deterioration.
Inspect the fuel vent in thefiller cap for obstructions, and then replacethefiller cap and
tighten it securely.
Use your fuel tester to take a fuel sample from the fuel tank drain and check thecolor to
verify that the fuel is the proper grade. If water or other contaminants are found in the
sample, continue draining fuel until there is no evidence of contamination.
in the air, or it may be presentin the fuel added to the

bottom of the fuel tester.
Removethe wing tiedownropeorchain.
LANDING GEAR (RIGHT SIDE)

Inspect the skin around the attachment points of the main landing gear for dents and
wrinkles.
Examinethetire for properinflation, cuts, and condition of the tread.
Check the wheelfairing (if installed) for cracks, dents, and security.
Inspect the brake pads for wear and the hydraulic brake lines for security and leaks.
If your airplane is equipped with oleo struts, ensure properstrut inflation.
@ Nose
Open the cowlaccess door to inspect the engine componentsfor loose wires and clamps,
worn hoses, and oil or fuel leaks.
Determine the oil quantity by removing and reading the dipstick. Add oil if the level is
below the minimum recommended by the manufacturer. Then, replace the dipstick and
tighten it securely.
Drain the fuel strainer (if located within the engine compartment) for several seconds to
eliminate any water or contaminants.
If there is a fuel drain directly below the fuel selector on the undersideofthe airplane, take
a fuel sample and check for contamination.
Check the engine cow]for security.

PREFLIGHT INSPECTION |
— e Inspect the propeller and spinnerfor security and check the propeller for nicks and cracks.
eee
pairedby an aviation technician priortoflight.
Peres
e If your airplane has a constant-speed propeller, check for oil leaks.
be detectedbyoil streaks on the backside of the

Se
—— a cptn Be
e Examine the nosewheeltire for properinflation, cuts, abrasions, and condition ofthetread.
e Check the wheelfairing (if installed) for cracks, dents, and security.
— ¢ Carefully inspect the nosewheelstrut for properinflation, leaks, and security.
a ¢ Inspect the steering linkages for security and the shimmy damperfor leaks or damage.
¢ Checkthe cowlflaps (if installed) for security.
e Check the exterior surface of the windshield for cleanliness and general condition.
soft clothees
ingcompoundspecifically designed for airp

ft RR A RE ta Bes ‘ pon
lane windshields. A
Soe et Shs SPeeS eas beets eee Rog FE = AAS IRE:
ee ce ae
e Ifa static port is located on the cowling, check for obstructions.
LANDING GEAR (LEFT SIDE)

e Examine the left main landing gear as you did the right main gear.
LEFT WING
¢ Inspect the left wing as you did the right wing.
a e Examinethe pitot tube for damage and checkthe openingfor obstructions.
e Ifthe static port is located on the pitot tube, ensure it is clean and free of obstructions.
__ e Checkthe stall warning vane(if installed) for freedom of movement.
e Ifthe airplane is equipped with a pneumatic stall warning device, check the opening for
obstructions.
>
ENGINE STARTING
2 — ENGINE STARTING _
Although engine starting procedures can vary from one make and modelof airplane to another,
there are some safety precautions which are common to most general aviation aircraft. You should
avoid starting the engine with thetail of the airplane pointed toward people standing nearby, prop-
erty on the ramp, open hangers, or other aircraft that could be damaged by the wind blast from the
propeller. Inspect the ground underthe propeller before you start the engine, especially if you are
operating on an unimprovedsurface. Rocks, pebbles, or any other loose debris can be picked up by
the propeller and cause damageto the blades or be hurled backward. Since there are a numberof
different procedures usedto start airplane engines, it is very important to follow the appropriate
printed checklist provided by the aircraft manufacturer. The POH normally contains a checklist and
expanded proceduresfor enginestarting.
Ji
bed
ws Place the carburetor heat control in the COLD position (if applicable).
Zs Fuel-injected—Set the mixture control to RICH.

ENGINE STARTING
Non-fuel-injected—use the engine primer to pump fuel into the intake system. The number
of primerstrokes required dependson the length of time the engine has been shut down and
— the temperature of the outside air. In cold weather, a greater numberof primer strokes may
be necessary than when operating in warmer temperatures. Refer to your airplane’s POH for
—— the manufacturer’s recommendation. Fuel-injected—Prime the engine by turning on thefuel
pump and opening thethrottle 1/4 to 1/2 inch so that you observe an indication on thefuel-
— flow meter for several seconds, then pull the mixture control back to IDLE CUTOFF.
©08e@ @ ©
Openthe throttle approximately 1/8 to 1/2 inch, depending on the manufacturer’s recom-
mendation.
Prior to starting the engine, ensure the area aroundthe airplane is clear. Open a window or
the door, call out, “CLEAR,” andlisten for a response.
With the area clear, turn the master switch ON.
Turn the anti-collision lights on to provide a visual warning to people approachingtheair-

plane that the engineis abouttostart.
Turn or press the ignition switch to engage the starter.

Fuel-injected—Advance the mixture control to RICH asthe enginefires.
To avoid damageto thestarter, return the switch to the BOTH position as soon as the
enginestarts.
Adjust the throttle to the recommendedidle powersetting.
Checkthe oil pressure gauge to ensure the oil pressure registers within the greenarc.If the oil
pressure does not register in the normal range within 30 seconds in warm weatheror within
60 secondsin cold weather, immediately shut down the engine to prevent possible damage.
Diy
TAXING
To becomeproficient at taxiing, you mustlearn directional control techniques and the proper
7
throttle usage to control speed. To maneuveron the ground, mostlight training aircraft have a
steerable nosewheel whichis linked to the rudder pedals. The main landing gear usually have
J J J
brakes which are differentially controlled by toe pressure on the rudder pedals. The ailerons
are normally used to maintain control while taxiing in windy conditions. You should refer to
the pilot’s operating handbook and the appropriate checklist for specific taxi procedures for
your airplane.
BASIC TAX! TECHNIQUES
|
}
|
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or) Clear the area around the airplane. Add powerslowly until the airplane beginsrolling and —
then reduce power. More poweris requiredto start the airplane rolling than is required to
eep it rolling. —
StSESES SSRINTbapeysarees Eh
SERRE SAR ed Bt SPS atte aany eRER EERE SL
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Neca ee bE it se eer eee Be
Ss reas- Seene ATS > De POR SST TSS CSSSSS SSE ees eee ee eee ee eee
e335 Ss en ane eee enn te
lecessarytostart and sustain an airplane in motion on a soft surface, such as grass, than on a
J _
ie
Test the brakes for proper operation and then readjust the powersetting to obtain a normal
taxi speed. Taxi speed is primarily controlled by the throttle and secondarily by the brakes.
Use the brakes only when a reduction of engine r.p.m. is not sufficient to slow theairplane.
| |
DP SS5C5SS SESS SESS
rakesto control speed while taxiing may cause excessive wearor overheating.
5 Se ee ee
er
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TAXING
Press the right rudder pedalto turn the airplaneto the right and the left rudder pedal to turn
to the left. It is recommended that you taxi no faster than a brisk walk. In a confined area,
— taxi at a speed slow enoughto enable you to stop by reducing the poweror shutting down
the engine in the event of a brakefailure.
cesinthe direction of a turn can be helpful in reducing the

tor oftheleft rudder pedal andthe right brake by press-
i TAXIING IN HEADWINDS
While taxiing in moderate or strong wind conditions, you must use special techniques to main-
tain aircraft control. The aileron, rudder, and elevator (or stabilator) controls are relatively inef-
fective at slow speeds. However, as the speed of air over the control surfaces increases, control
effectiveness also increases. The flight controls respond the same, whether you are taxiing at 5
knots with no windorsitting still with a 5-knot headwind. However, if you taxi the airplaneat
15 knots into a 15-knot wind, the controls have a 30-knot airflow over them and respondto that
velocity of airflow.
Hold the yoke neutral or slightly forward to maintain the elevator (or stabilator) in a neutral
or slightly downposition. This will exert normal pressure on the nose gear.
© Whentaxiing over rough ground, hold the yoke aft so the elevator (or stabilator) is raised.
This procedureforces the tail down and increases propeller clearance.
TAXIING
QIUARTERING HEADWINDS
In a strong quartering headwind,there is a tendencyfor the windto get under the upwind wing and
tip the airplane toward the downwindside. With improperaileron placement, the upwind wing can
be lifted which can cause directional control problems or even overturn the airplane. In addition,
windstriking the rudder can causethe airplane to turn into the wind. Improperelevator(or stabila-
tor) position can reduce nosewheelfriction and increase this weathervaning tendency.
ww Fully turn the yokein the direction of the wind placing the upwindaileron in the up position.
Due to reduced control effectiveness at slow taxi speeds, full aileron deflection is required.
J Hold the yoke to maintain the elevator (or stabilator) in a neutral or level position. A neutral
elevator position will help maintain sufficient nosewheelfriction and allow positive direc-
tional control.
TAXIING IN TAILWINDS ~
The effectiveness of the airplane controls also is influenced by tailwinds. For example, if you taxi
the airplane at 5 knots with a tailwind of 5 knots, the taxi speed and the wind speed are canceled,
and the controls respond as though no windexists. If you slow theairplane, the controls respond as
though there were an increasing tailwind component. When youstop the airplane completely, the
control surfaces are subjected to the direct effects of a 5-knot tailwind.
eZ Hold the yoke full forward to maintain the elevator (or stabilator) in a full down position.
This causes the windto strike the upper surface of the elevator (or stabilator) and to exert a
downward force on thetail.
- wind mayraise the tail causing the airplane to have a

1-10 cc
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2tiits
TAXING
QIUARTERING TAILWINDS
— A quartering tailwind is the most critical wind condition for taxiing a tricycle gear, high-wingair-
plane. Since quartering tailwinds have a tendency to flow beneath the elevator (or stabilator) and
— lift the tail, the airplane may tip over on the nosewheel and one main wheel.
Fully turn the yokein the direction away from the wind. In a right quartering tailwind turn
the yoke fully to the left, or left aileron up. Reverse the position of the aileron control when
— taxiing with a left quartering tailwind.
— @ Hold the yokefull forward to maintain the elevator (or stabilator) in a down position which
will counteract the airplane’s tipping tendency.
EESSEOSSes
TAXIING
To meet the PTS requirements, you must:
e Exhibit knowledge of the elements related to safe taxi procedures.
e Perform a brake check immediately after the airplane begins moving.
e Position the flight controls properly for the existing wind conditions.
e« Control direction and speed without excessive use of brakes.
¢ Comply with airport/taxiway markings, signals, ATC clearances, and instructions.
e Taxi so as to avoid otheraircraft and hazards.
1-117
4 — BEFORE TAKEOFF =
CHECK ~
The before takeoff check is an integral part of every flight. When performing the before takeoff —
check, you should use the checklist provided by the airplane manufacturer or operator. This helps
ensure that each item is checked in the proper sequence and that no items are omitted. After taxiing —
to the runuparea, position the airplaneso the propeller blast is not directed towardotheraircraft,
buildings, or vehicles. If possible, point the nose of the airplane into the wind to improve engine —
cooling. To prevent damage to the propeller and otherparts of the airplane, avoid engine runups
on loose gravel or sand. During the before takeoff check, you should divide your attention between —
your cockpit duties and outside the airplane. The before takeoff check may include, but is not lim-
ited to the following items. =
1. Set the parking brake.
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1-12 3. Checkthe flight controls for freedom of movement,full travel, and correct control surface deflection.
— 4. Check andsetthe flight instruments.
— Verify the airspeed indicator reads zero.
ao | The attitude indicator should be erect with the miniature airplane aligned with the horizon.
Set the altimeter to the current altimeter setting or to the correct

field elevation. If the altimeter does not indicate the field elevation
within 75 feet, you should consider postponing theflight.
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coordinator should be level and the
ball in the inclinometer centered.
Set the heading indicator to coincide with the magnetic compass.
Checkthat the vertical speed indicator (VSI) is pointing at zero.If the VSI is not pointing at zero, you may
fly the aircraft and use the indicated value as the zero indication.
— 5. Position the fuel selector

valve to the fullest tank or to
the BOTH position, as recom-
mended by the POH. BpALLFUGH ATTITUDES
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6. Set the mixture control to RICH as requiredforfield eleva-

tion or as required by the POH.
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—_ 7. Set the elevator trim and ruddertrim (if installed) to the TAKEOFFposition. 414
8. Smoothly add powerto the r.p.m. setting recommended by the manufacturer for the power
check (also called the runup). You should also hold the brakes to ensure the airplane does not
move forward during the runup.
. Check each magneto for proper operation. Test the magnetos by noting the r.p.m. with the mag-
neto switch in the BOTH position, then move the magneto switch to the RIGHT position and
note the r.p.m. drop. Next, return the magneto switch to BOTH, then switch to the LEFT posi-
tion and again note the r.p.m. drop. Finally, return the magneto switch to the BOTH position
for takeoff. The airplane manufacturer specifies the maximum permissible r.p.m. reductions for
each magneto, as well as the maximum differential.
10. Position the carburetor heat control to ON and check for a corresponding dropin r.p.m., then
return it to the COLD position. In some atmospheric conditions, carburetor ice may form while
taxiing. This may be noted by larger initial drop in r.p.m. followed by slight increase in
r.p.m. The initial drop may be accompanied by engine roughness which subsides with the
r.p.m. increase.
11. Check the engine instruments and ammeter for normal indications. With the exception of
the oil temperature gauge, the engine instruments should register in the green arcs. In cold
weather,oil temperature might not indicate in the normal range until after takeoff. An ammeter
discharge or low voltage light may indicate a faulty alternator, broken alternator belt, or exces-
sive electrical load.
1-14
12. Check the suction gauge for a normal indication. A low reading mayindi-
cate a dirty air filter. Unreliable gyro indications may result if sufficient
suction is not maintained.
13, Reduce powerto approximately 1,000 r.p.m.
14, Set the communication and navigation radios to the appropriate frequencies.
15, Set the transponder to the appropriate code. While you typically should use
the code 1200 for VFRflight, you may be assigned a discrete transpondercode at someairports.
hd GTX 330
IDENT FUNC rata;
START
STOP oe
16. Ensure yourlandinglight, navigation lights, flashing beacon and/orstrobelights are on as required.
17. Adjust the throttle friction as desired.
18. Review performanceairspeeds.
19. Release the parking brake.
20. Clear the area of traffic before taxiing into the takeoff position. After receiving your takeoff
clearance(if required), you should checkthe final approach path, any taxiways you maycross
to get to the runway, and the runwayitself.
BEFORE TAKEOFF CHECK
e Exhibit knowledge of the elements related to the before takeoff check. This shall include the reasons
for checking each item and how to detect malfunctions.
e Position the airplane properly considering other aircraft/vessels, wind and surface conditions.
e Divide attention inside and outside the cockpit.
e Ensure that engine temperature and pressure are suitable for run-up and takeoff.
¢ Accomplish the before takeoff checklist and ensuresthe airplane is in safe operating condition.
e Review takeoff performance airspeeds, takeoff distances, departure, and emergency procedures.
e Avoid runwayincursions and/or ensure no conflict with traffic prior to taxiing into takeoff position.
1-15
ie POSTFLIGHT PROCEDURES
> — POSTFLIGHT ~
PROCEDURES ~
Manypilots maintain a high level of vigilance throughouta flight; however, the flight is not over
once you arrive on the runway — youstill have several important tasks to perform as part of your
postflight procedures. These tasks include completing the after landing and engine shutdown
checklists as well as parking and securingtheairplane.
AFTER LANDING
After landing, gradually slow the airplane to normal taxi speed before turning off the runway. You
should use the manufacturer’s checklist to perform the after landing check oncetheairplaneis
stoppedclear of the active runway.
Oe
Retract the wingflaps.
Non-fuel-injected—Movethe carburetor heat control to the COLD position to prevent unfil-

tered air from being drawninto the carburetor, causing damageto the internal components
of the engine.
oO
At tower controlled airports, contact ground control for taxi clearance.
After receiving your taxi clearance, clear the area aroundtheairplaneto avoid taxi conflicts.
While taxiing, you should position the flight controls as appropriate for the prevailing wind
conditions.
1-16
PARKING AND SECURING
Whentaxiing into the parking area, you should usea safe taxi speed and follow any handsignals
you receive from ramp personnel. In general, there are two waysto park an airplane. One wayis
to taxi the airplane into its designated parking spot, shut down andsecure the engine, then safely
deplane any passengers. However, because of the proximity of other aircraft, this procedure may
not be possible. In this situation, you should taxi the airplane near your intended parking spot and
position the airplane so that the propwash doesnot endanger people or property on the ramp. Then,
shut down and secure the engine, safely deplane any passengers, and use a towbar to maneuverthe
airplane into parking. Once you have positioned the airplane in its parking spot, you should tie
downthe airplane and perform a postflight inspection.
ENGINE SHUTDOWN
Manyaircraft have specific procedures for engine shutdown. You should always follow the recom-
mendations contained in the POH.
oO Set the throttle to idle, or as recommendedby the manufacturer.
eo Turn OFFall electrical equipment.
we Turn OFF the avionics powerswitch.
oO Set the mixture control to IDLE CUT-OFF.
oO Turn the ignition switch OFF when the engine stops. As an added precaution, remove the
key from theignition.
~~ Turn the master switch OFF.
oO Install the control lock.

1-17
POSTFLIGHT PROCEDURES
TIEDOWN
To avoid damage from high windsor gusty conditions, you must secure the airplane properly. This oo
is usually accomplished using chocks and tiedownropesor chains.
1. Release the parking brake and position the airplane in the parking spot using a towbar, if necessary.
irplan bypushing on various components. You can push onthe leading

as longé you only apply pressure to the leading edge nearthe fuselage.
4. Install the pitot tube cover. —
5. Complete a postflight inspection using a checklist, if available. A typical postflight inspection —

includes checking for leaking fluids, airframe damage, propertire inflation, and a variety of
other items. _
1-18
POSTFLIGHT PROCEDURES | Z
6. Removeall personal materials from the cockpit, stow the seatbelts, and close andlock all doors
and windows.
a.
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1-19
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1-20
EXERCISES — GROUND OPERATIONS | a
EXERCISES —
GROUND OPERATIONS
1 — PREFLIGHT INSPECTION
1. What should you use to ensurethatall steps are completed when performing a preflight inspec-
tion?
__ 2. What documents are required on boardthe airplane?
3. How can youtell when wateris present in a fuel sample?
4. True/False. Nicks on the propeller can cause excessive stress and should be checked bya cer-
tificated mechanic.
5. What documentsare not required to be on board the airplane?

A. Airworthinesscertificate, aircraft logbooks
B. Airworthiness directives (ADs), maintenance records
—_ C. Airworthiness directives (ADs), approvedflight manual
_ 2 — ENGINE STARTING
1. True/False. Before you start the engine, a thorough look around the propeller eliminates the
need for opening a window or door and shouting “CLEAR!”
2. The primer pumpsfuel into what part of the engine?
3. Where would you find procedural information on starting the airplane with an external power source?
a 4. After you start the engine in cold weather, the oil pressure should register properly within
how many seconds?
5. After starting the engine, what action should you takein the event the oil pressure does not
register within the green arc in the recommendedtime?
- 3 — TAXIING
The following questions pertain to a tricycle gear airplane.
1. True/False. Taxi speed is primarily controlled by using the brakes.
2. Does the effectiveness of the aileron , rudder, and elevator (or stabilator) controls increase or
= decrease as the airplane’s speed decreases? 1-21

—| EXERCISES — GROUND OPERATIONS
Aa
3. What action is helpful in reducing the radius of a turn while taxiing?
4, How would youpositionthe flight controls for the surface wind conditions depicted inillustration A?
5. How would youposition theflight controls for the surface wind conditions depictedinillustration B?
4— BEFORE TAKEOFF GCHECK

1. Why should you position the nose of the airplane into the wind during the runup?
2. True/False. If the altimeter setting is not available during the before takeoff check, you can
adjust the altimeter to agree with field elevation.
3. As you apply carburetor heat during the runup should the r.p.m. increase or decrease (assum-
ing no carburetorice exists)?
4, What may occurif sufficient vacuum pressure(suction) is not maintained?
5. True/False. Unless you are assigned a discrete transponder code, you should use 1220 for VFR
flight.
5 — POSTFLIGHT PROCEDURES
1. Non-fuel-injected—Why should you ensure the carburetor heat is COLD while taxiing?
2. How can you checkfor accidental activation of your ELT?
3. True/False. You should install the control lock before engine shutdown.
4, If you move an airplane by pushing on the leading edge of a wing, where should you apply
pressure?
1-22 5. While securing your airplane, where should you normally place the chocks?
BASIC
MANEUVERS
MANEUVER SS veuweavareuastteasnencbesneeueckeece 2-2
STRAIGHT-AND-LEVEL FLIGHT
MANEUVER As woeppaneucuceceuseuauusscevceucucanc 2-4
CLIMBS
MANEUVER Po pen ccaneueaneuaud bueucuhessaucuauuues 2-6
DESCENTS
MANEUVER ) caueanedeseueuuaansbeeeasseeuusance 2-78
TURNS
EXE RGIS E Si ccuncccccccccccecccccccucuccncanacae 2" 1 3

Computer Training — Basic Maneuvers

Ag ee coocirinee rs
RNMRG Ee:Forsec~sanocerecreerae
6 — STRAIGHT-AND- -
LEVEL FLIGHT ~
Duringstraight-and-levelflight you can maintain a constant heading andaltitude by controlling the a
nose and wing positions with reference to the natural horizon. Although the flight instruments may
be used as a cross-check to confirm that you are maintaining straight-and-level flight, your primary 4
reference should be the horizon to the front and side of your airplane. Keeping your eyes primarily
focused outside the cockpit also helps you see and avoid otheraircraft. —
Trim adjustments eliminate the need for continuous forward or backward pressure on the yoke —
to maintain attitude. If the airplane feels nose-heavy, you are holding back pressure to maintain a
given attitude. Likewise, if forward pressure is required, the airplane will feel tail-heavy. Whenitis nn
properly trimmed, you will not have to apply either forward or back pressure to maintain a constant
pitch attitude. Use the trim tab only to removepressure; do notuseit to fly the airplane. The proper at
procedureis to set the airplane in the desired pitch attitude and at the selected airspeed, then trim
away any control pressure necessary to hold that attitude. With a few exceptions, trim tab adjust- oy
ments should be made whenever you must apply a continuous forward or rearward force to the
yoke. The sameprinciples apply to trimming the rudder however, sinceit is not as easy to feel the _e
control pressures, you shouldrefer to the turn coordinator while trimming the rudder to maintain
coordinated flight. —
When you are introduced to straight-and-level flight (or any other maneuver), your instructor will
normally demonstrate the maneuverfirst, then pass the controls to you. To ensurethat it is clear
as to who hascontrol of the airplane, the FAA strongly recommendstheuseof a three-step process
when exchanging the flight controls. During the preflight briefing, you should review with your
instructor the following procedures for passing controlof the airplane.
PILOT PASSING CONTROL: “You havethe flight controls.”
PILOT TAKING CONTROL: “I have the flight controls.”
PILOT PASSING CONTROL: “You havethe flight controls.”
Heading Wings Level 2000' Heading Nose Low 1800'

Altitude Attitude Altitude
2-2
STRAIGHT-“AND-LEVEL FLIGHT
Past
— The pilot passing the controls should continueto fly until the pilot taking the controls acknowl-
edges the exchange by saying, “I have the flight controls.” A visual check also is recommended
— to ensure that the other pilot actually has the controls. There may be times when yourinstructor
desires to assume control of the airplane from you. If this is necessary, your instructor should take
“ the controls while informing you, “I have the flight controls.”
wi Establish the airplane on a specfic heading andaltitude. Adjust the rudder to maintain coor-
dinated flight and trim to relieve control pressures.
¢ Maintain a wings-level position by keeping the wingtips a given distance above (high-
wing airplane) or below (low-wingairplane) the horizon.
¢ By keeping a point on the airplane’s nose or spot on the windshield in a constant posi-
tion in relation to a point on the horizon, you can maintain your desired altitude.
Brief periodsof inattention, power changes, turbulence, or wind gusts can cause yourairplane
to drift away from a desired course and altitude. Once you detect a changein the position of
your airplane’s reference points in relation to the horizon, determine the magnitude of the
deviation from the desired heading andaltitude by cross-checking yourflight instruments.
ed Adjust the elevator (or stabilator) and ailerons to return to the original heading andaltitude.
Simultaneously adjust powerto maintain the desired airspeed. Trim to relieve control pressures.
wee! Once you havereturned to the desired heading and altitude, adjust the controls to maintain
the proper wing and nosepositionsin relation to the horizon. Adjust powerto maintain air-
speed andtrim to relieve control pressures.
, STRAIGHT-AND-LEVEL FLIGHT
S@y> The PTS doesnotinclude specific criteria for straight-and-levelflight using visual references.
However, it does have performancestandardsfor basic instrument straight-and-level flight. (See
Maneuver #29.)
amenne
090
Heading Wings Level 2000'
Altitude
CLIMBS
cd ced eh ae es ee od el = = ee J} J J | _J
‘4 — GLIMBS
A climb is a basic maneuver designed to produce a gain in altitude. When practicing climbs, your
objectives are to become proficient in establishing the proper climb attitude, applying the appro-
priate control pressure, and learning the trim technique necessary to maintain the climbattitude.
During your training you will practice a variety of climbs; some will be constant-rate climbs and
others will be constant-airspeed climbs. The most commontypesof climb speedsare:
e Best angle-of-climb speed, Vx — Anairspeed that results in the greatest altitude gain in the
shortest distance.
e Best rate-of-climb speed, Vy — Anairspeed that provides the most gain in altitude in theleast
amountof time.
e Cruise climb speed — Anairspeedthat is normally used during cross-countryflight and results
in a relatively higher groundspeed while climbingto cruising altitude.
|
|
]
|
JJ J
CLIMBS
After clearing the airspace around yourairplane, simultaneously add powerand apply back
pressure on the yoke. Add right rudder to compensate for the left-turning tendencies which
result from the increase in pitch attitude and decrease in airspeed. Trim up elevator(orsta-
bilator) and right rudder(if available).
es Maintain climb airspeed and heading using outside references and instrument cross-checks.
_ Use changes in pitch attitude to maintain your airspeed and bank angle adjustments to cor-
rect for heading deviations. If changes are necessary, make small adjustments, allow the
—- airplaneto stabilize, then trim to relieve the control pressures.
If you are climbing at 500 f.p.m., return to straight-and-level flight by gradually lowering
the nose approximately 50 feet prior to the desired leveloff altitude. Maintain climb power
_ to accelerate to cruise speed. As the airplane accelerates, less right rudder pressure will be
needed(or increasing left rudder pressure against the right ruddertrim) as theleft-turning
a tendencies diminish.
@ Reduce powerto the cruise setting whenthe desired cruise speed is reached. Trim to relieve
_ the control pressures and, if necessary, lean the mixture.
2-5
DESCENTS
S — DESCENTS -
The descentis a basic flight maneuver whichresults in a loss of altitude without gaining excessive
airspeed, controlling the rate of descent with pitch attitude and, in some cases, power.Initially,
you will practice descents at the airspeed used for approachesto landings. After you learn this type
of descent, you will practice the cruise descent whichis flown atcruise airspeed andresults in a
higher groundspeed.
To find the specific airspeed correspondingto the type of descent you wantto perform, you should
refer to the POH for your airplane. When you perform a descent, you should develop the practice
of establishing the properflight attitudes using visual referencesfirst, then cross-check your param-
eters using the flight instruments.
After clearing the airspace around your airplane, apply carburetor heat (if applicable) and
reduce poweras required. Gradually apply back pressure to maintain altitude while theair-
plane slowsto the descentairspeed.
Whenyou reach the descent airspeed, lower the noseslightly to set the descent pitch attitude a
and maintain airspeed. Trim to relieve control pressures.
craft,thedescent attitude is nearly the same as that used for straight-and-level cruising flight. While you nor- |]
] entwithpowerand/orpitch attitude changes,you can also use configuration changes. Extending the
ggear(ifapplicable)orflapsincreases your descentrate without increasing your airspeed. =
ce Maintain descent airspeed and heading. Cross-check your airspeed andrate of descent using
the airplane nose position in relation to the horizon, the airspeed indicator, the vertical 4]
speed indicator, and the pitch attitude on the attitude indicator.
e Ina power-off glide, pitch attitude controls airspeed; raise the nose to decrease airspeed, —
and lowerthe noseto increase airspeed. Always trim after any adjustmentis madeto pitch
attitude. —
2-6
DESCENTS
e To maintain a constant airspeed in a powered descent, you will need to adjust the nose
attitude when you change power. A poweraddition requiresa slightly higher noseattitude,
while a slightly lowernoseattitude is needed for a power reduction. Alwaystrim after any
adjustmentis madeto pitch attitude or power.
e To maintain heading, refer to the position of each wingtip in relation to the horizon and
cross-check using the heading indicator. Also, check the turn coordinator to ensure you
maintain coordinatedflight. If changes are necessary, make small adjustments, allow the
airplane to stabilize again, then trim to relieve the control pressures.
w If you are descending at 500 f.p.m., return to straight-and-level flight by gradually rais-
ing the nose approximately 50 feet prior to the desired leveloff altitude. Add powerto
maintain airspeed.
ed Once the airplane is stabilized in straight-and-level cruising flight, trim to relieve control
pressures. Set the carburetor heat to COLD(if applicable) and, if necessary, enrichen the mixture.
DESCENTS
The PTS doesnot include specific criteria for descents using visual references. However,
it does have performancestandardsfor basic instrument constant airspeed descents. (See
Maneuver #29)
2-7
} J J J J | J
9 — TURNS
Turns are accomplished by using outside visual references and monitoring the flight instruments.
You will normally begin by practicing level turns and, once mastered, move on to climbing and
descending turns. Turns are dividedinto threeclasses:
¢ Shallow turn — A turn of less than approximately 20° angle of bank
¢ Medium turn — A turn between approximately 20° to 45° angle of bank
¢ Steep turn — A turn of approximately 45° angle of bank or more
|
J J
LEVEL TURNS
When you make turns by visual reference, the nose of the airplane appears to move in an arc with
respect to the horizon. You can determine when you have reached the proper angle of bank by
observing the angle of the cowling and instrument panel with respect to the horizon.
JJ) J LJ
TURNS
wy After clearing the airspace around yourairplane, add powerslightly, turn the airplane in the
desired direction, and apply a slight amountof back pressure on the yoke to maintain altitude.
Maintain coordinated flight by applying rudderin the direction of the turn.
es Ses
twhichtheairplane rolls depends on how much

)dependsonhow long youdeflectthe ailerons,
SS ee
— @ Whenyou reach the desired angle of bank, neutralize the ailerons. Trim to relieve control
pressures.
Leadthe roll-out by approximately one-half your angle of bank. Use coordinated aileron and
rudder control pressures as you roll out. Simultaneously, begin releasing the back pressure
_ on the yokesoaileron, rudder, and elevator (or stabilator) pressures are neutralized when the
airplane reaches the wings-level position.
CLIMBING TURNS
The objective of practicing climbing turns is to smoothly combine the techniques of climbs with
those of turns. Initially, you may practice climbing turns with a two-step process. First, you estab-
lish climb powerandattitude, then roll to the desired angle of bank. As you gain experience and
proficiency, you will enter the maneuver by establishing both the climb and bankattitude at the
same time.
You should use the same airspeed for straight climbs and climbing turns. However, yourrate of
climb will be less for climbing turns than straight climbs. Generally, you perform climbing turns
using shallow bank angles, because steep bank angles divert more of the vertical componentoflift,
which causes a reduction in rate of climb.
After clearing the airspace around your airplane, simultaneously add power, apply back Jt _J
J J
|
}
7
pressure on the yoke andturn the airplanein the desired direction with coordinated aileron
and rudder control input.
©
When you reach the desired angle of bank, neutralize the ailerons. Trim to relieve control
pressures.
©
Maintain the desired climb airspeed and angle of bank using outsidereferences, periodically
cross-checking yourflight instruments.
©
Leadthe roll-out by approximately one-half your angle of bank. Use coordinated aileron and
rudder control pressures as you roll out. Simultaneously, begin releasing the back pressure
on the yokeso aileron, rudder,andelevator(or stabilator) pressures are neutralized when the
airplane reaches the desired heading andaltitude.
2°10
TURNS
Once the desired cruise airspeed has been obtained, reduce power, trim to relieve control
pressures, and lean the mixture (if necessary).
_ CLIMBING TURNS
The PTS doesnotinclude specific criteria for climbing turns using visual references. However,
it does have performance standards for basic instrument constant airspeed climbs and turns to
headings. (See Maneuver #29.)
DESCENDING TURNS
Descendingturnsto preselected headings and altitudes combine the proceduresfor straight descents
with those used in turns. As with climbing turns, you may practice descending turns using a two-
step process. First, you establish the descent attitude, then roll to the desired angle of bank. As you
gain proficiency, you will learn to establish the descent attitude and bank simultaneously.
Maintain the same airspeed in descending turns as in straight descents. However, your rate of
— descent will be higher in a descending turn than in a straight descent with a comparable powerset-
ting becausethe vertical lift component is less when the airplane banks. You can compensate for
— this with a slight addition of power over whatis used in a straight descent.
2-11
After clearing the airspace around yourairplane, apply carburetorheat(if applicable), reduce
power, and lower the nose. Simultaneously, turn toward the desired heading using coordi-
nated aileron and rudder application.
When you reach the desired angle of bank, neutralize the ailerons. Trim to relieve control
pressures.
Maintain the desired descent airspeed and angle of bank using outside references, periodi-
cally cross-checking yourflight instruments.
Lead the roll-out by approximately one-half your angle of bank. Use coordinated aileron and
rudder control pressures as your roll out. Simultaneously, add powerto the cruise setting
and adjust the nose position so aileron, rudder, and elevator(or stabilator) pressures are neu-
tralized whenthe airplane reaches the desired heading andaltitude.
Set the carburetor heat to the COLD position, trim to relieve control pressures, and, if neces-
sary, enrichen the mixture. \
2-12
Oe |
EXERCISES — BASIC MANEUVERS | o~
~ EXERCISES — BASIG
~ MANEUVERS
— 6 — STRAIGHT-AND-LEVEL FLIGHT
a 1. During straight-and-level flight, what is the primary visual reference used for maintaining
altitude and heading?
2. Whatis a safety-related advantage of keeping your eyes primarily focused outside the cockpit?
3. True/False. To maintain straight-and-level flight, you normally need to make a continuous

— series of small adjustments in pitch and bank.
—7 4. Whatis the primary reason for making trim adjustments?

A. To correct heading
B. To changepitch attitude
C. To relieve control pressures
5. How can you determine the magnitudeof a deviation from your desired heading and altitude?
4 ‘7 — GLIMBS
1. Which type of climb speed results in the greatest gain in altitude in the shortest distance?
—_ 2. Which type of climb speed provides the most gain in altitude in the least amountof time?
3. True/False. As the pitch attitude is increased and the airspeed decreases, left-turning tenden-
cies become less pronounced.
4. Would you expect a need for a decrease or increase of right rudder pressure asthe aircraft
accelerates during leveloff?
— 5. What percentage of your vertical speed is normally used to determinethe leadforlevel-

off?
2°13
a EXERCISES — BASIC MANEUVERS
&
x
S — DESCENTS
1. True/False. You can control your rate of descent with pitch attitude.
2. Will a cruise descent result in a higher or lower groundspeedthan a typical descent used for
approachto landing?
3. During a 500 f.p.m. descent, you have been instructed to level off at 4,000 feet MSL. What —
altitude should you begin yourleveloff?
4. True/False. You can decrease your descentrate by lowering theflaps.
5. Would a powerincrease during a constant airspeed, power-on descent require you to raise or
lower the nose to maintain airspeed?
9 — TURNS 4
1. Turns are divided into three classes or types. What are the classes of turns and how many J
degrees of bank are associated with each?
2. True/False. During a level turn, you maintain the same amountof aileron deflection through-
out the turn.
3. What determines howfar an airplanerolls?
4. You are in a climbing turn to the right, using a 30° angle of bank, and have been directed to _
rollout on a heading of 090°. On what heading should you begin yourrollout?
5. How can you compensate for the increased rate of descent you experience in a descending
turn, as opposed to a straight descent?
2-14
AIRPORT
OPERATIONS
MANEUVER 10 BSS SS RBBB RBHRRRRERRRReeeeeeeewe

ee so-Z
NORMAL TAKEOFF AND CLIMB
MANEUVER 1 1 SESS SSBB RBBB eeeeeeeewwe eee

374
GCROSSWIND TAKEOFF AND CLIMB
MANEUVER 12 SSS SSB SSBB BRB RBRBRBBERBRBRBeeeeeeeew eee

376
TRAFFIG PATTERNS
MANEUVER 13 BESS SSB BRB BBR RBRBBRPeeeeeeeeewee se o7 1 A
NORMAL APPROACH AND LANDING
MANEUVER 14 SSS SSBB SSBB BERBER eeeeeeee eee 3-20
CROSSWIND APPROACH AND LANDING
EXE RGIS E Si ucccuncunanncccccnccccnnucnucu

une 3-23

Computer Training — Airport Operations

10 — NORMAL TAKEOFF
AND GLIMB
Each takeoff is affected by the wind conditions, runway surface and length, and possible obstruc-
tions at the end of the runway. The takeoff procedures outlined here are providedas general guide-
lines only. Be sure to consult your airplane’s POH for the proper checklists and procedures.
@ Complete the before takeoff check. With the exceptionof the oil temperature gauge, all engine
instruments must register within the normal operating rangeprior to takeoff.
3" Ensure that the runway,as well as the approach and departure pathsareclear of otheraircraft.
e Atan uncontrolled airport, broadcast your intentions for departure on the commontraffic
advisory frequency (CTAF).
¢ Ata controlled airport, contact the tower and inform them you are ready for departure.
You must obtain a clearance from the control tower prior to taxiing onto the runway, and
prior to takeoff.
© Taxi onto the runway, line up with the runwaycenterline, center the nosewheel, and neu-
tralize the ailerons. Check the windsock to determine the wind position in relation to the
runway and then begin thetakeoffroll.
e Advancethe throttle smoothly to takeoff power, andas theairplanestarts to roll, select a
point on the cowl through which the centerline of the runway passes anduseit as a refer-
ence pointfor directional control. Apply right rudder to counteract engine torque.
/sharply to the left due to the torque effects of the engine

takeoff toensurethatit does notslide back during the takeoff
Jecidetoabortthetakeoff.
¢ Check the engine instruments to ensure the engine is developing full power andis func-
tioning within its operational limits. Slow acceleration or any hesitation in power is suf-
ficient reason to discontinuethe takeoff.
¢ Maintain directional control with the rudder pedals and use a neutral aileron
position if
the wind is aligned with the runway.
PRGRGS Lesteres
c e s eroT teehee
As speedincreases and the controls become moreeffective, reduce rudder pre

ssure to main-
tain directional control and apply slight back pressure to the yoke,
==) Establish the takeoff attitude at the speed recommended by the manufactu
rer. As the air-
planelifts off the runway,notethe nose position in relation to the horizon and the
n maintain
this attitude by using elevator (or stabilator) pressure.
nise tweenholding the nose on the ground and selecting an attitude
> grou long, the airplane tendsto build excessairspeed, which
ude, the airplane may beforcedinto the air prematurely
way. eatsuchahigh angle of attack (high drag condition)thatit
Accelerate to the climb speed recommended by the manufacturer and adjust the
pitch attitude
to maintain the climb speed. Fly the departureleg ofthetraffic pattern straight
out on an exten-
sion of the runwaycenterline. Use right rudderto counteract the airplane’s left
-turning tendency.
Seu tes
ap positionand local conditions, such as the presenceof obstaclesin the

oat
sle c ince speed, best angle-of-climb speed(V), or best rate-of-climb

f Ss hats
wv Once you have reacheda safe altitude, adjust the powerto the recommendedclim
bsetting
and trim to relieve any control pressures. Complete the appropriate checkl
ist procedures,
and depart or remainin thetraffic pattern.
iveapprovalfor any type of departure. The standard pro-

( utorto make a 45° turn in the direction of thetraffic pattern.
TAKEOFF EMERGENCIES
Although an engine malfunction on takeoffis rare, the possibility does exist. If
you experience a power
loss on the takeoff roll, abort the takeoff quickly by movingthe throttle to the
idle position. Use the
rudder to maintain directional control and the brakes as necessary to stop the
airplane. If the engine
malfunction occursjust after liftoff, you should reduce the pitch attitude slig
htly and allow theair-
plane to settle back to the runway.If sufficient runway does not exist, and you
have notyetattained a
safe maneuveringaltitude, you have no choice butto land straight ahead. In this
situation, you should
make only small heading changesto avoid obstacles and should not attemptto
turn back to the runway.
NORMAL TAKEOFF AND CLIMB
¢ Exhibit knowledge of the elements related to a normal and crosswind take

off, climb operations, and rejected
takeoff procedures.
* Position theflight controls for the existing wind conditions.
* Clearthe area; taxiesinto the takeoff position and aligns the airplane on the
runwaycenter/takeoff path.
¢ Lift off at the recommendedairspeed and accelerates to VY.
¢ Establish a pitch attitude that will maintain VY +10/-5 knots.
* Retract the landing gear, if appropriate, and flaps after a positive rate of climb is esta
blished.
¢ Maintain takeoff powerto a safe maneuveringaltitude.
¢ Maintain directional control and proper wind-drift correction throughout the take
off and climb.
¢ Comply with noise abatement procedures.
¢ Complete the appropriate checklist.
3-3
CROSSWIND TAKEOFF AND CLIMB
Sneeeeen De ee ee
1 1
— GROSSWIND TAKE- _
OFF AND GCLIMB =
A crosswind takeoff is much like a normal takeoff, except you haveto use the flight controls to —
counteract the crosswind component. The term crosswind componentrefersto that part of the wind
which actsat a right angle to the airplane’s path on takeoff or landing. You can calculate this com- =
ponent with a crosswind componentchartor with a flight computer.
You should always use the aircraft manufacturer’s recommendedtakeoff checklist. Takeoffs with
strong crosswinds are normally made with the minimumflap setting necessary for the field length. _
This helps reduce the drift angle immediately after takeoff. The POH normally lists a maximum
demonstrated crosswind component for takeoff and landing. Your personal crosswindlimit is based —
on yourskill level, as well as any limitation specified by yourinstructor during training. In addition,
flight training operators often have specified limits based on pilot experience and/or proficiency. —
Complete the before takeoff check. With the exception of the oil temperature gauge, all engine —s
instruments must register within the normal operating range prior to takeoff.
J Ensure that the runway, as well as the approach and departure pathsare clearof otheraircraft.
~ After obtaining a clearance (at a controlled airport) or self announcing yourintentions (at an
En,
uncontrolled airport), taxi onto the runwayand line up with the runwaycenterline. Center the —
nosewheel and check the windsock to determine the windpositionin relation to the runway.
¢ Fully turn the yokein the direction of the wind, placing the upwindaileron in the up posi-
tion, For example, if the crosswind is blowing from yourleft, fully turn the yoke totheleft, =_
placing theleft aileron in the up position. This control deflection compensates forthe cross-
wind’s tendencyto push androll the airplane to the downwindside of the runway. 7
eaten 9ce elie ca
— ¢ Advancethe throttle smoothly to takeoff power, andas the airplanestarts to roll, select a
point on the cowl through which the centerline of the runway passes anduseit as a refer-
— ence point for directional control.
— ¢ Check the engine instruments to ensure the engine is developing full power andis func-
tioning within its operational limits. Slow acceleration or any hesitation in power is suf-
— | ficient reason to discontinuethetakeoff,
—, _ © Counteract the airplane’s weathervaning tendency with rudder application.
— As the airplane accelerates and the controls become moreeffective, reducethe aileron deflec-
tion gradually soit is just sufficient to counteract the rolling tendency. Apply right rudder
— pressure as necessary to compensate for engine torque.
fy Toallow the airplane to havea greater airspeed on liftoff with increased control capabilities,
— = hold the airplane on the runway until you attain a slightly higher-than-normalliftoff speed.
Then, lift the airplane off the runway promptly and establish a normal climb attitude. This
— technique also reduces the chanceof the airplane beinglifted off prematurely by a sudden
gust of wind.
Accelerate to the initial climb speed recommendedby the manufacturer and adjust the pitch
— attitude to maintain that airspeed. To track straight out on an imaginary extension of the
runway centerline, enter a crab by making a coordinatedturn into the wind.
Wg Once you havereached a safealtitude, adjust the power to the recommendedclimbsetting

— and trim the aircraft to relieve any control pressures. Complete the appropriate checklist
procedures and depart or remain in thetraffic pattern.
_ To meet the PTS requirements, you must:
¢ Exhibit knowledgeof the elements related to a normal and crosswind takeoff, climb operations, and
rejected takeoff procedures.
¢ Position the flight controls for the existing wind conditions.
¢ Clear the area;taxi into the takeoff position and align the airplane on the runway center/takeoff path.
¢ Lift off at the recommendedairspeed and accelerates to VY.
¢ Establish a pitch attitude that will maintain VY +10/-5 knots.
¢ Retract the landing gear, if appropriate, and flaps after a positive rate of climb is established.
— e Maintain takeoff powerto a safe maneuveringaltitude.
¢ Maintain directional control and proper wind-drift correction throughout the takeoff and climb.
¢ Comply with noise abatement procedures.
— ¢ Complete the appropriate checklist.
3-5
TRAFFIC PATTERNS |
12 — TRAFFIC PATTERNS
Standard traffic patterns are used to improve both the safety and efficiency of airport operations.
They are particularly important at airports without operating control towers. The standard traffic
pattern is rectangular and has five named legs; downwind,base, final, departure, and crosswind.
The direction of the pattern refers to the orientation of the pattern turns. For example, aircraft in
a left-hand traffic pattern makeleft turns to base, final, crosswind, and downwind. Normally, a
left-hand pattern is usedto givetheleft-seat pilot the best view of the runway andthe surrounding
environment. In somecases, a right-hand traffic pattern may be used to avoid obstacles, terrain,
restricted airspace, noise sensitive areas, or other runways. Both left-hand and right-handtraf-
fic patterns normally are used when simultaneous operations are conducted on parallel runways.
Other special considerations may require additional variations to the standard traffic pattern. You
can find information regarding specific airport traffic patterns in the Airport/Facility Directory,
Aeronautical Information Manual, FAR Part 93, and Notices to Airmen (NOTAMs).
Collision avoidance rests with you, the pilot in command. Airport operations require a constant ~
effort to see and avoid other aircraft. You should make a point of checking both the approach and
departure ends of the runwayprior to takeoff or landing. ~]
Fs]
Wy
|
TRAFFIC PATTERNS
A runway incursion is an occurrence at an airport involving an aircraft, vehicle, person, or object

on the groundthat creates a collision hazard or results in loss of proper separation with an aircraft
taking off or landing. Runwayincursions usually are caused by errors associated with clearances,
communications, airport surface movement, and positional awareness.
| eneficialinavoiding runwayincursions.
con, tructionand lighting.

oncentr ate onyourprimary responsibilities. Do not become
In addition to collision avoidance precautions, anytime you operate in close proximity to other
aircraft, such asin thetraffic pattern, you should be awareof the increased potential for wake turbu-
lence encounters. When possible, avoiding the area below and behindotheraircraft should prevent
you from experiencing most of the in-flight hazards associated with wake turbulence,
WW WA
.
AN
|
TRAFFIC PATTERNS
Since wind shear can occur during traffic pattern operations, you also should be knowledgeable of J
the conditions favorable for wind shear. Anticipate wind shear whenfrontal systems and thunder-
stormsare in thearea. —
At airports with operating control towers(controlled airports), you are required by regulations to
establish and maintain radio communication with the tower. At airports without control towers
(uncontrolled airports), you are not required to have or use a radio. However, if your aircraft is
radio equipped while operating within 10 miles of any airport, you should monitor and com-
municate on the common traffic advisory frequency (CTAF). The CTAF may be a UNICOM,
MULTICOM, flight service station (FSS), or tower frequency. Before you transmit on the CTAF.
you should monitorthe frequency for a shortperiod oftimeto get a picture ofthe traffic situation
and determine a plan of action for entry to the pattern. When making your radio calls, always
report youraircraft identification, position, and intentions. Also be sure to include the name of
the airport in broadcasts, since more than one airport may be assigned the same frequency. An
example of a radio call requesting airport information is as follows: “Coronado UNICOM, Cessna
23455, 10 miles northwest descending through 4,000, landing Coronado, request wind and run-
way information Coronado.”
In the absence of an FSS, UNICOM operator, or operating control tower, you should overfly the
airport at least 500 feet above thetraffic pattern altitude to determine the landing runway andthe J
associated pattern direction. Use visual indicators such as the segmentedcircle, wind direction
indicator, landing direction indicator, ortraffic pattern indicator. An exampleof a radio call for an
|
aircraft conducting an overflight of the airport to determine the landing informationis as follows:
“Coronadotraffic, Cessna 23455, 10 miles south descending through 4,000, overflying for landing
|
Coronado.”
J
peee tteets ge eeeeee
cetaceaneeteeeeeereer
|
:
Enter the traffic pattern at a 45° angle to the downwind leg, abeam the midpointof the
runway, at pattern altitude (normally 1,000 feet AGL). An example of a radio call at an
uncontrolled airport is as follows: “Coronadotraffic, Cessna 23455, entering downwind for
Runway 9, touch-and-go, Coronado.”
es Fly the downwindleg parallel to the runway. Maintain pattern altitude until at the 180°
position, or position abeam the intended landing point. At the 180° position, begin your
descent for landing.
of yourdescentto follow othertraffic in the pattern.
© Turn onto the base leg when the touchdownpoint is approximately 45° behind the inside
wingtip. An example of radio call at an uncontrolled airport is as follows: “Coronado traffic
Cessna 23455, base, Runway 9, touch-and-go, Coronado.”
Seo Sot oO
edusing approximately 30° angle of bank. Adjust the baselegto follow other traffic
id conditions. For example, with a strong wind you will need to begin your turn
to
you do notdrift too far downwind during your turn.
TRAFFIC PATTERNS
@ Complete the turn to final approach at least one-quarter of a mile from the approach end of
} J JJ J J J Ld]
the runway. Fly along an imaginary extension of the runway centerline, compensating for
crosswind conditions as needed. An example ofa radio call at an uncontrolled airportis as
follows: “Coronadotraffic, Cessna 23455,final, Runway 9, touch and go, Coronado.”
On the departureleg, climb out on runway heading until you are beyond the departure end
of the runway and within 300feet of pattern altitude. An example of a radio call at an uncon-
trolled airport for an aircraft remaining in thepatternis as follows: “Coronado traffic, Cessna
23455, departing Runway 9, remaining in the pattern, Coronado.”
} _|
J} |
6) If you are departing the traffic pattern, continue your climb to pattern altitude, then fly
straight out, or exit with a 45° turn to the pattern side of the runway. In either case, you
should comply with the departure procedures established for that airport. An example of a
radio call at an uncontrolled airport for an aircraft departing thetraffic pattern is as follows:
“Coronadotraffic, Cessna 23455, departing Runway9, departing the traffic pattern to the
northeast, climbing to 5,500, Coronado.”
tra kdoesnot penetrate the departure path
|
ou should monitor/communicate on the
JJ
ws If you are staying in thetraffic pattern, continue your climb to pattern altitude on the cross-
wind leg. Once at pattern altitude, level off and continue to fly 90° to the runwayuntil you
are ready to turn downwind.
5 vind.Ifnecessary, extend your departur

e
i ot)
3-10
TRAFFIC PATTERNS
3-11
13 — NORMAL APPROACH ~
AND LANDING —
The successful landingof an aircraft is probably the most challenging, as well as satisfying, phase of a
flight. Every landingis different due to varying wind conditions, runway surface and length, and pos-
sible obstructions at the approach end of the runway.In addition, the airplane can be configured for
landing with no flaps, partial flaps, or full flaps. When you usefull flaps for landing, you will typically
extend thefirst increment of flaps on the downwind leg and the next on base leg. Usually, you will
extend full flaps on the final approachleg. Since the full-flap stall speed is less than the no-flap or par-
tial-flap stall speed, landing with full flaps results in a slower touchdown speed andshorter groundroll.
The following discussion provides general procedures for a no-flap landingin a tricycle gear airplane.
APPROACH am
Prior to each landing, you should complete a before landing check using a printed checklist as rec-
ommended by the aircraft manufacturer. As you fly thetraffic pattern and approachto landing, be
sure to self-announce your position and/or intentions on the appropriate frequency in accordance
with recommended procedures or communicate with the control tower, as appropriate.
On downwind, ensure that the before landing checklist is completed and clear the area
ahead andto theleft and right of yourflight path for othertraffic. In addition, checkfortraf-
fic which may be above and descending or below and climbing through yourflight path.
e As you approach the 180° position, or position abeam the intended landing point, you —
should be at the designated traffic pattern altitude near the airplane’s cruising speed.
¢ At the 180° position, establish the descent power setting while maintaining altitude to
allow the airplane to slow to approachspeed.
e Maintain the approach speed recommended by the manufacturer andinitiate a descent.

ee oS — Te ee SS a ee ee ee
‘ Pare a‘ le
sl
7’
=— -
3-12
wd Checkfor traffic on the base leg and on the extended runway centerlineof the final approach.
Begin yourturn to the baseleg after the airplane has descended 100 to 200 feet and the land-
base, | newindtendstopush the airplane away from the runway. Therefore, it usually is necessary to turn
0 a £
appropriatecrabangle.
33 91
Seat sy otter EN
Pe et 53;
As the airplanerolls out on base, youare at the key position, an early decision point where
you must assess your situation. At the key position you should make any adjustments to
altitude, airspeed, and distance from the runway to ensure a smooth approach andto avoid
large or abrupt last minute corrections on shortfinal.
PER tt hinoe eee £5 55-4 : x - 2
aS > r> 2
heairplaneishighat 2 keyp OS ition, you should either reduce power, extend addi
ES
SyFs: <sseas SSS eS
: See
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qeehitioes IP ERs
aees t SI Se ee
ESS SEES Sets ese BS SiS
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tionalflaps, or both to avoid landing

aie ae es SS. 2 x
lesired ouchdownpoint.If the airplane is low or wide on baseleg,orif the wind is stronger than norm
al,
e Checkthe final approach pathfortraffic and, if clear, start your turn.

¢ Roll out on final approach between 300 and 500 feet above groundlevel, and approxi-
mately one-quarter mile from the end of the runway.
Janairplane with retractable landing gear, re-check that the
* Maintain the recommended approach speed. If an |) ———=—i.

se
approachspeedis not recommended in the POH, use — ae a ,

a final approach speedthatis 1.3 times the power-off
stall speed in the landing configuration (1.3Vs9).
e Use outside visual references to determinethe proper
descent angle, or glide path.
peea
$i
dage eeea
5 SESS ao pe
eSSS ters Se? Sees f-2 >
Sine S §S PeeTe Eee

PaeS"3158 poeeerearees
Gle
apparent shape of the runway will remain 4 ’ he LS

_ unchanged.If your approach becomesshallower, | =
runwaywill appear to shorten and become
wider.Conversely,if your approach is steepened,
1appeartobe longer and narrower.
ee vou maintain tantdescent angle, the sides
SN iy vag Bee
= at r ‘same relationsh
ip
3-13
¢ Simultaneously adjust pitch and poweras necessary to control descent angle and air- —
speed. If a deviation in pitch attitude, power, airspeed, or wind condition occurs, make
an appropriate control change to maintain the proper descent angle. on
n |mi ntain pitch attitude.

sr anddecreasethepitch attitude.
ethepitch attitude slightly. You should
1gli >byapplying back pressure onthe
¢ Estimate the point at which the airplane will actually touch down by finding the point
where the descent angle intersects the ground and addingthe approximate distance to be =
traveled in the flare. The descent angle intersection point, also called the aiming point, is
the spot on the groundthat has no apparentrelative movement. As the airplane descends, —-
all objects beyond the aiming point appear to move awayfrom the airplane, while objects
closer appear to move towardit. —-
SIDE VIEW OF AIMING POINT
LANDING
During the landing you use a combination of visual and kinesthetic cues. Practicing descents, slow
flight, and power-offstalls helps to increase your sensitivity to control responses and allowsyou to
develop smooth control application. However, your kinesthetic sense may not be fully developed
at the time you begin landing practice and you must rely primarily on visual cues. The landing
3-14 consists of three elements — the flare, the touchdown, andthe roll-out. The term flare refers to the
NORMAL APPROAGH AND LANDING
= process of changingtheattitude of the airplane from glide or descentto a landing attitude. Its pur-
pose is to reduce speed and decreasethe rate of descent. Theflare begins at different altitudes for
— airplanes at varying weights and approach speeds. However, for most training airplanesit beginsat
approximately 10 to 20 feet above the ground.
—— ¢ Begin the flare approximately 10 to 20 feet above the runway by gradually increasing back
pressure on the yoke to reduce speed anddecreasetherate of descent.
e Focus at an intermediate point between the noseofthe airplane and a distance downthe
runway. During the flare, you must look to oneside of the airplane, since its nose may
block your view ahead.
a ¢ The airplane should reach a near-zero rate of descent approximately 1 foot above the run-
wayat about 8 to 10 knots above a stall speed with the power atidle.
e Attempt to hold the airplane just off the runway by increasing back pressure. This
a causes the airplaneto settle slowly to the runwayin slightly nose-high attitude as
it approachesstall speed.
focusyourvision during the approachis important. For

HUT ;obje sonthe ground and youractions may be too
ratelyjudge height above the ground and your
ontothe runway withoutflaring.
© ToucHpown
_ ¢ Touch down on the main landinggear in a nose-high attitude with the engine idling and
the airplane at minimum controllableairspeed. 3-15
e lor so there is no tendency to use the brakes inadvertently.
¢ Use the rudderto keep the airplane’s longitudinal axis parallel to the direction the air-
plane is moving along the runway.
¢ Hold back pressure on the yoke to maintain a positive angle of attack for aerodynamic
braking and to hold the nosewheeloff the ground.
¢ Asthe airplane decelerates, gradually relax back pressure to allow the nosewheelto gently
settle onto the runway.
peedcan cause floating or

skipping and mayresult in
a loss of
es ROLL-OUT
¢ Maintain directional control with the rudderto keep the airplane on the centerline of
the runway.
e Clear the runway and complete the after landing checklist. Taxi to the designated
parkingor refuelingarea.
¢ Exhibit knowledge of the elements related to a normal and crosswind approach and landing.
¢ Consider the wind conditions, landing surface, obstructions, and select a suitable touchdown point.
¢ Establish the recommended approach and landing configuration and airspeed, and adjustpitch
attitude and poweras required.
¢ Maintain a stabilized approach and recommendedairspeed, or in its absence, not more than 1.3 Voso,
+10/-5 knots, with wind gust factor applied.
¢ Make smooth,timely, and correct control application during the roundout and touchdown.
¢ Touch down smoothly at approximate stalling speed.
¢ Touch downat or within 400 feet (120 meters) beyond a specified point, with no drift, and with the
airplane’s longitudinal axis aligned with and over the runway center/landing path.
¢ Maintain crosswind correction and directional control throughout the approach and landing sequence.
FORWARD SLIP TO A LANDING

A forward slip may be used to steepen the airplane’s descent angle to dissipate altitude without
increasing airspeed. This is accomplished by exposing as muchofthe airplane’s surface to the
oncoming air as possible, so the airplane’s frontal area produces considerable drag. A forwardslip
3-16 can be valuable when youare landingin fields with obstructions. In an airplane with side-by-side
NORMAL APPROAGH AND LANDING
——e Dee ee eed
Se eetttereer eee ee a ee eeee
Ae . Fs : :
seating, you will usually slip to the left since this provides you with an excellent view ofthe land-
ing area during theentireslip.
You should perform forward slips with the engine at idle powerto increase the rate of descent. To
initiate a forwardslip, lower one wing by turning the yoke andat the sametime, apply opposite rud-
der to keep the airplane from turning in the direction of the lowered wing. The airplane’s nose will
angle away from the runway, howeverthe airplane’s ground track remains in alignment with the
extended centerline of the runway. To preventthe airspeed from increasing, raise the noseslightly
above the normal gliding position. As soon as you lose sufficient altitude. begin the recovery by
raising the low wing and simultaneously easing rudder pressure. Level the Wings and adjust the
pitch attitude to a normalglide.
Anothertype of slip is the sideslip which is used to compensate for drift during crosswind land-
_ ings. During a sideslip, the airplane’s longitudinal axis remains parallel to the original flight path
and is aligned with the runway. You will learn more about performing sideslips when you examine
— crosswind landings.
. FORWARDSLIP TO A LANDING
~ To meet the PTS requirements, you must:
* Exhibit knowledge of the elements related to a normal and crosswind approach and landing.
¢ Consider the wind conditions, landing surface, obstructions, and select a suitable touchdown point.
* Establish the slipping attitude at the point from which a landing can be made using the recommended
approach andlanding configuration and airspeed; adjusts pitch attitude and power as required.
¢ Maintain a ground track aligned with the runway center/landing path and an airspeed, which results in
minimum float during the roundout.
¢ Make smooth, timely, and correct control application during the recovery from the slip, the roundout and
the touchdown.
¢ Touch down smoothly at approximate stalling speed, at or within 400 feet (120 meters) beyond a
specified point, with no side drift, and with the airplane’s longitudinal axis aligned with and over the
runway center/landing path.
(50-AROUND
Generally, if the airplane has not touched downinthe first third of the runway, you should execute
a go-around, and set up for another landing. The go-around also may be necessary when obstacles
are on the runway or when you feel uncomfortable with the approach dueto incorrect procedures
or other unsafe conditions. At times, you may perform landings that cause the airplane to bounce
into the air. Usually, it is wise not to attempt to salvage these landings and you should make an
immediate go-around. The decision to make a go-around should be positive, and you should make
it before a critical situation develops. Once the decision has been made, it should be implemented
without hesitation.
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|
Apply takeoff power immediately, place the carburetor heat in the OFF position, and adjust
the airplane’s pitch attitude to slow or stop the descent. After the descent has been stopped,
partially retract the flaps (if applicable) as recommendedby the manufacturer.
reco mmended that the flaps be retracted in small increments

2retractionofflaps causesa lossoflift which could result
Establish a positive rate of climb. If anotheraircraft is on the runway, make a shallow turn
to the non-pattern side of the runway, then turn parallel to the runway.In this position, you
can see the runwayandotheraircraft clearly.
Retract the landing gear(if applicable), and accelerate to Vy before retracting the remaining
flaps. Trim to relieve control pressures.
3-18
NORMAL APPROAGH AND LANDING LV
rt | \
@ After you have the airplane under control and have reacheda safe altitude, self-announce
your position and/or intentions on the appropriate frequency in accordance with recom-
mendedprocedures or communicate with the control tower, as appropriate. Maintain direc-
tional control and apply proper wind drift as you continue the flight parallel to the departure
leg. When youreach the crosswindlegallow for proper spacing, checkfortraffic, and then
reenter the traffic pattern as appropriate.
3-19
| GROSSWIND APPROAGH AND LANDING
\
14 — CROSSWIND
There are two basic techniques used to accomplish a crosswind approach and landing — the crab
method and the wing-low,or sideslip, method. The crab method requires you to establish a head-
ing (crab) into the wind onfinal approach with the wings level so that the airplane’s ground track
remains aligned with the extendedcenterline of the runway. The crab angle is maintained until just
prior to touchdown, whenthe longitudinal axis of the airplane must be quickly aligned with the
runway to avoid imposing any side loads on the main landinggear.
Since the crab method requires a high degree of judgment and timing, the wing-low methodisnor-
mally preferred for executing crosswind landings. The wing-low methodof crosswind approach and
landing is described here. Since the same general procedures used to execute a normal approach
and landing apply to a crosswind approach and landing, only the additional techniques required for
windcorrection are explained in this discussion. The wing-low method enables you to simultane-
ously keep the airplane’s groundtrack and the longitudinal axis aligned with the runwaycenterline
throughout the final approach,flare, touchdown, and roll-out. This technique prevents the airplane
from touching downsideways, imposing damagingside loads on the landinggear.
The degree to which flaps should be extended in a crosswind varies with the airplane’s handling
characteristics, as well as the wind velocity. Full flaps may be usedif the crosswind componentis
abilit yOL. lniesstheman ro icturerrecommendsotherwise.
<<
not in excess of the airplane’s Cap
‘“SEEe<3e3 ae Sos oe ee
APPROACH
If the crosswindexists at traffic pattern altitude as well as near the surface, you must apply the proper
windcorrection (crab) in the traffic pattern so your ground track remains rectangular. Since the wind
direction is perpendicular to the runway, you mustcrab into the wind on the downwind leg to remain
parallel to the runway. Onbase leg, you will either encounter a tailwind or headwind. Your ground-
speed increases with a tailwind component and you mayneedto start your turn to final sooner than
3-20 normal and/or use up to 30° of bankto avoid overshooting the runway. When encountering a headwind
on baseleg, avoid turningtoo early or using too much bankangle so you do not undershoot the runway.
Complete the turn to final on an extension of the runway centerline with the airplane in a
crab to correct for winddrift.
vs Align the airplane’s heading with the runwaycenterline, note the rate anddirection ofdrift,
and then apply correction by lowering the upwind wing. Simultaneously apply opposite
rudder to preventthe airplane from turning and keep the longitudinal axis aligned with the
runway. For example, if the crosswind is blowing from yourleft, turn the yoketo theleft,
placing the left aileron in the up position and apply right rudder.
rectionmustbe reducedortheairplane will no longer be aligned with the runway
you maynot have sufficient ruddertravel available to compensatefor the strong
In thissituation, you must go-around and land on a runwaywith morefavor-
LANDING
Maintaining accurate directional control while the airplane’s speed is decreasing is a challenge
during crosswindlandings.
) FLARE
e Asairspeed decreases in the flare, the flight controls becomelesseffective and you mustgradu-
ally increasethe rudderand aileron deflection to maintain the proper amountof windcorrection.
@ ToucHDown
¢ Maintain the crosswindcorrection as the airplane touches down.Initially, the airplanewill
touch down on the upwind wheel and then as forward momentum decreases, the weight of
the airplane causes the downwind main wheel to gradually settle onto the runway.
¢ Since you are holding opposite rudderpressureto correct for the crosswind, the nosewheel
may notbe aligned with the runwayas the airplane touches down. To prevent swerving on
the runway, you must relax the corrective rudder pressure just as the nosewheel touches
down.
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¢ Maintain directional control with the rudder while keeping the upwind wing from rising
by use of the aileron.
e As the airplane decelerates and the controls becomeless effective, increase your wind
correction with the ailerons. Turn the yoke fully into the windasthe airplane slows to a
taxi speed. Clear the runway and completetheafter landing checklist.
¢ Exhibit knowledge of the elements related to a normal and crosswind approach andlanding.
e Adequately survey the intended landing area.
* Consider the wind conditions, landing surface, obstructions, and select a suitable touchdown point.
e Establish the recommended approach andlanding configuration and airspeed, and adjustpitch attitude
and power as required.
e Maintain a stabilized approach and recommended airspeed,orin it absence, not more than 1.3 VSO,+10/-5
knots, with wind gust factor applied.
e Make smooth, timely, and correct control application during the roundout and touchdown.
¢ Touch down smoothly at approximatestalling speed.
¢ Touch downat or within 400 feet (120 meters) beyond a specified point, with no drift, and with the airplane’s
longitudinal axis aligned with and over the runway center/landing path.
¢ Maintain crosswind correction and directional contro! throughout the approach and landing sequence.
* Complete the appropriate checklist. 3-21

3-22
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EXERCISES — AIROPORT OPERATIONS
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EXERCISES — AIR-
PORT OPERATIONS
10 — NORMAL TAKEOFF AND CLIMB
1. What action should youtakeif the engineis not developing sufficient powerfor takeoff? ?
2, How can you counteracttheleft-turning tendency caused by engine torque on takeoff?
3. Why should you keep your hand onthe throttle throughout the takeoff?
4, What can occur if you attemptto lift off with an excessively nose-high attitude?
5. After a normal takeoff at an uncontrolled airport, what are the recommended proceduresfor
leaving the local area?
11 — GROSSWIND TAKEOFF AND CLIMB

1. How can you determine the maximum demonstrated crosswind componentfor yourairplane?
2. True/False. To counteract the effects of a crosswind from theleft during takeoff, you should
turn the yoke to theright, placing the left aileron in the down position.
3. As the airplane accelerates during the takeoff roll, will you normally need to increase or
decreaseaileron deflection used to compensate for a crosswind?
4, How can you determineif are using the proper amountof crosswindcorrection?
5. After takeoff, what action can you take to track straight out on an imaginary extension of the
runway centerline?
3°23
EXERCISES — AIRPORT OPERATIONS
12 — TRAFFIC PATTERNS
1. Whatare the five namedlegsof thetraffic pattern?
True/False. Both left-hand andright-handtraffic patterns are normally used when simultane-
ous operations are conducted on parallel runways.
. To aid in collision avoidance, you should turn on yourairplane’s landing light within how
many miles of the airport?
In the absence of an FSS, UNICOM operator, or operating control tower, you should overfly
the airport at least how manyfeet abovethetraffic pattern altitude?
. Your airplane is Piper 9163K and you are practicing touch-and-go landings to Runway 26 at
Front Range Airport (uncontrolled). Provide an exampleof the properradiocall after completing
the turn to final.
13 — NORMAL APPROACH AND LANDING

1. True/False. Landing with full flaps extended results in a faster touchdown speed and ground
roll.
. At what position on the downwindshould you normally begin your descent for landing?
. What corrective actions can youtakeif the airplane is high when youreach the key position?
. While on final approach, if the airplane’s descent angle is too shallow and the airspeed is too
low, what action should youtake?
. The landing phase offlight can be divided into what three elements?
While maintaining directional control with the rudder pedals, why should your heels be on
the floor as the airplane touches down?
3-24
EXERCISES — AIROPORT OPERATIONS | a
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7. During landing, floating can be caused by whaterror?
Whatis the primary purpose ofthe forward slip?
True/False. While executing a forward slip, the airplane’s longitudinal axisis aligned with
the runway.
10. Whatis the first step you should take wheninitiating a go-around?
14 — GROSSWIND APPROACH
AND LANDING
As Whatare the two basic methods usedfor crosswind landings?
If you experiencea tailwind on baseleg, whataction(s) can you take to avoid overshooting the
runway when turning onto final approach?
. If you encountera crosswind from theright on final approach and landing, how should you
position the controls to compensate for wind drift?
A. Turn the yoketo the left and apply left rudder pressure.
B. Turn the yoke to the left and apply right rudder pressure.
C. Turn the yoketo the right and apply left rudder pressure.
While making a crosswindcorrection on final approach, what action should you takeif you
do not have sufficient ruddertravel available?
. As the airplane decelerates during the roll-out, will you need to increase or decrease aileron
deflection to counteract a steady crosswind?
3-25
3-26
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EMERGENCY
LANDING
PROCEDURES
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SYSTEMS AND EQUIPMENT
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Computer Training — Emergency Landing Procedures

SYSTEMS AND EQUIPMENT MALFUNCTIONS —_—
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15 — SYSTEMS ‘
AND EQUIPMENT -
MALFUNCTIONS -
There are some emergency conditions that do not appear in checklists or in your airplane’s POH.
Althoughthese situations are not specifically addressed, the FAA provides some general recommen-
dations for dealing with them. The procedures are not intended to be used in lieu of the particular
recommendations that may be provided by a manufacturer, but rather in their absence.
IN-FLIGHT FIRE —
If you experience a fire while in flight, follow the checklist procedures specified in the POH for
your airplane and declare an emergencybyradio. The checklist may address only one type ofin- ee
flight fire or it might include proceduresfor different types of fires ranging from cabin and electrical
fires to enginefires. In any event, follow the appropriate procedure for the situation. In addition, a —
general recommendation maybeof benefit to you during such an emergency. Should thefire and
flames be visible outside the cabin during the emergencydescent, attempt to slip away from thefire —
as much as possible. For example, if the fire is observed on the left side of the airplane, slip to the
right. This may movethefire awayfrom the cabin. —
PARTIAL POWER LOSS —

It is possible that during a flight you may experience a partial loss of engine power. Two options
might be available to you, depending on the degree of power loss and the airplane’s resulting
decrease in performance. You maybe able to continuethe flight in a reduced power condition
as long as you are able to hold altitude or climb. In this situation, maintain an airspeed that will
provide the best airplane performanceavailable. In most cases, the best performanceairspeed will
be approximatelythe best glide speed. However, it is also possible the engine will not continueto
run in this condition and a forced landing will still need to be made. With an engine problem, you
should continually monitor your engine instruments and update your choice of landing options.
Alternatively, your airplane’s performance with partial power may not be sufficient to maintain
altitude. In this case, a forced landing is imminent. Consequently, you will need to declare an
emergency with ATC and begin the emergencyapproach and landing proceduresspecified in your
airplane’s checklist.
DOOR OPENING IN FLIGHT

A cabin or baggage compartment door openingin flight can be a disconcerting event. Although a
door generally will not open veryfar, the sudden noise can bestartling. Regardless of the noise
and confusion, it is important to maintain control of the airplane, particularly during departure.
Accidents have occurred on takeoff because pilots have stopped flying the airplane to concentrate
on closing cabin or baggage doors.
While an open doordoes not normally compromise airplane control, it is possible that control will
become more difficult. If such a condition should occur it may be necessary to increase airspeed
in all phasesof flight, including the approach, in order to ensure that you can control theairplane.
Once you have adequate airplane control, land as soon as practical and securethe door.
ASYMMETRICAL FLAP EXTENSION —

An unexpected rolling motion during flap extension maybe due to an asymmetrical or split flap
condition. If one flap extends while the other remainsin place, a differential in lift across the wing =
is the cause of the rolling motion. A split flap condition can be hazardous, particularly in thetraffic
pattern or during a turn at lowaltitude. —
en
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‘ous situation should an asymmetrical flap extension occur.If the

‘imme diately return the flap control to the up, or the previous
beinthe approach phaseofthetraffic pattern when an
SYSTEMS AND EQUIPMENT MALFUNCTIONS
¢ Exhibit knowledge of the elements related to system and equipment malfunctions appropriate to the
airplane provided for the practical test.
¢ Analyze the situation and take appropriate action for simulated emergencies appropriate to the
airplane provided for the practical test for at least three (3) of the following:
a. Partial or complete powerloss.
. Engine roughnessor overheat.
enna
. Carburetoror inductionicing.
Ca
. Loss of oil pressure.

momenta
. Fuel starvation.
ND
. Electrical malfunction.
let
. Vacuum/pressure, and associated flight instruments malfunction.

ae
. Pitot/static.
dad
. Landing gearor flap malfunction.

j. Inoperative trim.
k. Inadvertent door or window opening.
|. Structural icing.
m. Smoke/fire/engine compartment fire.
n. Any other emergency appropriate to the airplane.
e Follow the appropriate checklist or procedure.

EMERGENCY APPROAGH AND LANDING
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16 —EMERGENGCY
APPROAGH AND
LANDING
Modern airplane engines are extremely reliable and actual mechanical malfunctionsarerare.
However, due to inadvertent fuel exhaustion or an engine component malfunction you couldfind
yourself making an emergency approach and landing. Using a checklist is the best way to ensure
that items are not omitted from an emergencyprocedure. In some cases, however, you may not
have time to review or even access a checklist. To help you respond quickly to an emergency,
some checklists have immediate action items printed in bold type which should be committed to
memory. In addition, you should always maintain situational awareness and be constantly on the
alert for suitable emergency landing fields. The following guidelines, as well as frequent practice
with your flight instructor, will help you develop the ability to plan and methodically execute
emergency landing procedures.
Since most practice emergency landing approaches terminate in a go-around, it is possible for you
to fall into the habit of considering the procedure as just another training exercise. To avoidthis,
assumethat each simulated emergency may actuallyresult in a landing. The following generalsteps
are used to cope with an emergencylandingsituation.
1. Maintain control of the airplane and adjust the pitch to achieve best glide speed. Oncetheglide
speed is attained, trim to relieve control pressures and to aid in maintaining the properattitude
and airspeed.
eactionitem. Normally, you will need to apply back pressure to the yoke to slow
a e and speed. However, if your airspeed is below the best
glide speed at the
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2. Scan the terrain around the airplane andselect a suitable field that is within gliding distance
from your presentaltitude.
e Whenselecting a field, you must consider the wind direction and speed, length of the field,
obstructions, and surface condition. A long field positioned into the wind, with a firm, smooth
surface that is free of obstructions is the most desirable.
e Avoid fields which have large boulders, ditches, or other landing hazards. If you choose a
plowedfield, the landing should be madeparallel to the furrows. When considering a road, be
alert for powerlines, signs, and automobile traffic.
e Evaluate your options if a field with ideal landing features is not available. For example, it
may be better to accept a crosswind landing on a longfield, rather than attemptto land into
the wind on a very short field. On another occasion, a downwindlanding with light winds and
no obstructions maybe preferable to a landing into the wind with numerousobstacles.
the terrain aheadof the airplane, since you may havejust flown by field
e ‘the wing blocks the areato the right andleft of the airplane so you may
3. Turn toward the intended landing field.
e Dissipate any excessaltitude near the field so you are in a good position to observe thefield
carefully for wires, fences, holes, tree stumps, or other hazards.
e A circling approachoverthe field allows you to make adjustmentsfor altitude and keeps you
in a position from which you canreachthefield.
e Advise your passengersto fasten their seatbelts and shoulder harnesses.
urgroundspeedandglide distance. Conversely, turning downwindwil

increas de distance.Theestimation of glide distanceis difficult so it is inadvisable to circle
awe y tromtne Telaand 1 ryto.mak ce ¢ longstraight-in glide to the field.
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4. Follow an appropriate emergency checklist and attempt to determine the cause of the power
failure. Restart the engine, if possible.
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¢ If applicable, place the carburetor heat control to the ON position.
¢ Movethefuel selector to the BOTH position or select the fullest tank.
e Adjust the mixture to the full RICH position.
¢ Switch the fuel pump ON(if installed).
¢ Check the ignition switch and select the BOTH position, or engage the starter if the propeller
is stopped.
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5. Set up a landing approachto the selected field. Attempt to maneuverthe airplaneto be at the
180° position on downwind when you reach a normaltraffic pattern altitude. From this point,
you can perform a normal power-off approach.
ower fail : too low ort 2¢ istancetoa suitable landingfield is too great, you may
pc ccurs, plan theapproach sotheairplanecanintercept the nor-
nmay bethekey position. Keep in mindthe distance
a :ditch,the aiming point must be on the near side
e If time permits, use your radio and declare an emergency, giving your position as accurately
as possible. In addition, set your transponder to the emergency code of 7700.
6. Most POHs provide a checklist for shutting down the engine and configuring the airplane once
the landing is assured. During a practice emergency landing procedure, your instructor may
have you simulate performing items on the checklist.
¢ Set the mixture to IDLE CUT OFF.
¢ Movethe fuel selector to the OFF position.
4-7
¢ Turn the ignition switch to the OFFposition.
ot be lowered until you are confident of reaching the

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¢ Position the flaps as recommended by the POH.
¢ Toggle the master switch to the OFFposition.
7. In an actual emergency landing, touch down on the main wheelsfirst, then gently lower the nose
of the airplane. Apply the brakes as required to stop the airplane. During a practice emergency —_
landing, initiate a go-around whenyour instructor specifies.
EXERCISES — EMERGENCY LANDING PROCEDURES Le
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~ EXERCISES —
~- EMERGENGY LANDING
— PROCEDURES
15 — SYSTEMS AND EQUIPMENT
~~ MALFUNCTIONS
1. What should you do if you experiencean in-flightfire?
— 2. If you experiencea partial power loss, what options do you have?
3. Whataction is advised if a door opensin flight?
4. How can you counter a sudden, unexpected rolling motion following flap extension?
5. Why should youavoid flap extension during turns in thetraffic pattern?
— 16 — EMERGENCY APPROACH
AND LANDING
1. Whatis the first action you should take when an enginefailure occurs?
2. What are someof factors that you need to consider when selecting an appropriate field for an
emergency landing?
— 3. True/False. When making an emergencylanding, it is recommendedthat you circle away from

the field and then execute a long straight-in approachto the landingarea.
4, What code should youset in your transponderto indicate an emergency?
5. Why should you wait to lowerthe flaps until you are confident of making the landingfield?
4-10
FLIGHT
MANEUVERS
MANEUVER 17 cscucunasccnnccnccsccencssess OWS

SLOW FLIGHT
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POWER-OFF STALLS
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POWER-ON STALLS
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DEMONSTRATED STALLS
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Video Volume II— Flight Maneuvers, Ground Reference Maneuvers,

Performance Takeoffs and Landings, and Special Flight Operations
Computer Training — Flight Maneuvers
Collision avoidance is an important safety consideration everytime youfly and

particularly when maneuvering yourairplane in the practice area. In the prac-
tice environment you can be easily distracted so you should make special
effort to maintain yourvisual scan while maneuvering. Your instructor will help
vou with your scanning technique and encourage you to concentrate your vision
outside the airplane. Your instructor also will show you howto clear the area
prior to maneuvering.
Before you begin a maneuver, you should make clearing turns that usually
consist of at least a 180° change in direction, such as two 90° turns. Clearing
turns provide you with a viewof the area around yourflight path and makeit
easier to maintain visual contact with other aircraft in the practice area.
SLOW FLIGHT mt
17 — SLOW FLIGHT 7
The purpose of maneuvering during slowflight is to help you develop a feel for the airplane’s con-
trols at slow airspeeds, as well as gain an understanding of how load factor, pitch attitude, airspeed,
and altitude control relate to each other. Slow flight may be broadly defined as flight at an airspeed
below the normal cruise speed. However, during training you will normally practice this maneuver
at airspeeds well below the normal cruise speed. ‘I'he speed used to demonstrate slowflight for the
practical test is sufficiently slow so that any significant reduction in speed or power,or increase in
load factor, results in stall indications.
While in slow flight, any change in flight attitude, such as a level turn or increase in pitch
attitude, increases the airplane’s load factor, as well as its stall speed. Since the airspeed is
just above a stall speed during slowflight, any maneuvering should be accompanied by cor-
responding change in powerto preventthe aircraft from stalling. Coordinated flight is essential
throughoutall slowflight maneuvers.
Before beginning a slowflight maneuver, you should do a clearing turn to check fortraffic. You
may either execute one 180° turn or two 90° turns in opposite directions. Start the maneuver at an
altitude which will allow youto recover no lower than 1,500 feet AGL.It is a good ideato select an
entry altitude and heading which can be easily read on yourinstruments, such as 3,500 feet and 090°.
“} rey = — @ 2 c
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es Upon completion of your clearing turns, apply carburetor heat(if applicable), reduce power,
and gradually apply back pressure on the yoke to maintainaltitude. As airspeed decreases,
maintain coordinated flight with increasing right rudder. Trim to relieve control pressures.
ee As the airplane reaches the maximumairspeed for flap operation, lowerflaps in increments.
Asthe flaps extend, adjust pitch attitude and powerto maintain altitude. Extend the landing
gear (if applicable) as you reach V,,. Trimto relieve control pressures after each configura-
tion change.
ey Upon reaching your desired airspeed, increase power to maintain altitude and airspeed.
Trim to relieve control pressures.
5-2
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— instru eCcorrect procedure forregaining lost altitude is to apply power. When youdothis, it will also
Se oer
pitchattitudetomaintain the desired airspeed. To lose altitude, reduce power
— A) Once the airplane is stabilized, perform turns, climbs (if possible), and descents as directed
by your instructor. To climb, you must coordinate a pitch and powerincrease to maintain
airspeed. Correspondingly, a descent requires a coordinated pitch and power decrease to
maintain airspeed. The shallowturns you execute during slowflight will require you to add
powerto maintain airspeed and avoid a stall.
SSS >
es Whendirected by your instructor, set the carburetor heat to COLD(if applicable) and add
full power to return to cruise flight. While maintaining your heading and altitude, raise
the flaps slowly in increments. Also, raise the landing gear (if applicable). As the airplane
= accelerates, lower the nose attitude andanticipate the need for less right rudder to maintain
coordinated flight.
ues As you reach yourdesired airspeed, reduce powerandtrim to relieve control pressures.
MANEUVERING DURING SLOW FLIGHT
¢ Exhibit knowledge of the elements related to maneuvering during slowflight.
e Select an entry altitude that will allow that task to be completed no lower than 1,500 feet
(460 meters) AGL.
¢ Establish and maintain an airspeed at which any further increase in angle of attack, increase in
load factor, or reduction in power, would result in an immediatestall.
e Accomplish coordinated straight-and-levelflight, turns, climbs, and descents with landing gear and
flap configuration specified by the examiner.
—— ¢ Divide attention betweenairplane control and orientation.
— e Maintain the specified altitude, +100 feet (80 meters); specified heading +10 degrees; airspeed
+0 knots: and specified angle of bank, +10 degrees.
POWER-OFF STALLS
183 — POWER-OFF
STALLS
Stalls are practiced with two goals in mind. One objective is to help you gain familiarity with the
stall characteristics of your airplane so you can better avoid entering an inadvertentstall. The other
reason for stall practice is to condition you to recover from an inadvertentstall quickly and with a
minimallossof altitude. Power-off stalls are performed in the landing configuration and are used to
simulate an accidental stall during approach, therefore you normally practice power-off stalls using
the airplane’s normal approach speed.
As the airplane approachesa stall, the control feel is sometimes described as “mushy”or “soft”
as compared to the more solid feel of the controls at cruise speed. Consequently, you must use a
greater displacement of the controls to achieve the desired results. As the airplane slows you also
will notice a decrease in engine sound as well as the tone andintensity of the slipstream noise. The
airplane’s mechanical stall warning, which maybe a light, buzzer, horn, or other device, usually
begins 5 to 10 knots before the stall. You may notice buffeting and further decay of control effective-
ness just before thestall.,.
After you becomeproficient in straight-and-level stall entries and recoveries, you will learn how
to handle turning (up to 30° angle of bank) power-off stalls. Before you begin the maneuver, you
should perform clearing turns andestablish the airplane at an altitude which will allow you to
recover by 1,500 feet AGL.
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POWER:-OFF STALLS
STRAIGHT-AHEAD STALL
we Upon completion of your clearing turns, apply carburetor heat (if applicable), reduce power,
and gradually apply back pressure on the yoke to maintain altitude. As you reachthe safe
flap extension speed, lowerfull flaps and establish a normal glide. Extend the landing gear
(if applicable). Trim to relieve control pressures.
Maintain coordinated flight using right rudder and apply back pressure on the yoketo raise
the airplane’s noseto an attitude which will induce a stall. Maintain the pitch attitude until
a Tull stall occurs.
Simultaneouslyrelease back pressure, level the wings(if necessary), add full power, and set
the carburetor heat to COLD (if applicable). Adjust the rudder to maintain coordinatedflight.
Retract the flaps to an intermediatesetting.
Once vou establish a positive rate of climb, retract the landing gear (if applicable). Upon
reaching Vy, retract the remainder of the flaps. Trim to relieve control pressures.
Uponreaching the desired altitude, level off and accelerate to the desired airspeed. Ensure
you return to the proper heading, if necessary. Once youattain the proper airspeed, adjust
the powerandtrim to relieve control pressures.
SS
POWER-OFF STALLS
TURNING STALL ~
The power-off, turning stall is a variation of the power-off straight-ahead stall. It is designed to
simulate an accidental stall during a turn from baseto final. Entry procedures are the sameas the
straight-ahead, power-off stall except with the addition of up to a 30° angle of bank.
Upon completion of your clearing turns, apply carburetor heat(if applicable), reduce power,
and gradually apply back pressure on the yoke to maintain altitude. As you reach the safe
flap extension speed, lowerfull flaps and establish a normal glide. Extend the landing gear
(if applicable). Trim to relieve control pressures.
we Begin a turnto theleft or right (up to 30° angle of bank). Once established in the turn, main-
tain coordinated flight and apply back pressure on the yoketo raise the airplane’s nose to an
attitude which will inducea stall.
Sab,
g However, to simulate the turn from baseto final, the
Soe Eee ee tee
eo Ensure you maintain the desired angle of bank and coordinated flight. Maintain the pitch
attitude until a full stall occurs.
— POWER-OFF STALLS
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erceriziee:
& To recover from the stall, simultaneously release back pressure, level the wings, add full
a power, and set the carburetor heat to COLD (if applicable). Adjust the rudder to maintain
coordinatedflight. Retract the flaps to an intermediatesetting.
J Asflying speedis regained, adjust the pitch attitude to stop the descent and initiate a climb.
RhianeonCe
amountofbackpressure during stall recoveries. Applying back pressure too rapidly
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we Once you establish a positive rate of climb, retract the landing gear (if applicable). Upon
— reaching Vy, retract the remainderof the flaps. Trim to relieve control pressures.
— “s Uponreaching thedesired altitude, level off and accelerate to the desired airspeed. Ensure
you return to the proper heading, if necessary. Once you attain the properairspeed, adjust
— the powerandtrim to relieve control pressures.
POWER-OFF STALLS
e Exhibit knowledge of the elements related to power-off stalls.
e Select an entry altitude that allows the task to be completed no lower than 1,500 feet (460 meters) AGL.
e Establish a stabilized descent in the approachor landing configuration, as specified by the examiner.
¢ Transition smoothly from the approach or landing attitude to a pitch attitude that will induce a stall.
¢ Maintain a specified heading, +10 degrees,in straight flight; maintain a specified angle of bank not
— to exceed 20 degrees, +10 degrees;in turningflight, while inducing the stall.
— e Recognize and recover promptly after the stall occurs by simultaneously reducing the angle of attack,
increasing power to maximum allowable, and leveling the wingsto return to a straight-and-level flight
—e attitude with a minimum lossof altitude appropriate for the airplane.
— e Retract the flaps to the recommended setting; retract the landing gear,if retractable, after a positive rate of
climb is established.
¢ Accelerate to Vy or Vy speed beforethefinal flap retraction; return to the altitude, heading, and
ane airspeed specified by the examiner.
=a/
° POWER-ON STALLS —
19 — POWER-ON STALLS
Power-on stalls are usually practiced from straight climbs and climbing turns to simulate an
accidental stall during takeoffs and departure climbs. The straight-ahead stall can occur if you =
attempt to take off at too slow an airspeed and apply excessive back pressure on the yoke. This
produces an extreme nose-high attitude and high angle of attack. The power-on, turningstall
normally occurs during the departure turn following takeoff and results from distractions which
divert your attention from flying the airplane. The indications of the approachingstall are similar
to those you experience during a power-offstall (see Maneuver #18). As with all stalls, power-on
stalls should be practiced at an entry altitude which permits a safe recovery no lower than 1,500
feet AGL. Normally, you will practice in the takeoff and departure configuration and at theair-
craft’s takeoff speed. This may involve the extension of landing gear and/or flaps, depending on
the situation.
STRAIGHT-AHEAD STALL
Although you use a high powersetting during this stall, do not enter it from a high airspeed. An
extremely nose-high pitch attitude can result from high-power, high-airspeed stall entries.
es Upon completion of your clearing turns, reduce power andslow the airplane while using
back pressure on the yoke to maintainaltitude.
es As you reachliftoff speed, simultaneously set takeoff power (or the recommended climb
powersetting) and smoothly apply back pressure on the yoke to raise the airplane’s nose
to an attitude which will induce stall. Maintain the pitch attitude until a full stall occurs.
Ensure you maintain coordinated flight.
a ee
een et She
ig anan a
YOU W reasingrightruc naintaincoordinated flight as you increase the power andpitchatti-

tude.In many airplanes, the elevat or(or stabilato ’)may befully deflected by the timethe airplane fullystalls.
= Simultaneously release back pressure and applyfull power(if not alreadyat full power). If
tlaps were lowered, retract themto an intermediate setting.
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Applying back pressure too rapidly
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e airplane to build excessive airspeed
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< Once you establish a positive rate of climb, retract the landing gear(if applicable). Upon
reaching Vy, retract the remainderof the flaps. Trim to relieve control pressures.
we Upon reaching the desired altitude, level off and accelerate to the desired airspeed. Ensure
you return to the proper heading, if necessary. Once youattain the properairspeed, adjust
the power andtrim to relieve control pressures.
TURNING STALL
The power-on, turningstall is a variation of the power-on straight-ahead stall. Entry proceduresare
the same as the straight-ahead, power-onstall except with the addition of up to a 20° angle of bank.
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es Upon completion of your clearing turns, reduce power and slow the airplane while using
back pressure on the yoke to maintainaltitude.
es As you approachliftoff speed, begin a turn to theleft or right (up to 20° angle of bank). Once
established, and uponreachingliftoff speed, simultaneously set takeoff power(or the recom-
mended climb powersetting) and smoothlyapplyback pressure on the yoketo raise theair-
plane’s noseto an attitude which will induce a stall. Ensure you maintain the desired angle
of bank and coordinated flight.
o POWER-ON STALLS _
panktendsttosteepen in a left turn and becomeshallower in a right turn. This

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To recover from thestall, simultaneously release back pressure, roll wings-level using coor-
dinated rudder and aileron pressure, and applyfull power(if not already at full power). If
flaps were lowered, retract them to an intermediatesetting.
G> Asflying speed is regained, adjust the pitch attitude to stop the descent andinitiate a climb.
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< Once youestablish a positive rate of climb, retract the landing gear (if applicable). Upon
reaching Vy, retract the remainderof the flaps. Trimto relieve control pressures.
© Upon reaching the desired altitude, level off and accelerate to the desired airspeed. Ensure
you return to the proper heading, if necessary. Once youattain the proper airspeed, adjust
the powerand trim to relieve control pressures.
, POWER-ONSTALLS
e Exhibit knowledge of the elements related to power-onstalls.
¢ Select an entry altitude that allows the task to be completed no lower than 1,500 feet
(460 meters) AGL.
e Establish the takeoff or departure configuration. Set power to no less than 65 percent available
power.
e Transition smoothly from the takeoff or departure attitude to the pitch attitude that will induce stall.
e Maintain a specified heading, +10 degrees, in straight flight; maintain a specified angle of bank not
to exceed 20 degrees, +10 degrees; in turning flight, while inducing thestall.
e¢ Recognize and recover promptly after the stall occurs by simultaneously reducing the angle of
attack, increasing power to maximum allowable, and leveling the wings to return to a straight-and-level
flight attitude with a minimum lossof altitude appropriate for the airplane.
e Retract the flaps to the recommendedsetting: retract the landing gear,if retractable, after a positive
rate of climb is established.
e Accelerate to Vy or Vy speed beforethefinal flap retraction; return to the altitude, heading, and air
speed specified by the examiner.
5-10
20 — DEMONSTRATED
STALLS
A regulatory requirementfor everyrecreational, private, and commercial pilot applicant includes
aeronautical knowledgetraining in stall awareness, spin entry, spins, and spin recovery tech-
niques. A thorough discussion of these topics is contained in Chapter 3, Section B of the Private
Pilot Manual. As an applicant for a private pilot certificate, you are not required to demon-
strate flight proficiency in spin entries, spins, or spin recovery procedures. However, yourflight
instructor may demonstrate a spin sometime during yourprivate pilot training. Spins should
never be attempted without an experienced instructor on board. Demonstrated ability to perform
power-oif and power-on stalls are required for private pilot certification, whereas secondary,
accelerated maneuverstalls, crossed-control stalls, and elevator trim stalls may only be demon-
strated by your instructor and onlyif your airplane is certificated for these types of operations.
The procedures contained in the following discussion are only presented so you can more com-
pletely understand how and whythestalls occur and howthe associated recovery should be
accomplished. You should never practice these maneuverssolo.
SECONDARY STALLS
A secondarystall is caused bytrying to recover from stall before the airplane has obtained suf-
ficient flying speed. This type ofstall also mayoccur if you attemptto return to straight-and-level
flight prematurely during a spin recovery. The objective of demonstrating a secondarystall is to
showyou howto recognize the characteristics of the stall and the correct methodsof recovery. After
Clearing turns, your instructor will start the demonstration using the listed proceduresat an altitude
that will ensure a safe recovery no lower than 1,500 feet AGL.
1. Execute a normal power-on or power-offstall.
2. During recoveryfrom the stall, quickly increase the pitch attitude again while maintaining
directional control with aileron and rudder pressure. Allowthe airplane to enter the second-
arystall.
3. Recover from the secondarystall by releasing back pressure on the yoke to lowerthe nose.
Simultaneously, increase power(if not alreadyat full power).
4. Return to straight-and-level, coordinated flight.
ACCELERATED MANEUVER
STALL
An accelerated maneuver, or excessive back pressure, stall occurs at a higher-than-normalair-
speed in steep turns, pullups, or other abrupt changes in yourflight attitude. The stalls which
occur from these types of maneuvers tend to develop faster than normal unaccelerated stalls.
The objective of demonstrating accelerated maneuverstalls is to show you howto recognize the
characteristics leading up to the stall and correct methods of recovery. It is important to recover
at the first indication of the stall. A prolonged stall, with excessive airspeed may lead to a spin.
After clearing turns, your instructor will start the demonstration using the listed proceduresat
an altitude that will ensure a safe recovery no lower than 1,500 feet AGL.
=
1. Establish straight-and-level flight at V4 orless.
2. Roll into a 45° angle of bank level turn while gradually increasing back pressure to maintain
altitude.
3, Once the turn and bankare established, slowly increase back pressure while maintainingalti-
tude until the airplane stalls.
4. Whenthe airplane stalls, recover immediately by releasing back pressure on the yoke and
increasing power. If the turn is not coordinated, one wing may drop suddenly, causing the
airplane to roll in that direction. If this occurs, the excessive back pressure must be released to
break the stall before the addition of power.
5. Return to straight-and-level, coordinated flight.
CROSSED-GONTROL STALLS
A crossed-controlstall is most likely to occur during a poorly planned and executed baseto final
approachturn. Often this is the result of overshooting the extended runwaycenterline during the
turn. Typically, this happens when youapplyaileron pressure in one direction, rudder pressure
in the opposite direction, and use excessive elevator (or stabilator) back pressure. An example is
when you attempt to increase the rate of turn with rudder and back pressure while trying to keep
the bank angle from steepening withthe use of ailerons. In a crossed-control stall, the airplane often
stalls with little warning. The nose maypitch down, the inside wing may suddenlydrop, and the
airplane maycontinueto roll to an inverted attitude. This is usually the beginning of a spin which
is very dangerousat loweraltitudes. It is important that this type of stall does not occur during an
actual approachto a landing, since a safe recovery may be impossible due to the amountofaltitude
needed. After clearing turns, your instructor will start the demonstration using the listed proce-
dures at an altitude that ensures a safe recovery no lower than 1,500 feet AGL.
1. Slowly reduce power and extendthe landinggear(if applicable),
2. Continue reducing the powerto IDLE.
3. Maintain altitude until a normalglide speed is reached.
4. Establish a normal glide and trim to relieve control pressures.
5. Once established in the descent, roll into a medium bank turn. During the turn, apply heavy
rudder pressure in the direction of the turn. Maintain the bank by applying opposite aileron
pressure. As you doso, increase back pressure on the yoke to keep the nose from lowering.
6. Increaseall flight control pressures until the airplanestalls.
7. Whenthe stall occurs, release the control pressures. If necessary, allowthe roll to continue
until the airplane reaches upright and levelflight.
8. Increase powerto maintain straight-and-level flight.
5-12
DEMONSTRATED STALLS |
ES OrJ
— ELEVATOR TRIM STALLS
The elevator trim stall is a maneuver that demonstrates what can happen whenfull poweris applied
during a go-around and positive control of the airplane has not been established. This can happen
during a normal landing approach, a simulated forced landing approach, or immediately after take-
off. The objective of the demonstration is to show the recovery procedures for overcoming strong
trim forces and how to maintain control of the airplane by using proper and timely trim techniques.
The approaching stall should be recognized immediately and prompt recovery procedures should
be implemented to preventthestall. It is important that a power-on stall not occur from an actual
go-around because the amountof pitch change and altitude required for a safe recovery may not be
available. After clearing turns, your instructor will start the demonstration using the listed proce-
dures at an altitude that ensures a safe recovery no lower than 1,500 feet AGL.
1. Slowly reduce power and extend the landinggear (if applicable).
2. Lower one-half to full flaps.
— 3. Continue reducing the powerto IDLE.
4, Maintain altitude until normal glide speedis reached.
5. Establish a normal glide and trim the nose up to simulate a landing approach.
6. Once established in the simulated final approach glide, apply full powerto simulate a go-
around. The combinedforces of power, engine torque, and back elevator(or stabilator) trim will
make the nose pitch up sharply with left-turning tendency. As the pitch attitude increases to
a point well above the normal climb attitude, the potential for a stall exists.
7. To recover from the approachingstall, apply positive forward pressure on the yoke to lower the
— nose and return to a normal climbingattitude.
8. Trim to relieve excessive control pressure.
9. Continue normal go-around procedures andleveloff at the desired altitude.
S-13
\ STEEP TURNS a | ee
Zz I STEEP TURNS
A steep turn is a high performance maneuver whichis usually conducted in either direction with
an angle of bank of 45°, +5°. Due to high load factors, these turns should be accomplished at an —
airspeed that does not exceed the airplane’s maneuvering speed (V,). The objective of performing
steep turns is to develop smoothness, coordination, orientation, division of attention, and control —
techniques. It is a good idea to use section lines or prominent landmarksto aid in orientation. As
with mostflight maneuvers, you should select an entry altitude which will allow you to perform the —
maneuver no lower than 1.500 feet AGL.
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a Upon completion of your clearing turns, select a reference point on the horizon and note —
vour heading andaltitude.
Ks Roll into a 45° angle of bank turn at or below V4. During roll-in, smoothly add power and
slowly increase back pressure on the yoke to maintain altitude. Maintain coordinated flight —
and trim to relieve control pressures.
Maintain your angle of bank and altitude. Confirm your attitude by referring to both the —
natural horizon and attitude indicator. Use your altimeter and vertical speed indicator to
determine if changes in pitch are required. —-
S-14 wane
STEEP TURNS
ank first, then increase back pressure on the yoketo raise

- ired altite tothedesired angle of bank.
_ A) Anticipate the roll-out by leading the roll-out heading by approximately 20°. Roll out on the
entry heading andaltitude. During roll-out, gradually decrease back pressure on the yoke
and reduce power to maintain altitude and airspeed. Trim to relieve control pressures.
rn.Generally, you will need rudder andaileron pressure during theroll-out than you
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5-16
he.
EXERCISES — FLIGHT
~ MANEUVERS
1 ‘7 SLOW FLIGHT
1. What speed should you maintain during slowflight?
__ 2. What is the minimum AGLaltitude you should plan to recover from slowflight?
3. True/False. As your airspeed decreases you should anticipate the need for increasing right
rudder pressure.
4. Whenrecovering from slowflight, what technique should you use to raise the flaps?
5. What are the performance standards for maneuvering during slowflight?
- 18 POWER-OJFF STALLS
a 1. In what airplane configuration are power-off stalls performed?
2. When does a typical mechanicalstall warning activate?
3. What are the indications that a stall has occurred?
4. What is the cause of a secondarystall?
— 5. True/False. After recovering from stall, you should climb at Vx.
- 19 POWER-ON STALLS
a 1. In which phase(s) of flight would a power-onstall mostlikely occur?
2. Howshould the airplane be configured when performing a power-onstall?
3, True/False. You should execute a power-onstall at a high airspeed using high power.
4, As you approach a power-onstall in a right turn, will the angle of bank tendto increase or dec
rease?
>- 17
What is the maximum angle of bank you should use in a turning, power-onstall?
Ol
a EXERCISES — FLIGHT MANEUVER _—
|
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aer nies eeeienennseensSTS TTTTITTE«1h )beet tes eet Pee te ee sie cereneunsebeecnnerummennenes ,
20 — DEMONSTRATED STALLS -
1. True/False. An applicant for a private pilot certificate is required to demonstrate flight profi-
ciency with regard to stalls and spins.
2. True/False. A private pilot applicant must be able to demonstrate flight proficiency in elevator
trim stalls.
3. True/False. Any airplane can be used to perform an accelerated stall.
4, What is another namefor an accelerated maneuverstall?
5. Whenis a crossed-contro!stall likely to occur? —
21— STEEP TURNS

1. What angle of bank is normally used for steep turns?
2. Is overbanking tendency more apparent in a rightor left turn?
3. Howshould youcorrect for a loss of altitude during a steep turn?
4. How much should you lead yourroll-out from a steep turn?
5. True/False. In comparison to the roll-in, you need more rudderandaileron pressure during the
roll-out from a steep turn. —
16
GROUND
REFERENCE
MANEUVERS
MANEUVER 22 PURSE SHRP RPE 6-2

RECTANGULAR COURSE
MANEUVER 2S cssscsucscccncnnncncesneseses G74

S-TURNS
MANEUVER 2+ accuccaacccccncccssessesssssss O-G@

TURNS AROUND A POINT
EMER GIS Siccuccucccuccccuscuscscssceansenaeas 6-9
Video Volume IJ — Flight Maneuvers, Ground Reference

Maneuvers, Performance Takeofts and Landings, and Special Flight
Operations
Computer Training — Ground Reference Maneuvers
Since the ground reference maneuvers youare going to learn during your flight
training are practiced at relatively lowaltitude, you should alwaysbe vigilant for
appropriate emergency landing sites. Good choices for emergencylandingsites
might be open pastures, turf farms, and hard-packeddirt fields. A road is not
always a good option because some may have powerlines, trees, or heavy traffic.
22 — RECTANGULAR
COURSE
The objective of the rectangular course is to help you develop the skill to compensatefor effects of
the wind andfly a uniform traffic pattern byvisual reference to the ground. This maneuver requires
you to combineseveral flight techniques. First, you mayneed to use varying crab angles through-
out the straight flight segments. Second, you must track an imaginaryline parallel to a fixed line.
Third, you need to plan ahead and usedifferent angles of bank in orderto roll out of the turnsat the
proper distance from the field boundary. Finally, you must maintain a constantaltitude throughout
the maneuver. To help you accomplishthese tasks, do not forget to maintain coordinated flight and
trim to relieve control pressures, as needed.
Before starting the maneuver, select a field away from a populated area which is bounded on four
sides by section lines or roads. The field should have sides between one-half and one mile in
length. If possible, the wind should be blowingparallel to the long side of the rectangle. Clear the
area for traffic and check to ensure there are no obstructions such as towers or powerlines. Also,
select an emergency landing area within gliding distance. The patternis typically flown usingleft
turns (although you should also practice right-hand patterns) and at a distance of approximately
one-quarter to one-half mile outside the field boundary. If you fly too close to the boundaries, your
angle of bank in the turns will be excessive (greater than 45°) and you may have difficulty keeping
the edgesof the field insight.
wi Enter the maneuver at a 45° angle to the downwindleg, at an altitude of 600 to 1,000 feet
AGL.Flyparallel to the field boundary.
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— a RECTANGULAR COURSE —
Whenyou are abeam the crosswind segmentof the field boundary, begin a turn to the cross-
wind leg. To counteract the effect of the wind and remain parallel to the crosswindfield
boundary, you should continue the turn beyond 90°.
waeyouByeisen through thefirst turn, your groundspeed decreases.

—bank asue turn progresses. Onceestablished on the crosswind
© When youare abeam the upwind segmentof the field boundary, begin a turn to the upwind
leg. Since you were holding a crab angle into the wind on the crosswind leg, your turn to the
need leg will be less than 90°.
M4 When you are abeam the next crosswind segmentofthe field boundary, begin a turn to the
crosswind leg. To counteract the effect of wind and remain parallel to the crosswind field
boundary, you should turn less than 90°.
eshallowestangle of bank. As the headwind component decreases, you
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Ee Whenyou are abeam the downwind segmentofthe field boundary, begin a turn to the down-
wind leg. Since you were holding a crab angle to compensate for the crosswind, you will
need to turn greater than 90° to parallel the downwind field boundary.
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e Exhibit knowledgeof the elements related to a rectangular course.
~ e Select a suitable reference area.
—— ¢ Plan the maneuver so as to enter a left or right pattern, 600 to 1,000 feet AGL (180 to 300 meters) at
an appropriate distance from the selected reference area, 45 degrees to the downwindleg.
e Apply adequate wind-drift correction during straight-and-turningflight to maintain a constant ground

— track around the rectangular reference area.
— e Divide attention between airplane control and the ground track while maintaining coordinatedflight.
— e Maintain altitude, +100 feet (80 meters); maintain airspeed, +10 knots.
23 — &S-TURNS
An S-turn is a ground reference maneuver whichis intended to help you improve yourability to
compensate for wind drift during turns. It consists of a series of uniform 180° turns in opposite
directions crossing and recrossinga straight road, fenceline, or section line. The maneuver requires
you to divide your attention between the ground reference line and airplane control. Whenselect-
ing your ground reference, the road, fence line, or section line should be long enough to allowa
series of turns. Since this maneuver should be started on a downwind heading, tryto find a ground
reference line whichis oriented perpendicular to the wind. Clear the area for traffic and check to
ensure there are no obstructions such as towers or powerlines. You should fly the maneuverat
an altitude low enoughto easily recognize wind drift, but not any lower than 500 feet above the
highest obstruction. As with most ground reference maneuvers whichare performedat an altitude
of between 600to 1,000 feet AGL, you should select an emergency landing area within glidingdis-
tance prior to starting the maneuver. While flying the maneuver, maintain coordinatedflight and
trim to relieve control pressures, as needed.
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ew Upon crossing the referenceline, roll immediatelyinto a left turn. The downwind entry
provides the highest groundspeedin thefirst 90° of turn. This requires a rapid roll into a
relatively steep angle of bank.
“es Continue the turn, adjusting the angle of bank to compensate for the effect of the wind. As
you turn past the 90° point, the airplane’s groundspeed begins to decrease, requiring youto
progressively reduce the angle of bankto track a symmetrical half-circle.
5S - TURNS
ke You should cross the referenceline after 180° of turn with the wingslevel. At the instant you
cross the reference line, begin a turn in the opposite direction.
Jency to i nk toorapidly during theinitial part of the turn on the upwind side,
the completio efore recrossing thereferenceline. To avoid this error, you should visu-
ne ispeedrequiresa shallower angle of bank and, conversely, a high
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TREK ESS eae seer
ei) Continue the turn, adjusting the angle of bank to compensate for the effect of wind. As you
turn past the 90° point, the airplane’s groundspeed beginsto increase, requiring you to pro-
gressively increase the angle of bank to track a symmetricalhalf-circle.
You should cross the reference line after the second 180° of turn with the wingslevel.
a,
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y TURNS AROUND A POINT
24 — TURNS AROUND A
POINT
Turns around a point are intended to help you develop the ability to control the airplane while
dividing your attention betweenthe flight path and a ground reference point. During the maneu-
ver, you are required to maintain a constant radius turn around a reference point while remain-
ing at a constant altitude. The ground reference point you select should be easily identifiable,
away from populated areas, and within gliding distance of a suitable emergency landing field.
You canuse trees, isolated haystacks, or other small landmarks as reference points, but theyare
not as effective as the intersections of roads or fence lines. The latter items are more desirable,
because the wing may momentarily block your viewof the reference point during the maneuver.
Byselecting a road or fence line intersection, you can mentally project these lines to their logi-
cal intersection and maintain your orientation. You should plan to begin the maneuver from a
downwind entryat 600 feet to 1,000 feet AGL. The turns are initially executed to the left and
normally should not exceed a 45° angle of bank.
If any wind exists, a constantly changing angle of bank will be required to maintain a uniform
radius around a point. The closerthe airplane is to a direct downwind heading where the ground-
speed is the greatest, the steeper the bank required. Conversely, the more nearlythe airplane is
to a direct upwind heading where the groundspeed is least, the shallower the bank required. As
always, you should maintain coordinated flight and trim to relieve control pressures, as needed,
throughout the maneuver.
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_ TURNS AROUND A Point [|
When the reference point is abeam the airplane on the downwind heading, roll to the left
— to begin the maneuver. Flying a downwind entry provides the highest groundspeed and
requires the steepest initial angle of bank.
ir position andthe reference point. Failure to do so may result in
As you turn crosswind, sradually reduce the angle of bank to compensatefor the decreasing
tailwind.
Heading upwind, vour bank angle will be at its shallowest due to the slow groundspeed.
nerlveght.
— @ As you turn crosswind, gradually increase the angle of bank to maintain a uniform ground
track.
EXERCISES - GROUND REFERENCE MANEUVERS
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EXERCISES —
SGROUND REFERENCE
MANEUVERS
22 — RECTANGULAR COURSE
1. What other maneuverdoesthe rectangular course simulate?
2. True/False. When you select an area to perform a rectangular course, you should also select an
emergencylanding field which is within gliding distance.
3. What is the maximum angle of bank you should use when performing a rectangular course?
4. When should you begin your turn from the downwind leg to the crosswindleg?
5. Relative to angle of bank, which turn should be the shallowest whenflying a rectangular course?
23 — S-TURNS
1. During S-turns, how should the ground reference line be oriented with regard to the wind
direction?
2. True/False. To begin an S-turn, you shouldroll into a relatively shallowbank as you cross the
sround reference line.
3. When you turn from a downwind heading to an upwind heading, howwill your ground-
speed change?
4. Whyshould you change your angle of bank when turning from a tailwind to a headwind?
5. True/False. The ground track of the S-turn should be the same size on the upwindside as the
sround track on the downwindside.
6-9
EXERCISE - GROUND REFERENCE MANEUVERS
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24 — TURNS AROUND A POINT

1. In which direction should you initially begin your turns arounda point?
2. What is the maximum angle of bank normally used when flving turns around a point?
3. Whenflying turns around a point, where does the steepest angle of bank occur?
4. Whenflying turns around a point, where does the shallowest angle of bank occur?
5. How manyfeet can you deviate from your entryaltitude during turns around a pointand still
meet the PTS requirements?
6-10
PERFORMANCE
TAKEOFFS AND
LANDINGS
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EXER CIS
Video Volume I] — Flight Maneuvers, Ground Reference

Maneuvers, Performance Takeoffs and Landings, and Special
Flight Operations
25 — SHORT-FIELD
TAKEOFF AND GLIMB
Short-field takeoff and climb procedures may be required when the usable runwaylength is short,
or whenthe runwayavailable for takeoff is restricted by obstructions, such as trees, powerlines, or
buildings, at the departure end. During short-field practice sessions, it is usually assumed that you
are departing from a short runway and that you must clear an obstacle which is 50 feet in height.
To accomplish successful short-field takeoffs and climbs you must be familiar with the best angle-
of-climb speed (Vx) and the best rate-of-climb speed (Vy) for your airplane’s. Many manufacturers
also specify a best obstacle clearance speed. You should consult your airplane’s POHfor the appro-
priate speeds and specific procedures for performing short-field takeoffs. Since the same general
procedures used to execute a normaltakeoff and climb applyto this discussion, only the additional
techniques required to perform a takeoff and climb from a short runwayare explained here.
Complete the before takeoff check. Ensure that the runway, as well as the approach and
departure paths are clear of other aircraft. After obtaining a clearance (at a controlled air-
port) or self announcing yourintentions (at an uncontrolledairport), taxi into position at the
beginning of the runwayso as to allow maximum utilization of the available runway. Align
the airplane on the runwaycenterline.
we Set the flaps as recommended by the manufacturer. The appropriate flap setting varies
between airplanes and can range from noflaps to approximately one-half flaps. While hold-
ing the brakes, add full power smoothly and continuously and then release the brakes to
begin the takeoff roll.
ver snablesyouto determine that the engineis functioning properly before you
ailability iscriticalanddistance to abort a takeoff is limited.
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SHORT-FIELD TAKEOFF AND GLIMB
& Allowtheairplane to accelerate withits full weight on the main wheels by holding the yoke
— to maintain the elevator(or stabilator) in a neutral position. Smoothlyand firmly apply back
pressure to the yoketo liftoff at the recommended airspeed. Since the airplane accelerates
— quicklyafter liftoff, you may need to apply additional back pressure to establish and main-
tain Vx (or best obstacle clearance speed).
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G) Once you have cleared the obstacle and reached a safe altitude, lower the nose and accelerate
-- to Vy. Retract the landing gear (if applicable) and then retract the flaps (if applicable). If no
obstacles are present during training, you should maintain Vx until you are at least 50 feet
— above the runwaysurface. Trim to relieve control pressures.
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22 SHORT-FIELD TAKEOFF AND MAXIMUM PERFORMANCECLIMB
e Exhibit knowledge of the elements related to a short-field takeoff and maximum performanceclimb.
¢ Position the flight controls for the existing wind conditions; set the flaps as recommended.
— e Clear the area; taxi into takeoff position utilizing maximum available takeoff area and align the
airplane on the runway center/takeoff path.
e Apply brakes(if appropriate), while advancing the throttle smoothly to takeoff power.
— e Lift off at the recommendedairspeed, and accelerate to the recommendedobstacle clearance

airspeed or Vx.
e Establish a pitch attitude that will maintain the recommended obstacle clearance airspeed, or Vx,
+10/—5 knots, until the obstacle is cleared, or until the airplane is 50 feet (20 meters) above the surface.
e After clearing the obstacle, establish the pitch attitude for Vy, accelerate to Vy, and maintain Vy,
+10/—5 knots, during the climb.
e Retract the landing gear, if appropriate, and flaps after clear of any obstacles or as recommended by
the manufacturer.
— e Maintain takeoff power to a safe maneuvering altitude.
¢ Maintain directional control and proper wind-drift correction throughout the takeoff and climb.
7-3
SHORT-FIELD APPROAGH AND LANDING aa ae ee ee
6 — SHORT-FIELD :
APPROAGH AND -
LANDING
A short-field landing is necessary when you have a relatively short landing area or when an approach
must be made over obstacles which limit the available landing area. A short-field landing consists La
of a steep approach overan obstacle, using powerandflaps (normally full flaps). A minimum land-
ing speedis desired with a touchdownpoint as close to the thresholdas possible. During short-field __
landing practice, assume you are making the approach and landing over a 50-foot obstacle. You
should consult your airplane’s POH for the appropriate speeds and specific procedures for perform- __
ing short-field takeoffs. Since the same general procedures used to execute a normal approach and
landing apply to this discussion, only the additional techniques required to perform a short-field
approach and landing are explained here.
APPROAGH
Ensure that the before landing checklist is completed andthat the areais clear. Extend approxi-
mately one-third of the available flaps during the latter portion of the downwindleg and two-
thirds on base, while progressively reducing the airspeed. Trim to relieve control pressures.
Begin the final approachat least 500 feet higher than the touchdownarea. Maintain the rec-
ommended approach speed and extend the remainingflaps.
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SHORT-FIELD APPROACH AND LANDING | i
7 LANDING
ey As you begin the flare, reduce power smoothlyto idle and allow the airplane to touch down
oe
in a full-stall condition. Since the short-field approach is madeat a steep descent angle and
close to the airplane’s stalling speed, you must judge the initiation of the flare accurately to
avoid flying into the ground orstalling prematurelyand sinking rapidly.
—_ ei Whenthe airplaneis firmly on the runway, lowerthe nose, retract the flaps (if recommended)
and applythe brakes, as necessaryto further shortenthe roll-out.
s onthelandingroll. This transfers more weight to the main gear and

eee
e Exhibit knowledge of the elements related to a short-field approach and landing.
e Consider the wind conditions, landing surface, obstructions, and select the most suitable touchdown
point.
e Establish the recommended approach and landing configuration and airspeed; adjust pitch attitude
e Maintain a stabilized approach and recommended approachairspeed, orin its absence not more
than 1.3 Vso, +10/—5 knots, with wind gust factor applied.
e Make smooth, timely, and correct control application during the roundout and touchdown.
e Touch down smoothly at minimum contro! airspeed.
¢ Touch downator within 200 feet (60 meters) beyond a specified point, with no side drift, minimum
float and with the airplane’s longitudinal axis aligned with and over the runway center/landing path.
e Apply brakes as necessary, to stop in the shortest distance consistent with safety.

SHORT-FIELD TAKEOFF AND CLIMB
™“
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2°'7 — SOFT-FIELD
TAKEOFF AND GLIMB
A soft field may be defined as any runway that measurably retards acceleration during the takeotf
roll. The objective of the soft-field takeoff is to transfer the weight of the airplane from the landing
gear to the wings as quickly and smoothly as possible to eliminate the drag caused by surfaces such
as tall grass, soft dirt, or snow. Takeoffs and climbs from soft fields require special procedures, as
well as knowledgeof youraircraft’s performance characteristics including Vx and Vy.
You actually begin the soft-field procedure during the taxi phase. If the taxi area surfaceis soft, use
full back pressure on the yoke to maintain full-up elevator (or stabilator) deflection with a slight
amount of power to keep the airplane moving. This technique transfers some ofthe airplane’s
weight from the nosewheel to the main wheels, resulting in lower power requirements and greater
ease in taxling.
Complete the before takeoff check on a pavedor firm surface area,if practical. This helps to
avoid propeller damage and the possibility of the airplane becomingstuck.
e Set the flap position as recommended by the manufacturer.
e Clear the approach and departure areas and thetraffic pattern prior to taxiing onto the
runway. After obtaining a clearance (at a controlled airport) or self announcing yourinten-
tions (at an uncontrolled airport), taxi into position for takeoff without stopping.
we Align the airplane with the center of the runway and whilestill rolling, advance the throttle
smoothly to takeoff power. Maintain full back pressure on the yoke to raise the nosewheel
from the soft surface.
e As you increase speed andtheelevator (or stabilator) becomes moreeffective, reduce back
pressure slightly. Continue to use back pressure on the yoke to hold the nose up andto
f°@ reduce the amountof weight on the nosewheel.
As the airplane lifts from the runwaysurface, reduce back pressure to achieve a level
flight attitude.
a ntind ee Fy
& Allow the airplaneto accelerate in level flight, within ground effect, to Vx before starting
a climb.
es Once all obstacles are cleared (if applicable), accelerate to Vy. Retract the landing gear(if
applicable) andraise the flaps (if applicable) once you haveattaineda safe altitude and air-
speed. Trim to relieve control pressures.
SOFT-FIELD TAKEOFF AND CLIMB
¢ Exhibit knowledge of the elements related to a soft-field takeoff and climb.
¢ Position the flight controls for existing wind conditions and to maximizelift as quickly as possible.
e Clear the area; taxi onto the takeoff surface at a speed consistent with safety without stopping
while advancing the throttle smoothly to takeoff power.
e Establish and maintain a pitch attitude that will transfer the weight of the airplane from the wheels
to the wingsas rapidly as possible.
e Lift off at the lowest possible airspeed and remain in ground effect while accelerating to Vy or Vy, as
appropriate.
e Establish a pitch altitude for Vy or Vy, as appropriate, and maintain selected airspeed +10/—5 knots,
during the climb.
e Retract the landing gear, if appropriate, and flaps after clear of any obstacles or as recommended by
the manufacturer.
¢ Maintain takeoff powerto a safe maneuveringaltitude.
e Maintain directional control and proper wind-drift correction throughoutthe takeoff and climb.

a oa aoe a a Re
S — SOFT-FIELD -
APPROACH AND LANDING -
The objective of a soft-field landing is to ease the weight of the airplane from the wingsto the main
landing gear as gently and slowly as possible while keeping the nosewheeloff the soft surface dur- |
ing most of the landing roll. This technique will prevent the nosewheel from sinking into the soit
surface and reduce the possibility of an abrupt stop during the landing roll. You should consult a
your airplane’s POH for the appropriate speeds and specific procedures for performing soft-field
landings. Since the same general procedures used to execute a normal approach and landing apply
to this discussion, only the additional techniques required to perform a soft-field approach and
landing are explainedhere.
APPROACH
Ensure that the before landing checklist is completed and that the area is clear. Extend approxi- —
mately one-third of the available flaps during the latter portion of the downwindleg and two-
thirds on base, while progressively reducing the airspeed. Trim to relieve control pressures. _
Unless obstacles are in the approach path, maintain the same descent angle on final as you =
would during a normal approach. Maintain the recommended approach speed and extend
the remaining flaps. et
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es Hold the airplane one to two feet above the surface as long as possible to dissipate forward
speed. Maintain that attitude with power and slowly continue the descent until the airplane
touches downat the lowest possible airspeed with the airplane in a nose-high attitude.
wes After touchdown, maintain back pressure on the yoke to hold the nosewheeloff the surface
as long as practical. As the airspeed decreases on the roll-out, smoothly and gently lower the
nosewheel to the surface.
=) Increase the powerslightly, if necessary, to keep the aircraft moving and prevent it from
stopping suddenly on the soft surface. Avoid using the brakes since braking action may
cause the nosewheelto dig into the soft surface and may damagethelanding gear. Thesoft
surface should provide sufficient braking action to slowtheaircraft down.
SOFT-FIELD APPROACH AND LANDING

=
¢ Exhibit knowledge of the elements related to a soft-field approach and landing.
e Consider the wind conditions, landing surface and obstructions, and select the most suitable
touchdownarea.
e Establish the recommended approach and landing configuration, and airspeed; adjust pitch attitude
e Maintain a stablized approach and recommendedairspeed, orin its absence not more than 1.3 Vso,
+10/—5 knots, with wind gust factor applied.
¢ Make smooth, timely, and correct control application during the roundout and touchdown.
e¢ Touch downsoftly with no drift, and with the airplane’s longitudinal axis aligned with the runway/
landing path.
e Maintain crosswind correction and directional control thoughout the approach and landing sequence.
e Maintain proper position of the flight controls and sufficient speed to taxi on the soft surface.

7-10
— PERFORMANCE TAKEOFFS AND LANDINGS EXERCISE Le
- EXERCISES —
PERFORMANCE
— TAKEOFFS AND
- LANDINGS
40 = SHORT-FIELD
TAKEOFF AND GLIMB
1. Nametwo situations which require the use of a short-field takeoff and climb.
2. During short-field practice sessions, it is assumed that you must clear an obstacle whichis
— how manyfeet in height?
sis 3. True/False. You should use the best rate-of-climb speedto clear obstacles at the departure end
of the runway.
4, Whyshould you hold the brakes until you achieve full powerprior to beginning the takeoff
roll?
5. Whyshould you avoid raising the noseprior to the recommendedliftoff speed?
- 26 — SHORT-FIELD APPROACH AND

LANDING
1. In what situations would executing a short-field approach and landing be necessary?
2. Is the descent angle for a short-field approach steeper, shallower, or the same as that flown for
a normal approach to a landing?
3, What is the purpose of extending full flaps when executing a short-field approach?
— 4. True/False. While executing a short-field landing, you should reduce powerto idle in the flare
and allow the airplane to touch downin a full-stall condition.
5, What can occur if you maintain an excessive amountof airspeed during the short-tield
approach and landing?
7-11
2 E XERCISE PERFORMANCE TAKEOFFS AND LANDINGS
a
an P< en te oo - >= a eeree
2°'7 — SOFT-FIELD
TAKEOFF AND GLIMB
1. Whatis the objective of a soft-field takeoff?
2. What is the definition of a soft field?
3. True/False. The soft-field procedure begins during the taxi phase.
4. What can occur if vou do not release some back pressure while accelerating during the takeoitf
roll?
5. Since liftoff normally occurs at a speed belowthe safe climb speed, what action should you
take before starting a climb?
28 — SOFT-FIELD
1. Whatis the objective of a soft-field landing?
2. Whyis the extension of flaps normally recommendedfora soft-field approach and landing?
3, Whenexecuting a soft-field landing, why should you hold the airplane one to two feet above
the runwayas long as possible?
4, True/False. During a soft-field landing, you should lower the nosewheel to the surface as
quickly as possible after touchdown.
5. Whatis the correct procedure for the roll-out after a soft-field landing?
A. Maintain powerat idle and apply heavybraking.
B. Hold forward pressure on the yoke and avoid braking.
C. Maintain back pressure on the yoke and increase powerslightly, if necessary.
7-12

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i

JEPPESEN. A BOEING COMPANY

SUIDED FLIGHT DISCOV

EMERGENCY LANDING PROCEDURES

GROUND REFERENGE MANEUVERS

SPECIAL FLIGHT OPERATIONS

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speed indicator, and the pitch attitude on the attitude indicator.

in aquartering tailwind. The increasing tailwind

EXERCISES — GROUND OPERATIONS

2. What documents are required on board the airplane?

3. How can you tell when wateris presentin a fuel sample?

5. What documents are not required to be on board the airplane?

2. The primer pumpsfuel into what part of the engine?

1. True/False. Taxi speed is primarily controlled by using the brakes.

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Video Volume I — Ground Operations, Basic Maneuvers, Airport

Computer Training — Ground Operations

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© FUSELAGE (LEFT SIDE)

@ FUSELAGE (RIGHT SIDE)

in the air, or it may be presentin the fuel added to the

Removethe wing tiedownropeorchain.

LANDING GEAR (RIGHT SIDE)

Check the engine cow]for security.

e If your airplane has a constant-speed propeller, check for oil leaks.

be detectedbyoil streaks on the backside of the

ingcompoundspecifically designed for airp

e Ifa static port is located on the cowling, check for obstructions.

LANDING GEAR (LEFT SIDE)

Zs Fuel-injected—Set the mixture control to RICH.

With the area clear, turn the master switch ON.

Turn the anti-collision lights on to provide a visual warning to people approachingtheair-

Turn or press the ignition switch to engage the starter.

Adjust the throttle to the recommendedidle powersetting.

BASIC TAX! TECHNIQUES

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cesinthe direction of a turn can be helpful in reducing the

- wind mayraise the tail causing the airplane to have a

To meet the PTS requirements, you must:

e Exhibit knowledge of the elements related to safe taxi procedures.

e Perform a brake check immediately after the airplane begins moving.

e« Control direction and speed without excessive use of brakes.

¢ Comply with airport/taxiway markings, signals, ATC clearances, and instructions.

e Taxi so as to avoid otheraircraft and hazards.

1. Set the parking brake.

F eames) Sees >: : q

— 4. Check andsetthe flight instruments.

— Verify the airspeed indicator reads zero.

Set the altimeter to the current altimeter setting or to the correct