Debonair C33a Poh
Debonair C33a Poh
Debonair C33a Poh
lor tbc
9.o"h"..r, Debonair 35-C33A
I
and
E33A
I Ona nZA' E33c Acno1A7c
See Fllght Mahual
Srmlcment
FAAApprcr,.dby:
J llrrl/ * CA
lor w. H. scHt Lflz
BEECTI AIBCRAFT COBFORATION
DOA CE.2
_l
I
THIS I{AiIOB(X)I( SUPERSCOES ATL TEBCH ruELISHEO
(lI'T{CRs IIAT{UAL3. FLIGHT MAi'I'AL8, AIID CHECT LISTS
ISSUEO FOR THIS AIRPLAilE WITH THC EXCEPfl(r{ OF FAA
APPFOVEO A IR?LAI{E T L IGHT MAii'AL tU??LCME}'T8.
-J*
I P/N 33500003t8 P/t{ 33-59qxr}7Bt
Rchrurd: Octobcr 1079 Rcvhcd: March 1983
I
Debonair G33A and Bonanza E33A
Bl ... MARCH1983
LOG OF REVISIONS
PAGES DESCRIPTION
Page A
DEBONAIR C33A and BONANZA E33A
\- PILOT'S OPERATING HANDBOOK
and
LOG OF REVISIONS
..
oR|GTNAL(A) ..ocToBER1977
REISSUED(B) ... OCTOBER1979
PAGE DESCRIPTION
Title Page
,,A" PAgE
a thru b
1-1 thru 1-18
2-1 thru 2-30
3-1 thru 3-14
4-1 thru 4-20
5-1 thru 5-32
6-1 thru 6-22
7-1 thru 7-36
8-l thru 8-52
Section 9 See Log of SuPplements
lGl thru lG30
fa
A Page
BEECHCRAFT
DebonairC33A
Bonanza E33A
INTRODUCTION
WARNING
TABLE OF CONTENTS
SECTIONI .... General
SECT|ON5.... ....Performance
SECTION 6 .. .... . Weight and BalanceTEquipment List
SECTION I
GENERAL
TABLE OF CONTENTS
SUBJECT PAGE
IMPORTANT NOTICE
Section 2 Limitations
Section 3 Emergency Procedures
NOTE
WARNING
32',10"
I
8'3"
6',6" lll@
lr
tT- I
7.5" min.
34" DIAMETER
ts
AIRPLANE THREE-VIEW
DESCRIPTIVE DATA
ENGINE
One Teledyne Continental Motors Corporation engine
model lO-520-8, |O-520-BA or |O-520-BB. lt is a fuel-
injected, direct-drive, air-cooled, horizontally-opposed. 6-
cylinder, S2O-cubic inch-displacement, 28s-horsepower-
rated engine.
1-8 October 1979
BEECHCRAFT Section I
DebonairC33A General
Bonanza E33A
PROPELLER
NOTE
\-
ther propellers may be approved but not
installed as original equipment. These are
listed in the FAA Aircraft Specif ication 3Al 5 or
approved by Supplemental Type Certificate'
FUEL
STANDARD SYSTEM
Total Capacity.... '.. 5Ogal.
Total Usable .. 44 gal.
OPNONAL SYSTEM
Total Capacity . ... ..' 80 gal.
Toral Usable .. 74 gal.
OIL CAPACITY
WEIGHTS
Length Sft6in.
Heighr ..
4 ft 2 in.
Width ..
3 ft 6 in.
Cabin Door .. 37 in. wide by 36 in. high
DebonairC33A Genera!
Bonanza E33A
POWER TERMINOLOGY
and
Take off Highest power rating
Maximum not limited by time.
Continuous
sEcfloN ll
LIMITATIONS
TABLE OF CONTENTS
SUBJECT PAGE
cAs tAs
SPEEO KNOTS MPH KNOIS MPH REMARKS
.g o
cl
o o
u.t .>
o (D
c(E o c J
J
2 E
cCD
G
o
c
o o
c
E .9 o
tt CD
c ,
6 !
2,
(E
o o
Io o
o.
o
(u
o
o
.c.
o
CL
o
o 5'E E
gCL
o- f
TL
(E
E s6
oo
E
'i
CLtr .o
o
f
Lt- z ob =
ro c{ c{ (o
E c{t t (n N
N @
L N
(\l
(Y) N
E (o (o r\ o) o
q o
,
'D F(? @
(r,
.E
@ (o
a
F({
, (')c) I
(Y'
(D
o z ro tl, @ (o (J
(, I
.E
2
I oo
(r{ o
o,
lo
N
E'
!
o
G, I GI ro
N o
D.
E NGI
(o@ G'
I
o
o)
C{ E- 0,
= o .9&
G
o L<
F o 't, (',N
eN
rI)
@
io
(t)
.9p
aoc
rO
.o(E
Io c
z
I
t\t
lo lo @
I
(I, lo
@
(D
9o,
L<'
z * uT
o u.r
o c, o o (, B(J
ul z o
tr
60
.:>
UJ
o, v o c io J <E
o G .= o
o Eo E€
E E 6 FUJ
3 c, G at
I = I
OPERATING LIMITATIONS
FUEL GRADES
OIL SPECIFICATIONS
PROPELLER SPEClFICATIONS
McCauley constant speed, two blade propeller
Hub: 2A36C23
Blades: 84B-O
Diameter: Maximum 84 in., Minimum 82 in.
Pitch settings at 30 in. sta.:
Low - 13.3o,
High - not under 29.20
or
NOTE
OIL TEMPERATURE
' Caution (Yellow Radiall I OOoFl3SoC
Operating Range
(Green Arc) lOOo to 24QFfJBo ro 1l6oc
Maximum (Red Radial) 24OoF/116,C
OIL PRESSURE
Minimum Pressure (Red Radial) ""' 30 psi
Operating Range (Green Arcl .. 3O to 60 psi
Maximum Pressure (Red Radial) 1OO psi
TACHOMETER
Operating Range (Green Arc) . -. 18OO to 27OO rpm
Maximum RPM (Red Radial) " " ' 27OO rpm
MANIFOLD PRESSURE
Operating Range
(Green Arc) .... . 15 to 29'6 in' Hg
Maximum (Red Radial) " 29'6 in' Hg
FUEL FLOW
Minimum (Red Radial) " " " 1'5 psi
Operating Range (Green Arc) """ 6'9 to 24'3 gph
Maximum (Red Radial) ""' 17'5 psi
October 1979 2-7
Section ll BEECHCRAFT
Limitations DebonairC33A
Bonanza E33A
FUEL OUANTITY
Yellow Band (44-gallon system) E @ V2lull
Yellow Band (74-gallon system) E to 3rB full
WEIGHT TIMITS
Maximum Ramp Weight ..... 3312 lbs
Maximum Take'off
and Landing weight .'!TIf h
Zero Fuel Weight ...... No Structural Limitation
Maximum Baggage ComPartment
Load 27O lbs.
REFERENCE DATUM
Datum is 83.1 inches forward ol center line through
.forward jack points.
MAC leading edge is 66.7 inches aft of datum'
MAC length is 65.3 inches.
MANEUVER LIMITS
This is a utility category airplane. Spins are prohibited' No
acrobatic maneuvers are approved except those listed
below. Maximum slip duration is 3O seconds for airplanes
with baflled main fuel cells in both wings and 20 seconds
for airplanes with unbaffled main fuel cells in either wing'
Ocrobor 1979
2-9
Section l! BEECHCRAFT
Umitations DebonairC33A
Bonanza E33A
WARNING
LEGEND
a4
co
a.
o
(,
x
t{t
o
c, (v)
a? o?
o) o)
E, E
IL IL
o
(L
o)
o-
E
o
R, *
e
sg
F
5ur
E Bz
z EE 8
h.E ELo-
EE
(-r
6E8 .Y' <X
€ .9
c E(
-rtE r : oz ()9 : -Y
X
# ! E= =E 8F -E
C'
E E iE ;H frl i
BEECHCRAFT Section ll
DebonairC33A Limitationt
Bonanza E33A
(v,
a?p
FO
oD=6
OL
,9 3E
>o o
EE o_x
LF
0,
_ taN
=oC 6'au?
CLE
oo(E .8=
i asE
5EE9
6a - (o
t-5-
ES c
o
hB E 5 o= o o.
>ooE o-o.c
* o
FI F *
F* F *
Fl F *
robrob
NcN.c.
=(,
E
H? ,; s6 i
1=2 Eg EE
.fi
oL
gO
96
9.9 3=E ,:i 3P s
i;;t ;P
d)L
E
o
o ia= s
October 1979 2-13
Section ll BEECHCRAFT
Limitations DebonairC33A
Bonanza E33A
o
Ed
h-YL(EL
I cL
.Yo^O
.4
so :8;;
o-!.
=O
s_E
.go
a-
o
(J !H;* is
x
trl
o
s;E*
6 F AE
eE
E=
E 6 oE o . b E
a
:;;5t:ir
-o-E6Jo(I)-o-Y
sa:i;sE;
r\9
N(U c
a(, o
EJ
z uro 6c (o
EE i
uI 6Z
=-uI .ea
E3a
6E8 68 I9S e
droE 5 .9 o !u'!
o Et
iE ; H93 s
kE #
E
EE
IJ- U'
iEo.cti go
EEsE:
O 9_ (D
Eegl= ED
E#;;E
etEEe
.o(g
P: EEE cc
.9 .9
s€;i! o.
oo cL
F t F
--N
eeN F i F
eeN F I I
reN F I
'
oq o
N h- Gl
tr'i *if; E
EH E:E E E== E
65 e.g
g
PE Ei 3
-Ul =.=-
EA iHE iiapEiE 2-16
Ocrobor 1979
Section ll BEECHCRAFT
Umitations DebonairC33A
Bonanza E33A
ao,
o o o.tE?
t4
so R;;:;
P EO.H E
a
o
(J
,i *E I E;
o
E EE$SI
c
o tee";E.
CtUOO^C
*
(4
, ef fi6 3
a
E
E g a s; r
o
N
cl
F G c
o
=G Ht s .=.!
8e3
fU :
H$E rJs
G'E 3
o..c (E -
-.9-
@- o 0
O a O-C
E
o2 cD o6 cDo
o 3a P EE EE
PEPh
{3 E 5E5i
2-16 October 1979
BEECHCRAFT Section ll
DebonairC33A Limitations
Eonanze E33A
o
.:
o
o
CL
o rO
o ci, ro
IlGt
d
E5
EG
a)
E
e$
E ll
.e6
Jo- o
(L
aa I
t i FGt FF' F
FFI F
t I F(t) FF r F
rFFle
G)t
ot6ol
E,9E E
tr|
tr=fob? lll
b. ! - L-g Y o
E;EHa
EP : ;;;
isBg
EEA TE*;
EEE
6c
,9
CL
o
FFF+
e Ft F
re Eb
D I:etf
IilggItggslillg,g 2-19
October 1979
Section ll
Umitations
orx
t\; (l
F t 6.9
=a
p E2
3-=
6PP oOE
FI tl, 6P'=
tr
l-trr
.o
E eJ
nrtE !r H
tEP itl
tE=L
o
I9E E E
E'= bE
Octobar 1979
BEECHCRAFT Section ll
DebonairC33A Limitationr
Bonanza E33A
FUEL
STANDARD SYSTEM
. Total Capacity 5O gal.
Total Usable .. 44 gal.
OPTIONAL SYSTEM
Total Capacity . ... . .. gO gal.
Total Usable ..
s74 oal.
FUEL MANAGEMENT
Do not take
or with less
Q.'
SEATING
PLACARDS
On Fuel Selector Valve:
oFF
o
. Tt'sl,lo+ oii'#J
Optional 74 Gallon lUsable) Fuel System:
oFF o
T,'8XI O OT,'d[.*
@ WARNING @
EMERGENCY AIRSPEED STATIC SOURCE
SEE FLIGHT MANUAL NOAMAL
oFlF
ervrincerrlcv PRocEDURES
FOR AIRSPEED ALTIMETER //
CALIBRATION ERROR /
EMERGENCY
@
c WARNING
EMERGENCY AIRSPEED STATIC SOURCE
o
EMERGENCY
sEE PlLors CHECK LIST ---r\JI
(
3lEhi3i"#dJ"&i-." -- { flql
'"
FOR AIRSPEED & ALTIMETER
ERROR I\.,I
CALIBRATION
o *o?tJo,- o
On Left Side Panel (Near Vent Shutoff)
October 1979
2-23
ll
Section BEECHCRAFT
Umitations Debonair C33A
Bonanza E33A
PLACARDS (Cont'd)
NOTICE
REMOVE WINTER
BAFFLES WHEN
OAT EXCEEDS 70" I
BAGGAGE COMPARTMENT
EMERGENCY
LANDING GEAR
!NSTRUCTIONS
TO EXTEND
IN REAR OF
ENGAGE HANDLE
FRONT SEAT AND TURN
COUNTERCLOCKWISE AS FAR AS
POSSTBLE (50 TURNSI
On Storm Window:
r CAUTION
DO NOT OPEN ABOVE
r45 MPH lt26 KNOTSI
ROTATE O
HANDLE TO
FULL LOCKED
PLACARDS (Cont'd)
GENERATOR
CIRCUIT BREAKER
PUSH TO RESET
On Control Console:
o*/l
THFOTTLE !,/ PRoPELLER
PUSH OPEN ^EF PUSH HI RPM
@3 @
fr z 3En 9996 gg
v;I;E= ;Elffiif; iI
,? i3r';;;f ;;
3?'z-n.,lE=:=:; =:=
tE i3;i:[lPPPd 3==
lS:H5:ix- Ex ii:i r
fir,iEit;
,,,,8 ;EE
:::;? Hui
=i'=aiI[ ii.i;,\;
=rtl;e=i=-
i=
l=r'iE=ilfirE
oB @
@g
ftl IHliiiE ii
i;igEHflE=iii; 6EI
En:
=it[?;i**::::
Hi;=g;:g :::rrE[n
rI=IEiEI ...;[ B[;
=aEgeiiEi;;i;E=;E
iiEEE=E*EIEE=
arB @
2-2A october 1979
BEECHCRAFT Section ll
DebonairC33A Limitations
Bonanza E33A
*
"Hg,22i
ool
FF
II I
ool
ri?g:I ^ 22
YY
I
I
.nNl
Q(r) I
Itr
o. o-
l
==
loN
:P
;EiEEIiialiliHi
o: UJ
UJ:
c
o
ftn;ei=;E ,,,,eE 6O
ur u.l
a lll
sf
XE
u4
3s
zz
Il?niaaliagi:IlH 69
z.t,
I E iEaEEal* I
SH
==
)f
==
ii
I=iEliEli=HEfiHE
Iloo o. <=. ==
lo o
2-29
Octobsr 1979
Section !l BEECHCRAFT
Limitations DebonairC33A
Bonanza E33A \-'--
PLACARDS (Cont'dl
\-.
Below Lelt and Right Middte Windows after compliance
with EEECHCRAFT Service lnstructions l24l (E33A and
E33C with Optional Openable Cabin Windows):
EMERGENCY EXIT
LIFT LATCH . PULL PIN
PUSH WINDOW OUT
SECTION III
EMERGENCY PROCEDURES
TABLE OF CONTENTS
SUBJECT PAGE
SUBJECT PAGE
EMERGENCY AIRSPEEDS
CAUTION
ENGINE FAILURE
1. Throtrle - cLosED
2. Braking - MAXIMUM
3. Fuel Selector Valve - OFF
4. Battery and Alternator Switches - OFF
NOTE
ll No Restart
l. Select most favorable landing site.
2. See EMERGENCY LANDING procedure'
3. The use of landing gear is dependent on the terrain
where landing must be made.
ENGINE FIRE
IN FLIGHT
ON THE GROUND
EMERGENCY DESCENT
1. Porrver - IDLE
2. Propeller - HIGH RPM
3. Landing Gear - DOWN
4. Airspeed - ESTABLISH 154 kt$77 mph
1. Landing Gear - UP
2. Flaps - UP
3. Cowl FlaPs - CLOSED
LANDING EMERGENCIES
SYSTEMS EMERGENCIES
PROPELLER OVERSPEED
1. ThrOttIE .
RETARD TO RPM RED LINE
2. Airspeed - REDUCE
3. Oil Pressure - CHECK
WARNING
CAUTION
NOTE
CAUTION
WARNING
Do not operate the hnding gesr 6loctrically
with the handcrank engaged, 8s dEmago to tho
mechanism could occur. After emergoncY
landing gear oxtension, do not move any
landing gBEr oontrols or ro8ot any switches or
circuit breakers until airplane ig on iacks as
failure may have been in the gear up circuit
and gear might retract on the ground'
CAUTrcN
SPINS
SECTION IV
TABTE OF CONTENTS
'l'.--)
su"'c' PAGE
Section lV BEECHCRAFT
Normal Procedures DebonairC33A
Bonanza E33A
-.__
i..
TABLE OF CONTENTS (Continuedl
SUBJECT PAGE
, ,t.tt\
(t
,.; ,,-i ( )
, ' rr ,'i. )
\-/
"J
' Take-off
Lift-off 70 ktsl8l mph
50 Ft. 76 kts/87 mph
, ) Maximum Climb
Best Rate (Vr) 96 kts/l1O mph
Best Angle (V*) 77 kts/89 mph
PREFLIGHT INSPECTION
1. CABIN: !
2. RIGHT FUSELAGE:
a. Baggage Compartment Door - SECURE
b. Static Pressure Button - UNOBSTRUCTED
4-4 october 1979
BEECHCRAFT Section lV
DebonairC33A Normal Procedurec
Eonanza E33A
tt
,..,! 3. EMPENNAGE:
a. Control Surfaces - CHECK
b. Tie Down - REMOVE
c. Position Light - CHECK
n d. Cabin Air lntate - cHEcK (cE-26 and Aftert
4. LEFT FUSELAGE:
a. Static Pressure Button - UNOBSTRUCTED
i.- .ri b. All Antennas - CHECK
8. NOSE SECTION:
a. Left Cowl Flap - CHECK
b. Engine Oil - CHECK (See Servicing, Section 8)Cap
and Dipstick - SECURE
LEft COWI - SECURE
Propeller - CHECK, General Condition, Nicks, etc.
Wheel Well Doors, Tire and Strut - CHECK
lnduction Air lnlake - CLEAR
Landing Light (s) - CHECK
Ensine - CHECK GENERAL CONDITION
Right Cowl - SECURE
Right Cowl Flap - CHECK
Chocks - REMOVE
BEFORE STARTING
WARNING
, EXTERNAL POWER
STARTING
CAUTION
CAUNON
Do not engage starter for more than 3O seconds
in any 4-minute period.
NOTE
CAUTION
CAUTION
BEFORE TAKEOFF
NOTE
3. Avionics - CHECK
4. Engine lnstruments - CHECK
5. Flight lnstruments - CHECK AND SET
6. Ammeter - CHECK - for stabilized indication between O
and 25o/o of f ull charge at l OOO to 1 2OO rpm.
7. Auxiliary Fuel Pump - CHECK OFF
8. Throtrle - 1700 RPM
9. Propeller - EXERCISE to obtain approximately 3OO to
4OO rpm drop; return to high rPm
1O. Magnetos - CHECK at 17OO rpm (variance between
individual magnetos should not exceed 5O rpm,
maximum drop rtot to exceed 15O rpm.)
1 1. Trim - SET
a. Aileron - NEUTRAL
b. Elevator - 0o (3o nose up if only lront seats are
. occupied)
12. Flaps - Check operation, then UP
13. Door and Windows - SECURE
14. Flight Controls - CHECK PROPER DIRECTION, FULL
TBAVEL AND FREEDOM OF MOVEMENT
15. Mixture - FULL RICH (or as required by field elevation)
16. Brakes - RELEASED
17. lnstruments - CHECK (Make final check of manifold
pressure, fuel f low, and rpm at the start of the take-off
run.)
TAKE-OFF
CLIMB
CRUISE
CAUTION
DESCENT
l. Altimeter - SET
2. Cowl Flaps - CLOSED
' 3. Power - AS REOUIRED (avoid prolonged adle sertings
and low cylinder head temperatures)
4. Mixture - ENRTCH AS REQU|RED
BEFORE TANDING
NOTE
BALKED TANDING
SHUTDOWN
1. Brakes - SET
2. Electrical and Radio Equipment - OFF
3. Throttle - CLOSE
4. Mixture - IDLE CUT-OFF
5. Magnetq,Start Switch - OFF, after engine stops
6. Battery and Alternator Switches - OFF
7. Control Lock - INSTALL. if conditions warrant.
8. lnstall wheel chocks and release brakes if the airplane
is to be left unattended.
ENVIRONMENTAL SYSTEMS
OXYGEN SYSTEM
PREFLIGHT
D(AMPLE:
People 5
GagePressure ... 1SOOpsig
Oxygen Available (from chart) 80%
Cylinder Capacity (full) . .... 49 cu ft
Altitude (planned flight) . . . 15,OOO ft
Full Bottle Duration (from chart) 149 min
Duration (8O% full) I 19 min
CAPACITY
'6
octobor 1979 4-15
Section lV BEECHCRAFT
Normal Procedures DebonairC33A
Bonanza E33A
OXYGEN DURATION
CAUTION
NOTE
WARNING
IN FUGHT
AFTER USING
NOTE
PREFLIGHT INSPECTION
ENGINE
October 1979
4-18
BEECHCBAFT Section !V
DebonairC33A Normal Procedures
Bonanza E33A
NOTE
rcrNG coNorTloNs
BEECHCRAFT
DebonairC33A
Bonanza E33A
SECTION V
PERFORMANCE
TABLE OF CONTENTS
SUBJECT PAGE
SUEJECT
PAGE
CONDITIONS
At Denver:
Outside Air Temperature .. 15"C (59oF)
Field Elevation ... . 5330 ft
Altimeter Setting . .. ... 29.6O in. Hg
Wind . 27Oo at 1O kts
Runway 26L length 1O,O1O ft
Route of Trip
.DEN.V8'I-AMA
WIND OAT
11500 11500 ALT
ROUTE MAGNETIC DIST FEET FEET SETTING
SEGMENT COURSE NM DIRATS oc IN.HG
At Amarillo:
Outside Air Temperature .. 25oC l77oFl
FieldElevation .... 3605it
Altimeter setting ..... . 29.56 in. Hg
Wind 18Oo at 'lO kts
Runway 21 Length 135OO ft
NOTE
Cruise Climb:
Enter the graph for T|ME, FUEL AND DTSTANCE TO CUMB
ar 1 soc to 5650 fr and ro 33OO lbs. Enrer ar _SoC ro I 1,50O
ft and to 33OO lbs. Read:
TEMPERATURE
MAN. FUEL
ROUTE PRESS. FLOW TAS
SEGMENT IN. HG GPH KNOTS
NOTE
Start, Runup,
Taxi and Take-
off acceleration ooo 2.O o
(or
Enter the cruise power settings table for 45% MCP
full throttle). The fuel flow for 45% MCP is 9'6 gallons
per hour.
Reserve fug| = (45 min) (9.6 GPHI = 7'2 gallons
5-9
October 1979
Section V BEECHCRAFT
Performance DebonairC33A
Bonanza E33A
t
C
i
6 D
9= oz
;;
R8 -8
EFas
:l
el - ll-3r
iEsf;
*l?I sL-a
fiF:p
?L85
9L-E
ol
z Fx^2_
=
UJ
o -[s E
>5
thE
?LE
E!:88sR8
svl
<6 r
sroNxryorlsurvorrvE€nv3 I
gR9888R8893Re88BP
=3
G "*-
o3
2?
zg
9;
F?
8
(o E
o
trH 2 E
coe 2
6 !
J<
<3
o3 i
o
!
OE-. !
uJ
uEl 6
;:
o-yl 1
o
!c :
a I
'I
?83esR98
lI I
: ta
5l
I
x
il :
ilrt
-U
L.,
zU
(9
4
E
I
z
9
F
4
e
U t
o
g 1,6
U =i
B EI
4 1:
2,
EA
9:
-ot
Octobor 1979
Section V BEECHCRAFT
Performance DebonairC33A
Bonanza E33A
Le
t;
EI EElq
:A sll iFr;
I
l5
l6-
HI-3H
al^E
El-=<
< L- o
E lE -..8 sLse
=
lrj d IHEB
!o El . g-IE EI
rSElE 3E
EF::
*F;'
i *l EI2rl? !r
=
E
o lronlrl'lv
rlll
o3j.vf, loNl tloul -tlvulansl
ry Nol]Jl880f, alrll^llllv
z= rfl
o lo
tr
C)
UJ Ei
G L;
trs I L- -
oe
o2
9l-89
; Eir
t3 O L- u
ut= H I-EH
Fi
UJ oE < LsE
E
L- a
e L9.,
l-
=3Ea, sfEE
z lo-
'l-o
sZ
tLes
co L;
<N
o E;
6
4 F:
FI
ot
zl
l30nl[1v oflv3loNl woul lf,vurSns)
ll:U - NOllf,3BUOf, U3r3nlllv
:Z t
;;I
iic Eq
PBH TH
' ,f
; ZF
'l
,E
F<
=5
rF6H
60G
-iA
6ro
)-rI3
u! il2 t :i
;o i1
b *lr;E lSonlrllv qlrvf,loxl rcul l3Y!laflsl
zU ll!l a lollSlSaOS Ullltrtllv
(,
4
ut
tt
=
I o
z
I 2
t
f
(J
rat
4 4
o
4
o
IJ )
I
d a
ul
o
ua l
io
tsz
1E
= ,Y
9t
;e
z:
<a
fic
et
F
o
2
,
G
F
G
U
A
:
zi
Og
6"
EH
uJa
>5
70
o3
oE
<E
Q\
u
CE
f
o
o
U
a(
A
E8
HE
,rr, ".] ronr,r'',o rl'n..rr"
99
oo
2Z
)z
o
ai 9o
EBs a<
z
o
!l- o C
ildei
*IgTY
8
oE
o
UJ
st
.?
e
E Or
@
UJ No
E
o
(L z
o
o 8
o
u.l
lu
L 8
o
o
z
F:=
83
(,13 ^i F
I
o_
o
OE e
ir
E)1 5B
ii;
*z
uO
@c 8
o9
ox
o2
)
?3tr
339
2Za
{qi
E6o
rO_
o
2
5-16 October 1979
BEECHCRAFT Section V
DebonairC33A Performance
Bonanza E33A
WIND COMPONENTS
Demonsl.alod Crosswind Component is 17 kts
EXAMPLE:
FLIGHT PATH
o
F
o
zt
?
F
zU
z
o
o
o
o
z
=
U
I
o
CROSSWTND COMPONENTS ru KNOTS
tllJ^, lf,Nvlsro
E EEs I
i=
>i >!
eb oi
Co -i
9L r= EE oo
zz ,
F g8: 88
)az Eyt
-02 U?s
f;o
UJ d;EI
o "11 cEo
? ,*oo*
z :l 3Je dSHvr:
< ri
6E
dz
dlSrst 59o
an0
(t E}
6 h 8
l!
lt
o
tn
I q
I E;
ii l--
l-s;
"'.
T o rF )
I 2 sEgggq
] l
o *+u f
f,l- E
; F9;
E l-ei
i E
Ou , 1.,
a
5P
dI
aA ["8
t-tr E;
. E-^o
9l r&vd <o-
El jpSs (irlq
zl
ol
:l
EI
Ir
<l I
HIE; q?:
?t P trJ O
=
5-18 Octobsr 1979
BEECHCRAFT Section V
DebonairC33A Performance
Bonanza E33A
o
r
E
ro :-
=6E
J
Ot-
X:
o
c
o
=
E
UO
AEE' g
EtiR:i
E13kia55?E
5
$[B! 8nn] ,O_flw
:lEl-333,
EI; E $ia
October 19
Section V BEECHCRAFT
Perf ormance DebonairC33A
Bonanza E33A
=r3=
=l;
F; E:-
, F;*F;i
@
J
o
o
i:i
F
UJ
o
z 6T
i>
tt:E
b1
Io o
o
z )
tu
f
lt ;
o
ui
=
IF
Fg
C;
ES
o5i^
roO;o
z^:iza
sl -6^<O
EI
sl
ol
a,
il z-f
ol si 65:
,iil
<l O ,=o
5- 20 Octobor 1979
BEECHCRAFT Section V
DebonairC334 Performance
Bonanza E33A
ra $3E tr38B8
?
- --FIFif,**
F F AOO
t,a*E88
I N.!n*),l!t.ttcl
(, Ja a a99lDr?!f!-e
0
o 59
gI Ia
4
? e e1
Hfti il
o 2a C,
I :qqdr!qaq!
@
6 iH KXXSE$EgE
=
EE
c=
*H c fi f fi$'fi,$$f;fi
o 5S 8*,S'*! ee
F
6
J
F
o o E33tr:Etrtts
F
o cI ts-3641?Al
@oo6roal 66
og =
Oi F
F
! Eq isf,!g$
z1
-l Jl
T
A
..Y n.r Nt14qqe
OooOi6d-;
FE o P.ed*-
FE ? 39 I
aEa
luo EE
o; o
A
I
o
-J;-Sr
ooo6ia F
E ia o
E
zd
1H
I @ - o OntEl(ll€t
+ i ri eir;CdCtd
NNNNCBF?F iul
3
IIJ
o
9J
8s z
o
ia =
E oo
oo
gF
:o
t$
o-7 60 F OU
3b
I
E E EN.$$EB
E,
urE o
N o o @ dWE
r r?t * !, <j
o'o F
o
o
)= E
o SBggt*ng:r 7r
FF
E2
o; F
I
A
T
rF-{Sltaha
o@oo!,a',a'I az
F d=
E
a
EEE8,8'ilS99 6<
6 I
a 4ltr OG
ts
o
Ja o sg{!,j
HO EE
s EI I
& Ei
ac)
A@
I ia o osorH:Suor
)F
oz
I
o <U
z RRsNs*frd Zu
=F <c
I
ie ,i.:i:lni:arir r::i:: :' >ft
E UE
2 9H A
fi f F E.,*$
G F<
=o FU
oc
F
o
o TTiT ,Slfrig G<
I^
F;
o o R R: -i*r.!!I H
L ,JO
)<
@
@!
F
U
U
,EgE*'i T o
F< 2-c
9o =
=u
OU E
G EEFfi$,'f;f;.*fr
=h o Foo@6t6dt.id
ts
6 o E 6NO6ai5Ct
oo@FEa9e.a
J o
F
F rc F6B SS8tsEH
or
OF
o a
F
=
F
EiEQ,t.,S[EI
.**eab
zi f, a
I
c
onec?fial18Ft
oooolDil-rI€
l-r
FE
9_ dl
>:
o
rc oeoolrt(,r(G
uJ9 u
GE
3B3Silgf,tS F
Oc o (, otorAa?l}r
Po o zG I
t
LlJ
t@ tr
H: o SH z
r,riciGirldtiSr
N N N N Eft F F i x:
GF
z ts dY
o
o.i 9" F os E
c
d
EEH sgfisnf;
RRHilil
<;
UF
E
I roo@dd&Ft <j
F I :,:t l ti
98
]E
o E o@oN5&dlo6 z-
FF
rll
all
q@60Didi!a
FFF@oOOhF i!B
ed+F$ @z
2
=
ti,
F
gt EEEEESE.*.s
t!.T
al .,| c? e?
Q! .? 6<
AE
o _d= oll o o o o otta al UQ
EC
ao
o qqccqrlqti
R EI 99R9Rf,ETI O@
I l JF
o
26
<U +rl ci.ici-;{tiE.'d
o@o@o,ilrrtiit
NNNNNd$?f
IU
-6
Zw
@
o =E I <E
ti fisEsfi*f;3fi
I
EeI ud
)
NNNNNHLfifi L<
HH l-u
-; I
oFFro*** oG
E<
ol gt
t---SHg
I I l. 1.,,1. IO
<t N o o @ - Satilt
N N - Lt ijla .Jo
aJ<
!!fr
o
QF F
E ,EEBs o
g< u
E $$I z-oi
FE 2 59 I !q0qqoqe
c
t!o fI
c 6@@@@ 6{dl F
Oe o
zo (,
n
E Hc3:
o
E
TF
I
z
@F@-@d6iiO
ciei..ic.i;dddd
NNNNNdF'' I:
9F
qF
o 9o
2 tc 8888898ts8
6
o-z
35 F =u
OU
zh G NNNNNNftN(
:tr
-I
.l l--
lFo6o-ADtP
r t'ii <j
uJ2 =
o8 F
o
ol
F
Ll looo-ai6lrl,
!!,lffi
A)
(rr
4r
)=
E?
ol l@orsofrsli
I
cs 33EEF&fr$8
FF
h;
oi az
: ts F sssseS,tgQ f=
rF
6<
JT
o Ja
-G I ,F: Ct
ict G a! tl AE
6 6 cd
o 59 I 6@606 do
R EI C n*,*n,'l o@
JF
J iil o rstl oz
u <u I
o
t =F z tsf s Zu
-@
<G
>ft
:
I
Ee
I ou 4G 8888es,8[:,8 UE
)
N N N N N rl |l, .'l ft F<
FU
=h OG
F o
o rrj jj O c<
Io
tss
o o
JO
,-
aJ<
U]I
Ul
F
E
u
,RgEg o
s< E IifrT Z-N
I4
q
BtstsE8aS$,13
= oo@@OA-
F F 6000rr9! rH
I @@@@ooot4tdr
o E
o -,::::j:39:
R
3 5i I
d
6@@@@@@E
!r!:Ddrrs
I
o
I ,z
(, .t9qa.q.fqf,.
-OOO@@hGG
+ 3rr
=6
=u
OU A
=
E
8888888*.fi NNNNR
ao
F 0 tso66-FOOfr
66&NNFF
U
J o E;3sP3B$.,:t
F
l- to -o(@6o-Bl 6@@O5
os
(9F
o
F
9
F -o<@@ooit
600000Qt8
F F F#i:*
zi l a
L
A
o
@@q@qqqlq
6di66ooo6ali
l-E 2 @@@@qq9eF:
rug Hi I
4
4 oo6OO6OO0
U
F
OE
E u.-
o
o
tl
zO :2
(9
o N @ O I @ - 5'l
o o o d dj F r {igl
E
;1
u, 3l
=& TE o;
tri-
E
o 3E
9"
o
z
F
Ee
OU
E
d
88888888,8 PO
:tr
-t
o.l I
o 1a c nNNNNNNt(
Foo6-OF&S
Uts
tr.
<:
uJ2 o ! t'i'
o8 F
o
o
L d66Fn@o$16 ?t
l= dNFg
FF
6= 2
E
I
4
B !EDEETgEg i!B
az
E
F EEIiET9SS et
ir
6 JB
r
G @qqqqqqqtl @&
OU
U Ed
o 39 E @@@@@9q@ oo
R a iidAtstststs o6
i6hbo66on JF
-! 20 0 a@-oooFoil oz
o
E
II
:I I
Z
doiotdF;<jd{ IU
Zu
<G
>ft
I
Ee E
cE 888888888 )
Ud
HH
ildNNNNNNO !-<
FU
OtsFOOOF- oc
o E<
F o
"'i'i'i117
@oNocrar9
Io
o g
N-- r.i.i.i . JO
a)<
@fI
o.
UJ
ts
U
U
dEsEsEEgl ts[6
o
F< G Z-6;
CRUISE SPEEDS
ASSOCTATEO CONDTilOflS. EXAMPLE
AVERAGE CRUISE WEIGHT 3I@ LAS FFEEEUEE trrruoe r rsoorr
TEMPERATURE STAiiOARO OAY {ISA) POWER SETTING FULL IHRONLE
25M RPM
€o
1 6000
1 5000
I 4000
1 3000
r 2000
l 1000
ts
U
U 0000
u 1
?
U 9000
o
l
h
)
F 80@
G 7000
f
a
a
u 6000
E
c
sooo
4000
3000
2000
rooo
SL
su ,@ cau 3
'za
rd,
= d<
?o
ul
d.
f
r^
t/l
ur
&
G
o
o
=
z
=
October 1979
5-26
BEECHCRAFT Section V
DebonairC33A d
Perlormance
Bonanza E33A
! il-^,.e*oese"o*r" 213 75
75* MCP
@itDt1toN LEVEL FLIGHT CRUISE
BRAXE }IoESEPOWEF
Et
-P>l
1=&l
H:s I
;"-l
ol
fl
Fz I
<E I
erHH I
rl;5 I
*tpF I
oi
z
oit
Jo>
J?3
Oxk 1,
o
z
Ca
r\ s -q ;o
EI E
U
t9
lll o i;a a
JT qE U
rL Y ;Y] !
ol.
G
';2
sl95
J
o
L 9l*s tr
tr
UJ
2
o I
z U
(9
z
G; E
2
;gg
EdI
b< :
-o-i
az<o
e 93,
:to.
gBd
zl
ol 133J - lonllllv lunSSlSd
21
Fl Z
ol
2
:t
ul
r:
av
o
1l-
ali
n*
ol
3l s;;i
?lr*??z
5-24 Octobor 1979
BEECHCRAFT Section V
DebonairC33A Performance
Bonanza E33A
i
E
-tr8 tz
"Er
H:a
o
)
E9
>2
<E
arE
xl Eo
o3
z9t
odv
J^?
J, z)
<d
o3,
ta
rt c- e-E
;"xj
'i nfl
url
JE E5
J1
l!9 =;
O S -rUl
E. 5I'E
O- zt.it
u,t
(,
z
E, i,
2
6
z6
_=) 1lllj- 3OOlll'lv
$d*
u< *
SSnSSlUd
-d-<-
a2<o
eP3-
N<J]
Iloo
zl
ol ,"
Eta
6l^
2l
3l
ol
,i
E-
'-
iI. iJ
ol + oJ
ol o--<
ulgHH=
Octobor 1979 5-29
Section V BEECHCRAFT
Perf ormance DebonairC334
Bonanza E33A
e
:
-9>
LId
IE
H:s or
-fo r9
o
f
to
\=
^rt:-
:llf Q
xlEO
o
z E.
o Eg
J
o !3
a Fl
G
ta ba f,
o
I
3E
-ri @u?
6o
l!o .5
ot
G2
ut
9:
z
E
o.f Floi ozo
du
UJ
o 9l;;
z
G
f
o
zUJ
gEEEd
=
-Y9
5?:
to-<'
az<o l:l3J- lOnllr'lv lUnsslud
'i fo
IIo"
zl
Pl e
El i
vl
II-
oli B:
olo--<
o:
3lgH5 !
5-30 October 1979
BEECHCRAFT Section V
DebonairC33A Performance
Bonanza E33A
rri
E I'
P
-LrIt] >lEg
ElOo
^F
H:ellS
=
? Rl;s
E"l
>z I
<E lq
-r .'B lE
flEE IB
O@
ZI*
o:=
J=a
Ji*
6Ii
it eH
csE
r< at
6 lla
uJ 6"',
Ja =
6
)a
Oq
llo
-
OE
tr2
=5 n'=
Zi
o- i -,Bl
u "' El.'i
o
z
E
fr.
os
z3
ltJ =" ^
20
-i9
xd3
tso !
uq
69-<
az<o
5P3'
N<Jl
.
dl =5o-
6<@{
6l
EI
q
el
Ol
.q
Fr
6
EI
ol +
3H
di
Essi
Ql
Octobsr 1979 5-31
Section V BEECHCRAFT
Performance DebonairC33A
Bonanza E33A
o
2
;o llll^,lJNVlSiO
:Fqo
I
,Lof5
Eod
Eg E
I
I
z
o
OF
)2 LO
{X dea
.u5
:l 5*i.'1 t
35;
=l
*lAr-gi
LlJ
o
z
F
I
o
o
z
6 888888
z
J
5
5s
ES
tq
z_, 6
It
an ie
'o u,
9z
o<
i?>
di -=
>, Ovl2
3
Fl
iaaa3?i
6t
2lo
ul
ol
et
,.i o
gl or
<l
UI E
or?o
Z 3 A2
fls qetE:
?lP i1?tc
5-32 Octobor 1979
BEECHCRAFT
DabonairC33A
Bonanza E33A
SECTION VI
WEIGHT AND BALANCry
EOUIPMENT LIST
TABLE OF CONTENTS
SUEJECT PAGE
WEIGHING INSTRUCTTONS
LEVELING
POINTS
t
I
FRONT JACK POINTS REAR JACK POINT
F.S. 83.1 F.S. 271.O
NOTE
@$
(r) +
zUJ @@
GI
o o
= c
o
o
Lr.l
= '.2
E
E c
o
(, o)
o. N
F E c UJ o =
G E'
o
f E
o I o (o o.
c
.9
o,
E 3 (0 (o
lrl z o .9
o o
(J a .I o 6l (il
z q Etr
(E
o
5
o @ FN
c'i ztt o
6 o 3 tr
.9
o F o o
z E
r( lLl
(E
-o
F ci o
= G, f
I z o. cc F
o
(, d Y =o
IL
IL E
C
tr uJ o (U
3 E (, at
c
F
wZ .9
.l
o-
z <o
o<
E
E
o
=,
u AEB (,tuJG o
o =
o !t
o
o Hq-
O-cl
o
F =o
z-- 2 6' o E
L
L
.O
o
>o-
uJ
- 3 u-
z
o Oo 0 o LU u.t
z ,--a oy o
E ,?=
tro -rE .o
(,=14L
E.
UJ
=uJ o<
<-, -<=
27ts a
o
o
(E
gEfrH
ao
(r,
HHH llJ
G,J
r
3=5s
z*-)
N FUJS
z
u,
ul
r E*ep t923
>UJJ<
z EE8
o u,r trI
o
m =
6-6 October 1979
BEECHCRAFT Section Vl
DebonairC33A Wtand Ba[z€quip List
Bonanza E33A
(Jp
6i
<(9 Ble
.0tr
o3 =l-
o => -G
z EE
UJ iw
!3
(9
A -:-
o
ut
U:
z-
o sfi
E 6G E-
o .G
io A,Z
<=
o
UJ
E 93
u,
ut
o
3fl -G
zo o !3
o
s6 UJ
J
o
ok
2E
L
G
lt
ts-o o
6E
tr
z
elH
3 F>
=<
g6
ooE
u.r
F
c; )
z o
=
u,
o E z
z
UJ
s
G
UJ o
o
October 1979 6-7
Section Vl BEECHCRAFT
Wt and BalTEquiP Ust Debonairc33A
Bonanza E33A
9r
O- Elo
<o
oE
Olo
o3 =l-
o => ,lh
z ZE
ul -c'd
!3
o
o- -:-
o Elo
ut olo
UA =l-
z-
o s6
G 6E
o =-
.G tZ
o io <=
UJ
E 9?
UJ Ee ,o
o o :3
z oz o
z lrJ
to o J
ts o
o F
z G
F
G,
o lt
-(, o o
UJ
G z
UJ
3 fz
=o
=<
E+
36
UJE
oo
f
o o
z
=
UJ
E
o =
z
J
!G UJ
ul o
|t,
LOADING INSTRUCTIONS
It is the responsibility of the airplane operator to ensure
that the airplane is properly loaded. At the time of delivery,
Beech Aircraft Corporation provides the necessary weight
and balance data to compute individual loadings. All
subsequent changes in airplane weight and balance are
the responsibility of the airplane owner and/or operator.
The empty weight and moment of the airplane at the time
of delivery are shown on the airplane Empty Weight and
Balance form. Uselul load items which may be loaded into
the airplane are shown on the Useful Load Weight and
Moment tables. The minimum and maximum moments are
indicated on the Moment Limits vs Weight table. These
moments correspond to the forward and aft center of
gravity flight limits for a particular weight. All moments are
divided by IOO to simplify computations.
FS
PILOT &
f PASS
fwo Pos 85
Afl Pos 89
li-----: FS
142
liaror,rr, waGHI 270 pouNDS TNCLU'TNG EoutpMENT aNo BAG.AGE oR b,, .EAT AND
5 ersttrctn
| :) unxruuv wtronT
2m pouNDs toRwARo of R€AR sPAR INCLUoING €oulPM€ Nr ANo cABGo
: wtlH rru ANU 4rr, stAl5 HtMov€u
I i'r ro*,uuu wt,c6i 270 pouNos AFI of REAR sPAR tNcLUotNG EouIPMENT ANo cARGo wlTH
V 3td 4r\ AND 5lh StAr5 REMOV€O
2000
75 71 lg sr 83 85 87
weight and
Moment limits are based on the following
of gravity limit data (landing gear down)'
""n,ur.
WEIGHT
FORWARD
AFT CG LIMIT
CONDITION CG LIMIT
82.1 86.7
3300 lb. (take-off
or landing)
77.O 86.7
2800 lb. or less
October 1979
6-10
BEECHCBAFT SectionVl
DebonairC33A Wtand Ealz€quiP List
Bonanza E33A
MOMENT LIMITS vr WEIGHT (Continued)
Minimum Maximum
Moment Moment
Weight To- 100-
2100 1617 1 821
21lO 1 625 1 829
2120 1 632 1 838
2130 1 640 1847
2140 1 648 1 855
21 50 1 656 1 864
21 60 1 663 1 873
Minimum Maximum
Moment Moment
Weight - i66- -.ioo -
2700 2079 2341
2710 2087 2350
2720 2094 2358
2730 2102 2367
2740 2110 2376
2750 2118 2384
2760 2125 2393
2770 21 33 2402
2780 2141 2410
2790 2148 2419
2800 21 56 2428
z'aro 2167 2436
2820 2177 2445
2830 2188 2454
2840 21 98 2462
2850 2209 2471
2860 2220 2480
2870 2230 2488
2880 2241 2497
2890 2252 2506
2900 2263 2514
2910 2273 2523
2920 2284 2532
2930 2295 2540
2940 2306 2549
2950 2317 2558
2960 2328 2566
2970 2338 2575
2980 2349 2584
2990 2360 2592
Minimum Maximum
Moment Moment
Weight 100 100
3000 2371 2601
3010 2382 261 0
3020 2393 261 I
3030 2404 2627
3040 2415 2636
3050 2426 2644
3060 2437 2653
3070 2448 2662
3080 2460 2670
3090 2471 2679
3100 2482 2688
31rO 2493 2696
3120 2504 2705
31 30 2515 2714
31 40 2527 2722
31 50 2538 2731
31 60 2549 2740
31 70 2561 2748
31 80 2572 2757
31 90 2583 2766
3200 2595 2774
3210 2606 2783
3220 2617 2792
3230 2629 2800
3240 2640 2809
3250 2652 281 I
3260 2663 2826
3270 2675 2835
3280 2686 2844
3290 2698 2852
3300 2709 2861
COMPUTING PROCEDURE
9. SUB TOTAL
RAMP CONDITION 331 2 281 6
o
o
cir l: e l.() O) q @ c{ (o O tO O, (Yl lr -
tO f- @ (D N t ll, f\ c-,1 \t
N 5 t -FFFFFFFNNC{ @ O)
-
-c?
rt o
a.A E
lr.o =
=o E
o oooooooooooQooo
I
-<6@FOcDO-c{(')$ro@r- EFF
ru
o =
zul s tr !t o
o
o N
rt cD-str0@-(o(o@
o
= !t so sf(of-@O)eN(/rst
c
o
*o
a6 ee6,lNC{N
o- &
=
=
o t,
=
ip
oZ
G)
o
o c N
o
o cc .E
F< o o.9 Tf)NCDc\I{(o@ON n ul llJ
IA o {tO@q}o)OeG)sf troE
of ao i.E
LO
o
=
e-NN(rIC{
EP G, o- E= HEtn
BB = zS))
o o
o tr
o o
g) e=83
o
E,'F
<'E 5
F(Oc')<tc',1 -O(D@
Oeo,l('){tr,(0@f- ilI:8
f
lt
o
o o.
E
= o
FFE
9>=s
UJ
o oo
= 0Hefr
f, tF=>
(,OYa)
c g
o ro
o
o OurF{
tt o.9
l'E
o
5
c!oo@(ost(Y,olo
O--(rl('r$lI)@r\
FFFEFFFFF
th8;
2J^LT
o.
t=r o {cir.uF
= 5<k5
?,96 z
I(9 ooooooooo
ssEg
N(Yr{to@F@o)O ui@84
ul sHEd
zl20.
3
October 1979 6-19
Section V! BEECHCRAFT
Wt and Bal/Equip Ust DebonairC33A
Bonanza E33A
10 14 11 14
20 28 22 27
30 42 32 40
40 56 43 54
50 70 54 68
60 84 65 81
70 98 76 94
80 112 86 108
90 126 97 't22
100 140 108 135
110 154 119 148
120 168 130 162
130 182 140 176
140 196 151 189
150 210 162 202
160 224 173 216
170 238 184 230
180 252 194 243
190 266 205 256
200 280 216 270
210 294 284
220 308 297
230 322 310
240 336 324
250 350 338
260 364 351
270 378 364
USAELE FUEL
5 30 23
10 60 45
15 90 68
20 120 90
25 r50 113
30 180 135
35 210 158
& 2& 180
44 264 198
50 300 225
55 330 248
60 360 270
65 390 293
70 420 315
.G
.olL
Moment
Ouarts Weight 100
12 23 6
SECTION VII
SYSTEMS DESCRIPTION
TABLE OF CONTENTS
SUBJECT PAGE
Air{rame 7-5
Seating Arrangements ...' 7-5
Flight Controls . ". 7-5
Control Surfaces 7-5
Control Column 7-5
Rudder Pedals 7-6
Trim Controls .... 7-6
Electric Elevator Trim . 7-6
lnstrument Panel .. . 7-6
Flight lnstruments . 7-7
Power Plant lnstruments . . 7-7
Cluster TYPe
Power Plant lnstruments ' 7-7
lnstrument Panel Schematic . . 7-8
lnstrument Panel Legend '... 7-9
Tachometer, Manifold Pressure and
Fuel Flow Gage . 7-10
7 -11
Avionics Panel
Switches 7-12
Annunciator SYstem 7-12
Warning Light ... 7-12
Ground Control 7-12
Wing Flaps ..... 7-13
SUBJECT PAGE
7-3
October 1979
BEECHCBAFT SectionVll
DebonairC33A Systoms Doscription
Bonanza E33A
AIRFRAME
SEATING ARRANGEMENTS
FUGHT CONTROLS
CONTROL SURFACES
CONTROL COLUMN
RUDDER PEDALS
TRIM CONTROLS
INSTRUMENT PANEL
FLIGHT INSTRUMENTS
The lloating instrument panel contains all flight
instru-
panel are the
ments except the magnetic compass' On this
airspeed indicator, gyro horizon, altimeter' turn coordina-
with
tor, directional gyro, and vertical speed indicator'
piorislons tor an ADF indicator and a clock' Additional
can
navigation equipment, such as dual omni indicators'
be rirounted in the panel directly below the flight in-
strument grouPing.
C"
G'
c.ct
ot!
i3 u':t
,z-\
(!/
I I t\
=
(ir:t
.\I
3e@ e,
cD
@@" oo
et
r,'lt
+
6r:l
E9cr
-E
t- .9'=99
E 6-;2aE=EE
sE E E r; EE Y*84 .p
i5!;#H{;;:EEE,qp
,Hi5iE_?$EE-s$;?;5
o
2
ul
(,
u! iEFIIEf,Eif,EE}EE
uI -i
P9}PsRKNRXKRRRR
e3
o.;
it
f
= -9
oi
o)
!c q)i
"I [p i*
o
E
=
;i*tiE s;:qss EE
i:I:g:EEEF$*:=Er
c.id { d<t d o, ct
F. - oic'j <
-
tNJ')rl6h=i
,,
rhcHaS
mrnrunv
bSGAL /rfr
\_\ r0OO tO
-::v)-
/m rl
?0 Jl \) iooo:
-.]
TAKE-OFF &
CLIMB POWER
RANGE
ln the cruise power range, the green sectors cover the fuel
flow required lrom 45o/o to 75% power' The lowest value of
a given sector is the cruise-lean setting, and the highest
value of the sector is the best-power setting for that par-
ticular power range.
AVIONICS PANEL
Tuning and selecting equipment for the radios, to the right
of the center panel, is mounted in block form with switch-
ing on the lelt edge of the block and radio heads and tuning
on the right.
October 1979 7-11
Section Vll BEECHCRAFT
Systems DescriPtion DebonairC33A
Bonanza E33A
SWITCHES
ANNUNC]ATOR SYSTEM
WARNING LIGHT
-f\<\ad
NOTE
GROUND CONTROL
WING FLAPS
CAUTION
Never taxi with a flat strut.
CONTROL SWITCH
POSITION INDICATORS
Landing gear position indicator lights on the right side of
the control console show red when the gear is up, or green
when it is down, illuminating only when the actuator
assembly reaches either extreme. ln addition. a
mechanical indicator on the floorboard beneath the control
console shows the position of the nose gear. lts pointer is
linked by a cable to the actuating mechanism and moves
simultaneously with it. Limit switches and a dynamic
brake automatically stop the retract mechanism when the
gear reaches its full up or full down position.
SAFETY SWITCH
CIRCUIT BREAKER
The landing gear circuit breaker is located on the lelt
subpanel. This circuit breaker is a pull-and-reset type
breaker. The breaker will pop out under overload
conditions.
BRAKES
The brakes on the main landing gear wheels are operated
by applying toe pr.essure to the rudder pedals'
CAUTrcN
Continuous brake application of either the
pilot's or copilot's brake pedals in conjunction
with an overriding pumping action from the op-
posite brake pedals could result in the loss of
braking action on the side which continuous
pressure is being aPPlied.
The parkihg brake push-pull control is located on the right
subpanel. To set the parking brakes, pull control out and
depress both toe pedals until firm. Push the control in to
release the brakes.
CAUTION
The parking brake should be left off and wheel
chocis installed if the airplane is to be left un-
attended. Changes in ambient temperature can
cause the brake to release or to exert ex-
cessive pressures.
MANUAL EXTENSION
WARNING HORN
BAGGAGE COMPARTMENT
WARNING
Do not carry hazardous material anywhere in
the airplane.
SEAT ADJUSTMENTS
Armrests for both front and rear seat passengers are built
into the cabin sidewalls and the door. ln addition, an
armrest between the two front seats may be raised into
position or lowered flush with the seat cushions.
of the
Release latch front of bar, pull bar at the bottom
windowoutandupward.Windowwillopenapproximately
two inches.
To Close Window:
of the
Pull inward and down on the bar at the bottom
bar moves downward'
*indo*. Resistance will be felt as the position'
Continue moving bar downward to its lowest
Check that bar is locked by the latch'
NOTE
OPTIONAL
EMERGENCY EXITS (E33A, E33C WITH
OPENABLE CABIN WINDOWS)
WARNING
POWER PLANT
ENGINE CONTROLS
COWL FLAPS
and to the
The push-pull cowl flap control is located above
left of the control console on the subpanel' Except in
be open
extremely low temperatures, the cowl flaps should
ground operation, take-off, and as required in ftight'
during
7-19
Octobor 1979
Section Vll BEECHCRAFT
Systems Description DebonairC33A
Bonanza E33A
LUBRICATION SYSTEM
The engine oil system is the full pressure, wet sump type
and has a 12-quart capacity. Oil operating temperatures
are controlled by an automatic thermostat bypass control.
The bypass control will limit oil flow through the oil cooler
when operating temperatures are below normal and will
permit the oil to bypass the cooler if it should become
blocked.
STARTER
PROPELLER
FUEL SYSTEM
CAUTION
Before refueling, make certain the airplane and
fuel dispensing unit are properly grounded.
Failure to do so creates a fire hazard.
FUEL CELLS
ts
zU
ELECTRICAL SYSTEM
BATTERY
ALTERNATOR
UGHTING SYSTEM
INTERIOR UGHTING
EXTEBIOR UGHTING
The switches for all o, tho oxtsrior lights are located on tho
pilot's right subpanel.
NOTE
ENVIRONMENTAT SYSTEMS
CAEIN HEATING
When the control is pulled f ully out, the cold air is shut off
and only heated air enters the cabin. The forward vents,
located on the firewall forward of the rudder pedals,
deliver heated air to the forward cabin when the CABIN
HEAT control is pulled fully out.
To deliver heated air to the aft seat outlets, push the AFT
CABIN HEAT control. For maximum heat, the control is
moved to lull open position. To obtain heated air for
delrosting the windshield pull the DEFROST control out. lt
may be necessary to vary or close the AFT CABIN HEAT
control to obtain maximum arr flow for defrosting. To close
off all air lrom the heater system, pull the red VENT
SHUTOFF control located at the extreme left of the pilots'
lower subpanel.
CABIN VENTILATION
, OvtFaO^nO vE{I
I
MtxtR vAtvt r( otD PoslrloNr
I
fFESH AIfi INIA(T NOSF
I
fFESH AIA NIAKT
I€NGINT BAITLEI
I
wrNG FOOI rl rt i
I
OUI LE I
D6fFOST€'
VENT SHUIOfF
coxrBor
afr cABrN HEA! CONIFOT zi
OVEFH€AO 4A SCOOP
'FESH
ANO DIFTUSEF VATVT CONTROT
INDIVTOUAL OVERHTAD.--'-+
fFESH AIB OUTLEIS I
OVEFH€AD AOJUS]A8LE EXHAUSI
sHUIOfr CoNIROt--1
r-'u"-o':r_:-..
..-r...-...-
FRFSH AIR INTAXI --Q I
CE ! rh,u CE 25 t;
L
/\
::,t"*^ll*'-P[
ll
Ir
rl
MUffLTN
rntsH atn
WflG ROOI {FBl
A fOFWAAO OUTTET
ot rFosItF
i:L',-ill"*'.-*-+
1i\ AII oUTLEI
ra h fnotl stAIl
I
I
sT csrx oulltl
I
I
I
r
I
lO
\/,
l/'
I
Fresh ram air from the air intake on the upper side of the
aft fuselage is ducted to individual outlets above each seat,
including the optional seat. Each outlet can be positioned
to direct the flow of air as desired. The volume of in-
corning air can be regulated by rotating the outlet A
system shutoff valve is installed in the duct between the
overhead fresh air scoop and the individual fresh air out-
lets. The valve is operated by a push-pull control in the
overhead panel.
EXHAUST VENTS
OXYGEN SYSTEM
October 1979
7-33
Section Vll BEECHCRAFT
Systems Description DebonairC33A
Bonanza E33A
PITOT SYSTEM
STALL WARNING
warm
Minimize ground operation time. especially during
break-in period' avoid engine idling in
weather. during the
excess ol 15 minutes, especially in high ambient
temperatures.
sEciloN vlll
HANDLING, SERVICING AND
MAINTENANCE
TABTE OF CONTENTS
SUBJECT PAGE
lntroduction 8-5
Publications 8-6
Airplane lnspection Periods 8-6
Preventative Maintenance That May Be
Accomplished By A Certilicared Pilot . 8-7
Alterations or Repairs to Airplane 8-7
Ground Handling 8-8
Towing 8-8
Parking 8-9
Tie-Down 8-9
Main Wheel Jacking 8-10
Prolonged Out of Service Care . 8-10
Flyable Storage - 7 to 3O Days . 8-10
Mooring 8-10
Engine Preparation For Storage 8-11
Fuel Cells 8-1 1
SUEJECT PAGE
8-13
External Power
8-1 3
Checking Electrical EguiPment
8-14
Servicing
Fuel System 8-14
Fuel Cells 8-14
Fuel Drains 8-14
Fuel Strainers ... 8-15
8-15
Oil System
Oil Change Procedure 8-16
Battery
8-17
Tires .
8-18
8-18
Shock Struts
To lnflate Struts .
8-18
To Replenish Strut Hydraulic Fluid 8-19
Shock Strut ShinrmY DamPer
8-20
8-21
Brakes
8-21
lnduction Air Filter
To Remove and Clean the Filter 8-21
Vacuum System (C33A) 8-21
lnstrument Pressure System (E33A) 8-22
Propeller Blades 8-22
8-23
Oxygen System
Oxygen CYlinder Retesting
8-24
8-25
Minor Maintenance
8-25
Rubber Seals .
Alternator
8-25
8-26
Magnetos
8-26
Cleaning
Exterior Painted Surfaces
8-27
Windshield and Windows
SUBJECT PAGE
lnterior 8-28
Engine 8-29
Recommended Servicing Schedule 8-30
Lubrication Points . 8-36
Consumable Materials 8-42
Approved Engine Oils 8-44
Bulb Replacement Guide 8-46
Overhaul or RePlacement Schedule 8-47
Special Conditions Cautionary Notice 8-47
Landing Gear 8-48
Power Plant ......' 8-48
Fuel System 8-49
lnstruments 8-50
Electrical System 8-50
Flaps and Flight Controls ""' 8-51
Miscellaneous..... "" 8-51
8-3
October 1979
BEECHCRAFT Section Vlll
DebonairC33A Handling, Serv - Maint
Bonanza E33A
INTRODUCTION
PUBLICATIONS
NOTE
NOTE
GROUND HANDLING
'l
The three-view drawing in Section shows the minimum
hangar clearances for a standard airplane. Allowances
must be made for any special radio antennas.
CAUTrcN
TOWING
CAUTION
PARKING
CAUTION
TIE-DOWN
CAUTION
Persons should not be in or on the airplane
while it is on a main wheel jack.
the nose strut and reduce the angle ol attack of the wings'
Attach a line to the nose gear.
FUEL CELLS
GROUNDING
PITOT TUBE
lnstall cover.
WARNING
Remove all covers and tape, clean the airplane and give it a
thorough inspection. particularly wheel wells. flaps, and
control openings.
EXTERNAL POWER
CAUTION
SERVICING
FUEL SYSTEM
FUEL CELLS
grades'
See Consumable Materials for recommended fuel
CAUTION
FUEL DRAINS
FUEL STRAINERS
OlL SYSTEM
CAUTION
The engine oil filler cap and the dipstack are accessible by
opening the access door on lhe left upper engine cowl. The
sump capacity is 12 quarts. Normal operating level should
be 1O to 12 quarts.
2. Locate the oil sump drain plug at the low point of the
engine sump.
6. Replace the oil sump drain plug and fill the engine with
oil.
BAITERY
TIRES
NOTE
SHOCK STRUTS
TO INFLATE STRUTS:
CAUTION
lf a compressed air bottle containing air under
extremely high pressure is used, exercise care
to avoid over-inllating the shock strut.
WARNING
NEVEB FILL SHOCK STRUTS.WITH OXYGEN.
FLIJID: ,
TO REPLENISH STRUT HYDRAULIC
2. Remove the air valve cap, depress the valve core, and
allow the strut to fully deflate.
WARNING
Do not remove the valve body assembly until
all air pressure has been released or it may
blow off, causing iniury to personnel or
damage to equipment.
NOTE
BRAKES
least
This filter should be inspected lor foreign matter at
on"L orring each So-hour operating period' ln adverse
preflighr
climatic conditions, or if the airplane is stored'
inspection is recommended.
and remove
2. Remove the wing nuts securing the filter
the filter.
PROPELLER BLADES
WARNING
OXYGEN SYSTEM
WARNING
CAUTION
4. Slide the pilot's or copilot's seat aft until the f iller valve
is clear. then remove the cap from the filler valve and
attach the recharging outlet' Open valve on supply
bottle slowlY.
5. Open the cylinder shutoff valve and slowly fill the
cylinder to 1850 * 50 psi at a temperature of TOoF' This
pressure may be increased an additional 3'5 psi for
each degree of increase in temperature' Similarly' for
each degree of drop in temperature, reduce the
cylinder pressure 3.5 Psi.
6. Close the cylinder shutofl valve, close the supply bottle
valve, remove the recharging outlet, and replace the
filler valve caP.
MINOR MAINTENANCE
RUBBER SEALS
ALTERNATOR
MAGNETOS
WARNING
CLEANING
WARNING
Do not expose conlrol surface trim tab hinge
lines and their pushrod systems to the direct
slream or spray of high-pressure, soap-and-
water washing equipment. Fluid dispensed at
high pressure could remove the protective lubri-
cant, allowing moisture lrom heavy or pro-
longed rain to collect at hinge lines, and then to
freeze at low temperatures. After high-
pressure or hand washing, and at each periodic
inspection, lubricate trim tab hinge lines and
trim tab pushrod end fittings (Brayco 3OO per
8-26 Revised: March 1983
Section Vlll BEECHCRAFT
Handling. Serv - Maint DebonairC33A
Bonanza E33A
CAUTION
not be polished
for protection f rom the elements, but should
damaged
,nflss potisning or buff ing is required to restore a
although not
area. Waxing of polyester urethane finishes'
use abrasive cleaner
required, is pLrmitted; however, never
compounds' as these
type waxes, polishes, or rubbing
products cause eventual deterioration of the characteristic
on a
,rethane gloss. Epoxy finishes should be waxed
to restore
regular baiis, and may be polished and bulfed
upi""r"n"" should "chalking" occur' For waxing' select
a
product' Do not
nign quaf itV automotive or aircraft waxing
,rI" u'*rr'containing silicones' as silicone polishes are
of wax on any
difficult to remove from surfaces' A buildup
will yellow with age; therelore' wax
exterior paint finish
shouldberemovedperiodically.Generally,alphaticnaptha
and safe lor this
G"e Consrmable Materials) is adequate
purpose.
NOTE
clean,moistchamois.Rubbingthesurfaceoftheplastic
;it; ; dry cloth builds up an electrostatic charge which
attracts dust particles in the air'
a-27
Revised: March 1983
Section Vlll BEECHCRAFT
Handling, Serv - Maint DebonairC33A
Bonanza E33A
INTERIOR
ENGINE
3t!
dlL
6l
FE-9 c.E
?E iE =CL
9bHo r\
st:!
JJyI
--9b
J' :,
cao
q)
=o c ao
o
o
u.l c o
f
.9
o)c
CD CD
!o
q
ts'-(l) -6
€ o
o c=
UJ
T
.9^ a' cD !
o
E 3!
o
o
laQ
-lt
oJ e
E
;ii $ E
CD
.g
;o
E sE
t oc
o
tr o.g
(9
z <:o €s E ;- o o).E BE
oo
6 9Eg '6' .i
Ypts -.L
e c
c
s9 ou
Ei
ttr t o op
I U.-
3 .9
e8
o
-o
o 6 .E.E
E'
o o IEFEI3
clo-o o
!,
f,
c
:
ji
-c-c
oo
cto
o
UI
:ldl trt F
o
zlu
gL
B o)
co
og
o Eo
E Ep : o
C uO
.9 '6.9
o
=
o
ul
E =
lt.l
E
:s E
g=B* ;
#
o
o
o
-o
1
ssE;
= 9 9.9
PE E;
od € c
o
-o
EEfE
6 o'= ia
* c c'6.E
9l
-v
o cZcs
(EaEO=
o 9>91:
SE E*; E
o O (Jo
o o
CE I I
ll, '-C
ooD r(, o
z c\t lJ)
October 1979
8-30
BEECHCRAFT Section Vlll
DebonairC33A Handling, Serv - Maint
Bonanza E33A
st ro,N
.So
ctc
O
6P €cE E
;b
.,E E E
E E -
E
v
o
;E= E E sE E
q) E_J8 3 5- ; E io
[;# sc i
3
6o $ EE
E
B i,-*! BB # ; BE
€ g *.E ;
= ; a eE'rE E
E
B;
or'E I
o
5EE
tEr gc$ isligl ;r:
o-E
EH=
-!? LE
iEE gE5;;€E[Issstss
J (ll
aG
o o
o^ a
IC
I q
^o 8 a
ro !Z
I
c, 'trG
Fb_9
z:: o
< i -= {
oiH"
G4l--o \f*\tat(,, <f{-si
o E':9
lrYE
'z a
c
o
o
]U tr ?
f
o
UJ
.9
6
o
Ss
Eu,
oE
I
o =i E r 6 = - A eP^
o
3: : EE
= g fiEE
=
"=;e
(9
z
5
<:oE
o6- EE
qE: Ef.E E
5E E
* 8E:;
tG J L.=
gEqEEEqEEggiiig
o
G
UJ
-'-
^L
z :!)
a32 october 1979
BEECHCRAFT SectionVlll
DebonairC33A Handling, Seru- Maint
Bonanza E33A
F
{-)
C,' o
o
o.o
(r) N
o
tr
o
-o
!
9s
cc
C(9
CC
55 55 o
o-
o(E
oo (,
6.! (, r(!
}E c
.g.E 6 .E .S
EE o
ee
OG
E
CL
oo
oo
rDo
L
v
tE6
o@
u, tt aDO c -c= th
-cE = cD -cf Eo)
oo x-t E cc C^ (,o
LL
LL -J
E!
oo ;e
s;
3g
s€
ocD
to
9.E
oo
Ett >o
?c oo
OE '; i '=oi
.=!|
CDC
LLA cc cc C(E
:)l ti l) r!J
!r, , o
E
ai gts b-o
HE
o
o
c
EESA ssE
=
toop o;9
.EgE
Es r Se
=. Ic
8E s e e 95 o SBgBo g
;=t r'6 i
P E p HT
h 9s 6tri'
EsSBE gEg-
d' o-c o Q
EEAEE 8ix
c.9 6
>=>o .o >-C
$;HEi b E bo
oa EEEiE
JJ J
96(,
oa
o o at
cr
I - - G
o
8
(v)
8
@
I
(t)
o
cr^
o
GC-.;
rg
8-34 October 1979
BEECHCRAFT Section Vlll
DebonairC33A Handling, Seru - Maint
Bonanza E33A
n9P e
Op-
rlo6
? EE E
F-
E
EE
OE
ao
B
L
E 3s
o
B
B Ei
: R: !
o E
l
B E5 =6
5
B E*
; ;E
H
E
I eE E
E
.o d.
BH
e
E
I
:E :itE; a &
$E 3: s
le tE fi
oa 7 0
od ig:
Ee a5 f;
50 ;+ P
8E 58 tr
E
L JF L L
';L(Jro,
=
Ffi 8g 5E
a
ul
F
o
z
Octobor 1979 8-36
Section Vlll BEECHCRAFT
Handling, Serv - Maint DebonairC33A
Bonanza E33A
LUBRICATION POINTS
A B CDE F G
1 979 a-37
Section Vlll BEECHCRAFT
Handling, Serv - Maint DebonairC33A
Bonanza E334
CABIN DOOR
,6
j.--J"B
\
J
ELEVATOR TAB MECHANISM
RUDDER PEDALS
:
rtuto coNTAlNtr
NOTE : Letters are keyed
refer to items in
to 'l SOUIRT CAN
CONSUMABLE MATERIALS
is
Only the basic number of each Military Specification
included in the Consumable Materials Chart' No attempt
has been made to update the basic number with the letter
suffix that designates the current issues of the various
specifications.
the
It is the responsibility of the operator/user to determine
current revision ol the applicable Military Specilication
prior to usage of lhat item. This determination may be made
by contacting the vendor ol a specific item'
CONSUMABLE MATERIALS
fi:-*oMultiviscositv !
*16. Engine Fuel l OOLL (Blue)
I O. Grease, Aircraft
and lnstrument MIL-G-23827
tl 1. Lubricant. Rubber
Seal Oakite 6 Compound
....wD-40
.
Product of Bray Oil Co.,
1925 North Marianna
Los Angeles, Calif. 9OO32
oo Product of CRC Chemicals, lnc.,
Warminster, Pa. 18974
a.. Product of LPS Research Laboratories, lnc..
2O50 Cotner Ave,
W. Los Angeles, Calif. 90O25
oooo Product of WD-4O Company.
1O61 Cudahy Place,
San Diego, Calif. 9211O
NOTE
LOCATION NUMBER
R431 6
Strobe lights
NOTE
I.ANDING GEAR
POWER PLANT
NOTE
FUEL SYSTEM
INSTRUMENTS
ELECTR]CAL SYSTEM
COMPONENT OVERHAULORREPTACE
MISCELI.ANEOUS
Bonanza E33A
October 1979
8-52
BEECHCRAFT
DebonairC33A
Bonanza E33A
sEcTloN lx
SUPPLEMENTS
NOTE
94 December 1982
BEECHCRAFT Dobonalr/Bonanza
3$833, 3rc33, E33, F33, and G33
(Serlalc CD'388 thru CI)'13(E);
35433A, E3llA, and F3ilA
(Serlale CE-l thru GE-1013);
Bonarua E33C and F33C
(Serlale CJ-l thru CJ'155);
P35, S35, V35, V35TC, V35A, V35A-TC' V35B' and
v35B-TC
(Serlals D"687{ thru t}'10t103);
36 and A36
(Serlals E-l thru E'2061);
and A36TC
(Serlals EA'l thru EA'272 excapt EA'2421
LANDPLANES
GENERAL
FAA Approved
lssued: llarch, 1983
P/N 3&590002-39 1 ol4
NOTE
LIiiITATIONS
PLACARDS
and;
Espnsss sro;l
TURN HANDTE
L rooFF -I
EMERGENCY PROCEDURES
No Change
FAA Approved
lesued: Harch, l$Xl
2ol4 P/N 36-59m02-39
NORTAL PBOCEOURES
No Chanp
PERFORMANCE
No Change
No Change
SYSTEI'S DESCRIPTION
FUEL SYSTEM
FM Approved
tssued: llarch, 1983
P/til3&59m02-39
3 of4
inadvertant selection ol the OFF position' To select OFF,
depress the lock-out stop and rotate the handle to the lull
clockwise position. Depression of the lock-out stop is not
required when moving the handle counterclockwise from
OFF to LEFI MAIN or HIGHT MAIN. When selecling the
LEFT MAIN or RIGHT MAIN fuel tanks, position handle by
sight and by leeting lor detent.
FAA APProved
lssued: ilarch, 19811
SECTION X
SAFETY INFORMATION
TABLE OF CONTENTS
10-1
ilarch,1981
Scctlon X BEECHCBAFT
SrLty !n ormrflon
10-2 March,1901
BEECHCRAFT Soctbnl
Sth,ty lnlormrtbn
llarch,1981 1G3
Sectlon X BEECHCRAFT
Safety lnlormatlon
INTRODUCTION
WARNING
yourself and to
As a pilor, you are responsible to
pilots and their
those who fly with you' to other
ground' to fly
passengers' and ro people on the
wisely and safelY.
Section covers
The following material in this Safety
Here are some
several subiecrs in limited detail'
condensed Do's and Don'ts'
DO'S
briefing' in-flight
Use services available - Weather
weather and Flight Service Station'
DON'TS
Certificates required
Liquor and drugs
Flight plans
he-flight action
Fuel requirements
Flight rules
Maintenance, preventative maintenance'
atterations, inspection, and maintenance records
AIRWORTHINESS DIRECTIVES
ADVISORY INFORMATION
that
NOTAMS (Notices ro Airmen) are documents
that would
have information of a rime-critical nature
affect a pitot's decision to make a flight; for
example, an airport closed, terminal radar
out of
service, enroutenavigarionat aids out of service' etc'
March' 1981
t0-16
BEECHCRAFT S.ctbnX
Stitty lnlormetlon
FLIGHT Pi.ANNING
INSPECTIONS . MAINTENANCE
FLIGHT OPERATIONS
GENERAL
TIJRBULENT WEATHER
point
that he can no longer maintain altitude' At this
he has lost most, if not all, of his safety options'
including perhaps a 180 degree turn to retreat along
the course already traveled' The responsible and
well-informed pilot recognizes the limitations of
weather conditions, his'airplane and its systems
and
MOTINTAIN FLYING
VFR AT NIGHT
altitude
When flying VFR at night, in addition to the
pilots should
appropriare for the direction of flight'
*uin,uin a safe minimum altitude as dictated by
terrain, obstacles such as TV towers ' or
communities in the area flown' This is especially
true in mountainous terrain, where there is
usually
VERTIGO . DISORIENTATION
using the
Under VFR conditions, the visual sense'
horizon as a reference, can override the
illusions'
Under low visibiliry conditions
(night' fog' clouds'
10-35
March, 1981
Sectlon X BEECHCRAFT
Safety lnlormatlon
disorientationandmayfurtherjeopardizetheflight.
Disorientationinlowvisibilityconditionsisnot
limitedtoVFRpilots.AlthoughlFRpilotsare
to gain an
trained to look at their insrruments
for the
artificial visual reference as a replacement
lossofavisualhorizon,theydonotalwaysdoso.
physical condition
This can happen when the pilot's
on his
will not permit him to concentrale in flying
when the pilot is not proficient
instruments.,
instrumentconditionsintheairplaneheisflying;or'
whenthepilor.sworkloadofflyingbyreferenceto
llarch,1981
10-36
BEECHCRAFT Sectlon X
Satety lnlormatlon
Symbol
with
However, sudden engine failures rarely occur
all of the factors listed above, and therefore' the
may be a
actual Vmca under any particular situation
little slower than the red radial on the airspeed
10-41
llarch, t981
Sectlon X BEECHCRAFT
Safety lnformatlon
[!
o
f
b
\
LlJ
c.
f,
U)
a
u,
CE
(L
INDICATED AIRSPE
SPINS
entered by
Pilots are taught that intentional spins are
with the
deliberately inducing a yawing movement
spins
controls as the aircraft is statled' Inadvertent
resutt from the same combination stall
- plus yaw'
That is why it is important to use coordinated
controls and to recover at the first indication
of a
stall when Practicing stalls'
10-51
March, 1981
Sectlon X BEECHCRAFT
Salety lnlormatlon
DESCENT
or twin
tn piston-powered airplanes' whether single
.ngin"r, supercharged or normally aspirated'
it is
nJ""rrury to avoid prolonged descents with (l)
low
power, as f his produces two problems:
which
Excessively coot cylinder head temperatures
(2) excessively
cause premature engine wear' and
(and altitude)
rich mixtures due to idle enrichment
whichcausessootandleaddepositsonthespark
plugs (fouling). The second of these is
the more
respond to
..rtu. consideration; the engine may not
the
the thrortle when it is desired to discontinue
descent.
at or
lf it is necessary ro make a prolonged descent
at least
near idle, as in practicing forced landings'
plugs by
avoid the problem of fouted spark
frequently advancing the throrrle
until the engine
runssmoothly'andmaintainanappropriatemixture
r0-s5
March, 1981
Sectlon X BEECHCRAFT
Salety lnformatlon
water or
When taking off on runways covered with
f reezing slush, the landing
gear should remain
longer than
extended for approximately ten seconds
the
normat, allowing the wheets to spin and dissipate
then be
freezing moisture. The landing gear should
cycled up, then down, wait approximately five
seconds and then retract again'
the entire
Caution must be exercised to insure that
Landing
operarion is performed below Maximum
Gear Operating AirsPeed'
coveredbywarerorslushwhichcausehydroplaning
(aquaplaning), a phenomenon thal renders braking
and steering ineffective because of the lack
of
sufficient surface friction' Snow and ice
covered
GENERAL
FATIGUE
HYPOXIA
HYPERVENTIUTION
ALCOHOL
DRUGS
when
Self-medication or taking medicine in any form
you are flying can be extremely hazardous' Even
simpte home or over-the-counter remedies and drugs
such as aspirin, antihistamines, cold tablets' cough
mixtures. laxatives, tranquilizers, and appetite
judgment and
suppressors, may seriously impair the
coordination needed while flying' The safest rule
is
10-53
March. 1981
Sectlon X BEECHCRAFT
Safety Informatlon
SCUBA DIVING
ADDITIONAL INFORMATION
SPECIAL CONDITIONS
MAINTENANCE
BEECHCRAFT Scc,tlon X
Salcty lnlormatlon
NOTE