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    PA28-200 Arrow Performance

    Uploaded by

    Michael Linn
    This document provides performance charts and specifications for the Piper PA28R-200 Arrow aircraft. It includes information on operating speeds, takeoff and landing performance, range and endurance calculations, maneuver specifications, aircraft systems notes on fuel, engine, electrical, landing gear, and stall warning systems. Maximum demonstrated crosswind component is 15 knots.

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    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd

    PA28-200 Arrow Performance

    Uploaded by

    Michael Linn
    115 views4 pages
    This document provides performance charts and specifications for the Piper PA28R-200 Arrow aircraft. It includes information on operating speeds, takeoff and landing performance, range and endurance calculations, maneuver specifications, aircraft systems notes on fuel, engine, electrical, landing gear, and stall warning systems. Maximum demonstrated crosswind component is 15 knots.

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    PA28-200 Arrow Performance

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    This document provides performance charts and specifications for the Piper PA28R-200 Arrow aircraft. It includes information on operating speeds, takeoff and landing performance, range and endurance calculations, maneuver specifications, aircraft systems notes on fuel, engine, electrical, landing gear, and stall warning systems. Maximum demonstrated crosswind component is 15 knots.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    115 views4 pages

    PA28-200 Arrow Performance

    Uploaded by

    Michael Linn
    This document provides performance charts and specifications for the Piper PA28R-200 Arrow aircraft. It includes information on operating speeds, takeoff and landing performance, range and endurance calculations, maneuver specifications, aircraft systems notes on fuel, engine, electrical, landing gear, and stall warning systems. Maximum demonstrated crosswind component is 15 knots.

    Copyright:

    © All Rights Reserved
    Download as PDF, TXT or read online from Scribd
    Download as pdf or txt
    of 4

    PA28R-200 Arrow

    Rev: Oct 2006 P-1


    PERFORMANCE CHARTS
    PIPER ARROW OPERATING SPEEDS (mph) IAS
    SO LE NO
    V 64 V 150 V 170 *Gear Dwn/Up
    S1 LO NE
    V 71 V 125 V 214
    X FE
    V 85/96* V 125
    Y A
    V 95/100* V 131
    TAKEOFF CROSSWIND LIMIT - 15 KTS
    Rotate Climb* Flaps
    Normal 65 95/100 Up
    Short Field 65 85/96 25E
    Soft Field ASAP 95/100 25E
    ENROUTE @ 2500' PA (STANDARD TEMP)
    POWER IAS (mph) FF (gph)
    Climb 25"/2500 110 14
    Cruise (75% BPH) 25"/2400 151 10.2
    Cruise (55% BPH) 22"/2100 129 8
    Holding 17"/2100 105 6.5
    PA28R-200 Arrow
    Rev: Oct 2006 P-2
    PATTERNS/LANDINGS CROSSWIND LIMIT 15 KTS
    Power IAS (mph) Flaps
    Downwind 18"/2400 120
    Abeam Touchdown 15"/FP** 110 10E
    Base 100 25E
    Normal Final 90 40E
    Short Field Final 83 40E
    Soft Field Final 83 40E
    No Flap Final 95 40E
    Inst Approach 17"/2400 105 0E
    ILS Final (3E/480 fpm) 17"/FP** 105 0E
    **Full prop after reducing manifold pressure
    MAX RANGE GLIDE WITH ENGINE OUT & PROP AT LOW RPM
    Flaps & Gear Up 105 MIAS 1.3 NM / 1000'
    PERFORMANCE @ MAX GROSS WT (2650#)
    Density Altitude Ceilings T/O & Ldg (SL, 95E, No Wind)
    Absolute 17000 Acc to 65 mph & Stop 1810'
    Service 15000 Short Field T/O 1000' / 2150'
    Short Field Landing 810' / 1400'
    PA28R-200 Arrow
    Rev: Oct 2006 P-3
    MANEUVERS
    Power Entry IAS (mph) Altitude
    Chandelle 25"/2500 125 >1500' AGL
    Lazy 8 18"/2400 120 >1500' AGL
    Steep
    Turns
    18"/2400 120 >1500' AGL
    AIRCRAFT SYSTEM NOTES
    FUEL 48 gal usable: Tab in filler neck indicates
    17 gal usable per tank.
    Tanks are vented individually through a
    tube at the rear outboard corner of each
    tank.
    Start/Taxi/Takeoff Fuel approximately 1.5
    gal.
    ENGINE Lycoming IO-360-C1C; 200 BHP @2700
    RPM
    Fuel injected
    ELECTRICAL 12 Volt DC; one 60 amp alternator
    Ammeter shows electrical load on system
    not rate of battery discharge.
    LDG GEAR Nose gear 30 psi; Main gear 27 psi
    Engage parking brake by pulling back on
    lever and depressing knob. Disengage y
    pulling back on lever and releasing.
    STALL
    WARNING
    Warning light comes on 5 10 mph above
    stall.
    PA28R-200 Arrow
    Rev: Oct 2006 P-4
    INTENTIONALLY LEFT BLANK

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