24 CAPR 60-1 ATTACHMENT 3 10 JUNE 2004
ATTACHMENT 3 – AIRPLANE QUESTIONNAIRE
AIRPLANE QUESTIONNAIRE
Name _______Shlomo Zelkine___ Grade _1LT__ CAPID: _103728__ Unit NER-NY-379 Date _DEC-11-2004 __
Check Pilot__ Roland Zavada___ Grade _LTC__ CAPID: _XXXXX Score100%Type/Model Acft C 172N
(N8268E)
Complete this open book questionnaire using the Flight Manual/Pilot's Operating Handbook. If a question or part
of a question is not applicable, write in NA. The check pilot will review and grade the questionnaire. Minimum
passing score is 80%. The completed questionnaire will be filed in the pilot's flight records.
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Approved fuel grades and colors are:100LL blue_____________________________________________
Location/capacity of each fuel tank is:Wing, 54 USG each side.__________________________________
Total usable fuel under all flight conditions is _50__ gallons.
Endurance at 75% power, 7,500-foot MSL, with a 45-minute reserve is __ 5.3 hours.
What make and grade oil is used? Winter _SAE 30 Summer__50___
Oil capacity is __8___ quarts. Minimum oil quantity for takeoff is ___4___ quarts.
Minimum oil pressure is __25___ psi. Maximum oil pressure is __100__ psi.
Maximum oil temperature is __245__ degrees (F or C) ___F___
Magnetos are checked at __1700_ RPM. RPM drop should not exceed _125___ RPM on
either magneto or __50___ RPM differential between magnetos.
Maximum RPM and MP for takeoff are _2700__ and ___X___ in/Hg.
Maximum gross takeoff weight is _2300__ pounds. Empty weight is _1379__ pounds.
Useful load is _921__ pounds. Maximum landing weight is _2300__ pounds.
Baggage compartment locations/weights are: ____Rear, 125 LB.__________________________________
Give the IAS at maximum gross weight for:
a. Va (maneuvering speed)
__97___
b. Vso (stall, landing config, power off)
__47___
c. Vs1 (stall, cruise config, power off)
__53___
d. Vy (best rate of climb, sea level)
__73___
e. Vx (best angle of climb, sea level)
__59___
f. Vmc (minimum control speed - multi-engine only) __XX__
g. Best glide speed
___65__
Give the immediate action/memory items for:
a. Engine failure immediately after takeoff: _65 Kts, Mix. Off, Mags off, Master off, Flaps up.____________
b. Fire during cranking and engine fails to start: Continue cranking, Throttle open,_Mix._off.___________
c. Engine fire in flight:_ Mix._off, Fuel off, Master off, Heat off, Use fire Extinguisher._______________
d. Electrical fire in flight: Master off, Radio off, Eliminate smoke and fume, Use fire Extinguisher.______
Normal takeoff flap setting is __0_, short field takeoff setting is __10_, and soft field takeoff flap setting
is _10__.
Maximum demonstrated takeoff/landing crosswind component is __15_ knots.
Given: PA = 4,000 feet; Temp = 86o F; Runway 27; Wind 320o at 14 knots; runway is paved, level, and dry;
aircraft is at maximum takeoff weight.
Find: Total takeoff distance to clear a 50-foot obstacle __2550_ ft _.
Given: PA = 6,000 feet; Temp = 68o F; wind calm; runway is paved, level, and dry; aircraft is at maximum
landing weight.
Find: Total landing distance to clear a 50-foot obstacle __1490_ft__.
Landing runway 22; wind 190o at 22 gusting to 30 knots. Will the maximum demonstrated crosswind
component for this aircraft be exceeded? __No_