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Piper PA-28-140 — PA28-140 test

Piper PA-28-140 · standard normal

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Aircraft Pilot

Student and Instructor Information reference

Name: _________________________
Date: ________________
Instructor: ______________________ Grade: ____________________
NOTEUse Piper Cherokee 140B manual. However, the information in that manual does not provide all of the information necessary to safely fly the airplane. Therefore, this test will include questions from the Piper manual as well as the club's "Conditions of Flight" (COF) statement and the Club checklist which includes: "Normal/Abnormal/Emergency Procedures". These statements are downloadable from the website and are in binder located in the flight planning room.

Engine reference

2. Engine Model Number is: __ HP ____ Max RPM ____
3. Engine Oil Capacity is: ______

Landing Gear reference

4. Normal strut extension is ______ for nose gear and _____ for the main gear.
5. The toe brakes and the hand brake use their own ________ but have a common _________.

Fuel reference

6. Fuel capacity standard _________________ Reserve _________________
7. To obtain the standard fuel quantity, the pilot should fill the tanks to: __________________________________________________________
8. Minimum Fuel Octane is: ______________________________________
9. The electric fuel pump should be on when: ________________________

Control System reference

10. The flap may be used as a step only when _______________________________

Electrical reference

11. The electrical system includes a ________ volt _______ ampere alternator.
12. The ammeter displays the ______________________________________.
13. The maximum continuous load for night flight is with radios is _____________.

Engine Start before_start

14. As soon as the engine is started, checked oil pressure, if there is no rise within _______ sec shut down.

Weight and Balance weight_and_balance

15. What is maximum gross weight? ________________ Empty weight? _______________________
16. Arithmetically Compute the weight and balance for the following conditions:
Basic Aircraft Weight: WEIGHT 1464.0 lbs., Arm 87.8 in., Moment ____________ in./Lbs.
Pilot and Front Pax: WEIGHT 360.0 lbs., Arm 85.5 in., Moment ____________ in./Lbs.
Fuel 50 gal @ 6 lbs./gal: WEIGHT 300.0 lbs., Arm 95.0 in., Moment __________ in./Lbs.
Baggage: WEIGHT 25.0 lbs., Arm 117.0 in., Moment ____________ in./Lbs.
Totals: ________ lbs., Moment __________ in./Lbs.
CG = _____________ in./Lbs. = ______ in. Aircraft is within/not within both limitations. __________ Lbs.

Performance performance

17. What is the Density altitude at a pressure altitude of 8000 feet with a temperature of 15 C? __________________________________
18. At a DA of 4000', what is our rate of climb? __________________________________
19. What is our takeoff distance over a 50' obstacle at a density altitude of 4,000' (2150 lbs)? __________________
NOTE20. For a cross-country flight, you plan to cruise at 5500'. The temperature at 5500 feet is 24C and you plan to use 70% power. Winds at 5500' are 360 at 20 kts and your course is 075. (use the charts in your book and an E6-B "Whiz wheel").
What will be your true airspeed? __________
What is your groundspeed? ______________
Heading? _______________________
Indicated airspeed? _______________
NOTEQuestions 20-25 are closed book questions and come from "Normal/Abnormal/Emergency Procedures Statement". You should practice these questions, but they must be proctored without reference to any material.

21. Engine Failure Immediately After Takeoff 21. Engine Failure Immediately After Takeoff

1. ___________________
2. ___________________
3. ___________________
4. ___________________
5. ___________________

22. Loss of Fuel Pressure fuel_system_malfunction

1. ___________________
2. ___________________

23. Engine Fire on Ground engine_fire_ground

1. ____________________
2. ____________________
3. ____________________
4. ____________________
5. ____________________

24. Engine Fire in Flight engine_fire_in_flight

1. ___________________
2. ___________________
3. ___________________
4. ___________________

25. Electrical Fire electrical_fire

1. ___________________

Source: Piper/PA-28-140/PA28-140 test.txt

Rights: licensed

Checklist hash: c258be096f68c257e8a0b9fbc8b5f32f…

Generated from piper-pa-28-140-pa28-140-test.ocl.json by the Open Checklists reference renderer. Verify against the aircraft's own approved documentation before use.

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