Cessna 152 — C-152test
NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full
Source: Cessna/152/C-152test.txt
Rights: licensed
Checklist hash: 243f12b9c90cc75f2f3479293aa9dff28a2ce882ce75c2edec8a0824c8821c1c
Verify against the aircraft's own approved documentation before use.
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C-152TEST
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[ ] NAME _________________________
[ ] DATE _________
[ ] CFI
[ ] 1. Engine Model Number is                  HP          Max RPM
[ ] 2. Engine Oil Capacity is
[ ] 3. Minimum Fuel Octane is
[ ] 4. Maximum Takeoff Weight is
[ ] 5. Required Onboard Documents are
[ ] 6. Nose Strut Extension is
[ ] 7. Maximum Mag. Drop is
[ ] 8. Best Rate of Climb Airspeed is
[ ] 9. VNE is
[ ] 10. Clean Stall Speed is
[ ] 11. Minimum Oil Pressure is
[ ] 12. Total Usable Fuel is
[ ] 13. Maximum Demonstrated Crosswind is
[ ] 14. Engine Restart Procedures are
[ ] 15. Power off Emergency Glide Speed is
[ ] 16. Stall Recovery Procedure is
[ ] 17. In the Emergency Landing Pattern, Downwind Alt is
[ ] 18. The Basic Steps in an Engine Failure Situation are (List 5):
  [ ]    1.
  [ ]    2.
  [ ]    3.
  [ ]    4.
  [ ]    5.
[ ] 19. The First Step in an Engine Fire Emergency is
[ ] 20. How is an Alternator Failure Detected
[ ] 21. What are Alternator Failure Corrective Steps
[ ] 22. Most Probable Causes for Engine Roughness is
[ ] 23. How is the Engine Primed
[ ] 24. Maximum Starter Cranking Period is
[ ] 25. Recommend Final Approach Airspeed with Flaps Full is
[ ] 26. What is the Rate of Climb at 1670 lbs, 15 C, @ Sea Level
[ ] 27. What is the Takeoff Distance 1670 lbs, 20 C, @ Sea Level, no wind component
[ ] 28. At 75% Power, RPM is:  _____________  and GPH is approx.: _______________
[ ] 29. If OAT is 10 deg C, PA 3000 TAS is: ________________________
[ ] 30. Determine if the Aircraft is within weight and CG limits.
  [ ] Basic Aircraft Weight 1155.9 lbs. @ 29.93”
  [ ] Pilot and Front Pax 340.0 lbs. @ 39.0”
  [ ] Fuel 24.5 gal @ 6 lbs./gal 147.0 lbs. @ 42.0”
  [ ] Baggage 20.0 lbs. @ 64.0”
[ ] 31. Determine the takeoff distance over a 50’ obstacle and liftoff airspeed.
  [ ] Given: Pressure Alt: 3500 MSL, AOT 25 C, 1670lb. Gross Weight, 5 Knt. headwind.
[ ] 32. Determine fuel burn, time and distance to climb.
  [ ] Given: Max gross weight, climb speed 67 KIAS, 0 wind, takeoff pressure altitude 1500’ MSL, OAT 25 C, cruise pressure altitude 7500’ MSL, cruise OAT 8 C.
[ ] 33. Determine landing distance and approach airspeed over a 50’ obstacle.
  [ ] Given: Destination pressure altitude 525’ MSL, OAT 18’ C, landing weight 1580 lbs.,0 wind.