Cessna 152 — C-152test
Cessna 152 · standard normal
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NOT REVIEWED — nobody has checked this against a source document · never used in an aircraft
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C-152test Knowledge Test
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.