#	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.
section_id	phase	criticality	section_title	item_index	item_id	type	tickable	memory_item	indent	text	response	condition	detail
	Knowledge Test	normal	C-152test	0		challenge	yes	no	0	NAME _________________________			
	Knowledge Test	normal	C-152test	1		challenge	yes	no	0	DATE _________			
	Knowledge Test	normal	C-152test	2		challenge	yes	no	0	CFI			
	Knowledge Test	normal	C-152test	3		challenge	yes	no	0	1. Engine Model Number is                  HP          Max RPM			
	Knowledge Test	normal	C-152test	4		challenge	yes	no	0	2. Engine Oil Capacity is			
	Knowledge Test	normal	C-152test	5		challenge	yes	no	0	3. Minimum Fuel Octane is			
	Knowledge Test	normal	C-152test	6		challenge	yes	no	0	4. Maximum Takeoff Weight is			
	Knowledge Test	normal	C-152test	7		challenge	yes	no	0	5. Required Onboard Documents are			
	Knowledge Test	normal	C-152test	8		challenge	yes	no	0	6. Nose Strut Extension is			
	Knowledge Test	normal	C-152test	9		challenge	yes	no	0	7. Maximum Mag. Drop is			
	Knowledge Test	normal	C-152test	10		challenge	yes	no	0	8. Best Rate of Climb Airspeed is			
	Knowledge Test	normal	C-152test	11		challenge	yes	no	0	9. VNE is			
	Knowledge Test	normal	C-152test	12		challenge	yes	no	0	10. Clean Stall Speed is			
	Knowledge Test	normal	C-152test	13		challenge	yes	no	0	11. Minimum Oil Pressure is			
	Knowledge Test	normal	C-152test	14		challenge	yes	no	0	12. Total Usable Fuel is			
	Knowledge Test	normal	C-152test	15		challenge	yes	no	0	13. Maximum Demonstrated Crosswind is			
	Knowledge Test	normal	C-152test	16		challenge	yes	no	0	14. Engine Restart Procedures are			
	Knowledge Test	normal	C-152test	17		challenge	yes	no	0	15. Power off Emergency Glide Speed is			
	Knowledge Test	normal	C-152test	18		challenge	yes	no	0	16. Stall Recovery Procedure is			
	Knowledge Test	normal	C-152test	19		challenge	yes	no	0	17. In the Emergency Landing Pattern, Downwind Alt is			
	Knowledge Test	normal	C-152test	20		challenge	yes	no	0	18. The Basic Steps in an Engine Failure Situation are (List 5):			
	Knowledge Test	normal	C-152test	21		challenge	yes	no	1	   1.			
	Knowledge Test	normal	C-152test	22		challenge	yes	no	1	   2.			
	Knowledge Test	normal	C-152test	23		challenge	yes	no	1	   3.			
	Knowledge Test	normal	C-152test	24		challenge	yes	no	1	   4.			
	Knowledge Test	normal	C-152test	25		challenge	yes	no	1	   5.			
	Knowledge Test	normal	C-152test	26		challenge	yes	no	0	19. The First Step in an Engine Fire Emergency is			
	Knowledge Test	normal	C-152test	27		challenge	yes	no	0	20. How is an Alternator Failure Detected			
	Knowledge Test	normal	C-152test	28		challenge	yes	no	0	21. What are Alternator Failure Corrective Steps			
	Knowledge Test	normal	C-152test	29		challenge	yes	no	0	22. Most Probable Causes for Engine Roughness is			
	Knowledge Test	normal	C-152test	30		challenge	yes	no	0	23. How is the Engine Primed			
	Knowledge Test	normal	C-152test	31		challenge	yes	no	0	24. Maximum Starter Cranking Period is			
	Knowledge Test	normal	C-152test	32		challenge	yes	no	0	25. Recommend Final Approach Airspeed with Flaps Full is			
	Knowledge Test	normal	C-152test	33		challenge	yes	no	0	26. What is the Rate of Climb at 1670 lbs, 15 C, @ Sea Level			
	Knowledge Test	normal	C-152test	34		challenge	yes	no	0	27. What is the Takeoff Distance 1670 lbs, 20 C, @ Sea Level, no wind component			
	Knowledge Test	normal	C-152test	35		challenge	yes	no	0	28. At 75% Power, RPM is:  _____________  and GPH is approx.: _______________			
	Knowledge Test	normal	C-152test	36		challenge	yes	no	0	29. If OAT is 10 deg C, PA 3000 TAS is: ________________________			
	Knowledge Test	normal	C-152test	37		challenge	yes	no	0	30. Determine if the Aircraft is within weight and CG limits.			
	Knowledge Test	normal	C-152test	38		challenge	yes	no	1	Basic Aircraft Weight 1155.9 lbs. @ 29.93”			
	Knowledge Test	normal	C-152test	39		challenge	yes	no	1	Pilot and Front Pax 340.0 lbs. @ 39.0”			
	Knowledge Test	normal	C-152test	40		challenge	yes	no	1	Fuel 24.5 gal @ 6 lbs./gal 147.0 lbs. @ 42.0”			
	Knowledge Test	normal	C-152test	41		challenge	yes	no	1	Baggage 20.0 lbs. @ 64.0”			
	Knowledge Test	normal	C-152test	42		challenge	yes	no	0	31. Determine the takeoff distance over a 50’ obstacle and liftoff airspeed.			
	Knowledge Test	normal	C-152test	43		challenge	yes	no	1	Given: Pressure Alt: 3500 MSL, AOT 25 C, 1670lb. Gross Weight, 5 Knt. headwind.			
	Knowledge Test	normal	C-152test	44		challenge	yes	no	0	32. Determine fuel burn, time and distance to climb.			
	Knowledge Test	normal	C-152test	45		challenge	yes	no	1	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.			
	Knowledge Test	normal	C-152test	46		challenge	yes	no	0	33. Determine landing distance and approach airspeed over a 50’ obstacle.			
	Knowledge Test	normal	C-152test	47		challenge	yes	no	1	Given: Destination pressure altitude 525’ MSL, OAT 18’ C, landing weight 1580 lbs.,0 wind.