C182RG

References: 1978 Operating handbook C182RG

1. The recommended enroute climb for this aircraft is 90 to 100 KIAS and:

a. 25 inches Hg and 2500 RPM
b. 23 inches Hg and 2500 RPM
c. 23 inches Hg and 2400 RPM
d. 24 inches Hg and 2400 RPM

2. The minimum octane fuel and usable gallons for this aircraft are:

a. 100LL octane and 56 gallons
b. 100LL octane and 75 gallons
c. 80 octane and 56 gallons
d. 100 octane and 56 gallons

3. The Lycoming engine is rated at _____ horsepower.

a. 250
b. 235
c. 220
d. 200

4. Percent of maximum brake horsepower:

a. above 75%
b. 65-75%
c. 55-65%
d. less than 55%

5. Manifold pressure (inches of mercury):

a. 22 in Hg
b. 23 in Hg
c. 25 in Hg
d. full throttle

6. RPM:

a. 2400
b. 2500
c. 2300
d. 2100

7. True Airspeed:

a. 164 KTAS
b. 152 KTAS
c. 155 KTAS
d. 154 KTAS

8. Total fuel consumption:

a. 13.9 GPH
b. 12.6 GPH
c. 13.6 GPH
d. 13.3 GPH

9. Endurance (allowing 45 min fuel reserve at 75% power on landing and fuel for takeoff, taxi, and climb from 2000 ft pressure altitude to cruise altitude):

a. 2.8 Hours
b. 4.2 Hours
c. 4.9 Hours
d. 5.2 Hours

10. The 30 degree bank, power off, 40 degree flaps down stalling speed is (most forward center of gravity):

a. 42 KIAS/55 KCAS
b. 40 KIAS/56 KCAS
c. 45 KIAS/59 KCAS
d. 38 KIAS/54 KCAS

11. What happens to the stalling speed as bank angle increases:

a. always the same
b. depends on altitude
c. decreases
d. increases

12. The gross weight, sea level, best rate of climb (Vy) and best angle of climb (Vx) airspeeds are:

a. 88 KIAS/64 KIAS
b. 72 KIAS/50 KIAS
c. 80 KIAS/63 KIAS
d. 90 KIAS/60 KIAS

13. What is the normal approach speed with flaps down:

a. 70-80 KIAS
b. 65-70 KIAS
c. 65-75 KIAS
d. 60-70 KIAS

14. What is the minimum recommended short field approach speed with full flaps:

a. 70 KIAS
b. 65 KIAS
c. 63 KIAS
d. 75 KIAS

15. What is the maximum airspeed for gear extension (VLE) or operation (VLO):

a. 137 KIAS
b. 140 KIAS
c. 155 KIAS
d. 125 KIAS

16. What are the maximum airspeeds for 10 degrees and 10 degrees to 40 degrees flap extension:

a. 137 KIAS and 94 KIAS
b. 182 KIAS and 175 KIAS
c. 140 KIAS and 95 KIAS
d. 150 KIAS and 100 KIAS

17. What is the maneuvering speed (Va) for maximum gross weight and 2000 pounds gross weight:

a. 140 KIAS and 95 KIAS
b. 112 KIAS and 101 KIAS
c. 112 KIAS and 89 KIAS
d. 111 KIAS and 100 KIAS

The airport elevation is 7000 MSL, 9 knot headwind, 86F, and the aircraft is at maximum gross weight:

18. What is the takeoff distance to clear a 50ft obstacle:

a. 1730 ft
b. 3140 ft
c. 3425 ft
d. 3805 ft

19. What is the landing distance to clear a 50ft obstacle:

a. 820 ft
b. 1675 ft
c. 1508 ft
d. 1770 ft

20. What is the normal gear down and locked indication (in addition to observing the main gear by looking out the side windows):

a. three green lights
b. one green light
c. one amber light
d. one red light

21. What is the weight, moment, and is the loading acceptable for the following aircraft load:

Fuel - Half
Oil - Full
Pilot - 220lb
Copilot - 180lb
Passenger - 190lb
Passenger - 170lb
Baggage - 120lb in area "A".

a. 2948.8, 128.7, yes
b. 3948.8, 130.8, yes
c. 2948.8, 128.7, no
d. 3948.8, 130.8. no

22. If the flaps are extended beyond 25 degrees with the landing gear up:

a. A warning horn sounds
b. The gear automatically extends
c. Flap extension past 25 degrees is mechanically inhibited with the gear up.
d. Nothing will happen.

23. Maximum demonstrated crosswind velocity is:

a. 15 knots
b. 17 knots
c. 18 knots
d. 20 knots

24. Suggested flap setting and climb out speed for a short field takeoff is:

a. 10 deg. flaps and 55 kias
b. 10 deg. flaps and 63 kias
c. 20 deg. flaps and 55 kias
d. 20 deg. flaps and 63 kias

25. Redline speed (Vne) is:

a. 193 kias
b. 182 kias
c. 190 kias
d. 192 kias

26. Loss of oil pressure will cause the constant speed propeller to revert to:

a. low pitch, low RPM
b. low pitch, high RPM
c. high pitch, low RPM
d. high pitch, high RPM

27. A small increase in RPM can be obtained by:

a. Rotating the propeller control knob clockwise.
b. Rotating the propeller control knob counter-clockwise.
c. Pushing the propeller control in 1/2" to 1".
d. Rotating the throttle control Knob clockwise.

28. The propeller maintains a constant speed by means of:

a. Oil pressure and centrifugal force.
b. Oil pressure only.
c. Centrifugal force and an internal spring.
d. An internal spring only.

29. The landing gear emergency hand-pump is located:

a. on the lower left instrument panel
b. on the lower center instrument panel
c. on the floor between the front seats
d. on the floor under the pilot's seat

30. The fuel vents are located:

a. in the filler caps only.
b. the left fuel take only.
c. the right fuel tank and both filler caps.
d. the left fuel tank and both filler caps.

31. If the landing gear fails to extend, the emergency procedure calls for the gear lever to be down, extend the emergency hand pump and pump until resistance becomes heavy, about _____ cycles, then observe the green light and stow the handle:

a. 30
b. 20
c. 10
d. 50

32. In the event of vacuum failure during operations in cloudy conditions the _____ should be used in lieu of the artificial horizon and directional gyro:

a. turn coordinator
b. airspeed indicator
c. clock
d. vacuum gauge

33. Flight in icing conditions is:

a. Prohibited
b. Allowed in light icing.
c. Allowed in light icing with pitot heat and carb heat ON.
d. Allowed if you are on an IFR flight plan.