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20.  The recommended climb airspeed on single engine after take-off after immediate obstacles have been cleared is:
[[circled]] a. [[/circled]] 100 to 110 MPH.
b. 102 to 108 MPH.
c. 120 MPH.

21.  The approximate stalling speed in indicated MPH with flaps up, gross weight of 26,000 lbs. in a 45° bank is:
a. 92 MPH.
b. 80 MPH. 
[[circled]] c. [[/circled]] 88 MPH.

22.  For the C-47 aircraft, minimum control speed in flight is ^[[88 mph.]]

23.  Maximum allowable airspeed at gross weight of 26,000 pounds is:
a. 270 MPH.
[[circled]] b. [[/circled]] 255 MPH.
c. Not affected by gross weight.

24.  Recommended rough air penetration airspeed for the C-47 is:
a. 140 MPH.
b. 30% above stall speed
[[circled]] c. [[/circled]] 60 MPH above stalling speed for its gross weight.

[[underlined]] LANDING GEAR OPERATION [[/underlined]]

25.  After retracting the landing gear, placing the landing gear control handle to NEUTRAL will automatically return the safety latch control to the ^[[spring lock]] position.

26.  Maximum indicated airspeed for extending landing gear is ^[[160]] MPH.

27.  The correct procedure for extending the landing gear is:
[[circled]] a. [[/circled]] Gear down;  gear pressure 850 PSI;  gear handle neutral;  check for green light;  safety latch positive lock.
b. Gear down;  safety latch positive lock;  gear pressure 850 PSI;  gear handle neutral;  check for green light.
c. Gear down;  gear pressure 850 PSI;  gear handle neutral.

28.  Maximum indicated airspeed with the wing flaps full down is ^[[112]] MPH.

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