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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. 3