Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text
The airplane shall be satisfactorily controllable and maneuverable during takeoff, climb, level flight, drive, and landing with or without power. It shall be possible to make a smooth transition from one flight condition to another, including turns and slips, without requiring an exceptional degree of skill, alertness, or strength on the part of the pilot, and without danger of exceeding the limit load factor under all conditions of operation probable for the type, including for multiengine airplanes those conditions normally encountered in the event of sudden failure of any engine. Compliance with "strength of pilots" limits need not be demonstrated by quantitative tests unless the Administrator finds the condition to be marginal. In the latter case they shall not exceed maximum values found by the Administrator to be appropriate for the type but in no case shall they exceed the following limits: Pitch Roll Yaw (a) For temporary application: Stick 60 30 150 Wheel 1 75 60 150 (b) For prolonged application. 10 5 20 1Applied to rim.