Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text
The limit load factor in a lateral direction for this condition shall be at least equal to one-third of the limit load factor for flight condition A (see Fig. 3-1) except that it shall not be less than 1.33. Engine mounts and their supporting structure shall be designed for this condition which may be assumed independent of other flight conditions. CONTROL SURFACE LOADS