Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. 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 conditicz= ConTROL SurFace LOADS