Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
Flight load requirements shall be complied with at critical altitudes within the range in which the airplane may be expected to operate and at all weights between the minimum design weight and the maximum design weight, with any practicable distribution of disposable load within prescribed operating limitations stated in §§ 3.777-3.780.