Text in force at CAR3-14: from CAR3-14, effective 7 Feb 1956. OCR text
[(a) The positive limit maneuvering load factors shall not be less than the following values: nel + KLEv... STS WAS where: Ko» YO WeS1 (for WS <. 16 p.s.ti = 133 - 267 ifor WS > lh p.s.tj iWsjs except that n need not be greater than 3.8 and shall not be less than 2.5.] n = 4.4--------------------------------Category U n = 6.0--------------------------------Category A (b) The negative limit maneuvering load factors shall not be less than -0.4 times the positive load factor for the N and U categories, and shall not be less than -0.5 times the positive load factor for the A category. (c) Lower values of maneuvering load factor may be employed only if it be proven that the airplane embodies features of design which make it impossible to exceed such values in flight. (See also § 3.106.)
secs. 601, 603, 52 Stat. 1007, 1009, as amended, 49 U.S.C. 551, 553) By the Civil Aeronautics Board: /s/ M. C. Mulligan M. C. Mulligan Secretary (SEAL) Part 3 last printed November 1, 1949 ·