Text in force at CAR3R-8: from CAR3R-2, effective 12 Aug 1957. OCR text
NOTE: For a seaplane version of a landplane, it is normally acceptable to use the wing loading of the landplane in determining the limit maneuvering control surface loadings from Figure 3-3(b) provided: the power of the engines and the placard maneuver speed of the seaplane do not exceed those established for the landplane; the maximm certificated weight of the seaplane does not exceed the corresponding weight of the landplane by more than 10 percent; and service experience with the landplane is such that no evidence of any serious control-surface load problems is indicated and is such that the service experience is of sufficient scope to deduce with reasonable accuracy that no serious control-surface load problems will develop on the seaplane. 6. By adding a new heading and a new § 3,270 to read as follows: FATIGJE EVALUATION
secs. 601, 603, 52 Stat. 1007, 1009, as amended; 49 U.S.C. 551, 553) . By the Civil Aeronautics Boards /e/ H.C, Mulligan (SEAL) M,C. Mulligan Fart 3 last printed May 15, 1956. Secretary ·