| United States. Department of State - 1945 - 298 էջ
...specific control surface loading conditions. Resultant moments about the center of gravity of the airplane shall be reacted in a rational or conservative manner...principal masses furnishing the reacting inertia forces. For conventional control surface and structural arrangements, the specified loading conditions for... | |
| International Civil Aviation Conference - 1945 - 326 էջ
...specific control surface loading conditions. Resultant moments about the center of gravity of the airplane shall be reacted in a rational or conservative manner...principal masses furnishing the reacting inertia forces. For conventional control surface and structural arrangements, the specified loading conditions for... | |
| 2001 - 1142 էջ
...(a) and (b) §25.361 of this section. Unbalanced aerodynamic moments about the center of gravity mast be reacted in a rational or conservative manner, considering...masses furnishing the reacting inertia forces. (a) Maneuvering. The following conditions, speeds, and aileron deflections (except as the deflections may... | |
| 2000 - 1128 էջ
...conditions of §§23.349 and 23.351. Unbalanced aerodynamic moments about the center of gravity must be reacted in a rational or conservative manner, considering...principal masses furnishing the reacting inertia forces. (b) Acrobatic category airplanes certified for flick maneuvers (snap roll) must be designed for additional... | |
| 1965 - 1938 էջ
...paragraph (b) of this section, with — (1) Unbalanced aerodynamic moments about the center of gravity reacted in a rational or conservative manner considering...principal masses furnishing the reacting inertia forces ; (2) Maximum main rotor speed; and (3) Forward speeds up to VKE or Vn, whichever is less. (b) In unaccelerated... | |
| 1977 - 788 էջ
...paragraphs (a) and (b) of this section. Unbalanced aerodynamic moments about the center of gravity must be reacted In a rational or conservative manner, considering...the principal masses furnishing the reacting Inertia forcee. (a) Maneuvering. The following conditions, speeds, and aileron deflections (except as the deflections... | |
| 2001 - 1132 էջ
...with — (1) Unbalanced aerodynamic moments about the center of gravity which the aircraft reacts to in a rational or conservative manner considering the...principal masses furnishing the reacting inertia forces; and (2) Maximum main rotor speed. (b) To produce the load required in paragraph (a) of this section,... | |
| 1999 - 1064 էջ
...with — (1) Unbalanced aerodynamic moments about the center of gravity which the aircraft reacts to in a rational or conservative manner considering the...principal masses furnishing the reacting inertia forces; and (2) Maximum main rotor speed. (b) To produce the load required in paragraph (a) of this section,... | |
| 1997 - 1042 էջ
...paragraphs (a) and (b) of this section. Unbalanced aerodynamic moments about the center of gravity must be reacted in a rational or conservative manner, considering the principal masses furnishing the reaching inertia fores. (a) Maneuvering. The following conditions, speeds, and aileron deflections... | |
| 1964 - 1108 էջ
...treat the fa going conditions as two separate cal or he may combine them if he so desi [Supp. 10, 16 FB 3285, Apr. 14, 1951] TTNSYMMETRICAL FLIGHT CONDITIONS...from the aileron deflections and speeds specified in 5 3.222, in combination with an airplane load factor of at least two-thirds of the positive maneuvering... | |
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