 | 1939
...of the pilot to prevent a change of heading in excess of 20° before recovery is complete. § 03.132 Trim. The means used for trimming the airplane shall...airplane will maintain : (a) Lateral and directional trim in level flight at a speed of 0.9 V* or at Vc, if lower, with the landing gear and wing flaps retracted;... | |
 | International Civil Aviation Conference - 1945 - 284 էջ
...not exceed 180 1bs. (81.5 kg.), nor shall it be necessary to throttle the remaining engines. 2.132 Trim. The means used for trimming the airplane shall...airplane will maintain: (a) Lateral and directional trim in level flight at a speed equal to 90 percent of the high speed, Vh. (b) Longitudinal trim under the... | |
 | United States. Department of State - 1945
...not exceed 180 Ibs. (81.5 kg.), nor shall it be necessary to throttle the remaining engines. 2.132 Trim. The means used for trimming the airplane shall...airplane will maintain: (a) Lateral and directional trim in level flight at a speed equal to 90 percent of the high speed, Vh. (b) Longitudinal trim under the... | |
 | 1977
...degrees. Txm g 25.161 Trim. (a) General. Each airplane must meet the trim requirements of this section after being trimmed, and without further pressure upon, or movement of, either the primary controls or their corresponding trim controls by the pilot or the automatic pilot. (b) Lateral and... | |
 | 1994
...1980] TRIM .3161 Trim. (a) General. Each airplane must meet the trim requirements of this section tfter being trimmed, and without further pressure upon, or movement of, either the primary controls or their corresponding trim controls by the pilot or the automatic pilot. (b) Lateral and... | |
 | United States. Flight Standards Service - 1962 - 139 էջ
...and without danger of exceeding the limit load factor. Trim. — The means used for trimming should be such that after being trimmed and without further...primary control or its corresponding trim control, the glider will maintain (1) lateral and directional trim in unaccelerated forward flight at the speed... | |
 | 1962
...specified In (a) (3) of this section. Supp. 24, 19 PR 4466, July 20, 1954] TRIM } ; I.. I 1 0 General. The means used for trimming the airplane shall be such that after being rimmed and without further pressure ipon, or movement of, either the primary xmtrol or its corresponding... | |
 | 1962
...specified In (a) (3) of this section. [Supp. 24, 19 FR 4456, July 20. 1954] TRIM § 4b.l40 General. The means used for trimming the airplane shall be...by the pilot or the automatic pilot, the airplane shall comply with the trim requirements of §§4b.l41 through 4b.l44. § Hi. 1 10 I General trim qualities... | |
 | 1963
...May 22, 1956, as amended by Amdt. 3-2, 22 PJÎ. 6661, July 16. 1957] TRIM § 3.112 Requirements. (a) The means used for trimming the airplane shall be such that, after being trimmed ала without further pressure upon or movement of either the primary control or its corresponding... | |
 | United States. Department of State - 1940
...0.9 of the limit control force nor shall it be necessary to throttle the remaining engines. 2.132. Trim. The means used for trimming the airplane shall...airplane will maintain : (a) lateral and directional trim in level flight at a speed equal to 90% of the high speed, (b) longitudinal trim under the following... | |
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The means used for trimming the airplane shall be such that, after being trimmed and without further pressure upon or movement of either the primary control or its corresponding trim control by the pilot or the automatic pilot, the airplane will maintain... 
