 | Philippines - 2002 - 798 էջ
...speed at which the airplane can be rotated for take-off and shown to be adequate to safely continue the take-off, using normal piloting skill, when the critical engine is suddenly made inoperative. (2) The initial climb out speed V2, in terms of calibrated airspeed, must be selected by the applicant... | |
 | International Civil Aviation Conference - 1945 - 326 էջ
...zero wind velocity. 2.1220 Speeds -T (a) The critical engine failure speed, VI; is a true indicated the minimum speed at which the controllability is...critical engine is suddenly made inoperative. (b) The minimum take-off climb speed, V2, is a true indicated airspeed chosen by the applicant which shall... | |
 | United States. Department of State - 1945 - 298 էջ
...critical engine failure speed, V1, is a true indicated airspeed chosen by the applicant but shall not be less than the minimum speed at which the controllability...piloting skill when the critical engine is suddenly made inoperative(b) The minimum take-off climb speed, V2, is a true indicated airspeed chosen by the applicant... | |
 | United States. Department of State - 1948 - 862 էջ
...critical engine failure speed, Vi, is a true indicated airspeed chosen by the applicant but shall not be less than the minimum speed at which the controllability...critical engine is suddenly made inoperative, (b) The minimum take-off climb speed, V», is a true indicated airspeed chosen by the applicant which shall... | |
 | 1948 - 802 էջ
...These data, when corrected, shall assume a level take-off surface and zero wind velocity. 2.1220 Speeds the minimum speed at which the controllability is...critical engine is suddenly made inoperative, (b) The minimum take-off climb speed, V», is a true indicated airspeed chosen by the applicant which shall... | |
 | 1957 - 1296 էջ
...particular altitude. These data shall be based on a level take-off surface with zero wind. [Amdt. 04-8, 7 FR 986, Feb. 14, 1942] § 4a.748-T Speeds, (a) Critical-engine...inoperative. (b) Minimum take-off climb speed, denoted by V3, is a true indicated air speed chosen by the applicant, which shall permit the rate of climb required... | |
 | 1964 - 918 էջ
...based on a level take-off surface with zero wind. [Amdt. 04-8, 7 FB 986, Feb. 14. 1942] § 4a.74*-T Speeds. (a) Critical-engine failure speed, denoted...take-off climb speed, denoted by V,, is a true Indicated аиspeed chosen by the applicant, which shall permit the rate of climb required In § 4а.74в-Т... | |
 | 1961 - 1484 էջ
...which the controllability is demonstrated during the take-off run to be adequate to permit proceeding safely with the takeoff, using normal piloting skill,...critical engine is suddenly made inoperative. (b) The minimum take-off safety speed V2, in terms of calibrated air speed, shall be selected by the applicant... | |
 | 1963 - 1044 էջ
...which the controllability is demonstrated during the take-off run to be adequate to permit proceeding safely with the takeoff, using normal piloting skill,...critical engine is suddenly made inoperative. (b) The minimum take-off safety speed V2, in terms of calibrated air speed, shall be selected by the applicant... | |
 | 1977 - 788 էջ
...primary aerodynamic control! alone Is shown (during the takeoff run) to be adequate to safely continue the takeoff, using normal piloting skill, when the critical engine Is suddenly made inoperative. (b) Vt „,<„, in terme of calibrated airspeed, may not be less than— (1) 1.2 VB for— (1) Two-engine... | |
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In any case not less than the minimum speed at which the controllability is adequate to proceed safely with the take-off, using normal piloting skill, when the critical engine Is suddenly made Inoperative. 
