Code of Federal Regulations: Containing a Codification of Documents of General Applicability and Future Effect as of December 31, 1948, with Ancillaries and IndexDivision of the Federal Register, the National Archives, 1960 |
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Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1976 |
Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1976 |
Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1982 |
Common terms and phrases
accordance added by Amdt aircraft Airplane Flight Manual airplane's airport airworthiness altitude Amendment 4b-11 antenna Anti-collision light approved battery brake brake horsepower cabin pressure cable Civil Aeronautics Civil Air Regulations CODIFICATION compartment compliance configuration critical engine demonstrated determined effective electrical emergency exits engine inoperative equipment eye position FAA interpretations FAA policies failure Federal Aviation Agency feet flight crew Flight Instructor flight path flight test fuel system fuselage gradient of climb graph inches installation instrument issuance July 16 landing gear less located maneuvers ment minimum normal operational limits parachute rigger paragraph passenger percent performance pilot certificate plane policies which apply position lights power and/or thrust Powerplant prescribed pressure procedures propeller radio Revoked rotor rotorcraft runway seat sentence Sept specified stalling speed subparagraph Subpart Supp take-off path Technical Standard Order tificate tion transport category turbine type certificate weight
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Էջ 25 - ... knots, with: (1) Zero thrust at the stalling speed, or engines idling and throttles closed if it is shown that the resultant thrust has no appreciable effect on the stalling speed; (2) If applicable, propeller pitch controls in the position...
Էջ 31 - The speed 7,0 shall denote the calibrated stalling speed, or the minimum steady flight speed at which the airplane Is controllable. In...
Էջ 77 - If a range of heights exists at any speed, including zero, within which it Is not possible to make a safe landing following power failure, the range of heights and its variation with forward speed must be established, together with any other pertinent information, such as the kind of landing surface.
Էջ 35 - August 29, 1959 unless, in addition to the requirements of paragraph (b) of this section— (1) The accelerate-stop distance is no greater than the length of the runway plus the length of the stopway (if present); (2) The takeoff distance is no greater than the length of the runway plus the length of the clearway (if present); and (3) The takeoff run is no greater than the length of the runway.
Էջ 34 - ... maintain it In straight flight at that speed, either with zero yaw or. at the option of the applicant, with an angle of bank not In excess of 5 degrees.
Էջ 35 - A speed which, if the airplane is rotated at its maximum practicable rate, will result in a lift-off speed...
Էջ xvii - General, or any court of competent jurisdiction, under any provision of law repealed or amended by this Act, or in the exercise of duties, powers, or functions which, under this Act, are vested in the Administrator of the Federal Aviation Agency or the Civil Aeronautics Board, and which are in effect at the time this section takes effect, shall continue in effect according to their terms until modified, terminated, superseded, set aside, or repealed by the Administrator or the Board, as the case...
Էջ 36 - Fuel jettisoning will be approved if the certificate holder shows that the crew is properly instructed, that the training program is adequate, and that all other precautions are taken to ensure a safe procedure...
Էջ 9 - This means must be visible to the pilot and must be located and designed to prevent confusion. (b) Trimming devices must be designed so that, when any one connecting or transmitting element in the primary flight control system...
Էջ 35 - The critical engine inoperative, the remaining engine (s) operating at the available takeoff power and/or thrust; (2) The weight equal to the maximum landing weight; (3) A climb speed established by the applicant in connection with normal landing procedures, except that it shall not exceed 1.5 Vs (see §4T.111(c)).