The Code of Federal Regulations of the United States of AmericaU.S. Government Printing Office, 1961 The Code of Federal Regulations is the codification of the general and permanent rules published in the Federal Register by the executive departments and agencies of the Federal Government. |
Այլ խմբագրություններ - View all
The Code of Federal Regulations of the United States of America ..., Հատոր 1 Ամբողջությամբ դիտվող - 1939 |
The Code of Federal Regulations of the United States of America ..., Հատոր 3 Ամբողջությամբ դիտվող - 1939 |
Common terms and phrases
accordance Administrator aileron air speed air-speed aircraft Airplane Flight Manual airworthiness certificate altitude amended by Amdt approved brake carburetor center of gravity Civil Air Regulations climb compartment compliance comply components conducted configuration control surface control system critical engine demonstrated determined device dihedral angle equipment established FAA interpretations FAA policies factor of safety failure fire flight conditions flight path flight tests fuel system fuel tank ground gust indicator inspection installed instruments July 16 landing conditions landing gear landing weight level flight limit load load factor located maneuvers manufacturer maximum continuous power means ments minimum normal operating limitations paragraph percent pilot pitch placard plane policies which apply powerplant prescribed pressure procedure production certificate propeller retracted rotor rotorcraft specified stalling speed structure subchapter subparagraph Supp tail take-off power Technical Standard Order temperature tion trim type certificate type design vertical vibration wheel Wing flaps
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Էջ 634 - aircraft" means any contrivance now known or hereafter invented, used, or designed for navigation of or flight in the air, except a parachute or other contrivance designed for such navigation but used primarily as safety equipment.
Էջ 272 - When applied to fluid-carrying lines, other flammable fluid system components, wiring, air ducts, fittings, and powerplant controls, this term refers to a line and fitting assembly, component, wiring, or duct, or controls which will perform the intended functions under the heat and other conditions likely to occur at the particular location.
Էջ 478 - When applied to sheet or structural members, fire-resistant material means a material which will withstand heat at least as well as aluminum alloy in dimensions appropriate for the purpose for which it is to be used. When applied to fluid-carrying lines, other flammable fluid system...
Էջ 608 - Critical altitude" means the maximum altitude at which, in standard atmosphere, it is possible to maintain, at a specified rotational speed, a specified power or a specified manifold pressure. Unless otherwise stated, the critical altitude is the maximum altitude at which it is possible to maintain, at the maximum continuous rotational speed, one of the following...
Էջ 318 - Static directional and lateral stability. (a) The static directional stability, as shown by the tendency to recover from a skid with rudder free, shall be positive...
Էջ 635 - As defined in the Federal Aviation Regulations: " 'Maintenance' means inspection, overhaul, repair, preservation, and the replacement of parts, but excludes preventive maintenance." " 'Preventive maintenance' means simple or minor preservation operations and the replacement of small standard parts not involving complex assembly operations.
Էջ 353 - These loads must be multiplied by a factor of 1.15 unless the dynamic effects of failure under static load are otherwise considered.
Էջ 78 - This shall be so at any speed which can be obtained without excessive control force, except that such speeds need not be greater than the appropriate maximum permissible speed or less than the minimum speed in steady unstalled flight. (b) The air speed shall return to within 10 percent of the original trim speed when the control force is slowly released from any speed within the limits defined in paragraph (a) of this section.
Էջ 226 - 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.
Էջ 123 - Each seaplane mam float shall have a buoyancy of 80 percent in excess of that required to support the maximum weight of the seaplane in fresh water. (b) Compartmentation. Each seaplane main float shall contain...