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Code of Federal Regulations: Containing a Codification of Documents of ...
Ամբողջությամբ դիտվող - 1982
acceptable accordance addition Administrator aileron aircraft airplane airworthiness altitude amended by Amdt appropriate approved assumed brake climb compartment complete compliance comply components conducted considered continuous crew critical demonstrated determined device direction distance effect emergency engine equal equipment established exceed FAA policies failure feet fire flaps flight flight tests flow force forward fuel ground indicator inspection installed intensities July landing gear least less limit lines load load factor located maneuvers Manual manufacturer marked materials maximum means ments necessary normal NOTE obtained operation paragraph path percent performance permit pilot plane policies which apply portion position possible prescribed pressure procedure propeller protection range regulations result rotor rotorcraft safe safety side specified speed stalling standard structure Supp surface take-off tank temperature tests tion type certificate unless vertical weight wheel wing
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.