Code of Federal Regulations: Containing a Codification of Documents of General Applicability and Future Effect as of December 31, 1948, with Ancillaries and Index

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Division of the Federal Register, the National Archives, 1957

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Էջ 418 - Appliances" means instruments, equipment, apparatus, parts, appurtenances, or accessories, of whatever description, which are used, or are capable of being or intended to be used, in the navigation, operation, or control of aircraft in flight (including parachutes and including communication equipment and any other mechanism or mechanisms installed in or attached to aircraft during flight), and which are not a part or parts of aircraft, aircraft engines, or propellers. (12) "Authority" means the...
Էջ 36 - 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 448 - 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 237 - Flight tests shall be conducted to demonstrate the performance of the pressure supply, pressure and flow regulators, indicators, and warning signals in steady and stepped climbs and descents at rates corresponding with the maximum attainable without exceeding the operating limitations of the airplane up to the maximum altitude selected for certification.
Էջ 139 - 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...
Էջ 36 - ... 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 220 - If compliance with the specified limit landing conditions of § 3.352 (a) is demonstrated by free drop tests, these shall be conducted on the complete airplane, or on units consisting of wheel, tire, and shock absorber in their proper relation, from free drop heights not less than the following: h. (inches) =3.6 (W/S...
Էջ 57 - The airplane shall be assumed to be subjected to rolling and yawing maneuvers as described in the following conditions, unbalanced aerodynamic moments about the center of gravity shall be reacted In a rational or conservative manner considering the principal masses furnishing the reacting Inertia forces.
Էջ 418 - 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 274 - ... (b) Static air vent and pressure altimeter systems. (1) All instruments provided with static air case connections shall be vented to the outside atmosphere through an appropriate piping system.

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