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, 1957 Special edition of the Federal Register, containing a codification of documents of general applicability and future effect ... with ancillaries. |
From inside the book
Արդյունքներ 100–ի 1-ից 5-ը:
Էջ 47
... forward the information to the Washington office for final deci- sion . [ CAM 1 Rev. , 21 F. R. 8810 , Nov. 14 , 1956 ] § 1.109 Identification marks for ex- port aircraft . An aircraft manufactured in the United States for delivery ...
... forward the information to the Washington office for final deci- sion . [ CAM 1 Rev. , 21 F. R. 8810 , Nov. 14 , 1956 ] § 1.109 Identification marks for ex- port aircraft . An aircraft manufactured in the United States for delivery ...
Էջ 65
... forward through the local Safety Agent to the Chief , Manufactur- ing Inspection Branch , for coordination and approval , a detailed proposal regard- ing the procedure to be followed in es- tablishing the system outlined in this section ...
... forward through the local Safety Agent to the Chief , Manufactur- ing Inspection Branch , for coordination and approval , a detailed proposal regard- ing the procedure to be followed in es- tablishing the system outlined in this section ...
Էջ 73
... forward center of gravity position approved with the maxi- mum authorized weight , and under the most forward center of gravity position approved , regardless of weight , shall not exceed 1.5 times the stall speed for that configuration ...
... forward center of gravity position approved with the maxi- mum authorized weight , and under the most forward center of gravity position approved , regardless of weight , shall not exceed 1.5 times the stall speed for that configuration ...
Էջ 89
... forward to the wing attachment points , assuming that the fuselage load factor is equal to zero . The moment at the wing due to the above described loads need not be balanced out as a couple at the wing attachment points . However , the ...
... forward to the wing attachment points , assuming that the fuselage load factor is equal to zero . The moment at the wing due to the above described loads need not be balanced out as a couple at the wing attachment points . However , the ...
Էջ 101
... forward velocity . However , for exceptionally large wheels , a wheel peripheral velocity equal to the ground speed may not have been at- tained at time of maximum vertical gear load . This case is covered by the statement above that ...
... forward velocity . However , for exceptionally large wheels , a wheel peripheral velocity equal to the ground speed may not have been at- tained at time of maximum vertical gear load . This case is covered by the statement above that ...
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Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1976 |
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Common terms and phrases
accordance Administrator aileron air speed air-speed aircraft Airplane Flight Manual airworthiness certificate altitude amended by Amdt angle brake CAA interpretations CAA policies carburetor center of gravity compartment compliance comply components conducted configuration control system crew critical critical engine demonstrated determined device dihedral angle engine equipment factor of safety flight conditions flight tests fluid fuel system fuel tank fuselage ground gust Identification marks indicator inoperative inspection installed instrument July 20 landing conditions landing gear level flight load factor located maneuvers manufacturer material maximum continuous power maximum weight means ments minimum operating limitations paragraph percent pilot pitch placard plane policies which apply position lights powerplant prescribed production certificate propeller rate of climb regulations rotor rotorcraft sea level seaplane specified stalling speed static structure subchapter subparagraph Subpart Supp tail take-off power Technical Standard Orders temperature tion trim type certificate type design vertical vibration Wing flaps
Սիրված հատվածներ
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.