Code of Federal Regulations: Containing a Codification of Documents of General Applicability and Future Effect as of December 31, 1948, with Ancillaries and Index |
From inside the book
Արդյունքներ 5–ի 1-ից 5-ը:
Էջ 230
( b ) The descriptive data required in paragraph ( a ) of this section shall be
known as the type design and shall consist of such drawings and specifications
as are necessary to disclose the configu - ration of the airplane and all the design
...
( b ) The descriptive data required in paragraph ( a ) of this section shall be
known as the type design and shall consist of such drawings and specifications
as are necessary to disclose the configu - ration of the airplane and all the design
...
Էջ 412
Inspections and tests shall include all those found necessary by the Administrator
to insure that the rotorcraft complies with the applicable airworthiness
requirements and conforms to the following : ( a ) All materials and products are
in ...
Inspections and tests shall include all those found necessary by the Administrator
to insure that the rotorcraft complies with the applicable airworthiness
requirements and conforms to the following : ( a ) All materials and products are
in ...
Էջ 522
( 6 ) Any specific precaution deemed necessary for the particular area in - volved
. ( 7 ) Any specific precaution deemed necessary for the type of operation
involved . ( d ) Duration . The certificate will contain an expiration date which will
allow ...
( 6 ) Any specific precaution deemed necessary for the particular area in - volved
. ( 7 ) Any specific precaution deemed necessary for the type of operation
involved . ( d ) Duration . The certificate will contain an expiration date which will
allow ...
Էջ 528
of the engine , and such other data as are necessary to permit by comparison the
determination of the airworthiness of subsequent engines of the same type . 8 13
. 15 Inspections and tests . Inspections and tests shall include all those found ...
of the engine , and such other data as are necessary to permit by comparison the
determination of the airworthiness of subsequent engines of the same type . 8 13
. 15 Inspections and tests . Inspections and tests shall include all those found ...
Էջ 541
( a ) The applicant for a type certificate shall submit to the Administrator such
descriptive data , test reports , and computations as are necessary to
demonstrate that the propeller complies with the requirements of this part . ( b )
The descriptive ...
( a ) The applicant for a type certificate shall submit to the Administrator such
descriptive data , test reports , and computations as are necessary to
demonstrate that the propeller complies with the requirements of this part . ( b )
The descriptive ...
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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
acceptable accordance addition Administrator aileron aircraft airplane airworthiness altitude Amdt amended angle approved assumed brake CAA policies climb compartment complete compliance comply components conducted considered continuous cooling crew critical demonstrated determined device direction effect emergency engine equal equipment established factor failure fire flaps flight flight tests flow force Form forward fuel greater ground indicator inspection installed landing gear least less limit lines load load factor located maneuvers Manual manufacturer marks material maximum means ments necessary normal NOTE obtained operation paragraph percent performance pilot plane policies which apply portion position possible prescribed pressure prevent procedure production propeller protection range recorded regulations result retracted rotor rotorcraft safe safety side specified speed stall standard structure Supp surface tail take-off tank temperature tests tion type certificate unless vertical weight wheel wing
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.
Բիբլիոգրաֆիական տվյալներ
| Վերնագիր | Code of Federal Regulations: Containing a Codification of Documents of General Applicability and Future Effect as of December 31, 1948, with Ancillaries and Index |
| Աջակցող | United States. Office of the Federal Register |
| Հրատարակիչ | Division of the Federal Register, the National Archives, 1957 |
| Original from | Միչիգանի համալսարան |
| Digitized | 19 Մայիս 2005 |
| Export Citation | BiBTeX EndNote RefMan |