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, 1962 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 45
... demonstrate that the aircraft perform- ance is adequate for such operations with respect to takeoff , climb , and land- Ing at maximum and minimum weights , For which the aircraft is to be certificated . The aircraft will be demonstrated ...
... demonstrate that the aircraft perform- ance is adequate for such operations with respect to takeoff , climb , and land- Ing at maximum and minimum weights , For which the aircraft is to be certificated . The aircraft will be demonstrated ...
Էջ 59
... demonstrated for the issuance of and changes to type certificates for normal , utility , and acro- batic category ... demonstrated . § 3.74 . ) ( See ( 2 ) Minimum weight . The minimum weight of the airplane is that minimum at which ...
... demonstrated for the issuance of and changes to type certificates for normal , utility , and acro- batic category ... demonstrated . § 3.74 . ) ( See ( 2 ) Minimum weight . The minimum weight of the airplane is that minimum at which ...
Էջ 63
... demonstrated . Thereafter , the Administrator shall record the appli- cable regulations for each change in the type ... demonstrates the eli- gibility of the airplane by complying with the requirements of this part in addition to the ...
... demonstrated . Thereafter , the Administrator shall record the appli- cable regulations for each change in the type ... demonstrates the eli- gibility of the airplane by complying with the requirements of this part in addition to the ...
Էջ 73
... proven , or ( c ) the extremes for which compliance with all functional re- quirements were demonstrated , loading instructions shall be provided in the Air- plane Flight Manual as specified in § 3.777-3.780 . § 3.76-1 Center of gravity ...
... proven , or ( c ) the extremes for which compliance with all functional re- quirements were demonstrated , loading instructions shall be provided in the Air- plane Flight Manual as specified in § 3.777-3.780 . § 3.76-1 Center of gravity ...
Էջ 75
... demonstrated with : ( 1 ) Take - off power , ( 2 ) Most unfavorable weight , ( 3 ) Most unfavorable c . g . position . ( d ) It shall be demonstrated that the airplane will take off safely without re- quiring an exceptional degree of ...
... demonstrated with : ( 1 ) Take - off power , ( 2 ) Most unfavorable weight , ( 3 ) Most unfavorable c . g . position . ( d ) It shall be demonstrated that the airplane will take off safely without re- quiring an exceptional degree of ...
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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 aileron air speed air-speed aircraft Airplane Flight Manual airworthiness certificate altitude amended by Amdt angle approved brake carburetor cate center of gravity Civil Air Regulations climb compartment compliance comply components configuration control surface control system critical engine demonstrated determined device dihedral angle effect equipment established exceed FAA policies factor of safety fire flight conditions flight path flight tests fuel system fuel tank ground gust indicator inspection installed instruments July 20 landing conditions landing gear landing weight level flight limit load load factor located maneuvers manufacturer materials maximum continuous power means ments minimum normal operating limitations paragraph percent pilot placard plane policies which apply position lights powerplant prescribed pressure procedure production certificate propeller retracted rotor rotorcraft seaplane specified stalling speed structure subchapter subparagraph Supp tail take-off power Technical Standard Orders temperature tion trim type certificate type design vertical wheel Wing flaps
Սիրված հատվածներ
Էջ iv - Federal Credit Unions, Bureau of Federal Crop Insurance Corporation Federal Deposit Insurance Corporation Federal Home Loan Bank Board Federal Housing Administration Federal Maritime Commission Federal Mediation and Conciliation Service Federal National Mortgage Association Federal Power Commission Federal Prison Industries Federal Procurement Regulations Federal Procurement Regulations System Federal...
Էջ 605 - 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 550 - The identity and location of each passenger emergency exit must be recognizable from a distance equal to the width of the cabin. The location of each passenger emergency exit must be indicated by a sign visible to occupants approaching along the main passenger aisle. There must be a locating sign...
Էջ 480 - ... 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 178 - ... subscripts have the usual significance. When applied to an entire wing or surface, the coefficients represent average values and shall be properly correlated with local conditions (load distribution) as required in i 4a.99.
Էջ 608 - Takeoff power": (1) With respect to reciprocating engines, means the brake horsepower that is developed under standard sea level conditions, and under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for the normal takeoff, and limited in...
Էջ 246 - ... it shall be assumed that the airplane is not banked before reaching a height of 50 feet as shown by the net takeoff flight path data in the Airplane Flight Manual, and that a maximum bank thereafter does not exceed 15 degrees.
Էջ 196 - All members of the structure shall be suitably protected against deterioration or loss of strength in service due to weathering, corrosion, abrasion, or other causes. In seaplanes, special...
Էջ 31 - All reporting requirements of this agreement have been approved by, and subsequent reporting and recordkeeping requirements will be subject to the approval of the Bureau of the Budget in accordance with the Federal Reports Act of 1942.
Էջ 105 - If compliance with the limit landing conditions specified in paragraph (a) (1) of this section 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.