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 227
The maximum take - off weight for any altitude shall not exceed the maximum
design weight used in the structural loading conditions for flight loads ( $ $ 4a.72
– 4a.99 ) , and shall not exceed the design weight used in the structural loading ...
The maximum take - off weight for any altitude shall not exceed the maximum
design weight used in the structural loading conditions for flight loads ( $ $ 4a.72
– 4a.99 ) , and shall not exceed the design weight used in the structural loading ...
Էջ 301
These factors shall be obtained as follows : ( a ) For any specific airplane type ,
the average full temperature accountability shall be computed for the range of
weights of the airplane , altitudes above sea level , and ambient temperatures ...
These factors shall be obtained as follows : ( a ) For any specific airplane type ,
the average full temperature accountability shall be computed for the range of
weights of the airplane , altitudes above sea level , and ambient temperatures ...
Էջ 528
An auxiliary phere at a specified altitude , under rotor is one which serves either
to counthe maximum conditions of ... engines is the brake horsepower of no
feathering is the axis about which developed at specified altitudes , atmos there
is no ...
An auxiliary phere at a specified altitude , under rotor is one which serves either
to counthe maximum conditions of ... engines is the brake horsepower of no
feathering is the axis about which developed at specified altitudes , atmos there
is no ...
Էջ 569
this value at the rate of 3.6 ° F. per thousand feet of altitude above sea level until
a temperature of -67 ° F. is reached above which altitude the temperature shall
be constant at -67 ° F. ( c ) Correction factor for cylinder head , oil inlet ,
carburetor ...
this value at the rate of 3.6 ° F. per thousand feet of altitude above sea level until
a temperature of -67 ° F. is reached above which altitude the temperature shall
be constant at -67 ° F. ( c ) Correction factor for cylinder head , oil inlet ,
carburetor ...
Էջ 610
( iii ) Take - off thrust for turbine engines is the jet thrust developed under static
conditions at specified altitudes and ... for reciprocating engines is the brake
horsepower developed in standard atmosphere at a specified altitude and under
the ...
( iii ) Take - off thrust for turbine engines is the jet thrust developed under static
conditions at specified altitudes and ... for reciprocating engines is the brake
horsepower developed in standard atmosphere at a specified altitude and under
the ...
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Common terms and phrases
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 fuel ground indicator inspection installed intensities 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 shown side specified speed stalling standard structure Supp surface take-off tank temperature tests tion type certificate unless vertical weight wheel wing
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 621 - 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 566 - 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 494 - ... 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 192 - ... 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 624 - 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 260 - ... 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 210 - 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 47 - 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 119 - 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.
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, 1962 |
| Original from | Միչիգանի համալսարան |
| Digitized | 19 Մայիս 2005 |
| Export Citation | BiBTeX EndNote RefMan |