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 253
plicable provisions of this regulation and with $$ 4T.119 and 4T.120 ( d ) for
altitudes and ambient temperatures within the operational limits of the airplane (
see subparagraph ( 4 ) of this paragraph ) . ( 3 ) Take - off and accelerate - stop ...
plicable provisions of this regulation and with $$ 4T.119 and 4T.120 ( d ) for
altitudes and ambient temperatures within the operational limits of the airplane (
see subparagraph ( 4 ) of this paragraph ) . ( 3 ) Take - off and accelerate - stop ...
Էջ 258
During the landing , changes and / or thrust , and in speed shall be in
8Ccordance with procedures established by the applicant for the operation of the
airplane airplanes and shall not be less than 0.5 per procedures , except that it
shall not ...
During the landing , changes and / or thrust , and in speed shall be in
8Ccordance with procedures established by the applicant for the operation of the
airplane airplanes and shall not be less than 0.5 per procedures , except that it
shall not ...
Էջ 261
No airplane shall be flown along an intended route except in compliance with
either subparagraph ( 1 ) or ... ( 2 ) No airplane shall be taken off at a Teight in
excess of that which , according to he two - engine - inoperative en route net ight
path ...
No airplane shall be flown along an intended route except in compliance with
either subparagraph ( 1 ) or ... ( 2 ) No airplane shall be taken off at a Teight in
excess of that which , according to he two - engine - inoperative en route net ight
path ...
Էջ 265
iguration of the airplane , in power and / or hrust , and in speed . ( 2 ) The weight
of the airplane , the coniguration , and the power and / or thrust shall se constant
throughout each segment and hall correspond with the most critical conlition ...
iguration of the airplane , in power and / or hrust , and in speed . ( 2 ) The weight
of the airplane , the coniguration , and the power and / or thrust shall se constant
throughout each segment and hall correspond with the most critical conlition ...
Էջ 268
40T.81 Airplane's certificate limitations . ( a ) No airplane shall be taken off at a
weight which exceeds the takeoff weight specified in the Airplane Flight Manual
for the elevation of the airport and for the ambient temperature existing at the time
...
40T.81 Airplane's certificate limitations . ( a ) No airplane shall be taken off at a
weight which exceeds the takeoff weight specified in the Airplane Flight Manual
for the elevation of the airport and for the ambient temperature existing at the time
...
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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
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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.
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| 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 |