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 80
The stick force curve gear and wing flaps retracted . shall have a stable slope and
the stick ( b ) In addition to the above , multiforce shall not exceed 40 lbs . at any
engine airplanes shall maintain longispeed between 1.1 Vs , and 1.8 Vs , with ...
The stick force curve gear and wing flaps retracted . shall have a stable slope and
the stick ( b ) In addition to the above , multiforce shall not exceed 40 lbs . at any
engine airplanes shall maintain longispeed between 1.1 Vs , and 1.8 Vs , with ...
Էջ 193
The control force specified in Table 48-6 and Fig . 48–9 shall be assumed to act
in a lateral direction at the grip of a control stick , or shall be assumed to act as
part of couple equal to the specified force multiplied by the diameter of a control ...
The control force specified in Table 48-6 and Fig . 48–9 shall be assumed to act
in a lateral direction at the grip of a control stick , or shall be assumed to act as
part of couple equal to the specified force multiplied by the diameter of a control ...
Էջ 231
( b ) Where a stable slope of the stick force versus speed curve is specified , any
decrease in speed below trim speed shall require an increase in the steady pull
on the elevator control and any increase in speed above trim speed shall require
...
( b ) Where a stable slope of the stick force versus speed curve is specified , any
decrease in speed below trim speed shall require an increase in the steady pull
on the elevator control and any increase in speed above trim speed shall require
...
Էջ 316
24 , 19 F.R. 4457 , July 20 , 1954 ) $ 4b.151 Static longitudinal stability , In the
conditions outlined in $$ 4b.152 through 4b.155 , the characteristics of the
elevator control forces and friction shall comply with the following : ( a ) A pull
shall be ...
24 , 19 F.R. 4457 , July 20 , 1954 ) $ 4b.151 Static longitudinal stability , In the
conditions outlined in $$ 4b.152 through 4b.155 , the characteristics of the
elevator control forces and friction shall comply with the following : ( a ) A pull
shall be ...
Էջ 319
The curve of elevator control force vs. speed should have a stable slope between
85 percent and 115 percent of the trim speed and no reversal of elevator control
force should occur throughout the speed range tested . Further test procedures ...
The curve of elevator control force vs. speed should have a stable slope between
85 percent and 115 percent of the trim speed and no reversal of elevator control
force should occur throughout the speed range tested . Further test procedures ...
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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 |