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 14–ի 1-ից 5-ը:
Էջ 157
... intensities of position lights shall comply with the provisions of para- graph ( b ) of this section . The intensities pre- ( b ) Forward and rear position lights . The light distribution and intensities of forward and rear position ...
... intensities of position lights shall comply with the provisions of para- graph ( b ) of this section . The intensities pre- ( b ) Forward and rear position lights . The light distribution and intensities of forward and rear position ...
Էջ 158
... intensities in the horizontal plane of forward and rear position lights . 0 ° 0 ° to 5 ° 5 ° to 10 ° Angle above or ... intensities in any vertical plane of forward and rear position lights . Overlaps Green in dihedral angle L. Maximum ...
... intensities in the horizontal plane of forward and rear position lights . 0 ° 0 ° to 5 ° 5 ° to 10 ° Angle above or ... intensities in any vertical plane of forward and rear position lights . Overlaps Green in dihedral angle L. Maximum ...
Էջ 159
... intensities , shall be in accordance with Figure 3-18 . The following relation shall be assumed : where : I ta I ( t ) ... intensities for anti- collision lights . ( Interprets or applies sec . 603 , 52 Stat . 1009 , as amended ; 49 ...
... intensities , shall be in accordance with Figure 3-18 . The following relation shall be assumed : where : I ta I ( t ) ... intensities for anti- collision lights . ( Interprets or applies sec . 603 , 52 Stat . 1009 , as amended ; 49 ...
Էջ 331
... intensities equal to 85 per- cent of the values prescribed in § 4b.211 ( b ) . ( 2 ) Fatigue evaluation of the struc- ture shall take into account any increase in operating stresses resulting from the design condition of subparagraph ...
... intensities equal to 85 per- cent of the values prescribed in § 4b.211 ( b ) . ( 2 ) Fatigue evaluation of the struc- ture shall take into account any increase in operating stresses resulting from the design condition of subparagraph ...
Էջ 439
... intensities . ( a ) General . The intensities pre- scribed in this section are those to be provided by new equipment with all light covers and color filters in place . In- tensities shall be determined with the light source operating at ...
... intensities . ( a ) General . The intensities pre- scribed in this section are those to be provided by new equipment with all light covers and color filters in place . In- tensities shall be determined with the light source operating at ...
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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.