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 48
... Vertical tail surfaces . Identifica- tion marks at least 2 ' ' high shall be dis- played on the upper half of the vertical tail surface . They shall be displayed on both sides of a single tail surface and on the outer sides of multitail ...
... Vertical tail surfaces . Identifica- tion marks at least 2 ' ' high shall be dis- played on the upper half of the vertical tail surface . They shall be displayed on both sides of a single tail surface and on the outer sides of multitail ...
Էջ 49
... vertical ail surfaces or on the sides of the uselage . ( 1 ) Vertical tail surfaces . If identi- cation marks are displayed on the ver- ical tail surfaces , both surfaces of a ingle vertical tail or the outer surfaces f a multivertical ...
... vertical ail surfaces or on the sides of the uselage . ( 1 ) Vertical tail surfaces . If identi- cation marks are displayed on the ver- ical tail surfaces , both surfaces of a ingle vertical tail or the outer surfaces f a multivertical ...
Էջ 53
... VERTICAL TAIL SURFACES Maneuvering loads . .219-1 Vertical surface maneuvering loads ( FAA policies which apply to § 3.219 ) . Gust loads . .220 220-1 Gust loads ; vertical tail surfaces ( FAA policies which apply to § 3.220 ) ...
... VERTICAL TAIL SURFACES Maneuvering loads . .219-1 Vertical surface maneuvering loads ( FAA policies which apply to § 3.219 ) . Gust loads . .220 220-1 Gust loads ; vertical tail surfaces ( FAA policies which apply to § 3.220 ) ...
Էջ 77
... vertical acceleration , tendency to bounce , nose over , ground loop , porpoise , or water loop . FLIGHT CHARACTERISTICS § 3.105 Requirements . The airplane shall meet the require- ments set forth in §§ 3.106 to 3.124 at all normally ...
... vertical acceleration , tendency to bounce , nose over , ground loop , porpoise , or water loop . FLIGHT CHARACTERISTICS § 3.105 Requirements . The airplane shall meet the require- ments set forth in §§ 3.106 to 3.124 at all normally ...
Էջ 91
... vertical gusts as specified below while in level flight and the resulting loads shall be considered limit loads : ( a ) Positive ( up ) and negative ( down ) gusts of 30 feet per second nominal in- tensity at all speeds up to Vc , ( b ) ...
... vertical gusts as specified below while in level flight and the resulting loads shall be considered limit loads : ( a ) Positive ( up ) and negative ( down ) gusts of 30 feet per second nominal in- tensity at all speeds up to Vc , ( b ) ...
Այլ խմբագրություններ - View all
Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1976 |
Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1976 |
Code of Federal Regulations: Containing a Codification of Documents of ... Ամբողջությամբ դիտվող - 1982 |
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.