 | 1963 - 1044 էջ
...horsepower is the power delivered at the propeller shaft of the engine. (2) Take-off power or thrust. (1J Take-off power for reciprocating engines is the brake...the normal takeoff, and limited in use to a maximum 1 For engine airworthiness requirements see Part 13 of this subchapter; for propeller airworthiness... | |
 | 2000 - 1128 էջ
...takeoff. Takeoff power: (1) With respect to reciprocating engines, means the brake horsepower that is developed under standard sea level conditions, and...pressure approved for the normal takeoff, and limited in continuous use to the period of time shown in the approved engine specification; and (2) With respect... | |
 | 1982 - 880 էջ
...takeoff. "Takeoff power": (1) With respect to reciprocating engines, means the brake horsepower that is developed under standard sea level conditions, and...pressure approved for the normal takeoff, and limited in continuous use to the period of time shown in the approved engine specification; and (2) With respect... | |
 | 1964 - 918 էջ
...this subchapter. der the maximum conditions of engine rotor shaft rotational speed and gas temperature approved for the normal take-off, and limited in use...as indicated in the approved engine specification. (3) Maximum continuous power or thrust, (i) Maximum continuous power for reciprocating engines is the... | |
 | 1957 - 1296 էջ
...maximum conditions of crankshaft rotational speed and engine manifold pressure approved for use in the normal take-off, and limited in use to a maximum...as indicated in the approved engine specification. (3) Maximum continuous power. Maximum continuous power is the brake horsepower developed in standard... | |
 | 1961 - 1484 էջ
...power for reciprocating engines is the brake horsepower developed under standard sea level conditions, under the maximum conditions of crankshaft rotational...pressure approved for the normal take-off, and limited hi use to a maximum continuous period as indicated in the approved engine specification. (ii) Take-off... | |
 | 1960 - 270 էջ
...power for reciprocating engines is the brake horsepower developed under standard sea level conditions, under the maximum conditions of crankshaft rotational...as indicated in the approved engine specification. 1 For engine airworthiness requirements see Part 13 of this subchapter. (ii) Take-off power for turbine... | |
 | 1964 - 1108 էջ
...limited in use to a maximum continuous period as indicated in the approved engine specification. (11) Take-off power for turbine engines is the brake horsepower...specified altitudes and atmospheric temperatures, under the maximum conditions of engine rotor shaft rotational speed and gas temperature approved for... | |
 | 1977 - 894 էջ
...means the brake horsepower that Is developed under standard sea level conditions, and under the muTimmn conditions of crankshaft rotational speed and engine...pressure approved for the normal takeoff, and limited in continuous use to the period of tune shown in the approved engine specification; and (2) With respect... | |
 | 1962 - 902 էջ
...fuselage to the plane of symmetry in any reasonable manner. (9> Balancing tail load. A balancing tail load is that load necessary to place the airplane...as indicated in the approved engine specification. (11) Take-off power for turbine engines is the brake horsepower developed under static conditions at... | |
| |
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... 
