 | 1961 - 1484 էջ
...horsepower is the power delivered at the propeller shaft of the engine. (3) Take-off power or thrust, (i) Take-off power for reciprocating engines is the brake...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... | |
 | 1964 - 918 էջ
...horsepower is the power delivered at the propeller shaft of the engine. (2) Take-off power. Take-off power is the brake horsepower developed under standard sea...rotational speed and engine manifold pressure approved for use in the normal take-off, and limited in use to a maximum continuous period as indicated in the approved... | |
 | 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... | |
 | 1962 - 1714 էջ
...maximum continuous — the brake horsepower developed in standard atmosphere at a specified altitude under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for use during periods of unrestricted duration. For purposes of this system of accounts and reports, the... | |
 | 1962 - 392 էջ
...maximum continuous — the brake horsepower developed in standard atmosphere at a specified altitude under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for use during periods of unrestricted duration. For purposes of this system of accounts and reports, the... | |
 | 1975 - 944 էջ
...reciprocating engines — the brake horsepower developed In standard atmosphere at a specified altitude and under the maximum conditions of crankshaft rotational speed and engine manifold pressure, and approved for use during periods of unrestricted duration. Horsepower, maximum continuous for turbine... | |
 | 1999 - 612 էջ
...reciprocating engines. The brake horsepower developed in standard atmosphere at a specified altitude and under the maximum conditions of crankshaft rotational speed and engine manifold pressure, and approved for use during periods of unrestricted duration. Horsepower, maximum continuous for turbine... | |
 | 1960 - 270 էջ
...2593, Apr. 19, 1958] ***** (g) Powerplant installation.1 • • • (2) Take-off power or thrust, (i) Take-off power for reciprocating engines is the brake...as indicated in the approved engine specification. 1 For engine airworthiness requirements see Part 13 of this subchapter. (ii) Take-off power for turbine... | |
 | 1962 - 898 էջ
...see Part 13 of this subchapter. horsepower developed in standard atmosphere at a specified altitude, under the maximum conditions of crankshaft rotational speed and engine manifold pressure, and approved for use during periods of unrestricted duration. (ii) Maximum continuous power for turbine... | |
 | 1976 - 764 էջ
...reciprocating engines — the brake horsepower developed in standard atmosphere at a specified altitude and under the maximum conditions of crankshaft rotational speed and engine manifold pressure, and approved for use during periods of unrestricted duration. Horsepower, maximum continuous for turbine... | |
| |
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... 
