 | 1981 - 890 էջ
...horsepower that is developed under static conditions at a specified altitude and atmospheric temperature, and under the maximum conditions of rotor shaft rotational...shown in the approved engine specification. "Takeoff safety speed" means a referenced airspeed obtained after lift-off at which the required one-engine-inoperative... | |
 | 1999 - 1064 էջ
...conditions at a specific altitude and atmospheric temperature under the maximum conditions of rotorshaft rotational speed and gas temperature approved for...of time shown in the approved engine specification. Tandem wing configuration means a configuration having two wings of similar span, mounted in tandem.... | |
 | 1973 - 966 էջ
...conditions at a specific altitude and atmospheric temperature under the maximum conditions of rotorshaft rotational speed and gas temperature approved for...of time shown in the approved engine specification. "Time in service", with respect to maintenance time records, means the time from the moment an aircraft... | |
 | 1977 - 788 էջ
...Conditions, and under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for the normal takeoff, and limited in continuous...of time shown in the approved engine specification; and (2) With respect to turbine engines, means the brake horsepower that is developed under static... | |
 | 1964 - 918 էջ
...the Jet thrust developed under static conditions at specified altitudes and atmospheric temperatures and under the maximum conditions of rotor shaft rotational...temperature approved for the normal take-off, and limited in use to a maximum continuous period as Indicated in the approved engine specification. (4) 30-minute... | |
 | 1998 - 1264 էջ
...conditions, and under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for the normal takeoff, and limited In continuous...of time shown In the approved engine specification; and (2) With respect to turbine engines, means the brake horsepower that Is developed under static... | |
 | 1963 - 1044 էջ
...conditions at specified altitudes and atmospheric temperatures, under the maximum conditions of engine rotor shaft rotational speed and gas temperature approved for the normal take-off, and limited in use to a maximum continuous period as indicated in the approved engine specification. (3) Maximum continuous... | |
 | 1960 - 270 էջ
...the jet thrust developed under static conditions at specified altitudes and atmospheric temperatures and under the maximum conditions of rotor shaft rotational...speed and gas temperature approved for the normal take-oft, and limited in use to a maximum continuous period as indicated in the approved engine specification.... | |
 | 1968 - 2418 էջ
...conditions, and under the maximum conditions of crankshaft rotational speed and engine manifold pressure approved for the normal takeoff, and limited in continuous...to the period of time shown in the approved engine specCation; and (2) With respect to turbine engines, means the brake horsepower that Is developed under... | |
 | 1962 - 898 էջ
...brake horsepower developed under static conditions at specified altitudes and atmospheric temperatures and under the maximum conditions of rotor shaft rotational...temperature approved for the normal take-off, and limited in use to a maximum continuous period as indicated in the approved engine specification. (III) Take-off... | |
| |
... rotational speed and gas temperature approved for the normal takeoff, and limited In continuous use to the period of time shown in the approved engine specification. 
