 | 1964 - 918 էջ
...maximum continuous power, in the case of engines for which this power rating is the same at sea level and at the rated altitude. (11) The maximum continuous...which Is governed by a constant manifold pressure. (h) Propeller s and rotors' — (1) Rotor. Rotor is a system of rotating airfoils. (2) Main rotor.... | |
 | 1957 - 1296 էջ
...altitude, 1 For engine airworthiness requirements see Part 13 of this subchapter. 395012—57-28 Page 409 (11) The maximum continuous rated manifold pressure,...which is governed by a constant manifold pressure. (h) Propellers and rotors ' — (1) .Rotor. Rotor is a system of rotating airfoils. (2) Main rotor.... | |
 | 1991 - 872 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude. (2) The maximum continuous rated manifold pressure, in...which is governed by a constant manifold pressure. Critical engine means the engine whose failure would most adversely affect the performance or handling... | |
 | 1996 - 984 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude. (2) t & G E jP d W LЊmp á ꆯH Critical engine means the engine whose failure would most adversely affect the performance or handling... | |
 | 1961 - 1484 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude, (ii) The maximum continuous rated manifold pressure, in...continuous power of which is governed by a constant manif ola pressure [21 FR 4305, June 20, 1956, as amended, 22 FR 5569, July 16,1957] CERTIFICATION... | |
 | 1963 - 1044 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude, (ii) The maximum continuous rated manifold pressure, in...the case of engines the maximum continuous power of whicb is governed by a constant manifold pressure. (h) Propellers and rotors * — (1) .Rotor. '•'.otor... | |
 | 2001 - 1142 էջ
...rating, if appropriate, for the conduct of the flight. Pitch setting means the propeller blade setting as determined by the blade angle measured in a manner, and at a radius, specified by the instruction manual for the propeller. Positive control means control of all air traffic, within... | |
 | 1973 - 966 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude. (2) The maximum continuous rated manifold pressure, in the case of engines, the maximum conitnuous power of which is governed by a constant manifold pressure. "Critical engine" means the... | |
 | 1975 - 734 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude. (2) The maximum continuous rated manifold pressure, In the case of engines, the maximum conltnuous power of which is governed by a constant manifold pressure. "Critical engine" means the... | |
 | 1964 - 1108 էջ
...of the propeller. (3) Pitch setting. Pitch setting is fte propeller blade setting determined by to blade angle measured in a manner, and at a radius, specified in the instructici manual for the propeller. (4) Fixed-pitch propeller. A fix* pitch propeller is a propeller... | |
| |
... following: (1) The maximum continuous power, in the case of engines for which this power rating is the same at sea level and at the rated altitude. (2) The maximum continuous rated manifold pressure, in the case of engines, the maximum continuous... 
