 | 1957 - 1296 էջ
...13 of this subchapter; for propeller airworthiness requirements see Part 14 of this subchapter. (5) Critical altitude. The critical altitude is the maximum...which is governed by a constant manifold pressure. (6) Pitch setting. Pitch setting is the propeller blade setting determined by the blade angle measured... | |
 | 1964 - 918 էջ
...which it is possible to maintain, at the maximum continuous rotational speed, one of the following: (i) The maximum continuous power, In the case of engines...which is governed by a constant manifold pressure. (7) Pitch setting. Pitch setting is the propeller blade setting determined by the blade angle measured... | |
 | 1961 - 1484 էջ
...it is possible to maintain, at the maximum continuous rotational speed, one of the following : (i) The maximum continuous power, in the case of engines...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
...which it is possible to maintain, at the maximum continuous rotational speed, one of the following: (i) The maximum continuous power, in the case of engines...the case of engines the maximum continuous power of whicb is governed by a constant manifold pressure. (h) Propellers and rotors * — (1) .Rotor. '•'.otor... | |
 | 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... | |
 | 1999 - 1064 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... | |
 | 1964 - 1108 էջ
...rotational speed and gas temperature, and approved for use during periods of unrestricted duration. (iii) Maximum continuous thrust for turbine engines is the...constant manifold pressure. (h) Propellers and rotors* — U) Rotor. Rotor is a system of rotating airfoils. (2) Main rotor. The main rotor is the main system... | |
 | 1963 - 908 էջ
...pressure measured at the appropriate point in the induction system, usually in inches of mercury. (5) Critical altitude. The critical altitude is the maximum...which is governed by a constant manifold pressure. (6) Pitch setting. Pitch setting is the propeller blade setting determined by the blade angle measured... | |
 | 1962 - 902 էջ
...case of engines for which this power rating is the same at sea level and at the rated altitude. Ш) The maximum continuous rated manifold pressure, in...case of engines the maximum continuous power of which 1 For engine airworthiness requirements see Part 13 of this subchapter. For propeller airworthiness... | |
| |
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: (1) The maximum continuous power, in the case of engines for which this power... 
