| 1964 - 918 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... | |
| 1957 - 1296 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...constant manifold pressure. (h) Propellers and rotors 2 — (1) .Rotor. Rotor is a system of rotating airfoils. (2) Main rotor. The main rotor is the main... | |
| 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... | |
| 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... | |
| 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... | |
| 1964 - 1108 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...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... | |
| 1962 - 898 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...case of engines the maximum continuous power of which 'For engine airworthiness requirements see Part 13 of this subchapter. For propeller airworthiness... | |
| 1963 - 908 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...Rotor. Rotor Is a system of rotating airfoils. (2) ¡tain rotor. The main rotor Is the main system of rotating airfoils providing sustentation for the... | |
| 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... | |
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