 Gyroscopic instruments. All gyroscopic instruments shall derive their energy from engine-driven pumps or from auxiliary power units. Each source of energy supply and its attendant complete installation shall comply with the instrument manufacturer's recommendations...  International Organization and Conference Series I-IV. - Էջ 1100United States. Department of State - 1940Ամբողջությամբ դիտվող - Այս գրքի մասին
 | 1939 - 1220 էջ
...attendant complete installation shall comply with the instrument manufacturer's recommendations for satisfactory instrument operation. On multi-engine...the required load. Engine-driven pumps, when used, shah1 be on separate engines. The installation shall be such that failure of one source of energy or... | |
 | International Civil Aviation Conference - 1945 - 326 էջ
...looking out and forward along the flight path and they shall also be visible to the second pilot. 2. 5303 Gyroscopic Instruments. Each source of energy supply...functioning of the instruments by means of the other source. 2. 531 Safety Equipment Installation 2.5310 Fire Extinguishers. The portable fire extinguisher specified... | |
 | United States. Department of State - 1945 - 298 էջ
...looking out and forward along the flight path and they shall also be visible to the second pilot. 2. 5303 Gyroscopic Instruments. Each source of energy supply...functioning of the instruments by means of the other source. 2. 531 Safety Equipment Installation 2.5310 Fire Extinguishers. The portable fire extinguisher specified... | |
 | United States. Congress. House. Committee on Interstate and Foreign Commerce - 1947 - 1548 էջ
...de-icing equipment for each engine, (8) additional source of energy to supply gyroscopic instruments which shall be capable of carrying the required load....Engine-driven pumps, when used, shall be on separate engines and, in lieu of one such pump, an axuiliary power unit ma}' Iw used. The installation shall be such... | |
 | 1961 - 1484 էջ
...attendant complete installation shall comply with the instrument manufacturer's recommendations for satisfactory instrument operation. On multiengine...functioning of the instruments by means of the other source. SAFETY EQUIPMENT INSTALLATION §4a.565 Safety belts. Airplanes manufactured on or after January 1,... | |
 | 1957 - 1118 էջ
...(2) Additional sensitive altimeter, (3) Alternate source of energy to supply gyroscopic instruments which shall be capable of carrying the required load....Engine-driven pumps, when used, shall be on separate engines and, in lieu of one such source of energy, an auxiliary power unit may be used. The installation shall... | |
 | 1964 - 672 էջ
...(2) Additional sensitive altimeter, (3) Alternate source of energy to supply gyroscopic instruments which shall be capable of carrying the required load....Engine-driven pumps, when used, shall be on separate engines and, in lieu of one such source of energy, an auxiliary power unit may be used. The installation shall... | |
 | 1962 - 898 էջ
...attendant complete installation shall comply with the instrument manufacturer's recommendations for satisfactory instrument operation. On multiengine...functioning of the instruments by means of the other source. SAFETY EQUIPMENT INSTALLATION § 4a.565 Safety belts. Airplanes manufactured on or after January l,... | |
 | 1963 - 908 էջ
...attendant complete installation shall comply with the instrument manufacturer's recommendations for satisfactory instrument operation. On multiengine...failure of one source of energy or breakage of one Une will not interfere with proper functioning of the instruments by means of the other source. SAFETY... | |
 | 1962 - 902 էջ
...attendant complete installation shall comply with the instrument manufacturer's recommendations for satisfactory instrument operation. On multiengine...pumps, when used, shall be on separate engines. The ins t alla t ion shall be such that failure of one source of energy or breakage of one line will not... | |
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