Max takeoff weight: 155,000 lb (70,307 kg)【最大起飞重量:155,000磅(70,307千克)】 Powerplant: 4 × Allison T56-A-15 turboprop engines, 4,590 shp (3,420 kW) each【参考译文】发动机:4台艾里逊T56-A-15涡轮螺旋桨发动机,每台功率4,590轴马力(3,420千瓦) Propellers: 4-bladed Hamilton ...
Presents answers to queries regarding C-130 airplane takeoff and landing. Expectations that are asked when landing and aborting performance is discussed; Critical field length requirements of C-130; Definition of ...
The Lockheed C-130 Hercules is a four-engine turboprop military transport aircraft designed and built originally by Lockheed (now Lockheed Martin). Capable of using short and unprepared runways for takeoffs and landings, the C-130 was originally designed
This simulator provides students with flight crew (pilots and loadmaster) training that is directly transferable to the C-130J aircraft. Pilots practice and learn the use of all controls and instruments during takeoff, landing, crew coordination, transition, instrument flight, tactical missions to ...
290 gallon external fuel tanks and an increased maximum takeoff weight capability. June 1974 introduced the first of 308 C-130H's with the more powerful Allison T56-A-15 turboprop engine. Nearly identical to the C-130E externally, the new engine brought major performance improvements to the ...
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Function One Key Takeoff / Landing Other attributes Place of Origin Guangdong, China Capacity 1 ml Type Li-polymer Warranty 3months-1year Chargeable Yes Certification UN38.3 Packaging and delivery Packaging Details box Supply Ability Supply Ability ...
Max. takeoff weight: 31,000 lb (14,061 kg) Powerplant: 2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder radial engines, 1,200 hp (895 kW) each Performance Maximum speed: 224 mph (195 kn, 360 km/h) at 10,000 ft (3,050 m) ...
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