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[DOC File]FREEWHEELING UNIT/MAIN DRIVE SHAFT CONNECTION TO …
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The power train system provides a means of transmitting engine power to the main and tail rotor systems. ... What is the burn rate of the Allison C20J turbine engine? The burn rate is 20-29 gallons per hour. ... The aircraft cannot be flown unless the change …
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[DOC File]UNCONFIRMED MINUTES
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Rolls-Royce Corp (formerly Allison Engine Company) Thales. Parker Hannifin. Pratt & Whitney (US) Pratt & Whitney (Canada) GE Sikorsky. Honeywell. RR plc. Vought Bell Helicopter DCMA Cessna. MTU. RR Corp (Allison Engine Co) AVIO. Northrop Grumman GSA Hamilton Sundstrand. Boeing MD Helicopters Lockheed Martin. AIRBUS EADS MTAD Eurocopter EADS ...
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[DOC File]12 October 1997 - Federal Aviation Administration
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Capt. Roy Tucker Allied Signal Engines David Looper William Moring Allison Engine Company Donald Risser Barry Rohm Association of European Airlines Peter Malanik Atlantic Coast Airlines Ken Latour Atlantic Southeast Airlines (Regional Airline Association) Dean Karnatz Bombardier Aerospace Jim Donnelly David Lamb British Aerospace (BAe) Tim ...
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[DOC File]AIRCRAFT
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Applicability: Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) 250-B17, -B17B, -B17C, -B17D, -B17E, -B17F, -B17F/1, -B17F/ 2, 250-C18, -C20, -C20B, -C20F, -C20J, -C20R, -C20R/1, -C20R/2, -C20R/4, -C20S, and C20W series turboprop and turboshaft engines with the gas producer ...
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[DOC File]V-1710-A
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The Allison V-1710-C was the first engine to pass a 150-hr type test at 1,000 hp, which it did in April 1937. A total of 2,580 V-1710-Cs were built, with the majority being used in Curtiss P-40s. Aircraft that it powered included the Consolidated A-11A, Curtiss (X)YP-37, Curtiss XP-40, P-40, P-40B, P-40C, and Lockheed XP-38.
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[DOC File]2
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Aircraft type WC-130H, J Model Aircraft Powerplant Allison Turboprop (4), 4000+ horsepower Aircraft size 132’ 7” wingspan, 99’ 6” length, 38’ 6” height Speed >350 mph Ceiling >33,000 ft. Maximum Range >4000 miles Maximum takeoff weight 155,000 lbs. Crew 6 (pilot, copilot, navigator, flight engineer, aerial reconnaissance officer ...
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[DOC File]To: Judge Bailey
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The enhanced engine diffuser assembly was installed into the subject engine on October 5, 1993, by Airwork, an independent company that was a GM authorized maintenance facility. On December 1, 1993, Allison paid cash for the assets of GM/Allison.
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Allison aircraft engine company