Ch-53a/d/e Helicopter Parts

(Page 65) End item NSN parts page 65 of 66
Part Number
NSN
NIIN
65450-01022-014 Light Transmitt Indicating Panel
009413370
65450-01115-101 Thermal Resistor
002319666
65490-03002-102 Pitot Tube Support
001646210
65491-01027-103 Light Transmitt Indicating Panel
011302954
65502-03111-103 Crew Chief Seat Bracket
008553267
65503-00014 Aircraft Seat
000892397
65503-00014-102 Aircraft Seat
000892397
65503-00014-104 Aircraft Seat
009383566
65503-00014-106 Aircraft Seat
009383568
65503-00014-109 Aircraft Seat
000580739
65503-00014-112 Aircraft Seat
000653215
65503-00014-113 Aircraft Seat
000580753
65503-00014-114 Aircraft Seat
000580758
65503-00114-101 Troop Seat Bracket
009157419
65503-0014-112 Aircraft Seat
000653215
65506-09017-015 Fire Extinguishing Tube Assembly
004323441
65513-00009-104 Aircraft Seat
012851629
65523-00005-049 Door Assembly
012878047
65523-00009-047 Ceiling Panel Assembly
011318691
65523-00022-060 Aircraft Structural Panel
013181226
Page: 65

Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e Helicopter

The Sikorsky CH-53E Super Stallion is the largest and heaviest helicopter in the United States military. As the Sikorsky S-80 it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor and canting the tail rotor 20 degrees. It was built by Sikorsky Aircraft for the United States Marine Corps. The less common MH-53E Sea Dragon fills the United States Navy's need for long range minesweeping or Airborne Mine Countermeasures (AMCM) missions, and perform heavy-lift duties for the Navy. Under development is the CH-53K King Stallion, which will be equipped with new engines, new composite material rotor blades, and a wider aircraft cabin.

The CH-53 was the product of the U.S. Marines' "Heavy Helicopter Experimental" (HH(X)) competition begun in 1962. Sikorsky's S-65 was selected over Boeing Vertol's modified CH-47 Chinook version. The prototype YCH-53A first flew on 14 October 1964. The first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg) including 20,000 lb (9,072 kg) in payload.

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