Ch-53a/d/e Helicopter Parts

(Page 63) End item NSN parts page 63 of 66
Part Number
NSN
NIIN
65355-12142-101 Groove Pulley
001711961
65356-04001 Tube To Boss Cross
013588977
65356-04001-101 Tube To Boss Cross
013588977
65357-07016-041 Output Housing Assembly
004046179
65357-07016-042 Output Housing Assembly
004046179
65358-07040-101 Externally Threaded Ring
009491643
65358-07062-101 Linerxgear Box
009156850
65358-07062-106 Linerxgear Box
009156734
65360-12034-102 Fittingxsupport
009157158
65360-12034-104 Support Fitting
009157165
65362-05021-102 Sleeve Bearing
010077690
65363-06008-102 Couplingxflange
009157115
65363-06026-101 Adjusting Plate
009157235
65364-11302-102 Nonmetallic Strip Seal
008911378
65364-12305-041 Bracket Assembly
009156684
65364-12501-041 Nose Gear B Support
000239533
65370-04130-101 Seal Assembly
001264904
65375-04358-041 Toggle Assembly
008941522
Page: 63

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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