Ch-53a/d/e Helicopter Parts

(Page 58) End item NSN parts page 58 of 66
Part Number
NSN
NIIN
65209-04005-042 Fitting Assembly
006273716
65209-08023-041 Special Fitting Assembly
012429636
65209-08023-042 Special Fitting Assembly
012429636
65209-09027-103 Special Bushing
001502546
65211-02010-042 Fire Extinguisher Cover Assembly
011361390
65211-05105-105 Engine Door Hinge
011404064
65212-07026-102 Sleeve Bushing
011474650
65213-08002-044 Liner Assembly
011361377
65213-08002-045 Liner Assembly
011396873
65213-08002-052 Liner Assembly
011361378
65213-08002-066 Liner Assembly
011361379
65213-08002-068 Liner Assembly
011361380
65213-08002-072 Liner Assembly
011361382
65213-08002-074 Liner Assembly
011361383
65213-08002-212 Sponson Assembly Fairing
012382473
65213-08003-042 Panel Assembly
011396874
65213-08003-051 Panel Assembly
011318656
65213-08003-052 Panel Assembly
011396875
65213-08003-056 Panel Assembly
011396877
65213-08003-108 Liner Header
011396878
Page: 58 ...

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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