Ch-53a/d/e Helicopter Parts

(Page 57) End item NSN parts page 57 of 66
Part Number
NSN
NIIN
65207-01004-108 Follower Bearing
009389671
65207-01012-001 Bevel Washer
008285435
65207-01024-044 Window Latch Assembly
009157726
65207-02027-046 Electronic Compar Cover Assembly
009157411
65207-03005-041 Butt Hinge
009398582
65207-03021-082 Door Sill Assembly
000278760
65207-03053-041 Access Door Hinge
000279177
65207-03053-042 Access Door Hinge
000278993
65207-09004-135 Hinge-half
010073381
65207-10042-042 Ramp Floor Assembly
000145787
65207-10042-046 Ramp Floor Assembly
000145787
65207-10042-051 Ramp Floor Assembly
001639445
65207-10042-059 Ramp Floor Assembly
013154585
65207-10086-101 Receiver Assembly
001097079
65207-10088-102 Ramp Fitting
001682151
65207-10089-101 Roller Stowage Ramp Fitting
000145789
65208-04010-042 Tread Assembly
009157026
65208-04018-101 Support X
009157028
65209-01003-101 Windshi Wiper Shaft
008242593
Page: 57 ...

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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