Mh-53e Helicopter Parts

(Page 35) End item NSN parts page 35 of 238
Part Number
NSN
NIIN
03004-12-812 Electrical Contact
004626867
03005-09-020 Electrical Contact
000899520
0301-029 Diode Semiconductor Device
009047496
0301-BB1 Annular Ball Bearing
001448631
0301-BB1-001 Annular Ball Bearing
001448631
030197 Pipe Nipple
002221839
0302670-80 Electrical Plug Connector
011107027
0303-6-6 Tube Nipple
007816089
0303-8-8 Tube Nipple
007976567
030590 Lug Terminal
008253696
030821 Electromagnetic Relay
000819491
030892-002 Hexagon Self-locking Nut
009657092
031-020-02 Tapered Roller Cone And Rollers
001003095
031-030-02 Tapered Roller Cone And Rollers
001003541
031-031-02 Tapered Roller Cone And Rollers
009261379
031-033-02 Tapered Roller Cone And Rollers
007630259
031-1657 Extractor Post Fuseholder
010871951
031-187 Electrolytic Fixed Capacitor
008790123
031-205 Electrolytic Fixed Capacitor
000816159
031-3115-006 Electrical Contact
001901887
Page: 35 ...

Helicopter, Mh-53e

Picture of Mh-53e 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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