Mh-53e Helicopter Parts

(Page 6) End item NSN parts page 6 of 238
Part Number
NSN
NIIN
001941T Nonmetallic Hose
010252309
001965 Pressure Transmitter
005267864
002-003123 Clinch Self-locking Nut
008279286
002-003238 Clinch Self-locking Nut
007206591
002-003645-011 Hexagon Self-locking Nut
000796474
002-004048-006 Hexagon Self-locking Nut
000203260
002-004048-011 Hexagon Self-locking Nut
000509372
002-004095 Clinch Self-locking Nut
009349973
002-004261-003 Clinch Self-locking Nut
010156873
002-004261-004 Clinch Self-locking Nut
006825993
002-004261-006 Clinch Self-locking Nut
010904865
00205-0246 Pipe To Tube Straight Adapter
004418700
002107T Fuel Injector Holder
008331000
002121T Injector Rack
001269712
00213-0205 Tapered Roller Cone And Rollers
006061841
00213-1011 Tapered Roller Bearing Cup
001000542
002131T Metal Tube Assembly
000202733
002133T Nonmetallic Hose
010748373
002177T Pipe To Tube Straight Adapter
005402612
0022-074 Turnlock Fastener Eyelet
002822045
Page: 6 ...

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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