Mh-53e Helicopter Parts

(Page 16) End item NSN parts page 16 of 238
Part Number
NSN
NIIN
01-87-7009 Electrical Wire
005786072
01-91180-10850M-2 Indicator Light
005426393
01-91180-2 Indicator Light
005426393
010 508 2 Annular Ball Bearing
005545396
010-004630 Electrical Plug Connector
009329144
010-005413 Electrical Receptacle Connector
010856512
010-005631-002 Electrical Receptacle Connector
011299443
010-0117-00 Clinch Self-locking Nut
000277247
010-0117-03 Clinch Self-locking Nut
008279286
010-11647 O-ring
003431035
01001-392-11 Film Fixed Resistor
011877372
01002919 Flat Washer
008098540
01006-005-01 Transistor
009478263
010063-022 Tubular Rivet
008214995
010063-076 Tubular Rivet
007215245
010079-021 Cartridge Fuse
006696859
01009400 Manual Control Lever
010093814
01009403 Manual Control Lever
010093814
01009404 Manual Control Lever
010093814
0101-2211 Film Fixed Resistor
002431450
Page: 16 ...

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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