Mh-53e Helicopter Parts

(Page 183) End item NSN parts page 183 of 238
Part Number
NSN
NIIN
118515-001 Pneumatic Tank Valve
000429536
118536 Drain Cock
002769041
1187-0400 Lock Washer
006163554
118757 Pipe To Tube Elbow
002546215
1188 Diode Semiconductor Device
007525701
118830PC740 Pipe Bushing
002783167
11888 Electromagnetic Relay
000819491
1189-ATL Electrical Contact
010398438
1189AT Electrical Contact
010398438
118P10592S1 Paper Metallized Fixed Capacitor
001707170
118P2249254 Paper Dielectric Fixed Capacitor
006550159
118P22492S2 Paper Dielectric Fixed Capacitor
006550159
118P22492S4 Paper Dielectric Fixed Capacitor
006550159
118P4740254 Paper Metallized Fixed Capacitor
001489365
118P47402S2 Paper Metallized Fixed Capacitor
001489365
118P965 Paper Dielectric Fixed Capacitor
006550159
118S113 Clevis Bolt
001511971
118S114 Clevis Bolt
001511972
118UC57 Transistor
009249611
119-00-05-008 Sleeve Bearing
006258475
Page: 183 ...

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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