Mh-53e Helicopter Parts

(Page 179) End item NSN parts page 179 of 238
Part Number
NSN
NIIN
116P47494S4 Paper Metallized Fixed Capacitor
003086733
116P47494SA Paper Metallized Fixed Capacitor
003086733
117-057 Voltmeter
001930636
117-21-20-020 Sleeve Bearing
003219243
117-C-69 O-ring
002500222
1170-243-1-0 Plain Seal
011467307
117004-000 Turnlock Fastener Stud
005432418
117030PC740 Pipe Bushing
002783167
11704-2 Tapered Roller Cone And Rollers
006061841
11704-3 Tapered Roller Cone And Rollers
009261379
117054 Electrical Receptacle Connector
010856512
117062-000 Compression Helical Spring
002010272
11728318 Clinch Self-locking Nut
004250402
11728669 Hexagon Plain Nut
002320764
1172896 Paper Dielectric Fixed Capacitor
010891916
11729062 Electrical Contact
008407204
11731114-1 Synchro Clamp
006105044
11731119 Diode Semiconductor Device
000635804
11732653-1 Boot Protective
000049718
117344-002 Stud Terminal
000824890
Page: 179 ...

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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