Mh-53e Helicopter Parts

(Page 128) End item NSN parts page 128 of 238
Part Number
NSN
NIIN
10331328 O-ring
011071149
10332 Hexagon Self-locking Nut
002694040
1033201D Conductor Splice
002717741
10332293 Fluid Filter Element
014352603
10333130 Hexagon Head Cap Screw
000712511
10333733 O-ring
001675171
10334696 Electrical Plug Connector
011961873
103358-2 Plate Self-locking Nut
008207154
10338752 Pipe Plug
002212136
10338993 Packing Retainer
001715048
1033931-10 Nonwire Wound Variable Resistor
007638769
103397 Cotter Pin
008499857
1034 Incandescent Lamp
002951184
1034-D240-11 Spring Pin
008812253
103400 Cotter Pin
002004545
1034107-1 Toggle Switch
011127315
10342235 O-ring
004819987
10343131 O-ring
000517160
103434 Electrical Plug Connector
009329144
1034558-1 Electrical Contact
010856239
Page: 128 ...

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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