Mh-53e Helicopter Parts

(Page 67) End item NSN parts page 67 of 238
Part Number
NSN
NIIN
0915856-9 Pipe To Tube Straight Adapter
002784592
09160028 Fluid Filter Element
002380033
0919-120 Machine Screw
002349629
0919-141 Machine Screw
004110681
0919430-9 Cotter Pin
008499857
092-20341C004L Flat Washer
013893419
0921-432 Electrical Receptacle Connector
008831977
0925005P006 Induct Wire Wound Fixed Resistor
000610739
0927349-1 Tapered Roller Bearing Cup
001389994
0927350-9 Tapered Roller Cone And Rollers
001389993
0927435 Tapered Roller Cone And Rollers
007630259
0927435-8 Tapered Roller Cone And Rollers
007630259
0928002P009 Nonwire Wound Variable Resistor
007638769
093-00571 Glow Lamp
009513376
093-013 Lug Terminal
001567196
093-3 Lug Terminal
001567196
093-58807-7 Sealing Plug Assembly
009869445
0930679-6 Lubrication Fitting
001720015
0933-201 Sleeve Spacer
005804454
093705 Tapered Roller Cone And Rollers
007630259
Page: 67 ...

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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