Mh-53e Helicopter Parts

(Page 220) End item NSN parts page 220 of 238
Part Number
NSN
NIIN
13207E2942FN53 Electrical Wire
005786593
13207E2948FN1 Electric Temperature Transmitter
008145271
13207E3105 Tapered Roller Cone And Rollers
009261379
13207E3235FN45 S Chain Hook
002705436
13207E3301FN33 Retaining Ring
005307968
13207E3301FN4 Hexagon Head Cap Screw
007247224
13207E3409FN86 Headed Straight Pin
008258353
13207E3410FN156 Hexagon Plain Nut
008807745
13207E5347-2 Quick Disconnect Terminal
009260085
13207E5347-6 Quick Disconnect Terminal
009260085
13207E5471FN53 Machine Bolt
002258511
13207E5471FN88 Hexagon Head Cap Screw
002258507
13207E6761FN11 Hexagon Head Cap Screw
007262551
13207E6761FN48 Cotter Pin
008457787
13207E6761FN98 Flat Washer
009517209
13207E7300FN52 Hexagon Plain Nut
008421190
13207E7300FN61 Headed Straight Pin
009577056
13208E0324 Liquid Sight Indicator
007911419
13208E6819-6 Tube To Hose Straight Adapter
003746954
1320938 Pressure Switch
005034884
Page: 220 ...

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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