Mh-53e Helicopter Parts

(Page 118) End item NSN parts page 118 of 238
Part Number
NSN
NIIN
10159969 O-ring
001675135
10159985 O-ring
005299349
1016 Fluid Filter Element
009860276
10160009 Dust And Moistur Protective Plug
002923292
10160101 Serrated Lock Ring
004057576
10160356 Induct Wire Wound Fixed Resistor
010971627
10160593 Incandescent Lamp
000446914
101624-02 Blind Rivet
000051051
10163202 O-ring
001651938
10163230 O-ring
002500237
10163231 O-ring
002500238
10163237 O-ring
002526051
10163239 O-ring
002635173
10163246 O-ring
002651087
10163271 O-ring
002913274
10163306 O-ring
005421586
10163323 O-ring
007592010
10163324 O-ring
007592022
10163327 O-ring
007605719
10163333 O-ring
008087612
Page: 118 ...

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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