Mh-53e Helicopter Parts

(Page 222) End item NSN parts page 222 of 238
Part Number
NSN
NIIN
13216E6155-2 Liquid Sight Indicator
007783914
13216E6190-3 Tube Elbow
002546449
13216E6190-6 Tube Elbow
002546447
13216E6191 Quick Disconnect Terminal
009260085
13216E6191 Quick Disconnect Terminal
009489686
13216E6191-1 Quick Disconnect Terminal
009489686
13216E6191-2 Quick Disconnect Terminal
009260085
13217E3858 Lug Terminal
001141306
13217E3858-12 Lug Terminal
001141306
13217E3858-5 Lug Terminal
001141311
13217E3858-7 Lug Terminal
005574339
13217E3858-9 Lug Terminal
001155006
13217E4366 Fluid Filter Element
008498358
13217E6704-35 Lug Terminal
001155006
13217E8920FN3 Tube Coupling Nut
000116452
13218E0003-2 Electrical Box Connector
001521072
13218E0098-12 Pipe Reducer
006406330
13218E0098-18 Pipe Reducer
006406330
13218E0135-12 Pipe To Tube Straight Adapter
002891930
13218E0477-7 Gate Valve
002689157
Page: 222 ...

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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