Mh-53e Helicopter Parts

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Part Number
NSN
NIIN
004071 Connector Adapter
007012215
01-2560-1-0210 Connector Adapter
000539454
042-20063-013 Connector Adapter
010444448
04250416201850 Connector Adapter
007012215
052493 Connector Adapter
004021153
05B0716G01 Connector Adapter
009514231
0SM20200-1 Connector Adapter
004921954
0SM209SF Connector Adapter
003376770
0SM21051 Connector Adapter
004021153
1-0133 Connector Adapter
001054642
1-891-1 Connector Adapter
005390203
1000-0133 Connector Adapter
001054642
1002-0001 Connector Adapter
007012215
10135444 Connector Adapter
003376770
10145222 Connector Adapter
001054642
1026-0001 Connector Adapter
007167124
103-0029-00 Connector Adapter
006815013
103-0090-00 Connector Adapter
000539454
1040B9146-0001 Connector Adapter
003376770
1040B9146-1 Connector Adapter
003376770
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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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