Ch-53a/d/e Helicopter Parts

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Part Number
NSN
NIIN
033-0090-0001 Connector Adapter
006156889
1-891-1 Connector Adapter
005390203
10556107 Connector Adapter
004916302
1891-1 Connector Adapter
005390203
20AS111-1 Connector Adapter
005390203
229316 Connector Adapter
004916302
30-060-1B Connector Adapter
005390203
33-90 Connector Adapter
006156889
357-9335-00 Connector Adapter
006156889
357-9335-000 Connector Adapter
006156889
40-702-13 Connector Adapter
005390203
58A5A89-1 Connector Adapter
005390203
6166817 Connector Adapter
004916302
6951-1 Connector Adapter
005390203
70-101-1 Connector Adapter
004916302
7168-1 Connector Adapter
004916302
9115C1056 Connector Adapter
004916302
A101-891 Connector Adapter
005390203
FB-6-B Connector Adapter
005390203
FB-6-B59 Connector Adapter
005390203
Page:

Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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