Mh-53e Helicopter Parts

End item NSN parts
Filter By: Fixed Attenuators
page 1 of 1
Part Number
NSN
NIIN
10-10 Fixed Attenuator
007210255
146457-004 Fixed Attenuator
011752970
18N-20 Fixed Attenuator
004546924
18N-20-436 Fixed Attenuator
004546924
2-20 Fixed Attenuator
004546924
2-20N Fixed Attenuator
004546924
2-40 Fixed Attenuator
010143464
20620-20 Fixed Attenuator
011752970
2082-4156-20 Fixed Attenuator
011577870
2082-6043-20 Fixed Attenuator
011752970
4201-1001 Fixed Attenuator
011752970
46020-0000-0857 Fixed Attenuator
011752970
4782-20 Fixed Attenuator
011752970
4T-10.0 Fixed Attenuator
011577870
4T-20 Fixed Attenuator
011752970
50HF-020-N Fixed Attenuator
004546924
50MP20-944 Fixed Attenuator
004546924
5729-20 Fixed Attenuator
004546924
690.8647 Fixed Attenuator
011577870
6908647 Fixed Attenuator
011577870
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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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