Mh-53e Helicopter Parts

(Page 108) End item NSN parts page 108 of 238
Part Number
NSN
NIIN
10123743 Blind Rivet
004902237
10123768 Blind Rivet
005504791
10123775 Solid Rivet
005583824
10123814 Solid Rivet
007215208
10123815 Solid Rivet
007215210
10123820 Tubular Rivet
007215245
10123833 Solid Rivet
007540991
10123844 Blind Rivet
008006275
10123861 Tubular Rivet
008214995
10123876 Tubular Rivet
008660562
10123902 Blind Rivet
009375448
10123908 Solid Rivet
009739067
10124038 Blind Rivet
010861142
10124068 Solid Rivet
011196435
10124178-114 Dust And Moistur Protective Plug
012820812
10124312 Socket Head Cap Screw
000685407
101246 Intake Air Cleane Filter Element
009793806
10124912 Machine Screw
000572694
10124913 Machine Screw
000573800
10124921 Socket Head Cap Screw
000582067
Page: 108 ...

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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