Mh-53e Helicopter Parts

(Page 107) End item NSN parts page 107 of 238
Part Number
NSN
NIIN
10122612 Spring Pin
002758263
10122613 Cotter Pin
002857161
10122683 Cotter Pin
006197976
10122714 Headless Straight Pin
008021987
10122726 Headed Straight Pin
008111245
10122737 Headed Straight Pin
008123759
10122753 Spring Pin
008238746
10122756 Spring Pin
008324132
10122786 Spring Pin
008812253
101234 Intake Air Cleane Filter Element
001299757
10123428 Blind Rivet
000689986
10123454 Solid Rivet
001176813
10123468 Solid Rivet
001176839
10123476 Solid Rivet
001176885
10123489 Solid Rivet
001176943
10123490 Solid Rivet
001176945
10123493 Solid Rivet
001176949
10123499 Solid Rivet
001181973
10123542 Solid Rivet
002334781
10123742 Pin-rivet Collar
004894824
Page: 107 ...

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.

Compare Now »
Clear | Hide