Mh-53e Helicopter Parts

(Page 207) End item NSN parts page 207 of 238
Part Number
NSN
NIIN
128631-004 Machine Screw
000598249
1287-200OHM Non Wire Wound Variable Resistor
010674616
12873193 Pipe To Tube Elbow
008353003
1287424PC2 Hexagon Self-locking Nut
008150653
1287470-11 Annular Ball Bearing
007739554
1287472-4 Annular Ball Bearing
000732640
1287674PC25 Annular Ball Bearing
008123603
1287742-6 Hexagon Self-locking Nut
000203260
128806 Paper Dielectric Fixed Capacitor
010891916
12881-1 Spring Adjustment Lever
012204456
128834-8 Cartridge Fuse
001671391
12890-B-4 Stud Terminal
000795760
12890-B-4-5 Stud Terminal
000795760
12890-B-4.5 Stud Terminal
000795760
128935 Annular Ball Bearing
002938120
12897-60002 Cable Assembly
010823092
128C583H02 Electrical Contact
000684270
128C583H07 Electrical Contact
009699270
128C603BC009 Machine Screw
007808456
128C693H01 Annular Ball Bearing
006792598
Page: 207 ...

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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