Mh-53e Helicopter Parts

(Page 119) End item NSN parts page 119 of 238
Part Number
NSN
NIIN
10163366 O-ring
010431419
10163372 O-ring
010886108
10163382 O-ring
011074956
10163383 O-ring
011074958
10163384 O-ring
011101412
10163400 O-ring
011233299
10163553 Electrical Connector Backshell
011865611
10163729 Annular Ball Bearing
001861104
10163822 Flat Washer
001670830
10163853 Preformed Packing
011750713
10163865 O-ring
002500222
10163879 O-ring
006311346
10163885 O-ring
010460629
10163891 O-ring
011311896
10163996 Composition Fixed Resistor
004935249
10164-10 Pipe To Boss Straight Adapter
001969580
10164094 Electrolytic Fixed Capacitor
011194307
10165-10 Pipe To Tube Elbow
001869964
1016510 Pipe To Tube Elbow
001869964
10172712 Hexagon Self-locking Nut
004492378
Page: 119 ...

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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