Mh-53e Helicopter Parts

(Page 149) End item NSN parts page 149 of 238
Part Number
NSN
NIIN
108608 Hexagon Head Cap Screw
000187069
108633-303 Hexagon Self-locking Nut
008150653
10863416-1 Weapon System Resilient Mount
005728604
10874976 Pipe To Hose Straight Adapter
007225194
10876 Governor Housing Assembly
001047381
10884 Sleeve Bearing
000943552
10884Y Sleeve Bearing
000943552
10886307 Extension Helical Spring
008277077
108898 Electrical Wire
005786072
1088Z164 Electrical Engine Starter
011350091
108903BLACK Tip Jack
007295559
10894 Thrust Roller Bearing
001170754
108993-27 Film Fixed Resistor
011771905
108994-27 Film Fixed Resistor
011751520
108994-76 Film Fixed Resistor
011877463
108995-14 Film Fixed Resistor
011877374
108A23S20 Pipe To Tube Straight Adapter
002028470
109 Electrical Receptacle Connector
000683546
109-46-14 Electrical Card Holder
009349941
109-8307 O-ring
010902741
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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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