Mh-53e Helicopter Parts

(Page 159) End item NSN parts page 159 of 238
Part Number
NSN
NIIN
110236 Tubeaxial Fan
000186535
110238-0039 Electrical Contact
010242004
110238-0401 Electrical Contact
010242004
11024883 Electrical Box Connector
005783643
11024885 Electrical Box Connector
005783666
11024971 Tube Coupling Inverted Nut
002889390
11027GX Tube To Boss Elbow
010117736
11029 Pipe To Tube Elbow
002546215
1102DC Conduit Chase Nipple
002808558
1103/D Electrical Receptacle Connector
009281229
1103089 Ignition Coil
003361702
11031106-1 Tapered Roller Bearing Cup
001000542
110383A Hexagon Head Cap Screw
013510787
110384-154 Wire Wound Fixed Resistor
011855030
1104-00-00 Lock Washer
006163554
1104-00-00-0511 Lock Washer
006163554
11040704-1 Electrical Contact
008122082
11040811-1 Electronic Shielding Gasket
007722223
11043 Muffler- Protective Cap Assembly
004381551
1104443 Annular Ball Bearing
001448519
Page: 159 ...

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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