Mh-53e Helicopter Parts

(Page 237) End item NSN parts page 237 of 238
Part Number
NSN
NIIN
140460 Annular Ball Bearing
005545396
14047 Lock Washer
005146674
14050-007 Cartridge Fuse
010587648
1406AS720-3 Electrical Insulation Sleeving
000896041
1407-472-G Film Fixed Resistor Network
010938423
14076294 Toggle Switch
009788805
1408-4-45 Tube To Boss Elbow
005852309
1408M76P65 Pipe To Tube Straight Adapter
008367807
141 Vehicular Stop Light-taillight
008397461
141-0002-0001 Electrical Receptacle Connector
002232848
141-001-0317 Diode Semiconductor Device
007525701
141-0076 Cartridge Fuse
002407957
141-16612 Pipe To Hose Straight Adapter
005682200
141-7 Terminal Board
009836085
1410 STANDARD Universal Joint Parts Kit
007024578
1410-0023 Annular Ball Bearing
002938120
14100-001 Electrical-electron Mounting Pad
010281168
14101-005LC14RD Light Lens
007532834
14118-018 Glow Lamp
000142870
1412731000 O-ring
001651968
Page: 237

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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