Mh-53e Helicopter Parts

(Page 15) End item NSN parts page 15 of 238
Part Number
NSN
NIIN
00P00000-1524 Annular Ball Bearing
005543468
01 Electronic Shielding Gasket
000684328
01-005184-203 Annular Ball Bearing
001089247
01-005184-205 Annular Ball Bearing
001091157
01-005184-305 Annular Ball Bearing
001448519
01-005248-330 Annular Ball Bearing
001089247
01-009400 Manual Control Lever
010093814
01-01-0008 Electrolytic Fixed Capacitor
008790123
01-0296 ITEM NO 56 Machine Bolt
002258511
01-06287 Hand Driven Hydraulic Ram Pump
012719831
01-1031 Tip Jack
007295559
01-1060 Knob
007621489
01-115769 Retaining Ring
007217680
01-117702 Cartridge Fuse
006869204
01-159125 O-ring
002913274
01-2560-1-0210 Connector Adapter
000539454
01-50002 Transistor
004360953
01-65-7009 Electrical Wire
005786072
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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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