Mh-53e Helicopter Parts

(Page 51) End item NSN parts page 51 of 238
Part Number
NSN
NIIN
065-001756-052 Electrical Insulation Sleeving
009596336
065-98-00002 Electrical Contact
000613276
06530 Hose Clamp
012733671
0656303 Machine Bolt
002264826
0658415 Pipe Bushing
001871413
0659050182 Electrical Conduit Coupling Nut
002803311
0665258-0501 Power Transformer
008662486
06693A Annular Ball Bearing
001448519
067-65-541355 Tapered Roller Cone And Rollers
006061841
067916 Annular Ball Bearing
001448519
068-0155-000 Annular Ball Bearing
005545396
068-1055-000 Annular Ball Bearing
005545396
068149 Tapered Roller Cone And Rollers
007630259
0683-1565 Composition Fixed Resistor
001048374
0683175C60 Film Fixed Resistor
002851157
0683175C76 Film Fixed Resistor
001923488
0686-0515 Composition Fixed Resistor
001048372
0687-1251 Composition Fixed Resistor
001114732
0689-0275 Composition Fixed Resistor
004854564
068950-0002 Electronic Equipmen Hardware Kit
010572216
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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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