Mh-53e Helicopter Parts

(Page 9) End item NSN parts page 9 of 238
Part Number
NSN
NIIN
004071 Connector Adapter
007012215
0040896 Gasket
005510433
0040896-3 Gasket
005510433
0043809 Tapered Roller Bearing Cup
001000603
004467 Electrical Receptacle Connector
008388470
0045319283 Electrical Connector Retainer
000738885
0046903055 Transistor
004974280
0047737 Fluid Filter Element
002380033
0048737 Tapered Roller Bearing Cup
001000594
005-000925 Tubular Rivet
008214995
005-000942 Tubular Rivet
008660562
005-000951 Tubular Rivet
008260329
005149-000 Extractor Post Fuseholder
000181450
005154T Helical Gear
005370153
00519255 Push Switch
001118619
00519449-0001 Pressure Transmitter
004067377
0052-00-000-0106 Fluid Filter Element
010228183
005256 Transistor
009052926
00543102-0032 Tapered Roller Cone And Rollers
006061841
00543102-0033 Tapered Roller Cone And Rollers
001003541
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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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