Mh-53e Helicopter Parts

(Page 45) End item NSN parts page 45 of 238
Part Number
NSN
NIIN
050981-0001 Induct Wire Wound Fixed Resistor
000805899
051-043-0000 Electrical Receptacle Connector
009281229
051-043-0000220 Electrical Receptacle Connector
009281229
051-15100-45 Paper Dielectric Fixed Capacitor
001296260
0510-0034 Retaining Ring
006804619
051001 V Belt
005284287
051001-0000 V Belt
005284287
051111 Tapered Roller Bearing Cup
001000359
051112 Tapered Roller Cone And Rollers
001000744
05111422 Sleeve Bearing
005899414
05114335 Plain Encased Seal
002825906
051145 Needle Roller Bearing
002273244
051162 Annular Ball Bearing
001091157
05135268 Arm Assembly
009669103
05142266 Plain Encased Seal
000798421
05146680 Liquid Level Gage Rod
010659663
05147345 Headed Straight Pin
002519989
05177769 Lock Washer
002091543
05180250 Plain Solid Disk
007929020
05189294 Tube To Hose Straight Adapter
004462584
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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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