Mh-53e Helicopter Parts

(Page 168) End item NSN parts page 168 of 238
Part Number
NSN
NIIN
1126B06C-25 Paper Dielectric Fixed Capacitor
003682269
1127-23-268 Electrical Plug Connector
006860447
1127701 Turnlock Fastener Receptacle
005054798
1127723 Split Washer
006397435
11280 Incandescent Lamp
008362079
1128000-4 Turnlock Fastener Stud Assembly
005231376
11283B SOLDER Stud Terminal
000795760
1129-0007 Abrasive Wheel
002251955
1129-0007-P10 Abrasive Wheel
002251955
11293264 Radio Frequency Detector
008777148
112991 Nonmetallic Hose
006767936
1129E01 FIND 41 Hexagon Head Cap Screw
009474354
1129E01 ITEM 154 Hexagon Head Cap Screw
009474354
1129E01 ITEM 186 Hexagon Head Cap Screw
000712074
112B Pipe Nipple
002221837
112B1-2NPT Pipe Nipple
002221839
112B1-4 Pipe Nipple
002221837
112B1-4NPT Pipe Nipple
002221837
112E315 Annular Ball Bearing
001448519
112HMS20 Plain Encased Seal
008087595
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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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