Mh-53e Helicopter Parts

(Page 126) End item NSN parts page 126 of 238
Part Number
NSN
NIIN
102666EG Electrical Receptacle Connector
010413668
102666Z Electrical Receptacle Connector
005572054
1026859 Nonmetallic Hose
006767936
10276189-5 Headed Straight Pin
000801941
10279494 Electrical Connec Polarizing Key
009989281
1028-12-12S Pipe Coupling
009580384
10282545 Incandescent Lamp
001179957
10284618-6 Electrical Connector Guide
004979051
10287-1 Radio Frequency Power Divider
002615033
10291850 Electrical Contact
000613276
10293117 Tube Coupling Inverted Nut
004346464
1029AS261 Turnlock Fastener Receptacle
006388088
102A10001-10 O-ring
008079638
102A901764 Hexagon Self-locking Nut
000203260
102P11 Paper Dielectric Fixed Capacitor
008375109
103 Tubeaxial Fan
002265872
103 Annular Ball Bearing
005545396
103-0029-00 Connector Adapter
006815013
103-0090-00 Connector Adapter
000539454
103-0109-020 Sleeve Bearing
013548269
Page: 126 ...

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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