Mh-53e Helicopter Parts

(Page 182) End item NSN parts page 182 of 238
Part Number
NSN
NIIN
118084 Glass Dielect Variable Capacitor
005819197
118100 IT99 Circuit Breaker
008769216
11817-35 Pipe To Tube Elbow
002871766
118170-690 Radio Frequency Detector
008777148
118212-001 Radio Frequency Transmiss Switch
000052503
118226PC748 Pipe Bushing
002783167
118230PC748 Pipe Bushing
002783167
118270-1 Circuit Breaker
008769216
118271 Ceramic Dielectr Fixed Capacitor
005831997
118279 Keyer Group Adapter
006148008
118293 Plain Tapered Pin
001873216
11830621-160 Electrical Insulation Sleeving
008222775
11830621-163 Electrical Insulation Sleeving
009441328
11830621-165 Electrical Insulation Sleeving
007816826
11830708 Manual Control Lever
003554459
11830709 Electrical Contact
010242004
11830764-1 Ceramic Dielectr Fixed Capacitor
007880328
11838508-1 Airframe Ball Bearing
006215240
11842-302J Induct Wire Wound Fixed Resistor
011779465
11849-0006 Clinch Self-locking Nut
010904865
Page: 182 ...

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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