Mh-53e Helicopter Parts

(Page 68) End item NSN parts page 68 of 238
Part Number
NSN
NIIN
093706 Tapered Roller Cone And Rollers
009261379
09394 Composition Fixed Resistor
000052867
094012-KI Electrical Contact
011089214
094434-0000 Loop Clamp
002907273
0979207# Dial Indicating Pressure Gage
010462524
099-113 O-ring
011074951
099060 Film Fixed Resistor
001941691
0995468 Electrical Receptacle Connector
008388470
09B9251B Tube Coupling Nut
000116452
09F3602 Diode Semiconductor Device
005774345
09NE-101/MONEL/ Hexagon Self-locking Nut
010046946
09NE-1011 Hexagon Self-locking Nut
010046946
09NE101 Hexagon Self-locking Nut
010046946
09P222219-1 Plug-in Electronic Compon Socket
004778167
09P226565-17 Electrical Contact
008784714
0A1243 Clinch Self-locking Nut
006849765
0A172AP-11-1TB Tubeaxial Fan
011052015
0A388967-1 Machine Screw
009646032
0AK Thrust Ball Bearing
001008515
0BL118 Composition Fixed Resistor
001168565
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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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