Mh-53e Helicopter Parts

(Page 34) End item NSN parts page 34 of 238
Part Number
NSN
NIIN
03-006408 Pneumatic Tire Wheel
005287224
03-039522 Swivel Caster
008486017
03-06-2061 Electrical Plug Connector
010476313
03-09-2062 Electrical Plug Connector Body
004935425
03-09-FG-03K Heat Sink-insulator
011220470
03-207265-07 Electrical Wire
010464014
03-5107 Nonmetallic Hose
009335878
03-825-04 Self-aligning Plain Bearing
010069515
030 109 Nonwire Wound Variable Resistor
006435626
030-0065-00 Electrical Plug Connector
009310412
030-0065-01 Electrical Plug Connector
009310412
030-109 Nonwire Wound Variable Resistor
006435626
030-1975-001 Electrical Contact
007587244
030-2064-002 Electrical Contact
010242004
030-2064-010 Electrical Contact
010242004
030-817 Ceramic Dielectr Fixed Capacitor
007880328
030-9542-001 Electrical Contact
001107365
030-9542-001(CTA-CS) Electrical Contact
001107365
0300-12 S Electrical Insulation Sleeving
007564381
0300255 Electrical Special Purpose Cable
011367177
Page: 34 ...

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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