Mh-53e Helicopter Parts

(Page 93) End item NSN parts page 93 of 238
Part Number
NSN
NIIN
10086170 Boss Nipple
008259396
10086441 Packing Retainer
008489128
10086588 Gasket
014149436
10086607 O-ring
008460502
10086609 O-ring
010114057
10086610 O-ring
010460628
10086614 O-ring
011071149
10086615 O-ring
011074953
10086619 O-ring
011283955
10086627 Headless Straight Rod
000433723
10086638 Loop Clamp
001930095
10086641 Butt Hinge
002504970
10087143 Film Fixed Resistor
004193894
10087191 Electrical Connector Cover
003872147
10087193 Electrical Plug Connector
006860447
10087227 Lug Terminal
001155004
10087254 Electrical Insulation Sleeving
010444531
10087319 Electrical Special Purpose Cable
010154395
10087325 Electrical Special Purpose Cable
011277181
10087753 Machine Screw
009272068
Page: 93 ...

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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