Mh-53e Helicopter Parts

(Page 174) End item NSN parts page 174 of 238
Part Number
NSN
NIIN
114798 Pipe To Tube Elbow
002871766
1147AS367-4 Electrical Insulation Sleeving
009441328
1147AS626-3 Electrical Insulation Sleeving
007816826
114855 O-ring
005796495
114973PC408 Pipe Bushing
002783167
114D179-14 Nonmetallic Hose
004509156
114ES247-2 Electric Lantern
005334960
115-0038-001 Spline Plain Nut
008942565
115-00409-2034 Annular Ball Bearing
002274521
115-02413-01 Thyristor Semiconductor Device
004600815
115-0885 Induct Wire Wound Fixed Resistor
009835793
115-10-13 Loop Clamp
005984201
115-1231 Induct Wire Wound Fixed Resistor
000880635
115-1301 Induct Wire Wound Fixed Resistor
008917422
115-1804 Film Fixed Resistor
004805218
115-1857 Film Fixed Resistor
001996864
115-1908 Film Fixed Resistor
002585411
115-2119 Composition Fixed Resistor
010088376
115-2334 Film Fixed Resistor
002893418
115-2465 Composition Fixed Resistor
001550081
Page: 174 ...

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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