Mh-53e Helicopter Parts

(Page 157) End item NSN parts page 157 of 238
Part Number
NSN
NIIN
110-0005-055 Film Fixed Resistor
001892474
110-0005-070 Film Fixed Resistor
001381285
110-0005-075 Film Fixed Resistor
000255988
110-011-2448 Composition Fixed Resistor
004004482
110-0309-001 Film Fixed Resistor Network
010517994
110-045-22 Turnlock Fastener Receptacle
000369305
110-045-3 Turnlock Fastener Receptacle
000369305
110-098-1C Tube To Boss Tee
007571945
110-408 Alternator Assembly
001500038
110-412 Alternator Assembly
001500038
110-499-1 Film Fixed Resistor
004320420
110-5 Packing With Retainer
008059386
110-6752 Tube Coupling Inverted Nut
000137397
110-93-324 Plug-in Electronic Compon Socket
012516711
110-B 1/2X1/8 Pipe Bushing
002783885
110-B-08X02 Pipe Bushing
002783885
110-B-12X08 Pipe Bushing
002783167
110-DA Pipe Bushing
002783885
1100 4921 Fluid Filter Element
002380033
1100-9-2B Spring Pin
008437988
Page: 157 ...

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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