Mh-53e Helicopter Parts

(Page 58) End item NSN parts page 58 of 238
Part Number
NSN
NIIN
0727-0214 Film Fixed Resistor
005132956
07281-00549 Hose Clamp
012733671
073-5347 Tapered Roller Bearing
001005301
074-20017-004A Diode Semiconductor Device
001704430
0740655 Lubrication Fitting
001720031
0740680 Socket Head Cap Screw
009789384
0740682 Socket Head Cap Screw
009836660
0740712 Cotter Pin
005760421
0740750 Electrical Plug Connector
011771287
0740777 Machine Screw
006229486
0740861 Hexagon Head Cap Screw
002693239
0740883 Electrical Plug Connector
010506586
0741-55-500HMSP0RM5P Induct Wire Wound Fixed Resistor
000612089
074452 Incandescent Lamp
000193093
0757-0088 Film Fixed Resistor
007212387
0757-0095 Film Fixed Resistor
001420931
0757-0126 Film Fixed Resistor
006891966
0757-0143 Film Fixed Resistor
004320467
0757-0162 Film Fixed Resistor
001318907
0757-0338 Film Fixed Resistor
002524003
Page: 58 ...

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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