Mh-53e Helicopter Parts

(Page 145) End item NSN parts page 145 of 238
Part Number
NSN
NIIN
107617 Lock Washer
001941483
107710 Film Fixed Resistor
002431450
1077100-4 Electrical Plug Connector
009249652
1077100G4 Electrical Plug Connector
009249652
10772 Sleeve Bearing
008195532
1077458-1 Power Autotransforme Transformer
005049090
107907GP1 Shaft Lock
001566559
107947 Drain Cock
002769041
107994-101 Turnlock Fastener Receptacle
002820629
107A-0088 Tube To Boss Elbow
010117736
107A-0114 Tube To Boss Straight Adapter
011564835
107A-236 Pipe To Tube Straight Adapter
007182621
107A-942 Pipe To Boss Straight Adapter
011883184
107A114 Tube To Boss Straight Adapter
011564835
107A6 Pipe To Tube Elbow
002313012
107A88 Tube To Boss Elbow
010117736
107AX Metallic Tube
002033171
107B103M Plastic Dielectr Fixed Capacitor
008352710
107B8160P4 Clinch Self-locking Nut
006849765
107B8224P1 Turnlock Fastener Receptacle
005797825
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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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