Mh-53e Helicopter Parts

(Page 88) End item NSN parts page 88 of 238
Part Number
NSN
NIIN
10047-691-1213 Film Fixed Resistor
004193694
10047-691-2742 Film Fixed Resistor
004320409
10047-691-3322 Film Fixed Resistor
007584795
10047-709 Induct Wire Wound Fixed Resistor
002586955
10047-748 Nonwire Wound Variable Resistor
001074881
100476 Cable Assembly
001096133
1005-08 Nonmetallic Hose
000670454
1005-721 Spring Pin
008238746
1005-726-5593 Machine Screw
001509212
1005000041 Electrical-electron Mounting Pad
001400366
1005006860447 Electrical Plug Connector
006860447
100505-33P Fluid Filter
013201666
10050635 Turnlock Fastener Receptacle
008502240
10051537-3 Electrical Connector Retainer
000738885
10051572 Electrical Plug Connector
006831872
10051758 O-ring
008331428
10052 Electrical Receptacle Connector
004783338
1005218-003 Electrical Wire
007257091
1005218-010 Electrical Wire
006430645
100534 Tube To Hose Straight Adapter
008815536
Page: 88 ...

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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