Mh-53e Helicopter Parts

(Page 84) End item NSN parts page 84 of 238
Part Number
NSN
NIIN
1001-056-A002 Electrical Plug Connector
001649719
1001056A002-000 Electrical Plug Connector
001649719
100111-271 Film Fixed Resistor
010586429
100111-512 Film Fixed Resistor
011387889
10012 Hose Clamp
005551352
10012612 Fuel Screen
003158305
1001277-0404 Tube To Hose Straight Adapter
010878886
1001277-1212 Tube To Hose Straight Adapter
008815536
1001277-16 Tube To Hose Straight Adapter
009291107
10013274-1 Serrated Lock Ring
004057576
10013281 Fluid Filter Element
008498358
100139-002 Quick Disconnect Terminal
009489686
10014-01 Film Fixed Resistor
000386136
100140-193 Electrical Receptacle Connector
010413668
100140-195 Electrical Receptacle Connector
010413668
10015-29 Film Fixed Resistor
001392146
10015-79 Film Fixed Resistor
004320408
10015-99 Film Fixed Resistor
004315161
1001531-2REVA Non Wire Wound Variable Resistor
010489167
10015316-003 Pin-rivet
005310744
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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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