Mh-53e Helicopter Parts

(Page 78) End item NSN parts page 78 of 238
Part Number
NSN
NIIN
10-150921-123 Receptacle Dummy Connector
001684484
10-189002-202 Electrical Contact
008475535
10-189002-20F1 Electrical Contact
008475535
10-1948-28 Tube To Boss Straight Adapter
001257922
10-214220-04P Electrical Receptacle Connector
010853305
10-214220-04S Electrical Receptacle Connector
011449154
10-214220-19P Electrical Receptacle Connector
012349645
10-214224-10P Electrical Receptacle Connector
011347745
10-214228-16S Electrical Receptacle Connector
012290135
10-214516S-1P Electrical Plug Connector
010506586
10-214517-11S Electrical Plug Connector
006247660
10-243484-47 Induct Wire Wound Fixed Resistor
000803218
10-247116-103 Plastic Dielectr Fixed Capacitor
008352710
10-257937-103 Electrical Connector Cover
009592610
10-263999-143 Receptacle Dummy Connector
009471036
10-291759-103 Plastic Dielectr Fixed Capacitor
008352710
10-302-11-05 Stud Terminal
009260033
10-302-3-05 Stud Terminal
009260033
10-30335 Pipe Plug
001883509
Page: 78 ...

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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