Mh-53e Helicopter Parts

(Page 61) End item NSN parts page 61 of 238
Part Number
NSN
NIIN
07A568-128N O-ring
011283955
07A568-130N O-ring
011132083
07D03 Regu Diaphragm Assembly
004491445
08-009-0001 Tip Jack
007295559
08-0201 Knitted Wire Mesh
006016266
08-0301-0184 Electronic Shielding Gasket
000684328
08-203429 Hexagon Plain Nut
008421190
08-49003-21 Composition Fixed Resistor
001145352
08-49004-69 Film Fixed Resistor
004520764
08-49162-04 Nonwire Wound Variable Resistor
001074881
08-49163-04 Nonwire Wound Variable Resistor
001074881
08-50-0105 Electrical Contact
010357465
08-50-0106 Electrical Contact
010357465
08-56-0110 Electrical Contact
011328789
08-83283-155 Indicator Light
005017278
08-83283-82 Indicator Light
005426393
08-83283-88 Indicator Light
005017278
080-04273-2 O-ring
011074956
080-04273-21 O-ring
010463299
080-58532-8 O-ring
010460628
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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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