Mh-53e Helicopter Parts

(Page 28) End item NSN parts page 28 of 238
Part Number
NSN
NIIN
020-0067-000 Tapered Roller Cone And Rollers
006061841
020-11307 O-ring
007605719
020-42984-48 Filter Orifice Assembly
001368159
0200-51100 Setscrew
004625407
02000-4611 Electric Temperature Transmitter
008145271
02000005426 Universal Joint Parts Kit
007024578
0201002-9 Incandescent Lamp
001680411
020161 Tubeaxial Fan
005297463
020189 Tubeaxial Fan
000186535
0202-16-16 Pipe Coupling
008044616
020404 Vaneaxial Fan
000431981
0205618 Electrical Special Purpose Cable
010497503
0206503-00 Headed Straight Pin
002179576
0209-2103 Electrical Contact
006263538
0209894-5 Tapered Roller Cone And Rollers
001000233
0209987-7 Tapered Roller Bearing Cup
001000359
021-12109 Extended Washer Self-locking Nut
002726423
021-18718 Hexagon Self-locking Nut
002453419
021-26698-010 Nozzle Block Assembly
012228082
021-26698-10 Nozzle Block Assembly
012228082
Page: 28 ...

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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