Mh-53e Helicopter Parts

(Page 194) End item NSN parts page 194 of 238
Part Number
NSN
NIIN
121432153 Film Fixed Resistor
001862212
1214448 Pitot-static Tube
005267852
1214528-201 Electrical Contact
007641923
121464-4 Hose Clamp
000151418
1214913-201 Electrical Power Cable Assembly
010867960
1214AS122-3 Turnlock Fastener Receptacle
000369305
1215-2C24D Electromagnetic Relay
000678582
121601 Fluid Filter Element
002871912
121645 Serrated Lock Ring
002819224
1216E3164 Pipe To Tube Elbow
002634976
1217 Incandescent Lamp
001433159
1217-106 Tapered Roller Bearing Cup
001000603
1217026-201 Electrical Receptacle Connector
004930497
12177 Bearing Ball
001006147
1217743-201 Radio Frequency Power Divider
002615033
1218-261 O-ring
005796495
1218115H1 Engine Generator Regulator
011964882
1219-3150-C3Y Turnlock Fastener Lockspring
002853373
1219-3150-Z3CT Turnlock Fastener Lockspring
002853373
12194-005 Diode Semiconductor Device
001973524
Page: 194 ...

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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