Mh-53e Helicopter Parts

(Page 20) End item NSN parts page 20 of 238
Part Number
NSN
NIIN
012225004 Ceramic Dielectr Fixed Capacitor
012485659
01224813 Intake Air Cleane Filter Element
001299757
01228340-0001 Tapered Roller Cone And Rollers
009261379
01251-0463 Tip Jack
007295559
01251-1016 Electrical Receptacle Connector
008121188
01251-1313 Electrical Contact
000613276
01251-1326 Electrical Receptacle Connector
007553447
0126-R1K0899-1R1K Film Fixed Resistor Network
010829493
0126210-1 Turnlock Fastener Receptacle
000369305
0128-13 Nonmetallic Grommet
002764205
01283530 Fire Equipment Nozzle
012869772
0128392 Turnlock Fastener Receptacle
005054798
013-004-001 Electrical Connector Backshell
012451950
013-13029-1 Thyristor Semiconductor Device
000089784
013-3130-00 Pneumatic Tank Valve
000429536
013-3130-000 Pneumatic Tank Valve
000429536
013-461 Diode Semiconductor Device
008469125
01308 Electrical Power Cable
006351187
01308-15 Electrical Power Cable
006351187
0132 Glow Lamp
000142870
Page: 20 ...

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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