Mh-53e Helicopter Parts

(Page 192) End item NSN parts page 192 of 238
Part Number
NSN
NIIN
1209104 Annular Ball Bearing
005543468
1209162-2 Electrical Plug Connector
000018645
12092 Electrical Plug Connector
000670032
12093 Push Switch
001328368
1209403 Tubeaxial Fan
000953831
120A1537 Jack Part Kit
012061709
120B Pipe Coupling
004153172
120B1-8X1-8 Pipe Coupling
004153172
120PC Time Totalizing Meter
010051885
121-003 Ceramic Dielectr Fixed Capacitor
008056630
121-0202-001 Electrical Receptacle Connector
007553447
121-0576-6 Non Wire Wound Variable Resistor
010489167
121-206 Machine Bolt
009409079
121-31-20-019 Plug-in Electronic Compon Socket
002229828
121-39-21-016 Plug-in Electronic Compon Socket
002229828
121-39-22-011 Plug-in Electronic Compon Socket
002229828
1210 Wire Braid
001705274
1210 Cable Strain Relief Bushing
002464906
Page: 192 ...

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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