Mh-53e Helicopter Parts

(Page 112) End item NSN parts page 112 of 238
Part Number
NSN
NIIN
10131800 Electrical Receptacle Connector
010611483
10131813 Electrical Receptacle Connector
001621543
10131951 Electrical Connector Cable Clamp
011816652
10131957 Electrical Connector Cable Clamp
011794832
10131971 Electrical Connector Cable Clamp
004440249
10132134 Lug Terminal
005574343
10132137 Lug Terminal
001912714
10132142 Lug Terminal
002571262
10132155 Lug Terminal
001141306
10132187 Lug Terminal
005044703
10132666 Electromagnetic Relay
012076456
10133-3 Ceramic Dielectr Fixed Capacitor
008056630
10133028 Thyristor Semiconductor Device
000089784
10133031 Diode Semiconductor Device
000487106
10133037 Transistor
001048441
10133046 Diode Semiconductor Device
001724970
10133047 U Semiconductor Device Rectifier
001851824
10133050 Thyristor Semiconductor Device
001954094
10133064 Diode Semiconductor Device
003243085
10133090 Transistor
004601034
Page: 112 ...

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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