Mh-53e Helicopter Parts

(Page 146) End item NSN parts page 146 of 238
Part Number
NSN
NIIN
107B8253-46 Headless Straight Pin
006803038
108 Electrical Receptacle Connector
010611483
108-002-1729 Paper Dielectric Fixed Capacitor
006550159
108-0903-001 Tip Jack
007295559
108-1116-3 Turnlock Fastener Stud
005432418
108-16471 Electrolytic Fixed Capacitor
011196166
108-901-03 Tip Jack
007295559
108-903 Tip Jack
007295559
10805-1 Electrical Plug Connector
005005183
10807-002 Setscrew
008208367
108087-08 Electrical Conne Retaining Plate
004083777
108096 Connector Adapter
000539454
1080A18G43 Assembled Washer Plain Nut
006965173
1080A47H52 Tube Tee
002636480
1080DR Refrigerant Gas Leak Detector
011667059
1080H39H26 Control Dial
007218584
1080H80H20 Induct Wire Wound Fixed Resistor
000612089
1080H82H14 Diode Semiconductor Device
000680687
1081 Film Fixed Resistor
001585065
108103-2 Turnlock Fastener Lockspring
002853373
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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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