Mh-53e Helicopter Parts

(Page 87) End item NSN parts page 87 of 238
Part Number
NSN
NIIN
100289-201 Non Wire Wound Variable Resistor
010674616
10031-8 Loop Clamp
003378642
10031085-102 Electrical Contact
000096413
1003289-01 Electr Receptacle Connector Body
010144826
1003293-05 Electrical Connector Backshell
010144920
1003294-01 Electr Receptacle Connector Body
010234872
10034 Tapered Roller Cone And Rollers
008278646
1003951-01 Optoelectronic Coupler
010826031
1004048-03 Electrical Contact
000096413
100412 Diode Semiconductor Device
007526115
100413 Diode Semiconductor Device
001973524
10041561 Electrical Contact
000796624
100417-20 Stud Terminal
009260033
10042DAPW Electrical-electron Mounting Pad
010791174
1004355 Panel Light
009232425
100443-001 Transistor
001629773
10044510-4 Cap Self-locking Nut
000108385
1004471J7 Electrical Receptacle Connector
004930497
10045027 Bearing Ball
000442269
10047-561 Electrical Box Connector
002807763
Page: 87 ...

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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