Mh-53e Helicopter Parts

(Page 142) End item NSN parts page 142 of 238
Part Number
NSN
NIIN
10653083 Diode Semiconductor Device
009047496
10653103 Diode Semiconductor Device
007525701
1065492-001 Diode Semiconductor Device
008548470
10657401 Electrical Contact
003389879
10658399 Incandescent Lamp
009267603
106616 Transistor
001629773
10663160-001 Fluid Filter Head
010793494
1066445-1 Multiple Electron Tube Shield
008070273
1066466-5 Ceramic Dielectr Fixed Capacitor
011273762
1066620-1 Glow Lamp
000142870
106665-01 Diode Semiconductor Device
010554350
10668633-038 Film Fixed Resistor
001530178
10668633-223 Film Fixed Resistor
000046078
10668673 Electrical-electron Mounting Pad
010559501
10669451 Electrical Connec Polarizing Key
009989281
10670343 Electrical Receptacle Connector
013122496
10672085-034 Electrolytic Fixed Capacitor
000096747
10673229-9 Diode Semiconductor Device
001067189
106751-04-163C Machine Screw
007808456
10678 Plastic Dielectr Fixed Capacitor
006327554
Page: 142 ...

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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