Mh-53e Helicopter Parts

(Page 72) End item NSN parts page 72 of 238
Part Number
NSN
NIIN
1-012-0410 Diode Semiconductor Device
000454196
1-01264D6 Tube To Boss Straight Adapter
002776836
1-0133 Connector Adapter
001054642
1-015-1140 Transistor
000681985
1-015-1156 Transistor
004974280
1-015-1157 Thyristor Semiconductor Device
001063698
1-015-1158 Transistor
001629773
1-021-0120 Diode Semiconductor Device
001704430
1-021-0410 Diode Semiconductor Device
000454196
1-115266ISSUE1 Cable Strain Relief Bushing
003516114
1-115769 Retaining Ring
007217680
1-117702 Cartridge Fuse
006869204
1-117802-1003 Film Fixed Resistor
001315807
1-119960 Electrolytic Fixed Capacitor
009549830
1-119996 Composition Fixed Resistor
001411073
1-128182-1004 Film Fixed Resistor
001892454
1-128182-100R0 Film Fixed Resistor
004267133
1-128182-2002 Film Fixed Resistor
001956377
1-128182-5101 Film Fixed Resistor
001420931
1-128182-5600 Film Fixed Resistor
001127056
Page: 72 ...

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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