Mh-53e Helicopter Parts

(Page 96) End item NSN parts page 96 of 238
Part Number
NSN
NIIN
101-36-6 Clinch Self-locking Nut
000710199
101000022 Diode Semiconductor Device
009047496
101000032 Diode Semiconductor Device
011125544
101000051 Transistor
009466635
101000052 Transistor
001240117
101000094 Transistor
001629773
101000242 Diode Semiconductor Device
000487106
10100207 Diode Semiconductor Device
011879137
10101182-101 Composition Fixed Resistor
001550081
10101394-279 Film Fixed Resistor
001386996
10103635 Time Meter Split Mounting Flange
002588547
10103AS Extension Ladder
010921894
101045 Annular Ball Bearing
005545396
10104610 Filler Opening Cap
003072780
10104DAP Electrical-electron Mounting Pad
011987078
10105 19-3 Electrical Insulation Sleeving
000631495
10105368 Electrical Box Connector
002961669
10105489-1 Electrical Cable Nipple
005031440
10105719-4 Electrical Insulation Sleeving
000631496
10106 Ball Socket Seat
003835001
Page: 96 ...

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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