Mh-53e Helicopter Parts

(Page 196) End item NSN parts page 196 of 238
Part Number
NSN
NIIN
122-6602814 PC 30 Hexagon Self-locking Nut
002453419
122-6722634 PC 15 Hexagon Self-locking Nut
002453419
122-6776003 PC 23 Hexagon Self-locking Nut
002453419
122-6817720 PC 37 Hexagon Self-locking Nut
010046946
122-7312139 PC 37 Hexagon Self-locking Nut
010046946
122-90007 ITEM 22 Push Switch
001118619
122-C-69 O-ring
002500237
122057 Hexagon Plain Nut
007638912
122119 Hexagon Head Cap Screw
005434372
12218-1 Needle Roller Bearing
002273244
12219 Pipe Nipple
001961538
122202-1111 Film Fixed Resistor
012823102
122203-1065 Film Fixed Resistor
010782880
1222397-203 Manual Control Lever
003554459
1224 Lock Washer
001941483
1224244 Fluid Filter Element
002871912
1225357-11 Annular Ball Bearing
007739554
1225357-5 Annular Ball Bearing
000695597
1225357PC11 Annular Ball Bearing
007739554
12259041-3 Electrical Contact
010242004
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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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