Mh-53e Helicopter Parts

(Page 140) End item NSN parts page 140 of 238
Part Number
NSN
NIIN
105X3 Tube Coupling Inverted Nut
002889390
105X4 Tube Coupling Inverted Nut
000137397
106-023-013 Reed Relay
001735683
106-1-B7 S Electrical Insulation Sleeving
009896238
106006-000000 Transistor
000146458
106033-000000 Transistor
001279362
106043-000000 Transistor
000057002
1060464-1 Electrical Receptacle Connector
008121188
10605202-7 Non Wire Wound Variable Resistor
001530999
10605313 Plate Self-locking Nut
009640878
10606702-1 Tube To Boss Tee
007571945
10606986-197 Electrical Plug Connector
011077294
10607442-1 Loop Clamp
003378642
1060826Y00 Light Emitting Diode
011803913
106087 Induct Wire Wound Fixed Resistor
002586955
10613 Tapered Roller Bearing Cup
001000359
106141 Pressure Transmitter
009935546
10620SY10-4 Push Switch
011520625
10620TC10-131 Flat Washer
011453153
10627527-3 Drain Cock
002769041
Page: 140 ...

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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