Mh-53e Helicopter Parts

(Page 124) End item NSN parts page 124 of 238
Part Number
NSN
NIIN
10218661 S Electrical Insulation Sleeving
001461122
10218661-1 S Electrical Insulation Sleeving
000680790
10218661-2 S Electrical Insulation Sleeving
001461122
10219 Tapered Roller Bearing Cup
001000544
10222878-1 Electrical-electronic Heat Sink
009385157
10222992 Synchro Clamp
000565429
102231 Indicator Light
000507444
10225 Electrical Receptacle Connector
011601788
10228503724 Annular Ball Bearing
006798917
10228673 Transistor
000681985
10228799 Tubeaxial Fan
000186535
10229 Filler Opening Cap
014087241
102333 Hundre Counter Assembly
009452209
10235-0004 Electrolytic Fixed Capacitor
011328183
10236680-3 Spring Tension Washer
007534402
10236DAP Electrical-electron Mounting Pad
010559501
10237248-2 Synchro Clamp
000565429
1024 Bearing Ball
001006150
1024 V Belt
005290354
1024-3 Feedthru Terminal
007172907
Page: 124 ...

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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