Mh-53e Helicopter Parts

(Page 24) End item NSN parts page 24 of 238
Part Number
NSN
NIIN
0160-4084 Ceramic Dielectr Fixed Capacitor
007880328
0164-10 Pipe To Boss Straight Adapter
001969580
016787-4 Nonmetallic Hose
006767936
01719 Weapon System Resilient Mount
001133666
0172-115 Tubular Rivet
008214995
017264 Tapered Roller Cone And Rollers
009261379
017271 Tapered Roller Cone And Rollers
007630259
0174T2KYC52 Globe Valve
011062406
0177-31 Incandescent Lamp
001557784
0179132 Lug Terminal
001141311
018-001310 Electrical Contact
002568040
018-001456-001 Electrical Contact
010879279
018-001468-004 Electrical Contact
002568040
018-001551 Electrical Contact
000621608
018-001553 Electrical Contact
000613276
0180-0136 Electrolytic Fixed Capacitor
008790123
0180-0141 Electrolytic Fixed Capacitor
008790123
0180-0294 Electrolytic Fixed Capacitor
011194311
0180-0695 Electrolytic Fixed Capacitor
010829522
0180-2503 Electrolytic Fixed Capacitor
011328183
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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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