Mh-53e Helicopter Parts

(Page 23) End item NSN parts page 23 of 238
Part Number
NSN
NIIN
0154-1-4114-2 Electrical-electron Mounting Pad
001400366
01576585 Tapered Roller Bearing Cup
001389994
015961 Diode Semiconductor Device
000269661
016-00138 Ceramic Dielectr Fixed Capacitor
008225682
016-2000 Tip Jack
004930467
004930467
016-2000-203 Tip Jack
001057541
004930467
004930467
016-2003-209 Tip Jack
004930467
016-2003-319 Tip Jack
004930467
016-2003WHITE Tip Jack
004930467
016-7757 O-ring
010431419
004930467
016-8010-1 Tip Jack
004930467
016-90004-119 Vent Valve
007264719
0160-0141 Ceramic Dielectr Fixed Capacitor
011273762
0160-3123 Plastic Dielectr Fixed Capacitor
008352710
0160-3823 Plastic Dielectr Fixed Capacitor
009053320
0160-3877 Plug-in Electronic Compon Socket
002229828
Page: 23 ...

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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