Mh-53e Helicopter Parts

(Page 41) End item NSN parts page 41 of 238
Part Number
NSN
NIIN
04260026-005 Non Wire Wound Variable Resistor
009746426
042607 Plug-in Electronic Compon Socket
011475898
04271-0590-01 Electrical Contact
006263538
042979 Annular Ball Bearing
005545396
043-341 Induct Wire Wound Fixed Resistor
008793635
043-9101 Induct Wire Wound Fixed Resistor
000805899
043-91R0 Induct Wire Wound Fixed Resistor
008890010
0430012 Diode Semiconductor Device
007614631
04306-0103 Assembled Washer Screw
000366968
04306-3017 Liquid Quantity Indicator
009333600
04306-7098 Diode Semiconductor Device
007025763
04311-401 Clinch Self-locking Nut
007206591
0431537 Pipe To Tube Straight Adapter
002891930
04320003+001 Paper Dielectric Fixed Capacitor
001296260
04330001-026 Plastic Dielectr Fixed Capacitor
008352710
04352 Digital Display Indicator
010034223
0436-019 Hexagon Self-locking Nut
008574960
0436-12 Hexagon Self-locking Nut
008575547
04360001-030 Mica Dielectric Fixed Capacitor
007170169
043809 Tapered Roller Bearing Cup
001000603
Page: 41 ...

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.

Compare Now »
Clear | Hide