Mh-53e Helicopter Parts

(Page 198) End item NSN parts page 198 of 238
Part Number
NSN
NIIN
12340006 Matched Set V Belts
008652470
123415-001 Disk Drive Unit
013681056
123653+01 Transistor
010305322
123806 Ball Bearing Unit
001169034
12382107 Plug-in Electronic Compon Socket
011408059
1239242-49 Wire Wound Fixed Resistor
011866838
123929 Tapered Roller Cone And Rollers
008278646
1239900004 Turnlock Fastener Stud
005432418
123B Pipe Reducer
006406330
123B1-4 T0 1-8 Pipe Reducer
006406330
123B1-4X1-8 Pipe Reducer
006406330
123D504C3100E1 Electrolytic Fixed Capacitor
004877093
123SCH189-116 Fluid Filter Element
001498331
124-0029-274 Diode Semiconductor Device
000869165
124-0178 Diode Semiconductor Device
008981479
124-28105 Fluid Filter Element
011924622
124-3003-130 Machine Bolt
001562339
124-3003-202 Dust And Moistur Protective Plug
009179763
124-3003-385 Flat Washer
001670830
124-36 Pipe Bushing
002783167
Page: 198 ...

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