Mh-53e Helicopter Parts

(Page 26) End item NSN parts page 26 of 238
Part Number
NSN
NIIN
019-003713 Diode Semiconductor Device
009244587
019-004208 Diode Semiconductor Device
000717429
019-004449-049 Transistor
001070742
019-004449-050 Transistor
001070742
019-005108 Transistor
009305325
019-005559-001 Diode Semiconductor Device
002359393
019-005893-001 Diode Semiconductor Device
007613857
019-0826-000 Packing Assembly
007888713
019-35A368 Tapered Roller Bearing Cup
001000359
019-35A425 Tapered Roller Cone And Rollers
001003095
019001918 Diode Semiconductor Device
001704430
01902134 Fluid Filter Element
002380033
019076 Nonmetallic Hose
002893306
019118-2 Clinch Self-locking Nut
008207155
019336-001 Compression Helical Spring
011773426
019338-001 Push On Nut
011220953
0196046P017 Diode Semiconductor Device
007526115
0198983-00 Pipe To Tube Elbow
006401051
01A11000 Ceramic Dielectr Fixed Capacitor
007880328
01A233751A21-11 Radio Receiver Support
008954410
Page: 26 ...

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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