Mh-53e Helicopter Parts

(Page 89) End item NSN parts page 89 of 238
Part Number
NSN
NIIN
1005364-1 Hand Driven Hydraulic Ram Pump
007767180
1005372 Nonmetallic Hose
009335878
1005372-006 Nonmetallic Hose
006767936
10054026 Machine Screw
009646032
10054485 Setscrew
008208367
10054913 O-ring
008022130
1005572 Electrolytic Fixed Capacitor
012778529
10056040 Sleeve Bearing
008195532
1005620PCNAS51-200 Retaining Ring
002524758
1005620REVBPCNAS51-200 Retaining Ring
002524758
10056214 Machine Screw
004594687
10056354 Screw Thread Insert
004713745
100564 Pipe To Boss Straight Adapter
011883184
10056554 Cartridge Fuse
000040274
1005784-00 Plastic Dielectr Fixed Capacitor
008352710
100592 Electrical-electron Mounting Pad
011997462
1006-4 Lubrication Fitting
001720058
1006-552 O-ring
001651968
1006004 Diode Semiconductor Device
008469125
10061 Shaft Lock
001566559
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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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