Mh-53e Helicopter Parts

(Page 83) End item NSN parts page 83 of 238
Part Number
NSN
NIIN
10003740 Vent Valve
007264719
10004-404 Tube To Hose Straight Adapter
005551152
1000406 Plug-in Electronic Compon Socket
011475898
1000413 Spark Exhaust Arrester
002870336
10004214 Nonmetallic Hose
002889840
100046 Hexagon Self-locking Nut
008150653
10004B404 Tube To Hose Straight Adapter
005551152
10004B604 Tube To Hose Straight Adapter
005551152
100056-2 Tubular Rivet
008214995
100057022 Incandescent Lamp
001680411
100060-062 Incandescent Lamp
001680411
100061-009 Pipe Bushing
002783167
100063 Ceramic Dielectr Fixed Capacitor
007880328
1000638 Pipe To Hose Elbow
009400947
1000650 Tube To Hose Straight Adapter
010878886
100073-102 Ceramic Dielectr Fixed Capacitor
008225682
1000852-14 Film Fixed Resistor Network
013266635
100089 Fluid Filter
009480526
10008B408 Tube To Hose Straight Adapter
005422807
100095-1 Tube-hose Fit Compression Sleeve
011937390
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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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