Ch-53a/d/e Helicopter Parts

(Page 2) End item NSN parts page 2 of 66
Part Number
NSN
NIIN
012-597-324-000 Spur Gear
000106250
013-004-001 Electrical Connector Backshell
012451950
01513 Shoulder Screw
009870066
01719 Weapon System Resilient Mount
001133666
0183-6REVL Retaining Ring
002827127
02-0101-0157-02 Electronic Shielding Gasket
001030432
02-14229 Fluid Filter Element
009421935
02-14283 Fuel Pump Coupling
009408924
020-072-002 Liquid Quantity Transmitter
011741919
020-42984-48 Filter Orifice Assembly
001368159
0202-12-12 Pipe Coupling
011965217
020442 Vaneaxial Fan
005856016
021-26698-010 Nozzle Block Assembly
012228082
021-26698-10 Nozzle Block Assembly
012228082
026-3107-3 Voltmeter
007296723
02725 Packing Retainer
011174238
02749-MOD 8 Motional Pickup Transducer
013853111
030-1975-001 Electrical Contact
007587244
033-0090-0001 Connector Adapter
006156889
04010104 Fluid Passage Bolt
003386630
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Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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