Ch-53a/d/e Helicopter Parts

(Page 47) End item NSN parts page 47 of 66
Part Number
NSN
NIIN
542849 Plain Encased Seal
011358678
544-0257-002 Electronic Components Shield
006746488
546-6482-002 Ceramic Diele Variable Capacitor
008018982
546-7363-002 Shouldered Washer
008279173
5468434G007 Coil Freq Stator
009087802
5468434G7 Coil Freq Stator
009087802
547-3898-004 Light Transmitt Indicating Panel
000196300
5478214G1 Support Plate Assembly
009163036
548-3502-004 Electrical-electron Plug-in Unit
000196304
548-3528-002 Capacitor Divider Assembly
000196313
5480991P001 Electronic Chopper
000702271
5480991P1 Electronic Chopper
000702271
5483892G701 Impeller Assembly
003767046
549-5499-003 Gear Cluster
000152399
549-5504-002 Spring Tension Clip
000214718
549571-3 Nut Retainer
007825094
549838-1 Direct Current Power Filter
000103004
549838-2 Direct Current Power Filter
000103004
Page: 47 ...

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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