Ch-53a/d/e Helicopter Parts

(Page 39) End item NSN parts page 39 of 66
Part Number
NSN
NIIN
4176-4 Tube Coupling Nut
006847304
4180 Hand Driven Hydraulic Ram Pump
000606828
41822-1 Flight Control Panel
011395554
41850A1-45 Aircraft Landing Light
001027703
41850A3 Aircraft Landing Light
001027703
419471-1 Motor-tachometer Generator
009127345
41A1053 Direct Current Motor
012405586
41A230 Direct Current Motor
009951208
4213-788004 Fuel Pump Housing
013572498
42638 Power Transformer
004829384
42660307 Motor-tachometer Generator
009127345
4278C727M Grooved Clamp Coupling
004081666
4295 Bearing And Pivot S
008598703
42FLW-428 Extended Washer Self-locking Nut
006129003
42FLW428 Extended Washer Self-locking Nut
006129003
42P14141-8 Plain Tapered Pin
001873218
42R2047-15 Retaining Ring
002827127
43329 Power Transformer
000103005
43913-1 Turbine Nozz Shield
001047396
4400-1240 Ceramic Dielectr Fixed Capacitor
008892793
Page: 39 ...

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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