Ch-53a/d/e Helicopter Parts

(Page 32) End item NSN parts page 32 of 66
Part Number
NSN
NIIN
32-650-4609 Head Assembly
011879622
320064-08 Delay Line
009463855
3204-2 Pressure Switch
012343189
321HR Voltmeter
007296723
3225AS100 Communication Equ Interface Unit
013804583
3251W794-504 Nonwire Wound Variable Resistor
009320046
3252W794-504 Nonwire Wound Variable Resistor
009320046
32637-1 Discxassembly
009157154
327-000-S2L0-101M Ceramic Dielectr Fixed Capacitor
003217070
327-000S2L0-101M Ceramic Dielectr Fixed Capacitor
003217070
327-028-S2L0-101M Ceramic Dielectr Fixed Capacitor
003217070
327-028S2L0-101M Ceramic Dielectr Fixed Capacitor
003217070
327-100 Ceramic Dielectr Fixed Capacitor
003217070
327-101M Ceramic Dielectr Fixed Capacitor
003217070
327-157 Electrical Receptacle Connector
008401018
3283-110-120VAC Voltmeter
007296723
33-90 Connector Adapter
006156889
33103 Annular Ball Bearing
012236643
3313-AS-280-1 Stereomet Lens And Retainer Ring
014144950
3313-AS-403-1 Light Transmitt Indicating Panel
014144952
Page: 32 ...

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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