Ch-53a/d/e Helicopter Parts

(Page 19) End item NSN parts page 19 of 66
Part Number
NSN
NIIN
17M201-184A Paper Dielectric Fixed Capacitor
004099324
18-0017-2 Instrument Mounting Bezel
013530994
18-1600 Fire Sprinkling Automatic Drain
012204650
18-1600-1 Fire Sprinkling Automatic Drain
012204650
18-3110-2 Pressure Transmitter
000653235
18007 Control Motor
007299368
1800S610-3 Time Delay
006135527
183-0251-00 Electrolytic Fixed Capacitor
000804136
183-0251-000 Electrolytic Fixed Capacitor
000804136
184-9085-650 Electrolytic Fixed Capacitor
004439242
1855-0103 Transistor
001037410
18801 Direct Current Motor
006290967
1891-1 Connector Adapter
005390203
18D29 Vernatherm Valve
009434976
190605-9 Flat Washer
006328939
1910-2-203 Arbitrary Scale Meter
000257110
19808A5 Control Motor
000892884
1987638-1 Electrical Equipment Rack
000639358
1992868-1 Electrical Receptacle Connector
001187339
1995986-1 Radio Frequency Cable Assembly
000541073
Page: 19 ...

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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