Ch-53a/d/e Helicopter Parts

(Page 41) End item NSN parts page 41 of 66
Part Number
NSN
NIIN
45341 Electrical Equipme Mounting Base
005646680
4546K24 Pipe Coupling
011965217
458-0164-00 Arbitrary Scale Meter
000257110
45942400-9 Electrical Wire
013139878
45942500-9 Electrical Wire
013164050
460426 Tuning Insulator
001584343
4610215-1030 Compression Helical Spring
011436848
461B-3388-TL Aircraft Pneumatic Tire
009385964
464-TO-3 Electrical-electronic Heat Sink
012515166
47157601 Solid State Relay
004604476
471911 Knob
005198056
471911-501 Knob
005198056
472-0914-005 Transistor
001132427
475C61NXW Poppet Drain Cock
001713203
476-0257-000 Arbitrary Scale Meter
000257110
47864-0 Fuel Bearing And Valve
001047385
479-0719-002 Diode Semiconductor Device
010266123
4793W14G700 Control Dial
011635897
48-10R16-24S6(106) Electr Receptacle Connector Body
004687447
48-10R16-24S6-106 Electr Receptacle Connector Body
004687447
Page: 41 ...

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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