Ch-53a/d/e Helicopter Parts

(Page 4) End item NSN parts page 4 of 66
Part Number
NSN
NIIN
1-4113-1 Rotary Wing Metallic Seal
001103114
1-891-1 Connector Adapter
005390203
10-0055-9 Electric Lantern
005334960
10-0133-1 Light Transmitt Indicating Panel
013881504
10-10 Fixed Attenuator
007210255
10-22-3 Antenna Coupler
001688289
10-347366-1 Cable Assembly
009532195
10-380022-1 Cable Assembly
001248942
10-387650-1 Ignition Coil
001389494
100-048 Pin-rivet
001105723
100-048-10-18 Pin-rivet
001105723
10000-0101-01-5 Dual Module Lamp
012080400
100019-1 Shim
005960277
100077-001000 Clamp Bolt Assembly
000561231
100089 Fluid Filter
009480526
10015920-006 Watch Gauge Torque
008005361
10022104-101 Transistor
000976293
10023059-101 Coupler-shaft Assem
001134659
10033A Cooler
009398738
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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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