Ch-53a/d/e Helicopter Parts

(Page 30) End item NSN parts page 30 of 66
Part Number
NSN
NIIN
300R065 Electromagnetic Relay
010625154
301-126-038 Aircraft Pneumatic Tire
009385964
301-351-0 Aircraft Pneumatic Tire
009385964
3010078 Single Leg Chain Assembly
000030431
3010AN Motional Pickup Transducer
004750284
3013032-3 Pressure Transmitter
014582776
3013460-1 Paper Dielectric Fixed Capacitor
010634334
302-28 Electronic Chopper
000830687
3030-5131 Power Transformer
008793698
30300 Power Transformer
009495401
30399-81101 Plate Spacer
000515773
305036 Ignition Coil
001389494
305036-1 Ignition Coil
001389494
3051G63-001 Extended Washer Self-locking Nut
006129003
3061051 Fluid Filter Element
009465206
3074HH681T025JPB Electrolytic Fixed Capacitor
011275576
3081012RED Spacing Threaded Standoff
000068421
309-0804-00 Sleeve Bearing
008195532
309-0804-000 Sleeve Bearing
008195532
3090191 Shim Set
010064227
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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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