Ch-53a/d/e Helicopter Parts

(Page 10) End item NSN parts page 10 of 66
Part Number
NSN
NIIN
112-9191-003 Incandescent Lamp
013406497
11245-016-00 Hexagon Castellated Plain Nut
001671294
11269318 Plate Self-locking Nut
005848164
1128000-4 Turnlock Fastener Stud Assembly
005231376
112946 Delay Line
009091484
1132-9192 Voltmeter
007296723
11403G1 Pressure Bellows
009422091
114ES247-2 Electric Lantern
005334960
115-KSZZ Annular Ball Bearing
000943418
115015-001 Transistor
009989314
115234 Fluid Filter
000573834
115474-000 Electrical Receptacle Connector
008401018
11569663 Hand Driven Hydraulic Ram Pump
011088825
115KSZZ87 Annular Ball Bearing
000943418
1161664-1 Plastic Dielectr Fixed Capacitor
012463493
1161693-1 Electrical-electronic Heat Sink
012515166
11621308 Annular Ball Bearing
005165318
117-21-20-020 Sleeve Bearing
003219243
1170-243-1-0 Plain Seal
011467307
117157 Electromagnetic Relay
006445180
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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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