Ch-53a/d/e Helicopter Parts

(Page 21) End item NSN parts page 21 of 66
Part Number
NSN
NIIN
200-16417-00 Power Autotransforme Transformer
009384682
200-16417-1 Power Autotransforme Transformer
009384682
2000 Electrical Conductor Bushing
010907990
200184 Fluid Filter Element
009421935
200KDDGC7FS50160 Annular Ball Bearing
005165318
200KDDGFS50160 Annular Ball Bearing
005165318
200KDDGFS50166B Annular Ball Bearing
005165318
200KDDGFS56700 Annular Ball Bearing
005165318
200SFFGL107E006A75C4124R Annular Ball Bearing
005165318
20112-8 Electrical Equipme Mounting Base
005646680
20113 Machine Thread Plug
012246783
201C8560-01-038 Electrical Receptacle Connector
003908575
202019-1 Direct Current Motor
013958532
2046-112 Electrical-electronic Heat Sink
012515166
2051509 Diode Semiconductor Device
000869165
2066741 Metallic Eyelet
007275133
2066741-1 Metallic Eyelet
007275133
2067006 Electromagnetic Relay
007827924
2082-4156-20 Fixed Attenuator
011577870
20825399-001 Rotary Switch
009438047
Page: 21 ...

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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