Ch-53a/d/e Helicopter Parts

(Page 16) End item NSN parts page 16 of 66
Part Number
NSN
NIIN
1494896-1 Compression Ring
009286043
1496124 Alternating Current Motor
004040017
1496124-0000 Alternating Current Motor
004040017
14P236646 Tuning Insulator
001584343
15-28979G01 Filter Cap
009941501
15110 Solenoid Valve
009257511
151700-0485 Electrical Contact
012961056
151861 Transistor
009249611
151B940P2 Ceramic Dielectr Fixed Capacitor
003217070
1530879-1 Adapter Assembly
009910806
1536-001-5 Circuit Breaker
009418160
1538615 Regulator Connector
008681774
1539262-1 Transistor
009249611
15540 Power Transformer
000103005
1560-911-1 Dial Pointer
005193354
1560CH37-253-3 Sleeve Bearing
007872420
157-2 Electronic Shielding Gasket
001030432
1572020-1 Spline Self-locking Nut
010578778
159-2171 Antenna Lobe Switch
002021104
159-2630 Electromagnetic Relay
000594814
Page: 16 ...

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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