Ch-53a/d/e Helicopter Parts

(Page 49) End item NSN parts page 49 of 66
Part Number
NSN
NIIN
56B17C Electric Temperature Transmitter
002497668
572-523-9202 Vent Plug
000742617
572-9-153 Mounting Plate Assembly
009461041
572-9-154 Mounting Plate Assembly
009437899
5722-0009-HSX Electromagnetic Relay
006445180
5722-9HS Electromagnetic Relay
006445180
5722-9HSX Electromagnetic Relay
006445180
579153-1 Semiconductor Device Holder
001051171
5800335-0110-000 Scale Dial
005827778
5800583-942002-104 Transistor
009989314
58130847 Electromagnetic Relay
007827924
5816-2 Pitot-static Tube
005267852
58199C Regu Diaphragm Assembly
004491445
583524-3 Electrical Receptacle Connector
003908575
5877 Pump Piston Assembly
001049293
5887 Return Plate Clip
001017836
58887 Valve Stem
009231063
58901A008138 O-ring
008006353
58A5A89-1 Connector Adapter
005390203
58FH-1612 Hexagon Self-locking Nut
010348889
Page: 49 ...

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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