Ch-53a/d/e Helicopter Parts

(Page 6) End item NSN parts page 6 of 66
Part Number
NSN
NIIN
10118574 Shim
005960277
10118655 Sleeve Spacer
008102918
10119652 Packing Retainer
011174238
101239-3 Ceramic Dielectr Fixed Capacitor
008892793
10128136 Plastic Dielectr Fixed Capacitor
010174120
10131971 Electrical Connector Cable Clamp
004440249
10135DAP Electrical-electron Mounting Pad
009166189
10139084 Electrical Card Retainer-ejector
011223431
10139788 Electrical End Bell
011663874
10143-297 Film Fixed Resistor
001084254
1014360 End Chain Link
012560470
1014365 End Chain Link
012560470
101443 Electronic Shielding Gasket
009027407
101624-02 Blind Rivet
000051051
10162889 Antirotation Plate
011866506
10163778 Socket Head Cap Screw
000521488
10180302-1 Thrust Washer Bearing
009028470
10180302-5 Thrust Washer Bearing
008279783
10196829 Push Switch
007586020
10199290 Wire Rope Swaging Sleeve
011325671
Page: 6 ...

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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