Ch-53a/d/e Helicopter Parts

(Page 12) End item NSN parts page 12 of 66
Part Number
NSN
NIIN
120-45705-1 Feedback Cam
001017830
1201-00011-09 Socket Head Cap Screw
001503496
1201-02011-05-2 Glass Cover
004486170
12030 Shoulder Screw
002642685
12030B Shoulder Screw
002642685
12032-0024 Diode Semiconductor Device
000507309
1204-0304 Blind Rivet
003251240
1204-0312 Blind Rivet
008357334
1204-304 Blind Rivet
003251240
1204-312 Blind Rivet
008357334
1207276-1 Adjustment Bellows
007159696
121-45309 Annular Ball Bearing
001018552
1214448 Pitot-static Tube
005267852
122-2020C020 Sleeve Bearing
003219243
123D7952 PT0.5 Electrical Card Retainer-ejector
011223431
123D7952P2 Electrical Card Retainer-ejector
011223431
123D7952P5 Electrical Card Retainer-ejector
011223431
124-0029-274 Diode Semiconductor Device
000869165
124-1553927 Sleeve Bearing
006861011
124-1553927 PART NO. 96 Sleeve Bearing
006861011
Page: 12 ...

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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