Ch-53a/d/e Helicopter Parts

(Page 44) End item NSN parts page 44 of 66
Part Number
NSN
NIIN
5058-10-01 Control Motor
000892884
5058-19-01 Control Motor
000892884
507006 Waveguide Seal
007249766
507006-1 Waveguide Seal
007249766
507107 Hexagon Head Cap Screw
005587182
507938-1 Alternating Current Motor
008693353
5082-2187 Diode Semiconductor Device
004974091
5082-7010 Optoelectronic Display
010290612
50M195ZB2 Semiconductor Device Set
009004819
50M200ZB1 Semiconductor Device Set
009004819
5100-19C Retaining Ring
002827127
513-4-4CR Tube To Hose Elbow
007280520
5131 Electric Light Control
009389525
515 587-9 Electrical Wire
013139878
515 591-9 Electrical Wire
013164050
516-12D Hose Coupling Nut
006333703
516-2776-001 Electrical Conne Maintenance Kit
006954914
51721 Cylindrical Roller Bearing
000831282
51H3977-1 Aircraft Safety Belt
005166542
51P236584-08 Delay Line
009463855
Page: 44 ...

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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