Ch-53a/d/e Helicopter Parts

(Page 54) End item NSN parts page 54 of 66
Part Number
NSN
NIIN
65072-15001-017 Helicopter Rotor Parts Kit
012204385
65072-15001-025 Helicopter Rotor Parts Kit
012155504
65072-15004-012 Rotary Wing Blade Parts Kit
013597383
65072-15004-013 Rotary Wing Blade Parts Kit
013618898
65072-15004-015 Rotary Wing Blade Parts Kit
013597385
65072-15004-018 Rotary Wing Blade Parts Kit
013597388
65101-11017-101 Recessed Washer
009474169
65102-11003-041 Adjuster Assembly
002410012
65102-11008-109 Pitch Lock Arm
001697761
65102-11014-043 Rotary Win Link Set
009184404
65102-11043-102 Thrust Washer Bearing
009576585
65102-11065-084 Tube Assembly
008898313
65102-11080-101 Sleeve Bushing
009484735
65102-11082-102 Flat Washer
009474206
65102-11088-115 Sleeve Bushing
009465239
65102-11524-103 Fold Blade Bolt
011002815
65102-11529-121 Sleeve Bushing
011128018
65102-11543-102 Hinge Sleeve Liner
011002856
65102-11558-101 Sleeve Bushing
013585596
65102-11580-101 Sleeve Bushing
011087674
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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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