Ch-53a/d/e Helicopter Parts

(Page 62) End item NSN parts page 62 of 66
Part Number
NSN
NIIN
65315-12000-053 Cowling
011428949
65316-12010-045 Nacelle Crotch Assembly
011298279
65316-12018-101 Strut Fitting
011298322
65316-12044-101 Torsion Helical Spring
011237574
65317-08064-101 A Fuel-air Mixture Control Valve
011293688
65317-08064-102 A Fuel-air Mixture Control Valve
011293688
65317-08074-042 Tee Assembly
011302823
65317-12003 Flange To Tube Straight Adapter
011232948
65317-12003-101 Flange To Tube Straight Adapter
011232948
65351-11089-103 Machine Bolt
009389549
65351-11195-101 Bevel Gear
009421657
65351-11227-105 Spur Gear
000016558
65351-11519-103 Thrust Washer Bearing
010387293
65351-11519-104 Thrust Washer Bearing
010365826
65351-11575-041 Gearbox Shield Assembly
002348291
65355-12016-101 Rotary Wing Metallic Seal
001103114
65355-12016-102 Rotary Wing Metallic Seal
001103114
65355-12016-103 Rotary Wing Metallic Seal
001103114
65355-12135-101 Gear Box Retainer
008941542
65355-12135-102 Gear Box Retainer
008941542
Page: 62

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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