Ch-53a/d/e Helicopter Parts

(Page 59) End item NSN parts page 59 of 66
Part Number
NSN
NIIN
65213-08003-142 Liner Header
011396879
65213-08003-150 Liner Fillet
011396880
65213-09020-042 Panel Assembly
011396928
65213-09029-103 Main Rotor Pylon Inlet
011396902
65215-06004-078 Panel Assembly
012568217
65215-07003-132 Fairing Screen
011444124
65215-09004-116 Hinge Half
011396892
65215-09015-042 Drive Shaft Fairing
011310534
65215-09016-049 Door Assembly
011310536
65216-03000-102 Window Seal
011474657
65216-05003-041 Aircraft Window Panel
011529735
65217-03023-001 Bell Crank
011424373
65218-04028-044 Aircraft Floor Cargo Rail
012502238
65219-02153-041 Presure Refueli Fitting Assembly
011361391
65219-07002-041 Rod End Plain Bearing
011468174
65219-09059-103 Support Installation Screen
011396894
65219-09062-106 Special Deflector
012770834
65227-09003-041 Panel Assembly
011310540
652400-103 Scale Dial
005827778
65251-08030-102 Machine Thread Bushing
001623877
Page: 59 ...

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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