Ch-53a/d/e Helicopter Parts

(Page 36) End item NSN parts page 36 of 66
Part Number
NSN
NIIN
381371 Electrical Temperature Indicator
006033913
38253-2 Solid State Relay
004604476
38950-00903-103 Airframe Ball Bearing
001426571
38950-00906-104 Airframe Ball Bearing
011436742
39-1504-001 Display Handle
004890661
39-1509-001 Handle Insert Assembly
004890666
390265-16 Quick Disconnect Coupling Half
009226247
3906 Directional Coupler
002645504
3911-1-2 Valve Disk
009432017
3911-2-1 Mechanical Co Lever
009432016
39422 Spring Guide
012213658
39577-12 Aircraft Window Panel
011510829
39652 Valve Disk
012192290
397464-016 Indicator Housing
013151854
397562 Fuel Amplifier Module
009437960
397562-07403 Fuel Amplifier Module
009437960
397849-07403 Power Transformer
009576725
39R12FX Electromagnetic Relay
002581780
3A031-3 Fluid Pressure Regulating Valve
009447516
Page: 36 ...

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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