Ch-53a/d/e Helicopter Parts

(Page 55) End item NSN parts page 55 of 66
Part Number
NSN
NIIN
65103-11521-042 Bracket Assembly
011002811
65105-11505-103 Shouldered Shaft
011002729
65105-11556-102 Droop Stop Weight
011002860
65106-11105 Self-aligning Plain Bearing
009487307
65106-11105SBS48ATC78 Self-aligning Plain Bearing
009487307
65106-11125-101 Bearing Housing Liner
009303446
65106-11134-101 Helicopter Rotor Cover
001055256
65106-11136-101 Plate Spacer
001107194
65113-07107-104 Stepped Spacer
004840987
65150-00067-112 Shoulder Bolt
010074088
65152-00009-043 Tip Cap Assembly
008898305
65155-00125-101 Concave Washer
012862559
65155-00125-102 Concave Washer
012867881
65160-00035-081 Counterweight Assembly
009157007
65160-00037-082 Bracket Assembly
009509661
65170-11025-105 Tip Cap Assembly Shim
011310506
65170-11083 Aircraft Channel
014814108
65170-11083-101 Aircraft Channel
014814108
65170-11917-101 Marine Navigational Light
011258331
651C-2 Watch Gauge Torque
008005361
Page: 55 ...

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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