Mh-53e Helicopter Parts

(Page 123) End item NSN parts page 123 of 238
Part Number
NSN
NIIN
102-0322 Tube To Boss Straight Adapter
002266772
102-0556 Pipe Nipple
010061263
102-0971 Pipe To Tube Elbow
002216215
102-10004 Tube Coupling Nut
000114627
102-1084 Pipe To Tube Elbow
009951568
102-1091 Tube Reducer
006284816
102-221-00 Electrical Special Purpose Cable
011033078
102-9209-2 Intake Air Cleane Filter Element
001299757
102-TP916 Fluid Filter Element
010228183
10201283 Electrical Wire
008518505
10203045 Diode Semiconductor Device
000269661
10204738 Electrical Plug Connector
011104745
10204891 Electrical Plug Connector
011658675
10204893 Electrical Receptacle Connector
011718728
10205-0244 Mica Dielectric Fixed Capacitor
010537975
10206-DAP Electrical-electron Mounting Pad
011997476
10206211 O-ring
011604327
10206240 Packing Retainer
001715902
10209-2 Plate Insulator
002464898
10218 Tapered Roller Cone And Rollers
001003541
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Helicopter, Mh-53e

Picture of Mh-53e 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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