Mh-53e Helicopter Parts

(Page 226) End item NSN parts page 226 of 238
Part Number
NSN
NIIN
134159 Diode Semiconductor Device
000635804
13418019-1 Push On Nut
011220953
13420007 Fluid Filter Element
007928985
13420008 Intake Air Cleane Filter Element
001299757
13420142 Fluid Filter Element
011229517
13421 V Belt
002882665
13430AB16AWG Electrical Wire
001288696
13430AB20S0L Electrical Wire
008397432
13436-1 Pendant Hook Keeper
011057783
1345-9-29 Electrical Dummy Load
011450138
134557-0000 Transistor
000146458
134584-0007 Film Fixed Resistor
007213712
13459044-289 Film Fixed Resistor
012868945
134619-0000 Diode Semiconductor Device
007744420
134654 Indicator Light Assembly
012268889
134740-0000 Glow Lamp
009513376
1348-0285 Setscrew
001631930
1348-0285-P10 Setscrew
001631930
1349-000-G000 Connector Adapter
004921954
1349000G000-000 Connector Adapter
004921954
Page: 226 ...

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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