Mh-53e Helicopter Parts

(Page 195) End item NSN parts page 195 of 238
Part Number
NSN
NIIN
121A030590 Lug Terminal
008253696
121A4MA Knob
006193837
121B8 Liquid Oxygen Valve
007969680
121C4MA Knob
005791210
121J-335-C3C Turnlock Fastener Stud
002828132
121J-430-C3Y Turnlock Fastener Stud
002883164
121P10502S1 Paper Metallized Fixed Capacitor
001707170
121P47494S4 Paper Metallized Fixed Capacitor
003086733
122-00023 Push Switch
001118619
122-0186-001 Electrical Connector Jackscrew
000432820
122-2020C020 Sleeve Bearing
003219243
002857161
122-5008264 PC 32 Lubrication Fitting
000481788
122-5277660 ITEM 49 Cotter Pin
002857161
122-5277664 ITEM 58 Hexagon Self-locking Nut
002453419
122-5277665 ITEM 58 Hexagon Self-locking Nut
002453419
122-5277668 ITE Hexagon Self-locking Nut
002453419
122-6602812 PC 30 Hexagon Self-locking Nut
002453419
122-6602813 PC 30 Hexagon Self-locking Nut
002453419
Page: 195 ...

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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