Mh-53e Helicopter Parts

(Page 193) End item NSN parts page 193 of 238
Part Number
NSN
NIIN
1210 Woodruff Key
006165531
1210-2C115A Electromagnetic Relay
007873068
121020 Machine Screw
009576265
1210386 Rotary Pump Unit
010753497
1210719 Tubeaxial Fan
005297463
1210C1686-142 Electrical Compone Tiedown Strap
002237543
1210C1686-143 Electrical Compone Tiedown Strap
002237543
1210C1686-42 Electrical Compone Tiedown Strap
002237543
1210C1686-43 Electrical Compone Tiedown Strap
002237543
1210C1686-92 Electrical Compone Tiedown Strap
002237543
1210C1686-93 Electrical Compone Tiedown Strap
002237543
1213829-201 Tubeaxial Fan
011052015
1213831-201 Fan Impeller Guard
011541041
1213AS623-6-5 Pin-rivet
009590461
1213AS624-6-3 Pin-rivet
009590150
1213AS624-6-5 Pin-rivet
009694521
1213D0-2 Pneumatic Tire Wheel
005287224
1213FF Annular Ball Bearing
001556306
1213FF-1V1 Annular Ball Bearing
001556306
121413 Quick Disconnect Terminal
009489686
Page: 193 ...

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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