Mh-53e Helicopter Parts

(Page 154) End item NSN parts page 154 of 238
Part Number
NSN
NIIN
10TXS Tube Fitting Flared Sleeve
002775357
010144296
10V60-141-003 O-ring
002638011
10V60-141-028 O-ring
002651093
10V60-141-03 O-ring
002638011
10V60-141-036 O-ring
005856661
10V60-141-111 O-ring
002483839
10V60-141-117 O-ring
002500222
10V60-141-122 O-ring
002500237
10V60-141-135 O-ring
002917336
10V60-141-136 O-ring
002917295
10V60-141-139 O-ring
002526052
10V60-141-143 O-ring
002526058
10V60-141-150 O-ring
004358522
10V60-141-151 O-ring
009359226
10V60-141-210 O-ring
002500221
10V60-141-215 O-ring
002500235
10V60-141-216 O-ring
002500238
10V60-141-230 O-ring
002913274
10V60-141-238 O-ring
002913077
Page: 154 ...

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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