Mh-53e Helicopter Parts

(Page 155) End item NSN parts page 155 of 238
Part Number
NSN
NIIN
10V60-141-239 O-ring
002913076
10V60-141-24 O-ring
002638036
10V60-141-242 O-ring
002913310
10V60-141-245 O-ring
002638041
10V60-141-258 O-ring
005993072
10V60-141-32 O-ring
002975362
10V60-141-326 O-ring
002651087
10V60-141-330 O-ring
002526051
10V60-141-342 O-ring
002519374
10V60-141-347 O-ring
005853353
11 Accelerometer Calibrator
010778349
11-00599-126 Electrolytic Fixed Capacitor
009593298
11-00670-0 Electrical Wire
009686586
11-00671-91 Electrical Wire
009686566
11-011-2448 Composition Fixed Resistor
004004482
11-012-7446-7 O-ring
005796495
11-0441-9 Electrical Wire
000905411
11-0499-1 Reflector
006235969
11-0602 Steering Tie Rod End
003508643
11-09988-00 Diode Semiconductor Device
007526115
Page: 155 ...

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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