Mh-53e Helicopter Parts

(Page 46) End item NSN parts page 46 of 238
Part Number
NSN
NIIN
05190 Transistor
009790108
05199561 Metering And Distribut Fuel Pump
008082655
052-0009-05 Weapon System Resilient Mount
007942936
052-199 Nonwire Wound Variable Resistor
007638769
05228770 Fuel Injection Nozzle
009110139
05229192 Nonaircraft Fue Nozzle Spray Tip
001198494
052493 Connector Adapter
004021153
05282520 Tapered Roller Bearing Cup
001000544
05282580 Tapered Roller Cone And Rollers
001003541
052J Telephone Jack
001924789
0530-9 Retaining Ring
006804619
0534-008 Retaining Ring
007217680
0536-21 Alternating Current Motor
001860023
054-039 Telephone Jack
001924789
054-0900-024 Fluid Filter Element
010256853
054-0900-025 Fluid Filter Element
010228183
054000151 Ceramic Dielectr Fixed Capacitor
008215215
054478-0102 Nonwire Wound Variable Resistor
001074881
055-9 Induct Wire Wound Fixed Resistor
000803218
0550-7705 Transistor
009305325
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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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