Mh-53e Helicopter Parts

(Page 69) End item NSN parts page 69 of 238
Part Number
NSN
NIIN
0BT2720 Tapered Roller Bearing Cup
001000359
0BT33462 Tapered Roller Bearing Cup
001000572
0BT3984 Tapered Roller Cone And Rollers
001003095
0BTT101 Thrust Roller Bearing
001170754
0C6AZ6507A Engine Poppet Valve
004813552
0D1B Knob
008132078
0D71610-1K8 Metallic Shielded Cable Ferrule
005496220
0E1B Knob
007621489
0E3754 Induct Wire Wound Fixed Resistor
005185334
0E4751 Composition Fixed Resistor
001048332
0EFER90797 Annular Ball Bearing
001089247
0F279 Fluid Filter Body
000153609
0F28479 Fluid Filter Element
007928985
0G1055 Composition Fixed Resistor
002478684
0G3005 Composition Fixed Resistor
004103837
0G3935 Composition Fixed Resistor
002521050
0G5125 Composition Fixed Resistor
004351723
0H2231 Composition Fixed Resistor
001406155
0H2235 Composition Fixed Resistor
001406155
0H2241 Composition Fixed Resistor
004224129
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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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