Mh-53e Helicopter Parts

(Page 151) End item NSN parts page 151 of 238
Part Number
NSN
NIIN
109537-3 Electrical-electron Mounting Pad
001388797
10956131 Machine Bolt
002264832
1096-0025 Retaining Ring
007217680
109614-9 Metallic Eyelet
000156276
10962611 Diode Semiconductor Device
007525351
109700-1205 Machine Screw
001829411
10973600 Serrated Lock Ring
006825877
10973604 Serrated Lock Ring
006825877
109975 Composition Fixed Resistor
001406155
109A032606 O-ring
006182517
109A2A46 Setscrew
007239385
109A9201-3 Plate Self-locking Nut
007827094
109B106-1 Knob
007218376
109D107C2025T0 Electrolytic Fixed Capacitor
011262071
109D107X0025F0 Electrolytic Fixed Capacitor
011262071
109D107X0025T2 Electrolytic Fixed Capacitor
011262071
109D107X9025T2 Electrolytic Fixed Capacitor
011262071
109D336X0015C0 Electrolytic Fixed Capacitor
011194307
109D336X9015C0 Electrolytic Fixed Capacitor
011194307
109D336X9015C2 Electrolytic Fixed Capacitor
011194307
Page: 151 ...

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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