Mh-53e Helicopter Parts

(Page 33) End item NSN parts page 33 of 238
Part Number
NSN
NIIN
029488-0001 Electrical Connector Cover
011847188
029558-0000 Telephone Jack
006832746
02P207389 Hexagon Plain Nut
002320764
02P238368-2 Clinch Self-locking Nut
008279286
03-0005-112 Film Fixed Resistor
003482707
03-0005-124 Film Fixed Resistor
001120972
03-0005-128 Film Fixed Resistor
004315164
03-0005-142 Film Fixed Resistor
000052698
03-0005-152 Film Fixed Resistor
004315161
03-0005-166 Film Fixed Resistor
004320409
03-0005-172 Film Fixed Resistor
007213712
03-0005-178 Film Fixed Resistor
002505968
03-0005-187 Film Fixed Resistor
002644027
03-0005-216 Film Fixed Resistor
001120966
03-0005-220 Film Fixed Resistor
002431450
03-0005-223 Film Fixed Resistor
002585411
03-0005-232 Film Fixed Resistor
003041303
03-001-0250 Self-aligning Plain Bearing
005285336
03-001-04 Self-aligning Plain Bearing
005285336
03-0017-17 Induct Wire Wound Fixed Resistor
000805899
Page: 33 ...

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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