Mh-53e Helicopter Parts

(Page 44) End item NSN parts page 44 of 238
Part Number
NSN
NIIN
04981AB Push Switch
001328368
04EM002-1 Linear Microcircuit
011281851
05-010-002 Tube Coupling Inverted Nut
004346464
05-0393-00 Composition Fixed Resistor
000052868
05-0473-00 Composition Fixed Resistor
008740147
05-0536 Tapered Roller Cone And Rollers
006061841
05-0715-03 Plug-in Electronic Compon Socket
002323758
05-0915-04 Plug-in Electronic Compon Socket
002229828
05-114835 Film Fixed Resistor
002009602
05-652018 Lug Terminal
005044703
05-803316 Universal Joint Parts Kit
007024578
050-128-0000220 Electrical Plug Connector
000639010
050-17 Induct Wire Wound Fixed Resistor
000803218
050-265 Hexagon Plain Nut
002320764
05005020 Diode Semiconductor Device
000454196
05012-0061 Annular Ball Bearing
007739554
0502-0034 Alternating Current Motor
000613089
050755 Dial Indicating Pressure Gage
004252373
05084AB Tapered Roller Cone And Rollers
001000233
05087-60007 Electrical Contact
001301746
Page: 44 ...

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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