Mh-53e Helicopter Parts

(Page 216) End item NSN parts page 216 of 238
Part Number
NSN
NIIN
1305-037G003 Electrical Plug Connector
009329144
1305-8 Tube Nipple
007976567
1305001 Tapered Roller Cone And Rollers
006061841
1305037G003-000 Electrical Plug Connector
009329144
130503H Tapered Roller Bearing Cup
001000544
1305282 Composition Fixed Resistor
004723470
13053418 Key Washer
003081651
1305422-00 Film Fixed Resistor
001126911
13058987-2 Film Fixed Resistor Network
013267820
1305FFHT Annular Ball Bearing
001448631
13060860 Electronic Shielding Gasket
007722223
13060912 Electronic Shielding Gasket
007722223
13063 Retaining Ring
008042772
1307361PC17 Serrated Lock Ring
002819224
13079937-1 Electrical Receptacle Connector
001031657
1308 Electrical Power Cable
006351187
13084455-2 Electrical Conne Retaining Plate
004083777
13084496-2 Electrical-electronic Heat Sink
007893794
13084615 Annular Ball Bearing
009129200
13084683 Synchro Clamp
006105044
Page: 216 ...

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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