Mh-53e Helicopter Parts

(Page 218) End item NSN parts page 218 of 238
Part Number
NSN
NIIN
131-69-5 Plastic Dielectr Fixed Capacitor
009053320
131-90038-087 Plug-in Electronic Compon Socket
012516711
13100 Conduit Chase Nipple
002808558
131033R1 Access Cover
007143113
1311025-001 Pump Rotor
012766097
131154 Breather
006403774
13120003 Fluid Filter Element
001365066
131282 Incandescent Lamp
000131282
131286-01 Synchro Rotor
007161869
1312945 Retaining Ring
006197229
131297-413 Film Fixed Resistor
011866795
13129DA Lubrication Fitting
001720031
1313 Annular Ball Bearing
005555210
13136 Swivel Caster
004777202
131376-16-157 O-ring
007294655
131390 Tapered Roller Bearing Cup
001000359
13153280-1 Spring Tension Washer
009542353
13153312-2 Annular Ball Bearing
007739554
13153387-2 Electrical Tiedown Mounting Base
010135864
131548 Electrical Plug Connector
005735709
Page: 218 ...

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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