Mh-53e Helicopter Parts

(Page 230) End item NSN parts page 230 of 238
Part Number
NSN
NIIN
1366AS154 Shouldered Stud
012822708
1366AS163 Multiple Disk Brake
012871062
1366AS305 Push-pull Control Assembly
012892436
1366AS642 Extension Shaft
012877796
1366AS998 Electrical Connector Cover
000444101
1368 Knockout Reducing Washer
002657773
1369AS132-1 Butt Hinge
002823753
1369AS157-3 Butt Hinge
002823753
137-0035-001 Ferrule
008705350
137-009-5135 Composition Fixed Resistor
001219858
137-071-7300 Annular Ball Bearing
007739554
137-0900-200 Light Lens
000787626
137-0937-003 Light Lens
000787626
137-317-9001 Airframe Roller Bearing
002710009
137-937 Light Lens
000787626
137-937W Light Lens
000787626
137-95990-01 Extractor Post Fuseholder
008814636
137.053 Pre Wire Wound Variable Resistor
012325593
137022P27 Electrolytic Fixed Capacitor
009593298
137030P124 Electrolytic Fixed Capacitor
009593300
Page: 230 ...

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.

Compare Now »
Clear | Hide