Mh-53e Helicopter Parts

(Page 73) End item NSN parts page 73 of 238
Part Number
NSN
NIIN
1-1500MH-11 Lamp Ballast
014157902
1-16 Bearing Ball
001006150
1-2 301 Nonmetallic Hose
009896479
1-2 8-20630-1 Tube To Hose Straight Adapter
009520038
1-2 8-21230-1 Tube To Hose Straight Adapter
008843920
1-2-10P4M7 Composition Fixed Resistor
001048332
1-202-729-00 Composition Fixed Resistor
001219923
1-210761-6 Annular Ball Bearing
001419561
1-213-158-00 Composition Fixed Resistor
001368338
1-214-144-00 Film Fixed Resistor
000255988
1-214-160-00 Film Fixed Resistor
001956377
1-214-164-00 Film Fixed Resistor
002009294
1-222259 O-ring
002913274
1-246-853-00 Composition Fixed Resistor
004697359
1-265969-604R0 Film Fixed Resistor
002739608
1-265969-90001 Film Fixed Resistor
001923488
1-281851-10003 Film Fixed Resistor
010184514
1-281851-16601 Film Fixed Resistor
002954291
1-281851-30002 Film Fixed Resistor
001120966
1-281851-500R0 Film Fixed Resistor
004320420
Page: 73 ...

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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