Mh-53e Helicopter Parts

(Page 27) End item NSN parts page 27 of 238
Part Number
NSN
NIIN
01G009701-89 Lug Terminal
008253700
01G009710-33 Film Fixed Resistor
010813628
02-06-1101 Electrical Contact
003389879
02-06-1103 Electrical Contact
003389879
02-06-2103 Electrical Contact
003389875
02-06-2103TL Electrical Contact
003389875
02-09-1102 Electrical Contact
010398438
02-09-1104 Electrical Contact
010398438
02-09-2103 Electrical Contact
006263538
02-09-2118 Electrical Contact
004173811
02-1065-10 Induct Wire Wound Fixed Resistor
002111319
02-14229 Fluid Filter Element
009421935
02-14283 Fuel Pump Coupling
009408924
02-2191 Film Fixed Resistor
007584792
02-49031-15 Diode Semiconductor Device
004446607
02-49053-01 Light Emitting Diode
010642643
02/101753 Nonmetallic Hose Assembly
012682338
02/911007 Hexagon Head Cap Screw
011934506
02/911007A Hexagon Head Cap Screw
011934506
020-0067-00 Tapered Roller Cone And Rollers
006061841
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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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