Mh-53e Helicopter Parts

(Page 176) End item NSN parts page 176 of 238
Part Number
NSN
NIIN
1158-8D Tube Coupling Nut
002870288
11581-34 Pipe To Tube Elbow
002871766
115858 Electrical Receptacle Connector
005572054
11589477-2 Lamp Assembly
013384949
1159010 Voltmeter
001930636
115910 Preformed Hose
003586107
115935-031 Knob
008132078
115956-001 Turnlock Fastener Lockspring
002853373
115A905375 Diode Semiconductor Device
004503015
115A905498 Wire Wound Fixed Resistor
004287487
115D6 Tapered Roller Cone And Rollers
001003095
115J14ITEM1A2 Annular Ball Bearing
001448519
115X00402X0000 Annular Ball Bearing
001861104
115X00409X2000 Annular Ball Bearing
002274521
116-0243 Fluid Filter Element
002380033
116-30 Electronic Shielding Gasket
004779931
116.000.201 O-ring
001651967
1160052P9 Electrical Receptacle Connector
000683546
1160243 Fluid Filter Element
002380033
11602713 Electromagnetic Relay
007359542
Page: 176 ...

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