Mh-53e Helicopter Parts

(Page 22) End item NSN parts page 22 of 238
Part Number
NSN
NIIN
01408 Film Fixed Resistor Network
010938423
0142-7377 O-ring
008331428
01438 Hexagon Head Cap Screw
000712511
01455AB Tapered Roller Bearing Cup
001000359
014761-1 Pin-rivet Collar
006313429
0148844 Electrical-electronic Heat Sink
007893794
014949-1 Tapered Roller Cone And Rollers
009261379
014952-1 Tapered Roller Cone And Rollers
007630259
015-0208-000 Electrical Contact
010879283
015-0377-000 Ferrule
008705350
015-1955-000 Wire Rope Swaging Sleeve
001329163
015-377-000 Ferrule
008705350
015-870145-3-16 Inter Reel Assembly
014370396
015-90003-60 Pipe To Tube Elbow
002546215
015-90003-92 Fluid Filter Element
010228183
015-90010-58 Pipe Bushing
002783167
0150-0019 Ceramic Dielectr Fixed Capacitor
008047566
015032S1-12D Quick Disconnect Coupling Half
005401268
01513 Shoulder Screw
009870066
01527-6S Tube Elbow
007192618
Page: 22 ...

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