Mh-53e Helicopter Parts

(Page 213) End item NSN parts page 213 of 238
Part Number
NSN
NIIN
13-05421-00 Film Fixed Resistor
002585411
13-06-242 O-ring
002913310
13-08-16/1 Air Cleaner Cap Assembly
013219990
13-09418-00 Film Fixed Resistor
001386996
13-1-10762 Tapered Roller Cone And Rollers
006061841
13-100028 Plastic Dielectr Fixed Capacitor
008352710
13-114 Incandescent Lamp
000802012
13-116007-1 Transistor
006868578
13-122143-1 Transistor
000871078
13-12404-00 Film Fixed Resistor
002110230
13-12479-00 Film Fixed Resistor
000065407
13-1248 Hexagon Head Cap Screw
009474354
13-13153-00 Film Fixed Resistor
007584792
13-13344-00 Film Fixed Resistor
002644027
13-16509-00 Composition Fixed Resistor
004351722
13-193240-02 Incandescent Lamp
001680411
13-19735 Pressure Switch
013801013
13-3-6 Tube Nipple
007816089
13-305 Tube Coupling Nut
000114627
13-644 Hexagon Head Cap Screw
002693219
Page: 213 ...

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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