Mh-53e Helicopter Parts

(Page 117) End item NSN parts page 117 of 238
Part Number
NSN
NIIN
10154085 O-ring
010463299
10154086 O-ring
010470435
10154088 O-ring
011019486
10154109 Locking Device
009152369
10154111 Screw Thread Insert
010069404
101542 Annular Ball Bearing
001089247
10154238 Film Fixed Resistor
011771906
10154239 Film Fixed Resistor
011772012
10154272 Nonwire Wound Variable Resistor
012620853
10154290 Ceramic Dielectr Fixed Capacitor
012148790
10154295 Toggle Switch
000888762
10154400 Quartz Crystal Unit
011098484
10154513 Electrical Lead
007225707
10154573 Nonelectrical Wire
003556072
10154575 Nonelectrical Wire
009907799
10159518 Self-aligning Plain Bearing
005285336
10159829 O-ring
005306990
10159953 O-ring
003431035
10159955 O-ring
011171076
10159963 O-ring
013970829
Page: 117 ...

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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