Mh-53e Helicopter Parts

(Page 211) End item NSN parts page 211 of 238
Part Number
NSN
NIIN
12X11987A Intake Air Cleane Filter Element
009793806
12Z1007-6 Socket Head Cap Screw
009640077
12Z10600-12 Tapered Roller Bearing
002273280
12Z1077PC17 Setscrew
002813120
12Z12002-36 Nonmetallic Grommet
001850003
12Z12002-40 Nonmetallic Grommet
001850001
12Z12002-55 Nonmetallic Grommet
002024004
12Z12002PC43 Nonmetallic Grommet
002765954
12Z12009-57 Ferrule
008705350
12Z12025PC6 Hose Clamp
012733671
12Z12127-34 Turnlock Fastener Stud
005432418
12Z13006-81 Incandescent Lamp
002690944
12Z13110-837 Induct Wire Wound Fixed Resistor
000880635
12Z2007-244 Hexagon Self-locking Nut
008150653
12Z22PC101 Lock Washer
006163554
12Z24-125 Hexagon Head Cap Screw
007247224
12Z315-145 Annular Ball Bearing
001448519
12Z315-153 Annular Ball Bearing
005555210
12Z33460-12 Nonmetallic Hose
005951089
12Z33460-8 Nonmetallic Hose
009998994
Page: 211 ...

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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