Mh-53e Helicopter Parts

(Page 228) End item NSN parts page 228 of 238
Part Number
NSN
NIIN
1353AS111-1 Ratchet Disc Unit
012328936
1353AS115-1 Hoist Frame
013214526
13554 Tubeaxial Fan
002265872
135541 Tubeaxial Fan
002265872
135567 Incandescent Lamp
002690944
135571 O-ring
009843762
135888-01 Transistor
007875305
13591 Annular Ball Bearing
001089247
13593P11 Tapered Roller Bearing Cup
001000603
135A905361 Diode Semiconductor Device
002359393
135AS111-1 Ratchet Disc Unit
012328936
135B6234-2 Clinch Self-locking Nut
008207155
135PS135 Pipe Nipple
001961535
136-0010-00 Plug-in Electronic Compon Socket
002323758
136-1090-16D Tube To Hose Elbow
005806453
136-1090-16L Tube To Hose Elbow
005806453
136-1391-001 Conductor Splice
001683401
136-1502-22 Film Fixed Resistor
001956377
136-3090-16D Swivel Flange To Hose Elbow
010788600
136-5 Plug-in Electronic Compon Socket
002323758
Page: 228 ...

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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