Mh-53e Helicopter Parts

(Page 65) End item NSN parts page 65 of 238
Part Number
NSN
NIIN
09-17420C6 Loop Clamp
003585711
09-28507 Pipe To Tube Elbow
002216215
09-31267 Headed Straight Pin
002179576
09-50-3081 Electrical Plug Connector Body
001484254
09-50-3081 8PIN Electrical Plug Connector Body
001484254
09-5244 Vent Valve
007264719
09-56038C3 Nonmetallic Hose
000097259
09-7008 Compression Helical Spring
002179600
09-9126-1-0710 Tip Jack
007295559
090-03339-0072 Push-pull Control Assembly
012892436
090009600 Electrical-electronic Compo Oven
004489601
0900988 Hexagon Slotted Plain Nut
009980608
0900988-7 Hexagon Slotted Plain Nut
009980608
0901477 Pipe Nipple
001961538
0901477-0 Pipe Nipple
001961538
0901651-0 Pipe Plug
002212136
0903-001 Tip Jack
007295559
091-00033 Extractor Post Fuseholder
000181450
0910128 Pipe To Tube Elbow
002634976
0910138 Tube Coupling Nut
000116452
Page: 65 ...

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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