Mh-53e Helicopter Parts

(Page 8) End item NSN parts page 8 of 238
Part Number
NSN
NIIN
00301-0262 Tube Reducer
007068711
0032-5020-00 Electrical Wire
008397432
003202 Pipe Nipple
002221839
00323-0036 Electrical Fuel Pump
006764957
00338-0499 Plain Seal
006316649
003440 Electrical Plug Connector
010476312
003509 Plug-in Electronic Compon Socket
000314417
003652-25 Electrical Plug Connector
011104745
00372-0223 Drain Cock
002769041
003770 Lock Washer
001848971
003770-5 Lock Washer
001848971
00381-5 Bearing Ball
001151238
00384549 Pipe To Tube Elbow
006401051
00384710 Tube Coupling Inverted Nut
002889390
004-003005-034 Lock Washer
009340226
004-003005-079 Lock Washer
001848971
004-003081-001 Flat Washer
001670830
004-003081-006 Flat Washer
005159371
004-351-0 Aircraft Pneumatic Tire
009385964
0040398 Headless Straight Pin
000141346
Page: 8 ...

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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