Mh-53e Helicopter Parts

(Page 85) End item NSN parts page 85 of 238
Part Number
NSN
NIIN
10015340 Breather
006403774
1001550-0000-1616 Pipe To Tube Straight Adapter
007182621
10015524-009 Lug Terminal
002430409
10015708-001 Transistor
000445749
10015867-005 Thrust Ball Bearing
001008515
10015920-006 Watch Gauge Torque
008005361
1001597 Pipe Reducer
008730110
100160-001 Transistor
009790108
100163-102 Nonwire Wound Variable Resistor
001074881
100185 Ceramic Dielectr Fixed Capacitor
008047566
10018762-044 Machine Screw
009646032
10018772-003 Screw Thread Insert
008644958
10018772-005 Screw Thread Insert
009909916
10019 Transistor
009305325
1001975 Pipe To Tube Elbow
008353003
1001SPEC1424 Radio Frequency Detector
008777148
1002 Electrical Box Connector
001521072
1002 Angle Valve
002894383
1002-0001 Connector Adapter
007012215
10020 Transistor
009052926
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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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