Mh-53e Helicopter Parts

(Page 122) End item NSN parts page 122 of 238
Part Number
NSN
NIIN
10195323 Hexagon Slotted Self-locking Nut
000664289
10196829 Push Switch
007586020
10197438 O-ring
010573133
1019744-001 Turnlock Fastener Receptacle
006388088
10198960 Transistor
002439159
10199-42472 Electrolytic Fixed Capacitor
009593298
1019900086 Annular Ball Bearing
008123603
1019900127 Annular Ball Bearing
000196390
10199290 Wire Rope Swaging Sleeve
011325671
101A10002-04 Retaining Ring
008129828
101A710AA-8 Cotter Pin
008457787
101A743AD PIECE Spring Pin
008369628
101F9207-3 Plate Self-locking Nut
007793601
101FTM15A03 Dial Indicating Pressure Gage
009988058
101R01304 Film Fixed Resistor
001956377
101T1900 Electrical Plug Connector
001366912
102-00000 Electric Temperature Transmitter
003739004
102-0070 Pipe To Tube Straight Adapter
005402612
102-0191 Tube To Boss Elbow
008525581
102-0195 Tube To Boss Elbow
010117736
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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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