Ch-53a/d/e Helicopter Parts

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Filter By: Shear Bolts
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Part Number
NSN
NIIN
73989-8-16 Shear Bolt
010675184
73989-9-20 Shear Bolt
011250922
73989-9-24 Shear Bolt
000837056
MIL-B-8831 Shear Bolt
013591380
MS21250-08011 Shear Bolt
013591380
NAS1304-25 Shear Bolt
008265338
NAS464-6-24 Shear Bolt
002926452
NAS6203-9 Shear Bolt
008693694
NAS6206-18 Shear Bolt
011006948
NAS627-9 Shear Bolt
011237107
NAS628-13 Shear Bolt
009738980
NAS630-24 Shear Bolt
007205932
NAS630-36 Shear Bolt
008222024
NASM8831 Shear Bolt
013591380
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Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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