Ch-53a/d/e Helicopter Parts

(Page 56) End item NSN parts page 56 of 66
Part Number
NSN
NIIN
651C-3 Torque Gage
008053652
65201-02008-101 Air Structural Component Support
012467225
65201-02053-102 Mirror Fitting
011361392
65201-03013-044 Corner Fittingxassembly
009157420
65201-03015-041 Corner Fittingxassembly
009157420
65201-04017 Nonmetallic Tubing
009157709
65201-04017-104 Nonmetallic Tubing
009157709
65202-03052-084 Duct Assembly
010071095
65202-03082-042 Aircraft Access Door
000429939
65202-05051-041 Fitting Assembly
000145790
65202-05051-042 Fitting Assembly
000145791
65202-06034-104 Thrust Washer Bearing
009988414
65205-02006-107 Fairing Sleeve
000511696
65205-06014-041 Ramp Supportxassembly
009157339
65205-07001-045 Aircraft Fairing
001093041
65205-08025-041 Fuel Tank Fairing
008904160
65205-08026-042 Fuel Tank Support Fairing
001111590
65205-08028-101 Support Fairing
002052277
65206-01006-102 Aircraft Window Panel
009389589
65207-01004-107 Follower Bearing
009389670
Page: 56 ...

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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