Ch-53a/d/e Helicopter Parts

(Page 61) End item NSN parts page 61 of 66
Part Number
NSN
NIIN
65302-12147-084 Aircraft Fairing
000239512
65302-12544-041 Separator Blower Wire Fairing
008292189
65302-12554-041 Separator Blower Wire Fairing
008292189
65302-12559-106 Pressure Switch
012343189
65302-12607-041 Left Hand Support Assembly
010062204
65302-12619-101 Suppressor Serrated Strap
010036817
65307-03008-102 Poppet Drain Cock
001713203
65307-03028-101 Tube To Boss Tee
007615453
65307-03043-106 Quick Disconnect Coupling Half
000573072
65307-03058-101 Fuel System Connector
000278778
65307-03066-041 Fuselage Tube
000500931
65307-03095-101 Float Type Liquid Quantity Gage
001105430
65307-08015-101 Pressure Indicator
009437949
65307-08075-042 Sponson Connector Assembly
000501821
65308-12047-103 Liquid Level Switch
011217066
65311-03012-102 Push-pull Control Assembly
011293916
65312-12026-103 Fitting
012967222
65313-09021-101 Air Bleed Reservoir
011396916
65313-09028-047 Exhaust Pipe
011476259
65315-12000-051 Cowling
011428949
Page: 61

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.

Jetzt vergleichen»
Klar | Verstecken