Ch-53a/d/e Helicopter Parts

(Page 34) End item NSN parts page 34 of 66
Part Number
NSN
NIIN
353-6443-010 Semiconductor Device Set
009004819
354-1028-00 Electronic Chopper
000830687
354-1028-000 Electronic Chopper
000830687
3567742-4701 Pressure Transmitter
000653235
357-7902-050 Electrical Plug Connector
012757271
357-9335-00 Connector Adapter
006156889
357-9335-000 Connector Adapter
006156889
357-9418-00 Electrical Receptacle Connector
006863479
357-9418-000 Electrical Receptacle Connector
006863479
357-9607-00 Electrical Receptacle Connector
000614641
357-9607-000 Electrical Receptacle Connector
000614641
3582AS111-001 Welding Stud
014593105
360-62-431SH Hose Clamp
009885290
360301748 Needle Roller Bearing
002272980
361C7422-01-020 Electrical-electron Mounting Pad
009166189
362-0415 End Chain Link
012560470
365-41682 Branched Wiring Harness
010624001
3676K70P002 Flywheel
004318229
368SW Rotary Switch
009438047
Page: 34 ...

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