Ch-53a/d/e Helicopter Parts

(Page 40) End item NSN parts page 40 of 66
Part Number
NSN
NIIN
440HJ030NF2309-16H2 Electrical Connector Backshell
014601701
44140 Ignition Coil
001389494
443-1402-297 Film Fixed Resistor
001084254
44381 50201 Diode Semiconductor Device
000507309
447-015 Pipe Cap
009387848
44A253487-001 Diode Semiconductor Device
004578045
44A253487P1 Diode Semiconductor Device
004578045
44A258956-005 Diode Semiconductor Device
004578045
44A350028-011 Diode Semiconductor Device
004578048
44B256259-121 Paper Metallized Fixed Capacitor
000899745
44B256259-171 Paper Metallized Fixed Capacitor
000899745
44B256259P121 Paper Metallized Fixed Capacitor
000899745
44B256259P171 Paper Metallized Fixed Capacitor
000899745
44B355787-001 Power Transformer
004829384
44G26451 Aircraft Safety Belt
005166550
45-0253-1 Aircraft Landing Light
013247046
45-0253-17 Aircraft Landing Light
013247046
45-1706 Aircraft Safety Belt
005166542
45-6084-0000 Indicating Pyrometer
012902935
4506232 Solid State Relay
004604476
Page: 40 ...

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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