Ch-53a/d/e Helicopter Parts

(Page 23) End item NSN parts page 23 of 66
Part Number
NSN
NIIN
2271 Electronic Chopper
000702271
229316 Connector Adapter
004916302
2296922P3 Electrical Plug Connector
000639010
22NCFMA2-40 Spline Self-locking Nut
010578778
22NTM60 Hexagon Self-locking Nut
007272809
23-0200-0600 O-ring
001051122
23-S-125-0937 Spring Pin
002347456
230-304SS Machine Screw
008160032
23038-1 Base Shock Mount
010383221
23038-1A Base Shock Mount
010383221
23075 Chronograph Spring
007992965
23111388 Air Bleed Reservoir
011396916
2312634 Direct Current Motor
006290967
2312G8 Indicating Pyrometer
003083862
231P103 Paper Dielectric Fixed Capacitor
004688352
23200 Electron Panel Assembly
009563848
234SP-002 Composition Fixed Resistor
000619550
235-007-2005 Turnlock Fastener Stud
006527289
235-9058P4 Diode Semiconductor Device
000507309
23591 Pipe Nipple
007848498
Page: 23 ...

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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