Ch-53a/d/e Helicopter Parts

(Page 13) End item NSN parts page 13 of 66
Part Number
NSN
NIIN
124-1553929 PART NO. 35 Sleeve Bearing
006861011
124008B0144C305 Nonmetallic Hose Assembly
013991881
126-108 Pitot-static Tube
005267852
12621-1 Adapter Assembly
009910806
12636-1 Branched Wiring Harness
011603815
128-007-0010 Electrical-electron Mounting Pad
009166189
128236 Electronic Components Shield
006746488
12881-1 Spring Adjustment Lever
012204456
12908-1 Ring Spacer
011465818
12Z10003-366 Sleeve Bearing
006861011
12Z64PC4 Retaining Ring
002827127
130560 Locked In Stud
006378908
130D826X0050F2 Electrolytic Fixed Capacitor
010314489
1311025-001 Pump Rotor
012766097
131286-01 Synchro Rotor
007161869
1338-90C Aircraft Instruments Filter
004761396
1338-91C Dehydrator
004761460
13380-2B Arbitrary Scale Meter
000257110
13380-2C Arbitrary Scale Meter
000257110
134-002 Tachometer Generator
005568195
Page: 13 ...

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.

Compare Now »
Clear | Hide