Ch-53a/d/e Helicopter Parts

(Page 7) End item NSN parts page 7 of 66
Part Number
NSN
NIIN
101A10002-04 Retaining Ring
008129828
101PT100A1 Synchro Assembly
009390461
102-07526 Plug-in Electronic Compon Socket
000891868
102187 Radio Receiver Support
008666837
10250039-1 Spring Tension Washer
010989978
103-0109-020 Sleeve Bearing
013548269
10368143 Voltmeter
007296723
10399486 Wire Rope Swaging Sleeve
000655088
103P36 Paper Dielectric Fixed Capacitor
010634334
103P608 Paper Dielectric Fixed Capacitor
010634334
1046938 Scale Dial
005827778
10510553 Pump Piston Assembly
001049293
10510557 Hydraulic Mo Cylinder Block Unit
001362424
10510559 Compression Helical Spring
011608053
10510574 Wearing Ring
001466880
10556107 Connector Adapter
004916302
10606702-1 Tube To Boss Tee
007571945
10620SY10-4 Push Switch
011520625
10638480 End Chain Link
012560470
106447 Radio Receiver Support
003980460
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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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