Mh-53e Helicopter Parts

(Page 191) End item NSN parts page 191 of 238
Part Number
NSN
NIIN
12047-0046 Transistor
009281006
120470 O-ring
008331428
1205-0011 Electrical-electronic Heat Sink
007893794
120512-007 Annular Ball Bearing
008123603
1205RRANG25 Annular Ball Bearing
001091157
120605018 Ceramic Dielectr Fixed Capacitor
010904098
12062 Electrical Power Cable Assembly
004194305
1206200 Linear Microcircuit
011281851
120655H1 Ball Stud Adjusting Plug
013023051
1207-0043 Tip Jack
007295559
1207387H1 Electromagnetic Relay
007359542
12074-0007 Transistor
001629773
120744-000 Radio Frequency Cable
008355840
120750ITEM9 Tubeaxial Fan
000186535
120751ITEM9 Tubeaxial Fan
000186535
12076FX Nonmetallic Grommet
001850001
1207AS130 Fluid Filter Element
010271434
1207AS130-1 Fluid Filter Element
010271434
12085A Filler Opening Cap
001419758
1208803H1 Ignition Coil
003361702
Page: 191 ...

Helicopter, Mh-53e

Picture of Mh-53e 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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