Mh-53e Helicopter Parts

(Page 217) End item NSN parts page 217 of 238
Part Number
NSN
NIIN
13086283-1 Hexagon Self-locking Nut
004780259
1309 Annular Ball Bearing
005543468
1309-0020-P1 Solder Extractor Filter
011490247
1309-0027 Solder Extractor Filter
011487954
1309-0027-P10 Solder Extractor Filter
011487954
13090020 Solder Extractor Filter
011490247
13090027 Solder Extractor Filter
011487954
1309412 Film Fixed Resistor
004315163
130972 Flat Washer
001861295
130A2335 O-ring
008116503
130D686X0040T0 Electrolytic Fixed Capacitor
011194332
130D686X9040T2 Electrolytic Fixed Capacitor
011194332
130D826X0050F2 Electrolytic Fixed Capacitor
010314489
130MAN1 Lock Washer
005146674
131-016-0001 Multimeter
010904458
131-0510 Mica Dielectric Fixed Capacitor
010537975
131-0589-00 Electrical Contact
002750213
131-0792-00 Electrical Contact
010231578
131-10270 Drain Cock
002769041
131-313-3 Annular Ball Bearing
005555210
Page: 217 ...

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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