Mh-53e Helicopter Parts

(Page 62) End item NSN parts page 62 of 238
Part Number
NSN
NIIN
0800-117 Tubular Rivet
008214995
0800-215 Tubular Rivet
007215245
0800-329 Tubular Rivet
008260329
080023 Film Fixed Resistor Network
010517994
0801223Q00 Packing Retainer
008218848
0801225S00 Packing Retainer
008204142
0802100 Tapered Roller Cone And Rollers
006061841
0805-016Z5U0103Z Ceramic Dielectr Fixed Capacitor
008011005
080A37000 Plate Insulator
002464898
080A50600 Machine Bolt
001822016
08100-9752 Incandescent Lamp
009418488
0811-0653 Nonind Wire Wound Fixed Resistor
005066460
0811-1200 Induct Wire Wound Fixed Resistor
000455422
0811-1219 Induct Wire Wound Fixed Resistor
000818672
0811-1226 Induct Wire Wound Fixed Resistor
009882156
0811-1718 Induct Wire Wound Fixed Resistor
008890010
0811-3293 Induct Wire Wound Fixed Resistor
007075032
0811010X5U0 822M Ceramic Dielectr Fixed Capacitor
008139353
0811040W5R0 102K Ceramic Dielectr Fixed Capacitor
008225682
0812-0049 Wire Wound Fixed Resistor
011866838
Page: 62 ...

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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