Mh-53e Helicopter Parts

(Page 152) End item NSN parts page 152 of 238
Part Number
NSN
NIIN
109D406X0030C2 Electrolytic Fixed Capacitor
011194321
109D406X9075T2 Electrolytic Fixed Capacitor
011194333
109D686X0030FZ Electrolytic Fixed Capacitor
011194323
109D805C7030C2 Electrolytic Fixed Capacitor
011194306
10A17018 Electric Temperature Transmitter
008145271
10A200B2 Semiconductor Device Set
000876963
10A201 Electrical Plug Connector
005005183
10A6751 Tapered Roller Cone And Rollers
001000233
10A7838 Breather
006403774
10AM274 Fluid Filter Element
002871912
10AMPFB Cartridge Fuse
010587648
10B000218-11 Hexagon Plain Nut
008421190
10B000218P46 Hexagon Self-locking Nut
002694040
10B000221-8 Flat Washer
001670827
10C-0001-0009 Electrical Connector Cover
010597370
10DH-845-1 Electromagnetic Relay
005081815
10EJ3 Incandescent Lamp
000802012
10EJ4 Glow Lamp
000142870
10F100WL Induct Wire Wound Fixed Resistor
002586955
10F20 Induct Wire Wound Fixed Resistor
005491816
Page: 152 ...

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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