Mh-53e Helicopter Parts

(Page 214) End item NSN parts page 214 of 238
Part Number
NSN
NIIN
130-017-5682 Transistor
010169906
130-087 Ceramic Dielectr Fixed Capacitor
009371328
130-0935-003 Light Lens
004019773
130-0937-003 Light Lens
004813334
130-1015-020 Electrical Wire
008397432
130-249 Transistor
001798478
130-7757 O-ring
011132083
1300-26 Electromagnetic Relay
010389192
13000-256F16 Socket Head Cap Screw
009528492
13000041-007 Plastic Dielectr Fixed Capacitor
009053320
13001 Diode Semiconductor Device
007614631
1300219 Film Fixed Resistor
011782225
1300275 Film Fixed Resistor
011707738
1300S3-3 Wire Wound Fixed Resistor
011866855
1301-015-G003 Electrical Plug Connector
009310412
1301015G003-000 Electrical Plug Connector
009310412
1301313-13 Diode Semiconductor Device
005430490
13014410-8 Hexagon Head Cap Screw
007813927
1301643-00 Induct Wire Wound Fixed Resistor
000603771
1301694 Tapered Roller Bearing Cup
001000594
Page: 214 ...

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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