Mh-53e Helicopter Parts

(Page 40) End item NSN parts page 40 of 238
Part Number
NSN
NIIN
040896 Gasket
005510433
041-010 Ceramic Dielectr Fixed Capacitor
008225682
041-593 Composition Fixed Resistor
001145352
041-675 Composition Fixed Resistor
005046897
0411161-139 O-ring
008008718
041508101807EWS Electrical Wire
005003079
0419-544 Hexagon Head Cap Screw
007088385
041K60900 Machine Screw
005147506
042-20063-003 Electrical Plug Connector
005735709
042-20063-013 Connector Adapter
010444448
042-977 Film Fixed Resistor
002016784
042022-3 Electrical Plug Connector Body
010878450
04210008+008 Composition Fixed Resistor
001048332
04210008-008 Composition Fixed Resistor
001048332
04247306 Strapping
002459440
04248305 Strapping Seal
002447327
04250004+007 Induct Wire Wound Fixed Resistor
000612089
04250004+010 Induct Wire Wound Fixed Resistor
009516735
04250004-007 Induct Wire Wound Fixed Resistor
000612089
04250416201850 Connector Adapter
007012215
Page: 40 ...

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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