Mh-53e Helicopter Parts

(Page 221) End item NSN parts page 221 of 238
Part Number
NSN
NIIN
1321-0 Electrical Wire
001647026
1321-M09-F09-440 Spacing Threaded Standoff
008576189
1321-M09-F16-440 Spacing Threaded Standoff
008576189
132105 Machine Screw
005432753
13211-6755 Pipe Reducer
006406330
13211E3363 Turnlock Fastener Eyelet
002822045
13211E3364 Retaining Ring
005981474
13211E4015 Liquid Sight Indicator
007911419
13211E4043-42 Tube Tee
002636482
13211E4930 Dust And Moisture Protective Cap
000713831
13211E6755 Pipe Reducer
006406330
13211E9143 Breather
006403774
1321324-4 Annular Ball Bearing
005543468
13213E0643-3 Liquid Sight Indicator
007783914
132143291-5 Assembled Washer Plain Nut
006965173
13214E3290-18 Assembled Washer Screw
000366968
13215E7891 Electrical Box Connector
002807763
13215E9649 Electrical Receptacle Connector
005572054
13216E3177 Electric Temperature Transmitter
008145271
13216E3789-3 Blind Rivet
008828388
Page: 221 ...

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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