Mh-53e Helicopter Parts

(Page 234) End item NSN parts page 234 of 238
Part Number
NSN
NIIN
138917-8 Film Fixed Resistor
001470269
13896-1 Knob
013533816
13897D Lock Washer
005146674
138C515H02L2-1 Synchro Clamp
006105044
139-2230-000 Spring Tension Clip
000262135
139-2504-00 Crystal Holder Retainer
007951217
139-467 Electrical Contact
007896272
139-6845 Electrolytic Fixed Capacitor
013268362
1390-0046 Turnlock Fastener Receptacle
002820629
1390-0088 Fastener
010410678
1391939 Electric Temperature Transmitter
008145271
1392 PLAIN Lock Washer
001848971
1392 PLAINADX Lock Washer
001848971
139205008 Incandescent Lamp
002690944
139205011 Incandescent Lamp
001437432
1395AS790 Manual Control Lever
003554459
1397320 Electrical Plug Connector
006860447
139AS105 Wire Rope Swaging Sleeve
001329163
13AT271T2 Toggle Switch
002084674
13B23947-00 Transistor
000581178

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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