Mh-53e Helicopter Parts

(Page 187) End item NSN parts page 187 of 238
Part Number
NSN
NIIN
11SM1 Sensitive Switch
005836582
11TA-0541 Motor-tachometer Generator
010918181
11TX-300-N-22A/10 Transmitter Synchro
000188604
12 Muffler- Protective Cap Assembly
004381551
12 070115C Tube Fitting Flared Sleeve
004333377
12 080110C Tube Coupling Nut
004602086
12 V5OLO-S Tube To Boss Elbow
013511581
12-1 Synchro Clamp
006105044
12-100024 Transistor
009478263
12-1016 Transistor
008280723
12-12 070220CA Tube To Boss Elbow
010117736
12-12 130239B Pipe Elbow
009477474
12-12 140130C Pipe Coupling
009580384
12-12 160143CA Pipe To Hose Straight Adapter
005682200
12-12 250146CA Tube To Hose Straight Adapter
008815536
12-12246-0A Film Fixed Resistor
004320430
12-12354-0A Film Fixed Resistor
001120972
12-12600-0A Film Fixed Resistor
001892454
12-13013-008 Diode Semiconductor Device
009042020
12-13202-0A Wire Wound Fixed Resistor
011840764
Page: 187 ...

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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