Ch-53a/d/e Helicopter Parts

(Page 20) End item NSN parts page 20 of 66
Part Number
NSN
NIIN
1995994 Radio Frequency Cable Assembly
012635337
1995994-1 Radio Frequency Cable Assembly
012635337
1MR 3319 Pressure Switch
011496864
1MR3319A Pressure Switch
011496864
1MR3319P1 Pressure Switch
011496864
1N1345A Diode Semiconductor Device
008560083
1N1838 Diode Semiconductor Device
000113581
1N1893AR Diode Semiconductor Device
010266123
1N2846 Semiconductor Device Set
009004819
1N4436 Thyristor Semiconductor Device
004117614
1N5920B Diode Semiconductor Device
004578048
1N953 Diode Semiconductor Device
000507309
1RA12 Inner Bearing Ring
009355757
1VC1085-14 Aircraft Seat
000580758
2-138 47-071 O-ring
008006353
2-236 47-071 O-ring
006847795
006847795
2-268 N506-65 O-ring
008267751
2-320572-3 Lug Terminal
002424608
20-198 Shoulder Screw
009870066
Page: 20 ...

Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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