Mh-53e Helicopter Parts

(Page 227) End item NSN parts page 227 of 238
Part Number
NSN
NIIN
134AV45511-13 Electrical Wire
005786593
134MKC1 Nonmetallic Hose
006767936
134MNX1 Nonmetallic Hose
010748373
134MPF1 Nonmetallic Hose
000097259
134WS239 Resistance Element
005721372
135-0682 Plastic Dielectr Fixed Capacitor
009053320
135-250 Arbitrary Scale Meter
000257110
135-30HM5 Induct Wire Wound Fixed Resistor
000603771
135-C-69 O-ring
002917336
135/100HM5PCT Induct Wire Wound Fixed Resistor
008890010
135/3300HM5PCT Induct Wire Wound Fixed Resistor
009847704
135001 Vent Plug
000742617
1350FX Pipe Bushing
001930869
1351813 Hose Clamp
012733671
1352 Hexagon Plain Nut
008911798
1352-4302 Composition Fixed Resistor
001145430
135272 Dial Indicating Pressure Gage
009988060
135283-003 Electrical Wire
007522038
13534 Annular Ball Bearing
001091157
1353AS109-1 Webbing Strap
012329199
Page: 227 ...

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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