Mh-53e Helicopter Parts

(Page 31) End item NSN parts page 31 of 238
Part Number
NSN
NIIN
0251299 Hexagon Plain Nut
008421190
0251368 Hexagon Self-locking Nut
000679507
0251401 Hexagon Head Cap Screw
002258507
0251426 Hexagon Head Cap Screw
002259093
0251428 Machine Bolt
002259095
0251561 Machine Bolt
002259087
0253199 Straight Flute Drill
012951985
025481-0003 Quick Disconnect Terminal
009260085
025738-0003 Light Lens
000801048
025997-0006 Lug Terminal
001141311
026-C-69 O-ring
009513150
026165 Tubeaxial Fan
002265872
026202 Diode Semiconductor Device
004503015
0265 V Belt
005284451
0266768-00 Hydraulic Brak Cylinder Assembly
000322638
026676800 Hydraulic Brak Cylinder Assembly
000322638
0270467 Igniter Assembly
002936481
02717 Electrical Power Cable
010429008
02725 Packing Retainer
011174238
027380-0001 Conductor Splice
011357085
Page: 31 ...

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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