Mh-53e Helicopter Parts

(Page 14) End item NSN parts page 14 of 238
Part Number
NSN
NIIN
009-7188 O-ring
006842070
0097815 Electrical Insulation Sleeving
000523301
0097815-FH00 Electrical Insulation Sleeving
000523301
0097815-FH00-001 Electrical Insulation Sleeving
000523301
0097816 Electrical Insulation Sleeving
000523297
0097816-FH00 Electrical Insulation Sleeving
000523297
0097816-FH00-001 Electrical Insulation Sleeving
000523297
0097817 Electrical Insulation Sleeving
000896041
0097817-FH00 Electrical Insulation Sleeving
000896041
0097817-FH00-001 Electrical Insulation Sleeving
000896041
0097819 Electrical Insulation Sleeving
009596336
0097819-FH00 Electrical Insulation Sleeving
009596336
0097844 Electrical Insulation Sleeving
007670511
0097844-FH00 Electrical Insulation Sleeving
007670511
0098-LL-TJ2-2552 Compression Helical Spring
004103130
0098-LL-TJ2-2553 Compression Helical Spring
011773426
0098-LL-TJ2-2686 Glass Dielectric Fixed Capacitor
001317444
009876-66502 Power Supply Assembly
011872559
009895 Extractor Post Fuseholder
008814636
009A4145 Plain Encased Seal
008087595
Page: 14 ...

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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