Mh-53e Helicopter Parts

(Page 205) End item NSN parts page 205 of 238
Part Number
NSN
NIIN
127-61335-38 Induct Wire Wound Fixed Resistor
004451640
127-61338-38 Induct Wire Wound Fixed Resistor
004451640
127-65 Sleeve Bearing
009340249
12700E-02 Plate Self-locking Nut
007827094
12701 Electromagnetic Relay
011026488
12701954 Retaining Ring
005981474
12703463 Compression Helical Spring
004103130
12713-90 Windshield Wiper Arm
004022176
12715322 Electrical Receptacle Connector
010856512
1272955-23 Film Fixed Resistor
002233229
1272955PC23 Film Fixed Resistor
002233229
127517 Nonmetallic Hose
009335878
127574R91 Universal Joint Parts Kit
007024578
12759-00079 Hexagon Head Cap Screw
002253842
1276-08-129 Packing Retainer
001715073
1276-18-482 Machine Screw
006140246
1276-19-825 Spiral Wrap Plastic Tubing
007246175
127606637 O-ring
008331429
12775 Immersion Thermocouple
005514811
127855 Hexagon Plain Nut
008807745
Page: 205 ...

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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