Mh-53e Helicopter Parts

(Page 121) End item NSN parts page 121 of 238
Part Number
NSN
NIIN
10186003-2 Electrical-electronic Heat Sink
009276803
10186314 O-ring
001661055
101873 Nonmetallic Grommet
002766343
101882-4 Vehicular Stop Light-taillight
009610509
1018877-001 Electrical-electronic Heat Sink
007893794
1018905-100 Induct Wire Wound Fixed Resistor
008890010
1018907-004 Induct Wire Wound Fixed Resistor
000515557
1018917-821 Mica Dielectric Fixed Capacitor
010493153
1018935-001 Nonwire Wound Variable Resistor
005811403
10189474 Electrical Wire
005786593
008132078
007621489
006193837
1018989-003 Sleeve Spacer
003028099
1018997-029 Lock Washer
006163554
1018G1 Electric Temperature Transmitter
008145271
101916F Nonwire Wound Variable Resistor
007638769
10193 Electrical-electron Mounting Pad
010801971
10194483-002 Electrical Compone Tiedown Strap
009376691
10194683-1 Cartridge Lamp
009103282
Page: 121 ...

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.

Compare Now »
Clear | Hide