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CH-53K King Stallion

CH-53K King Stallion

Utility & Transport Helicopters
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Basic Information
Name
CH-53K King Stallion
Designation
CH-53K King Stallion
Alternate Designation
CH-53X, HLR
Equipment Type
Utility & Transport Helicopters
Manufacturer
Sikorsky Aircraft Corporation, Aurora Flight Sciences, Exelis, GKN Aerospace, Rockwell Collins, Spirit AeroSystems
Date of Introduction
2022
Description

The US Marine Corps Heavy Lift Replacement (HLR) program was launched for the development and production of 156 new-built helicopters derived from the CH-53E Super Stallion. The HLR program started in 2004 with an initial risk reduction contract award to Sikorsky. According to the USMC plans the first HLR test aircraft should be delivered to the Corps in 2014. The intended HLR/CH-53X helicopter features upgraded engines, improved rotor blades, new avionics, new rotorhead, improved survivability, and longer service life than Super Stallion. Based on the CH-53E Super Stallion the CH-53X will nearly double to 27,000 pounds over 110 nautical miles. The aircraft's maximum gross weight will increase to 84,700 pounds. On April 5, 2006 Sikorsky received a $3 billion contract from the United States Marine Corps for the CH-53K, previously known as the CH-53X, heavy-lift helicopter System Development and Demonstration (SDD). Work was to be centered at Stratford facility, Connecticut, with the SDD completion expected by December 2015. In late June 2006, Sikorsky Aircraft announced the Rockwell Collins selection to provide the CH-53K avionics management system (AMS). AMS consists of five fully integrated active matrix liquid crystal multifunction displays (MFD), dual integrated processing cabinets (IPC), dual control display units (CDU), and dual data transfer units (DTU). On May 5, 2014, the CH-53K was revealed as the King Stallion. The first CH-53K King Stallions are planned to achieve initial operational capability within the USMC by 2019 but finally they were cleared for operational use on April 25, 2022.

Air & Air Defense Specifications
Range 203.7 km
Overview (Deagel)
Group Utility & Transport Helicopters
Status Active
Also Known As CH-53X, HLR
Origin United States of America
Contractors Sikorsky Aircraft Corporation*, Aurora Flight Sciences, Exelis, GKN Aerospace, Rockwell Collins, Spirit AeroSystems
Initial Operational Capability (IOC) April 25, 2022
First Flight October 27, 2015
Total Production 212
Unitary Cost USD $112 million
Specifications (Deagel)
Main Rotor Blades 7
Number of Engines 3
Tail Rotor Blades 4
Mass — Max Takeoff Weight 74,000 pound
Mass — Max Takeoff Weight with External Load 88,000 pound
Mass — Payload 27,000 pound
Performance — Max Range 110 nautical mile
Gear (Deagel)
Item 1 ESM & Warning Systems: AN/APR-39D(V)2
Item 2 Tactical Vehicles: LSV (1)
Item 3 Turboshaft Engines: T408-GE-400 (3)
Variants
Variant 1 CH-53D Sea Stallion
Variant 2 CH-53E Super Stallion
Variant 3 MH-53J Pave Low III
Variant 4 CH-53K King Stallion
Details
Country of Origin United States
Category Transport Helicopter
Air > Transport Helicopter
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
33566.4 kg
Related Equipment (1)
Operators (2)
United States
Israel
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