At a ceremony on May 6, 2015 at Royal Australian Air Force Base Townsville in northern Queensland, Australia commissioned their first two Boeing CH-47F Chinook advanced configuration aircraft. It is a major milestone in the updating of the Australian Army’s cargo helicopter fleet.
The acquisition is part of an ongoing transformation that is allowing Australia to build one of the world’s newest and most technologically advanced armed forces. Five additional new Chinooks will be delivered this year, eventually replacing an existing fleet of six older Boeing CH-47D Chinooks.
«The outgoing CH-47D Chinooks have proved highly effective in Australian operations, and the new CH-47F Chinook will deliver an improved cargo helicopter for Australia’s Army», said Rear Admiral Tony Dalton of Australia’s Defence Materiel Organisation. «Furthermore, the project to deliver the new Chinooks remains on schedule and under budget».
Australia was among the Chinook’s first international customers and now there are almost twenty countries operating the helicopter.
«Working with our Australian allies to build a modernised Chinook fleet enables more seamless operations with U.S. and other forces», said Colonel Robert Barrie, project manager, U.S. Army Cargo Helicopter Office.
«The Australian Army values the features and capabilities of the advanced CH‑47F Chinook and we delivered them as promised», said Steve Parker, Boeing vice president, Cargo Helicopters and H-47 program manager. «These aircraft will meet their demanding mission requirements now and well into the future».
The Australian Chinook fleet is flown by the Army’s 5th Aviation Regiment, 16th Aviation Brigade. Under the scope of the contract, Boeing Defence Australia will provide delivery and on-site operational maintenance support to the seven aircraft.
For more than 70 years, Boeing and Australia have maintained a partnership operating and supporting a broad range of platforms that now includes, in addition to Chinook, the Wedgetail Airborne Early Warning and Control System and C-17 Globemaster III.
|Rotor Diameter||18.29 m/60 feet|
|Length with Rotors Operating||30.14 m/98 feet, 10.7 inch|
|Fuselage||15.46 m/50 feet, 9 inch|
|Height||5.68 m/18 feet, 7.8 inch|
|Fuselage Width||3.78 m/12 feet, 5 inch|
|Fuel Capacity||20,411 kg/45,000 lbs|
|Maximum Gross Takeoff||36,700 kg/81,000 lbs|
|Maximum Gross Weight||22,680 kg/50,000 lbs|
|Useful Load||10,886 kg/24,000 lbs|
|Maximum Speed||170 KTAS/196 mph/302 km/h|
|Cruise Speed||157 KTAS/181 mph/291 km/h|
|Service Ceiling||6,096 m/20,000 feet|
|Mission Radius||200 NM/370.4 km|