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Adam A700  
Initial Operational Capability (IOC): 2008
Maiden Flight: 6 February 2006
Total Production: ?
Unitary Cost: USD$2.5 million
Also Known As: A700 AdamJet
Origin: United States of America
Corporations: Adam Aircraft
Parent System: Adam A700
Initial Operational Capability (IOC): 2008
Maiden Flight: 27 July 2003
Total Production: ?
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Description: The Adam A700, formerly known as A700 AdamJet, is a light twin-turbofan business jet designed to carry two pilots and five passengers over ranges of up to 1,100 nautical miles (2,000 kilometers). Adam Aircraft launched the A700 project in 2002 with the first prototype performing its maiden flight in July 2003. The first production aircraft took to the air on February 6, 2006. FAA aircraft type certification and first customer deliveries are anticipated in 2008 with EASA certification expected sooner thereafter to enable European operations.

The Adam A700 jet is powered by two pylon-mounted Williams International FJ33-4A turbofan engines on the aft fuselage. Each engine develops 1,350 pounds of thrust at takeoff. The FJ33-4A engine has a mid-life inspection at 1,750 hours and overhaul at 3,500 flight hours. The aircraft features a top speed of 0.7 Mach and a maximum range of 1,400 nautical miles (2,500 km) with fuel reserves. The Adam A700 outstands by its aerodynamic configuration combining blended high horizontal tail with tailless carbon fiber composite materials fuselage.

Adam A700 Specifications

Crew: 2
Number of Engines: 2
Passengers: 5
Dimensions
Cabin Height: 52 inch (1.31 meter)
Cabin Length: 16 foot (192 inch)
Cabin Width: 54 inch (1.37 meter)
Performance
Ceiling: 41,000 foot (12,497 meter)
Max Range: 1,400 nautical mile (1,611 mile)
Take Off Run Distance: 3,400 foot (1,036 meter)
Pressure
Differential Pressurization: 8.33 psi
Speed
Cruise Speed: 340 knot (629 kph)
Top Speed at High Altitude: 0.70 mach (452 KTAS)
Volume
Fuel Tank Capacity: 394 galon (1,497 liter)
Weight
Fuel Load: 725 pound (329 kilogram)
Max Landing Weight: 9,000 pound (4,082 kilogram)
Max Takeoff Thrust: 2,700 pound
Max Takeoff Weight: 9,350 pound (4.24 ton)
Max Zero Fuel Weight: 5,980 pound (2,713 kilogram)
Operational Weight: 6,200 pound (2,812 kilogram)
Payload: 3,150 pound (1,429 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Adam A700 News

There is 1 news
on 9 Apr 2008
Wednesday, April 9, 2008AAI Acquisition Purchases Assets of Adam Aircraft Industries

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
FJ33-4Ax2
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