Program launch date 2002
First flight date July 27, 2003
Certification date 2008
First delivery date 2008
Number of crew + pax 2 crew + 5 including private lavatory
Cabin dimensions
      Length 16 ft (4.88m)
      Height 4.3 ft (1.31m)
      Width 4.5 ft (1.37m)
Engine make & model Williams FJ33
Number of engines on a/c Two
Engine certification date 2004
Engine thrust rating (sl, ISA, flat-rated) 2,700 lbf (12.01 kN)
Avionics suite Avidyne 3-screen FlightMax Entegra
Max takeoff weight 9,350 lbs (4,250 kg)
Max landing weight 9,000 lbs (4,091 kg)
Zero fuel weight 5,980 lbs (2,718 kg)
Basic operating weight (includes req’d. flight crew, 200 lb each) 6,200 lbs (2,818 kg)
Max fuel weight 2,647 lbs (1,203 kg)
Vmo/Mmo 260/.7
High-speed cruise speed 340 KTAS (630 km/h)
NBAA IFR range (nm) at long-range cruise* 1,100 NM (2,037 km)
Balanced field length (ISA, sl) 3,400 ft (1,036m)
Certified ceiling 41,000 ft (12,497m)
Cabin altitude at certified ceiling 8,000 ft (2,438m)
Standard equipped price (Jan. 2008) $2.45 million


General Disclaimer: The Adam A700 is currently in the FAA certification process. The certification process is complex and unpredictable and may result in design, performance, and other specification changes to the aircraft. The company cannot predict or commit to the time of certification. Until the FAA issues the final type certification for the aircraft, Adam Aircraft specifically disclaims responsibility for and makes no representation as to the final design, performance, capabilities, and specifications of its aircraft. Nothing in this document shall in any way bind the company to a certification date, design, performance, or specifications for the aircraft.

* 100 nm alternate, 45 min reserve.


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