Adam A700
| Adam A700 | |
|---|---|
 Adam A700 |
|
| Type: | Business jet |
| Design country: | |
| Manufacturer: | |
| First flight: |
July 28, 2003 |
| Commissioning: |
In flight testing |
| Production time: |
In production |
| Number of pieces: |
2 |
The Adam A700 aircraft is a twin- engine business jet with a low- wing design . The Minijet - Very Light Jet - has a takeoff weight of less than 4540 kg.
The two jet engines are mounted on the rear right and left of the airframe. The double tail girders are connected to one another by the horizontal tail. The machine has a pressurized cabin and a retractable undercarriage and is largely made of carbon fiber reinforced plastic . The machine is based around 80% on the design of the Adam A500 . The prototype first flew on July 28, 2003.
Technical specifications
| Parameter | Data |
|---|---|
| length | 12.38 m |
| span | 13.41 m |
| height | 2.89 m |
| Cabin length | 4.87 m |
| Cabin width | 1.37 m |
| Cabin height | 1.31 m |
| Cabin pressure | corresponds to 2,400 m at an altitude of 12,500 m |
| Range | 2,590 km |
| Top speed | 630 km / h |
| Service ceiling | 12,500 m |
| Max. Takeoff weight | 3,175 kg |
| Max. Payload | 328 kg at max. Fuel loading |
| Pilots | 2 |
| Max. Seats | 8th |
| Engines (2 ×) | Williams FJ33-4A turbofan engine with 545 kp (5.33 kN) static thrust each |
| Tank capacity | 1,500 l |
See also: List of aircraft types
Individual evidence
- ^ Planes of the World 2007, ISBN 3-613027-40-2 , page 13