TAM AIR JET
A joint memorandum envisaging the establishment of a joint company was signed between JSC TAM-TBILISI AIRCRAFT MANUFACTURING and AIR LLC on May 5 of 2005.
The employees of JSC TAM and AIR LLC designed and assembled the mentioned aircraft. Flight tests of Tam Air Jet are planned by the end of April of 2007.
|
Specification |
|
|
Passenger |
6-8 |
|
Structure |
Carbon Fiber |
|
Sealing |
6.5 |
|
Engine |
Williams International FJ-33-4A |
|
Overall dimensions |
|
|
Length |
36.8 ft |
|
Takeoff run |
43 ft |
|
Height |
12.5 ft |
|
Net wing area |
203.6 sq. ft |
|
Cockpit length |
15 ft |
|
Cockpit width |
4.6 ft |
|
Cockpit height |
4.9 ft |
|
Weights |
|
|
Empty weight |
4,200 lbs |
|
Max. takeoff weight |
7,329 lbs |
|
Max. load with fuel |
1,200 lbs |
|
Specifications |
|
|
Max. cruising |
350 KTAS |
|
Economic |
289 KTAS |
|
Max. roofing |
28,000 ft |
|
Ascension |
28,000 ft., 11 min. |
|
Range ability at max. cruising speed |
1369 NM |
|
Range ability at economic cruising speed |
1608 NM |
|
Takeoff |
1,600 ft |
|
Landing |
1,840 ft |
|
Fuel qty |
288 gallons usable |