FAA approves TAM’s LPV-modification for the Saab 2000
Örebro, Sweden: On Wednesday, October 25th, TAM’s new, easy-to-install, LPV-solution for the S...
| Maximum take-off weight | 29000 lb | 13155 kg |
| Maximum landing weight | 28500 lb | 12925 kg |
| Maximum zero fuel weight | 26500 lb | 12020 kg |
| Operational empty weight (average) | 17100 lb | 7755 kg |
| Maximum payload | 9400 lb | 4264 kg |
| Maximum fuel capacity | 5690 lb | 2580 kg |
| Maximum cruise speed | 283 kt | |
| Maximum operating altitude | 25000 ft | 7620 m |
| SL, optimal flaps | ISA | ISA+10°C | ISA+20°C | |
|---|---|---|---|---|
| Maximum take-off weight | Ib | 29000 | 29000 | 29000 |
| kg | 13155 | 13155 | 13155 | |
| Take-off distance required | ft | 4320 | 4575 | 4800 |
| m | 1315 | 1395 | 1465 |
| 5000 ft MSL, optimal flaps | ISA | ISA+10°C | ISA+20°C | |
|---|---|---|---|---|
| Maximum take-off weight | Ib | 29000 | 29000 | 29000 |
| kg | 13155 | 13155 | 12860 | |
| Take-off distance required | ft | 5490 | 6590 | 6985 |
| m | 1675 | 2010 | 2130 |
| SL, ISA optimal flaps, max cruise (Includes 100 nm diversion & reserves) | 100 nm | 200 nm | 300 nm | 400 nm | 500 nm | |
|---|---|---|---|---|---|---|
| Take-off weight | lb | 27540 | 28033 | 28475 | 28808 | 29000 |
| kg | 12492 | 12716 | 12923 | 13067 | 13154 | |
| Block fuel | lb | 609 | 1078 | 1499 | 1816 | 1972 |
| kg | 276 | 489 | 680 | 824 | 895 | |
| Block time (4 min ground time) | min | 31 | 53 | 74 | 96 | 122 |
| Cargo | lb | 9400 | 9400 | 9400 | 9400 | 8957 |
| kg | 4264 | 4264 | 4264 | 4264 | 4063 |
| Dowty Rotol | Hamilton Sundstrand |
||
|---|---|---|---|
| Fly-over | EPNdB | 78.5 | 78.3 |
| Sideline | EPNdB | 85.9 | 86.1 |
| Approach | EPNdB | 91.6 | 90.1 |
| Length | 64 ft 9 in | 19.73 m |
| Height | 22 ft 11 in | 6.97 m |
| Wing span | 70 ft 4 in | 21.44 m |
| Propeller ground clearance | 1 ft 8 in | 0.51 m |
| Cargo door (H x W) | 51 in x 53 in | 1.30 m x 1.35 m |
| Sill height, passenger door | 5 ft 4 in | 1.64 m |
| Sill height, cargo door | 5 ft 6 in | 1.68 m |
| Production serial no. | SAAB 340B: 160-359 SAAB 340B Plus: 360-459 |
|
| ENGINE | (2)GECT7-9B |
| Maximum take-off power (ISA, APR) | 1870 shp |
| Propeller | DowtyRotol/ HamiltonSundstrand |
| Length | Volume | Floor load limits | ||||
|---|---|---|---|---|---|---|
| Section A | 6 ft 11 in | 2.1 m | 75 cu ft | 2.1 cu m | 75 lb/sqft | 365 kg/sq m |
| Section B | 25 ft 10 in | 7.9 m | 901 cu ft | 25.5 cu m | 100/150* lb/sq ft | 485/730* kg/sq m |
| Section C | 10 ft 5 in | 3.2 m | 300 cu ft | 8.5 cu m | 150 lb/sq ft | 730 kg/sq m |
| Total | 43 ft 2 in | 13.2 m | 1276 cu ft | 36.1 cu m | *using spreaders as per 340 cargo WBM |
Örebro, Sweden: On Wednesday, October 25th, TAM’s new, easy-to-install, LPV-solution for the S...
Örebro, Sweden: On Monday, March 6th, the new Saab 2000F took to the air for the first time.The ...
Örebro, Sweden: On Monday, March 6th, the new Saab 2000F took to the air for the first time.The ...