| 1 | A | B | C | D | E |
| --- | --- | --- | --- | --- | --- |
| 2 | Piper PA-46 - Specifications |  |  |  |  |
| 3 | Model | Matrix | M350 | M500 | M600 |
| 4 | Seating | 6 | 6 | 6 | 6 |
| 5 | Cabin Volume | 201 cu ft (5.7 m3) | 201 cu ft (5.7 m3) | 201 cu ft (5.7 m3) | 201 cu ft (5.7 m3) |
| 6 | Pressurization | 0 | 5.6 psi (390 hPa) | 5.6 psi (390 hPa) | 5.6 psi (390 hPa) |
| 7 | Wingspan | 43.0 ft / 13.11 m | 43.0 ft / 13.11 m | 43.0 ft / 13.11 m | 43.16 ft / 13.15 m |
| 8 | Length | 28.11 ft / 8.6 m | 28.11 ft / 8.6 m | 29.6 ft / 9.02 m | 29.7 ft / 9.05 m |
| 9 | Height | 11.3 ft / 3.44 m | 11.3 ft / 3.44 m | 11.3 ft / 3.44 m | 11.3 ft / 3.44 m |
| 10 | MTOW | 4,340 lb / 1,969 kg | 4,340 lb / 1,969 kg | 5,092 lb / 2,310 kg | 6,000 lb / 2,721 kg |
| 11 | OEW | 3,003 lb / 1,362 kg | 3,050 lb / 1,383 kg | 3,436 lb / 1,559 kg | 3,650 lb / 1,656 kg |
| 12 | Fuel Capacity | 120 USgal / 454 L | 120 USgal / 454 L | 170 USgal / 644 L | 260 USgal / 984 L |
| 13 | Constant-speed propeller | 3 blade | 3 blade | 4 blade feathering, reversible | 4 blade feathering, reversible |
| 14 | Engine | Lycoming TIO-540-AE2A | Lycoming TIO-540-AE2A | Pratt & Whitney PT6A-42A | Pratt & Whitney PT6A-42A |
| 15 | Power | 350 hp (260 kW) | 350 hp (260 kW) | 500 hp (370 kW) | 600 hp (450 kW) |
| 16 | Maximum cruise | 213 kt / 395 km/h | 213 kt / 395 km/h | 260 ktas / 482 km/h | 274 ktas / 507 km/h |
| 17 | Ceiling | 25,000 ft / 7,620 m | 25,000 ft / 7,620 m | 30,000 ft / 9,144 m | 30,000 ft / 9,144 m |
| 18 | Range (45 minute reserve) | 1,343 nm / 2,487 km | 1,343 nm / 2,487 km | 1,000 nm / 1,852 km | 1,484 nm / 2,668 km |
| 19 | Takeoff (50 ft obstacle) | 2,090 ft / 637 m | 2,090 ft / 637 m | 2,438 ft / 743 m | 2,635 ft / 803 m |
| 20 | Landing (50 ft obstacle) | 1968 ft / 600 m | 1968 ft / 600 m | 2,110 ft / 643 m | 2,659 ft / 810 m |

Question: At what speed and altitude does the Piper PA-46 cruises at?
Answer: Piper PA-46 cruises at 260 kn (482 km/h) at an altitude of 30,000 ft (9,144 m).