Twin Engine • Mitsubishi • MU-2B, MU-2F, MU-2G, MU-2J, MU-2L
| Manufacturer | Mitsubishi |
| Model | MU-2 |
| Category | Twin Engine |
| Variants | MU-2B, MU-2F, MU-2G, MU-2J, MU-2L |
| Production Years | 1963 – 1986 |
| Seating | 4, 5, 6, 7, 8 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Japan, Canada, Indonesia, Philippines |
| Price Range | $180K – $950K |
The Mitsubishi MU-2 is a Japanese-built twin-engine utility aircraft that has served as a workhorse in regional aviation since the 1960s. Known for its exceptional climb performance, rugged construction, and ability to operate from unprepared airfields, the MU-2 has earned a reputation as one of the most capable light twins ever produced. The aircraft features a pressurized cabin, retractable landing gear, and twin Lycoming engines, making it suitable for cargo operations, passenger transport, and special mission work. The MU-2 is particularly valued in remote regions and has been extensively used by civil operators, military forces, and government agencies worldwide. Its high wing design provides excellent visibility and cargo access. While production ended in 1986, the MU-2 remains actively flown in numerous countries, with a strong aftermarket support community. The aircraft is popular among operators seeking reliable twin-engine performance with genuine utility capability, though it requires type-rated pilots and specialized maintenance. Its longevity in service speaks to both its design robustness and operational efficiency.
Maximum Speed: 288 mph
Cruise Speed: 260 mph
Range: 1,520 nautical miles
Service Ceiling: 28,000 feet
Engines: Two Lycoming IO-540-A1B (290 hp each)
Maximum Takeoff Weight: 5,512 lbs
Empty Weight: 3,433 lbs
Fuel Capacity: 244 US gallons
Pressurization: 5.0 psi differential