M-346 Master
| Country | Italy | |
| Builder | Alenia Aermacchi | |
| Users |
FUTURE PROSPECTS | |
| Comparable Aircraft | ||
| span | 9.72 m | 31.89 ft |
| length | 11.49 m | 37.70 ft |
| height | 4.98 m | (16,33 ft) |
| wing area | 23.52 sqm | 253.20 sqft |
| Weight empty | 4,610 kg | 10.165 lb |
| takeoff (clean) | 6,700-7,400 kg | 14.770-16,310 lb |
| takeoff (maximum) | 9,500-10,200 kg | 20.945-22,490 lb |
| Max weapon load | 3,000 kg (6,610 lb) | |
| Power Plant | Honeywell 2 x F-124GA-200 | |
| Thrust, max, SLS, ISA | 2 x 2,850 kg | 2 x 6,280 lb |
| Internal fuel (usable) | 2,000 kg | 4.410 lb |
| Performance (clean, ISA) | ||
| Max level speed (sea level) | 590 KTAS | |
| Limit speed | 572 KEAS / 1.2 MN | |
| Stall speed (landing, 20% fuel) | 90 KCAS | |
| Stall speed (reference) | 95 KCAS | |
| Rate of climb (SL) | 21,000-22,000 ft/min | |
| Service ceiling | 45,000 ft | |
| Range / 3 ext. tanks (10% reserve) | 1,120 / 1,540 nm | |
| Range, ext. tanks | 2,720 km (1,470 nm) | |
| Range, clean | 1,980 km (1,070 nm) | |
| Endurance, clean / ext. tanks | 2h 45 min / 4 h | |
| Max sustained Load Factor (S.L.) | 8.0 g | |
| Max sustained Load Factor (15,000 ft) | 5.2 -5.8 g | |
| Max sustained Turn Rate (15,000 ft) | 14 deg/sec | |
| Takeoff ground run (S.L.) | 320-400 m | (1.050-1,310 ft) |
| Landing ground roll (S.L., 20% internal fuel) | 470-550 m | (1,540-1,800 ft) |
| Limit Load factor | + 8 g / - 3 g |
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