Specifications (IA 63)
Data from Jane's All The World's Aircraft 1988–89
General characteristics
- Crew: two
- Length: 10.93 m (35 ft 10¼ in)
- Wingspan: 9.69 m (31 ft 9¼ in)
- Height: 4.29 m (14 ft 1 in)
- Wing area: 15.63 m² (168.2 ft²)
- Airfoil: Dornier DoA-7
- Empty weight: 2,821 kg (6,219 lb)
- Loaded weight: 3,500 kg (7,716 lb)
- Max. takeoff weight: 5,000 kg (11,023 lb)
- Powerplant: 1 × Garrett TFE731-2-2N turbofan, 15.57 kN (3,500 lbf)
Performance
- Never exceed speed: Mach 0.81 (at 9,500 m (31,170 ft))
- Maximum speed: 819 km/h (442 knots, 509 mph) at 7,000 m (22,965 ft)
- Cruise speed: 747 km/h (403 knots, 464 mph) at 4,000 m (13,125 ft)
- Range: 1,500 km (809 nmi, 932 mi)
- Service ceiling: 12,900 m (42,325 ft)
- Rate of climb: 30.2 m/s (5,950 ft/min)
Armament
- Guns: 1× 30 mm (1.18 in) Defa-Giat 554
- Hardpoints: 5 with a capacity of
- 400 kg (880 lb) on inboard underwing pylons
- 250 kg (550 lb) on fuselage centerline and outer wing pylons
Read more about this topic: FMA IA 63 Pampa