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At a glance
Measured figures
IA 63 · Length
Single source10.93 m (35 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | FMA IA-63 Pampa | Pilatus PC-24 |
|---|---|---|
| Type | Trainer aircraft[source] | Light business jet[source] |
| National origin | Argentina[source] | Switzerland[source] |
| Manufacturer | FAdeA[source] | Pilatus Aircraft[source] |
| Status | In service[source] | In production |
16.85 m (55 ft 3 in)[source]
Empty; IA 63 · Empty weight
Single sourceGross; IA 63 · Gross weight
Single sourceMaximum take-off; IA 63 · Max takeoff weight
Single source2,821 kg (6,219 lb)[source]
3,500 kg (7,716 lb)[source]
5,000 kg (11,023 lb)[source]
Empty; Empty weight
Single sourceMaximum take-off; Max ramp weight
Single sourceCruise; IA 63 · at 4,000 m (13,000 ft)
Single sourceMaximum; IA 63 · at 7,000 m (23,000 ft)
Single source819 km/h (509 mph, 442 kn) at 7,000 m (23,000 ft)[source]
747 km/h (464 mph, 403 kn) at 4,000 m (13,000 ft)[source]
Cruise; Cruise speed
Single source810 km/h (510 mph, 440 kn)[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Argentine Air Force[source] | — |
|---|
| Number built | 41[source] | 212 (Q1 2024)[source] |
|---|
| Manufactured | 1984-present[source] | 2015–present[source] |
|---|
| Introduction date | April 1988[source] | 1 April 2018[source] |
|---|
| First flight | 6 October 1984[source] | 11 May 2015[source] |
|---|
| Airfoil | Dornier DoA-7[source] | — |
|---|
| Never exceed speed | M0.81 at 9,500 m (31,200 ft)[source] | — |
|---|
| Guns | 1 × 30 mm (1.18 in) Defa-Giat 554 with 145 rounds of ammo. 4 × 7,62 mm Colibri Pods[source] | — |
|---|
| Hardpoints | 5 with a capacity of[source] | — |
|---|
| Missiles | LAU-32/51 rocket pods LAU-10 rocket pods ARM-657 Mamboretá pods[source] | — |
|---|
| Bombs | Mk81/ Mk82 bombs CBLS 200 practice bombs[source] | — |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Capacity | — | 10 passengers[source] |
|---|
| Aspect ratio | — | 9.35[source] |
|---|
| Fuel capacity | — | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Cabin | — | 7.01 m × 1.69 m × 1.55 m long × wide × high ( 23 ft 0 in × 5 ft 7 in × 5 ft 1 in)[source] |
|---|
| Cabin altitude | — | 2,438 m at 13,716 m (8,000 ft at 45,000 ft), 8.78 psi (0.605 bar)[source] |
|---|
| Stall speed | — | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Time to altitude | — | 45,000 ft (14,000 m) 27.1 mins[source] |
|---|
| Wing loading | — | 259 kg/m 2 (53 lb/sq ft)[source] |
|---|
| Fuel consumption | — | 0.58 kg/km (2.1 lb/mi) Mach 0.72/416 kn (770 km/h) cruise, 15,375 lb (6,974 kg) weight, FL 450, ISA+3C[source] |
|---|
| Thrust/weight | — | 0.36[source] |
|---|
| Take-off | — | 942 m; 3,091 ft (MTOW, ISA, sea level, dry paved runway)[source] |
|---|
| Landing | — | 734 m; 2,408 ft (Over 50 ft obstacle, MLW, ISA, sea level, dry paved runway)[source] |
|---|
Maximum take-off; Max takeoff weight
Single source