FORCETALLY
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At a glance
Measured figures
AMD Zodiac XL · Length
Single source20 ft 0 in (6.1 m)[source]
KT-1 · Length
Single sourceConfiguration
| Specification | AMD Zodiac | KAI KT-1 Woongbi |
|---|---|---|
| Type | Kit aircraft[source] | Basic trainer and light attack aircraft[source] |
| Manufacturer | Aircraft Manufacturing and Design[source] | Korea Aerospace Industries[source] |
| Designer | Chris Heintz[source] | Agency for Defence Development Korea Aerospace Industries[source] |
| Status | In production[source] | In service |
10.3 m (33 ft 10 in)[source]
Cruise; AMD Zodiac XL · Cruise speed
Single sourceMaximum; AMD Zodiac XL · Maximum speed
Single source140 kn (161 mph, 257 km/h)[source]
111 kn (130 mph, 211 km/h)[source]
Maximum; KT-1 · at 4,570 m (14,993 ft)
Single source644 km/h (400 mph, 348 kn) at 4,570 m (14,993 ft)[source]
AMD Zodiac XL · Range
Single source608 nmi (715 mi, 1,158 km)[source]
Ferry; KT-1 · at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)
Single sourceKT-1 · at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)
Single source1,333 km (828 mi, 720 nmi) at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)[source]
2,070 km (1,290 mi, 1,120 nmi) at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)[source]
KT-1 · < at 6,100 m (20,013 ft) with max internal fuel (
Single sourceKT-1 · reserve
Single source<4 hours at 6,100 m (20,013 ft) with max internal fuel (30 minutes reserve)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | private pilots[source] | Republic of Korea Air Force Indonesian Air Force Turkish Air Force Peruvian Air Force Senegalese Air Force[source] |
|---|
| Number built | More than 1,000[source] | 186[source] |
|---|
| Manufactured | Eastman, Georgia[source] | 1999–present[source] |
|---|
| First flight | 1984[source] | November 1991[source] |
|---|
| Retired | N/A[source] | — |
|---|
| Capacity | 1 passenger and 550 lb (250 kg) useful load[source] | — |
|---|
| Airfoil | NACA 65-018[source] | root: NACA 63-218 ; tip: NACA 63-212[source] |
|---|
| Stall speed | 37 kn (44 mph, 71 km/h)[source] | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Never exceed speed | 140 kn (161 mph, 257 km/h)[source] | 648 km/h (403 mph, 350 kn)[source] |
|---|
| Wing loading | 10 lb/sq ft (48 kg/m 2 )[source] | 206.8 kg/m 2 (42.4 lb/sq ft) with external stores[source] |
|---|
| Power/mass | 13.2 lb/hp (0.125 W/kg)[source] | 0.2137 kW/kg (0.1300 hp/lb)with external stores[source] |
|---|
| Country of origin | Canada[source]Inventory Origin column; table 1, row 28, cell 2; revision 1377598795; retrieved 2026-09-30 | — |
|---|
| National origin | — | South Korea[source] |
|---|
| Introduction date | — | 2000[source] |
|---|
| Fuel capacity | — | 551 L (146 US gal; 121 imp gal) in two wing tanks with provision for two 189 L (50 US gal; 42 imp gal) drop-tanks on the inboard pylons[source] |
|---|
| Aspect ratio | — |
|---|
| Maximum fuel weight | — | 408 kg (899 lb)[source] |
|---|
| Propellers | — | 4-bladed Hartzell HC-E4N-2/E9512CB-1, 2.44 m (8 ft 0 in) diameter constant-speed fully feathering reversible propeller[source] |
|---|
| g limits | — | + 7 - 3.5 (aerobatic, clean)[source] |
|---|
Maximum take-off; KT-1 · (and Maximum Landing Weight)with external stores
Single source