Credit
Alan Wilson from Stilton, Peterborough, Cambs, UK · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
DHC-1 Chipmunk · Length
Single source25 ft 5 in (7.75 m)[source]
Configuration
| Specification | De Havilland Canada DHC-1 Chipmunk | Guizhou JL-9 |
|---|---|---|
| Type | Trainer[source] | Advanced jet trainer Light combat aircraft[source] |
| Manufacturer | de Havilland Canada[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| Status | In limited service; many examples in private use[source] | In service[source] |
| Primary users | Royal Air Force (historical) Royal Canadian Air Force (historical) Portuguese Air Force[source] |
FTC-2000 · excluding nose-probe
14.555 m (47 ft 9 in) excluding nose-probe[source]
Empty; DHC-1 Chipmunk · Empty weight
Single sourceGross; DHC-1 Chipmunk · Gross weight
Single sourceMaximum take-off; DHC-1 Chipmunk · Max takeoff weight
Single source1,517 lb (688 kg)[source]
2,014 lb (914 kg)[source]
2,200 lb (998 kg)[source]
Gross; FTC-2000 · clean
Single sourceMaximum take-off; FTC-2000 · Max takeoff weight
Single sourceCruise; DHC-1 Chipmunk · Cruise speed
Single sourceMaximum; DHC-1 Chipmunk · at sea level
Single source138 mph (222 km/h, 120 kn) at sea level[source]
103 mph (166 km/h, 90 kn)[source]
Cruise; FTC-2000 · Cruise speed
Single sourceMaximum; FTC-2000 · / Mach 0.89
Single sourceDHC-1 Chipmunk · Range
Single source259 mi (417 km, 225 nmi)[source]
DHC-1 Chipmunk · 1 × de Havilland Gipsy Major 1C 4-cylinder air-cooled inverted in-line piston engine
Single source1 × de Havilland Gipsy Major 1C 4-cylinder air-cooled inverted in-line piston engine, 145 hp (108 kW)[source]
FTC-2000 · 1 × Guizhou Liyang WP-13F (C) afterburning turbojet thrust dry
Single sourceFTC-2000 · thrust dry and
Single sourceFTC-2000 · with afterburner
Single sourceFTC-2000 · with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G
Single source1 × Guizhou Liyang WP-13F (C) afterburning turbojet, 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G, 53.89 kN (12,110 lbf) thrust dry and 76.53 kN (17,200 lbf) with afterburner.)[source]
FTC-2000 · Endurance
Single source3 hours[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] |
| Number built | 1,284 (including Canadian, British, and Portuguese production)[source] | — |
|---|
| Manufactured | 1947–1956[source] | — |
|---|
| Introduction date | 1946[source] | — |
|---|
| First flight | 22 May 1946[source] | 13 December 2003[source] |
|---|
| Retired | 1955 (Belgium) 1972 (Canada) 1996 (United Kingdom)[source] | — |
|---|
| Airfoil | root: NACA 1415 ; tip: USA 35B[source] | — |
|---|
| Propellers | 2-bladed fixed-pitch propeller[source] | — |
|---|
| Wing loading | 11.71 lb/sq ft (57.2 kg/m 2 )[source] | 374.8 kg/m 2 (76.8 lb/sq ft)[source] |
|---|
| Power/mass | .072 hp/lb (0.118 kW/kg)[source] | — |
|---|
| Country of origin | Canada[source] | Volksrepublik China[source]Country of design · Entwurfsland |
|---|
| Designer | — | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] |
|---|
| Developed from | — | Chengdu JJ-7[source] |
|---|
| Fuel capacity | — | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[source] |
|---|
| Guns | — | 1 × 23 mm cannon[source] |
|---|
| Hardpoints | — | 5 with a capacity of 2,000 kg (4,409 lb) maximum, with provisions to carry combinations of: Other: up to 3 x fuel tanks[source] |
|---|
| Unstick and touchdown speed | — | 260 km/h (160 mph; 140 kn)[source] |
|---|
| Minimum flying speed | — | 210 km/h (130 mph; 110 kn)[source] |
|---|
| Stall speed | — | 125 km/h (78 mph, 67 kn)[source] |
|---|
| g limits | — | + 8 - 3[source] |
|---|
| Thrust/weight | — | 0.00645 kN/kg (0.658 lb f /lb)[source] |
|---|
| Take-off run | — | 400–500 m (1,300–1,600 ft)[source] |
|---|
| Landing run | — | 700 m (2,300 ft)[source] |
|---|
| Other | — | up to 3 x fuel tanks[source] |
|---|
| Missiles | — | ** Short range air-to-air missile 2 × PL-8 AAMs (on inboard pylons) 2 × PL-9 AAMs (on outboard pylons) Beyond-visual-range air-to-air missiles SD-10 (Only on FTC-2000G) Anti-radiation missiles CM-102 (Only on FTC-2000G)[source] |
|---|
| Beyond-visual-range air-to-air missiles | — | SD-10 (Only on FTC-2000G)[source] |
|---|
| Anti-radiation missiles | — | CM-102 (Only on FTC-2000G)[source] |
|---|
| Reported operators | — |
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