FORCETALLY
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At a glance
Measured figures
Q-5D · Length
Single source15.65 m (51 ft 4 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Nanchang Q-5 | TAI TF Kaan |
|---|---|---|
| Type | Ground-attack aircraft[source] | Stealth multirole / air superiority fighter[source] |
| National origin | China[source] | Turkey[source] |
| Manufacturer | Nanchang Aircraft Mfg. Co.[source] | Turkish Aerospace Industries[source] |
| Status | In service with the Myanmar Air Force[source] |
Preliminary specifications (KAAN development aircraft) · Length
Single source20.3 m (66 ft 7 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
20,3 m (66 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Q-5D · Wingspan
Single source9.68 m (31 ft 9 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wingspan
Single sourcePreliminary specifications (KAAN development aircraft) · Wingspan
Single source13.4 m (44 ft 0 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
13,4 m (44 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Q-5D · Height
Single source4.33 m (14 ft 2 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Height
Single sourcePreliminary specifications (KAAN development aircraft) · Height
Single source5 m (16 ft 5 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
5 m (16 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Empty; Q-5D · Empty weight
Single sourceGross; Q-5D · Gross weight
Single sourceMaximum take-off; Q-5D · Max takeoff weight
Single source6,375 kg (14,054 lb)[source]
9,486 kg (20,913 lb)[source]
11,830 kg (26,081 lb)[source]
Maximum take-off; Preliminary specifications (KAAN development aircraft) · Maximum takeoff weight
Single source34,750 kg (76,500 lb)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
34.750 kg (76,500 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Maximum; Q-5D · Maximum speed
Single source1,190 km/h (740 mph, 640 kn)[source]
Q-5D · Range
Single source2,000 km (1,200 mi, 1,100 nmi)[source]
Q-5D · lo-lo-lo with maximum payload
Single source400 km (250 mi, 220 nmi) lo-lo-lo with maximum payload[source]
Q-5D · 2 × Liming Wopen-6A afterburning turbojet engines thrust each dry
Single sourceQ-5D · with afterburner
Single source2 × Liming Wopen-6A afterburning turbojet engines, 29.42 kN (6,610 lbf) thrust each dry, 36.78 kN (8,270 lbf) with afterburner[source]
Preliminary specifications (KAAN development aircraft) · 2 × General Electric F110-GE-129 Turbofan thrust each dry
Single sourcePreliminary specifications (KAAN development aircraft) · with afterburner
Single sourceQ-5D · Wing area
Single source27.95 m 2 (300.9 sq ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wing area
Single sourcePreliminary specifications (KAAN development aircraft) · Wing area
Single source71.6 m 2 (770 sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
71,6 m2 (771 ft2)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Q-5D · Service ceiling
Single source16,500 m (54,100 ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Service ceiling
Manufacturer claimPreliminary specifications (KAAN development aircraft) · Service ceiling
Single source16,764 m (55,000 ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
16.764 m (55,000 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Q-5D · 20,300 ft/min
Single source103 m/s (20,300 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Under development[source]
| Primary users | People's Liberation Army Air Force (historical) People's Liberation Army Navy Air Force (historical) Pakistan Air Force (historical) Myanmar Air Force[source] | — |
|---|
| Number built | 1,300 (approx.)[source] | — |
|---|
| Manufactured | 1969–2012[source] | — |
|---|
| Introduction date | 1970[source] | 2030s (planned)[source] |
|---|
| First flight | 4 July 1965[source] | 21 February 2024[source] |
|---|
| Retired | 2017 by PLA Air Force 2011 by Pakistan Air Force 2015 by Bangladesh Air Force[source] | — |
|---|
| Developed from | Shenyang J-6[source] | — |
|---|
| Wing loading | 423.3 kg/m 2 (86.7 lb/sq ft)[source] | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | 0.588[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Guns | 2× Norinco Type 23-2K 23 mm (0.906 in) cannon , 100 rounds per gun[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 10 (4× under-fuselage, 6× under-wing) with a capacity of 2,000 kg (4,400 lb), with provisions to carry combinations of:[source] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | 57 mm, 90 mm, 130 mm unguided rocket pods[source] | — |
|---|
| Missiles | PL-2 , PL-5 , PL-7 air-to-air missiles[source] | Air-to-air missiles : GÖKTUĞ missile program: Gökdoğan BVR active radar homing Gökhan ramjet engine powered BVR active radar homing Bozdoğan short-range infrared homing Air-to-surface missiles : SOM Cruise Missile (B1, B2, and J variants) KUZGUN-TJ, Turbojet-powered Air-to-surface missile KUZGUN-KY, Solid fuel Rocket-powered Air-to-surface missile KUZGUN-ER, Turbojet-powered , Air-to-surface missile (According to TUBITAK-SAGE, this missile will be equivalent to Penguin Missiles .) KUZGUN-EW, KUZGUN-EW will be able to carry miniaturised EW payload which will act as a stand-in jammer and suppress enemy air defences to significantly increase the survivability of the aircraft of the Turkish Air Force . AKBABA, Air-to-surface , Anti-radiation Missile (ARM) ROKETSAN ÇAKIR Missile Family , Anti-ship , Air-to-surface , surface-to-surface Cruise Missile .[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Others | Fuel tanks: 400 L (105 U.S. gal), 760 L (200 U.S. gal), 1,100 L (300 U.S. gal)[source] | — |
|---|
| Fuel tanks | 400 L (105 U.S. gal), 760 L (200 U.S. gal), 1,100 L (300 U.S. gal)[source] | — |
|---|
| Other name | — | TF or MMU[source] |
|---|
| Designer | — | BAE Systems TAI[source] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Initiated | — | 2010[source] |
|---|
| g limits | — | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Bombs | — | Teber-81 ( Mark 81 bomb w/ ROKETSAN Laser Guidance Kit) HGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) Teber-82 ( Mark 82 bomb w/ ROKETSAN Laser Guidance Kit) HGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) HGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) LHGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Laser Sensitive Guidance Kit) SARB-83, Bunker buster NEB-84, Bunker buster MAM (Smart Micro Munition) (MAM-T variant) KUZGUN-SS, Glide bomb ASELSAN Miniature Bomb[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated RF System (IRFS) | — | MURAD-600A AESA radar Radar warning receiver[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Electro-Optical System (IEOS) | — | KARAT-200 Infrared Search and Track (IRST) TOYGUN Electro-optical reconnaissance, surveillance and targeting system İRİS-300 Missile approach warning system (IR-MWS/360° day/night imaging) YILDIRIM-300 Directional Infrared Counter Measures (DIRCM) LİAS-300 Laser warning receiver (LWS)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Communications Navigation and IFF (ICNI) | — | ICNAir-ASQ9683 communications suite ARVEN radio-navigation equipment IdentIFF Mode-5 identification friend or foe[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Advanced Cockpit / Human Machine Interface | — | TULGAR Helmet-mounted display (HMDS) LAD-208 Large area display (LAD)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Positive / Negative G Limit | — | +9 / -3,5 G[source]KAAN development aircraft; manufacturer technical data, configuration not stated |
|---|
2 × General Electric F110-GE-129 Turbofan , 76.3 kN (17.155 lbf) thrust each dry, 131 kN (29,000 lbf) with afterburner[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
2 x 13.150 kgf (2 x 29,000 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated