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| aa. | Vehicle | English Electric Canberra B(1)12 |
| ab. | Weight | Empty: 10 500kg; Max take-off: 24 945kg (55 000lb) |
| ac. | Length | 19.96m (65ft 6 in) |
| ad. | Width | Wingspan: 19.51m (63ft 11½ in) |
| ae. | Height | 4.77m (15ft 8 in) |
| af. | Crew | Pilot and a second crew member in cockpit |
| ag. | Armour | None |
| ah. | Primary Armament | 2720 kg bombs internally and up to 454 kg on a hardpoint under each wing |
| ai. | Secondary Armament | |
| aj. | Engine | Two Rolls-Royce Avon 109 turbojets of 7 400lbs st (3 357kg) |
| ak. | Power/Weight | |
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| as. | Operating Range | 1 300km with reaching a distance of 6 100km |
| at. | Speed-Offroad | Mach 0.83 (901km/h) at 12 200m; Mach 0.68 (821km/h) at sea level |
| au. | Speed-Road | |
| av. | Fuel Capacity | |
| aw. | Fuel Consumption | |
| ax. | Fuel Type | |
| ay. | Clearance | |
| az | Gradient | |
| ba. | Side Slope | |
| bb. | Vertical Step | |
| bc. | Trench | |
| bd. | Fording | |
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| ca. | Propellers | |
| cb. | Endurance | |
| cc. | Service Ceiling | 14 630m |
| cd. | Rate Of Climb | 3,400 ft/min (17 m/s) |
| ce. | Wing Area | Wing area: 960 sq ft (89 m2) |
| cf. | Aspect Ratio | |
| cg. | Airfoil | root: RAE/D 12% symm ; tip: RAE/D 9% symm |
| ch. | Wing Loading | 48 lb/sq ft (230 kg/m2) |
| ci. | Take-off Run | |
| cj. | Landing Run | |
| ck. | Time to Altitude: | |
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