Active Aerospace (for $6000 CDN 320 series type rating) tell Walt that Danny sent you.
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Airbus 320 series general info
Specifications
| A318-100 | A319-100 / A319LR /A319CJ | A320-200 | A321-200 | |
|---|---|---|---|---|
| Cockpit crew | Two | |||
| Seating capacity | 132 (1-class, maximum) 117 (1-class, typical) 107 (2-class, typical) |
156 (1-class, maximum) 134 (1-class, typical) 124 (2-class, typical) |
180 (1-class, maximum) 164 (1-class, typical) 150 (2-class, typical) |
220 (1-class, maximum) 199 (1-class, typical) 185 (2-class, typical) |
| Length | 31.44 m (103 ft 2 in) | 33.84 m (111 ft 0 in) | 37.57 m (123 ft 3 in) | 44.51 m (146 ft 0 in) |
| Wingspan | 34.10 m (111 ft 11 in) | |||
| Wing area | 122.6 m2 (1,320 sq ft) | |||
| Wing sweepback | 25 degrees | |||
| Tail height | 12.56 metres (41 ft 2 in) | 11.76 m (38 ft 7 in) | ||
| Cabin width | 3.70 m (12 ft 2 in) | |||
| Fuselage width | 3.95 m (13 ft 0 in) | |||
| Cargo capacity | 21.21 m3 (749 cu ft) | 27.62 m3 (975 cu ft) 4× LD3 |
37.41 m3 (1,321 cu ft) 7× LD3 |
51.73 m3 (1,827 cu ft) 10× LD3 |
| Empty weight, typical | 39,500 kg (87,000 lb) | 40,800 kg (90,000 lb) | 42,600 kg (94,000 lb) | 48,500 kg (107,000 lb) |
| Maximum take-off weight (MTOW) | 68,000 kg (150,000 lb) | 75,500 kg (166,000 lb) | 78,000 kg (170,000 lb) | 93,500 kg (206,000 lb) |
| Cruising speed | Mach 0.78 (828 km/h/511 mph at 11,000 m/36,000 ft) | |||
| Maximum speed | Mach 0.82 (871 km/h/537 mph at 11,000 m/36,000 ft) | |||
| Maximum range, fully loaded | 3,100 nautical miles (5,700 km; 3,600 mi) | 3,600 nautical miles (6,700 km; 4,100 mi) LR: 5,600 nmi (10,400 km; 6,400 mi) CJ: 6,500 nmi (12,000 km; 7,500 mi) |
3,200 nautical miles (5,900 km; 3,700 mi) | 3,000 nautical miles (5,600 km; 3,500 mi) |
| Take off run at MTOW (at Sea Level, ISA) | 1,355 m (4,446 ft) | 1,950 m (6,400 ft) | 2,090 m (6,860 ft) | 2,180 m (7,150 ft) |
| Maximum fuel capacity | 24,210 L (5,330 imp gal; 6,400 US gal) | 24,210 L (5,330 imp gal; 6,400 US gal) standard 30,190 L (6,640 imp gal; 7,980 US gal) optional |
24,050 litres (5,290 imp gal; 6,350 US gal) standard 30,030 L (6,610 imp gal; 7,930 US gal) optional | |
| Service ceiling | 12,000 m (39,000 ft) | |||
| Engines (×2) | Pratt & Whitney PW6000 series CFM International CFM56-5 series |
IAE V2500 series CFM International CFM56-5 series | ||
| Thrust (×2) | 96–106 kilonewtons (22,000–24,000 lbf) | 98–120 kilonewtons (22,000–27,000 lbf) | 111–120 kilonewtons (25,000–27,000 lbf) | 133–147 kilonewtons (30,000–33,000 lbf) |
Engines
| Model | Date | Engines |
|---|---|---|
| A318-111 | 2003 | CFM56-5B8/P |
| A318-112 | 2003 | CFM56-5B9/P |
| A318-121 | 2007 | PW6122A |
| A318-122 | 2007 | PW6124A |
| A319-111 | 1996 | CFM56-5B5 or 5B5/P |
| A319-112 | 1997 | CFM56-5B6 or 5B6/P or 5B6/2P |
| A319-113 | 1997 | CFM56-5A4 or 5A4/F |
| A319-114 | 1997 | CFM56-5A5 or 5A5/F |
| A319-115 | 2002 | CFM56-5B7 or 5B7/P |
| A319-131 | 1997 | IAE Model V2522-A5 |
| A319-132 | 1997 | IAE Model V2524-A5 |
| A319-133 | 2002 | IAE Model V2527M-A5 |
| A320-111 | 1988 | CFM56-5A1 or 5A1/F |
| A320-211 | 1988 | CFM56-5A4 or 5A4/F |
| A320-212 | 1990 | CFM56-5A3 |
| A320-214 | 1996 | CFM56-5B4 or 5B4/P or 5B4/2P |
| A320-216 | 2005 | CFM56-5B6 |
| A320-231 | 1989 | IAE Model V2500-A1 |
| A320-232 | 1993 | IAE Model V2527-A5 |
| A320-233 | 1995 | IAE Model V2527E-A5 |
| A321-111 | 1995 | CFM56-5B1 or 5B1/P or 5B1/2P |
| A321-112 | 1995 | CFM56-5B2 or 5B2/P |
| A321-131 | 1995 | IAE Model V2350-A5 |
| A321-211 | 1997 | CFM56-5B3 or 5B3/P or 5B3/2P |
| A321-212 | 2005 | CFM56-5B1 or 5B1/P or 5B1/2P |
| A321-213 | 2005 | CFM56-5B2 or 5B2/P |
| A321-231 | 1997 | IAE Model V2533-A5 |
| A321-232 | 2005 | IAE Model V2530-A5 |