MSFS 2024 · Airliner
Airbus A310 Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vmcg | 113 KIAS | Minimum control speed on ground |
| Vmca | 117 KIAS | Minimum control speed in air |
| Vfe (Slats 15 / Flaps 0) | 245 KIAS / M 0.54 | Takeoff |
| Vfe (Slats 15 / Flaps 15) | 210 KIAS | Takeoff and approach |
| Vfe (Slats 20 / Flaps 20) | 195 KIAS | Takeoff, approach and landing |
| Vfe (Slats 30 / Flaps 40) | 180 KIAS | Landing |
| Krueger flaps jammed | 300 KIAS / M 0.65 | Do not exceed if they cannot be retracted |
| Vlo | 270 kts / M 0.59 | Max gear operation, extension or retraction |
| Vle | 270 kts / M 0.65 | Max gear locked down |
| Max Tire Ground Speed | 195.5 kts (225 mph) | - |
| Max Wiper Operation | 230 kts | - |
| Max Open Cockpit Window | 225 kts | - |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | Throttles to at least 40% N1, then trigger the Go-Levers |
| Takeoff Config | Slats 15 / Flaps 0, or Slats 15 / Flaps 15 |
| Autobrake (takeoff) | MAX |
| Go-Around | Go Levers triggered, throttles to go-around thrust |
| After Landing | Pitch trim 1 degree nose up, slats/flaps to 0/0 |
| Parking | Beacon off below 20% N2 |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| Clean | Any | Cruise / Climb |
| Slats 15 / Flaps 0 | <= 245 kts / M 0.54 | Takeoff |
| Slats 15 / Flaps 15 | <= 210 kts | Takeoff and approach |
| Slats 20 / Flaps 20 | <= 195 kts | Takeoff, approach and landing |
| Slats 30 / Flaps 40 | <= 180 kts | Landing |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Start - fuel introduction | Fuel lever ON at 20% N2 |
| Start sequence | Engine 2 first, then Engine 1 once the blue OPEN light goes out |
| N1 rotation after start | Within 30 seconds of reaching N2 idle |
| Takeoff spool-up (GE) | Both engines at least 40% N1 before Go-Levers |
| Load limits (clean) | +2.5 g / -1 g |
| Load limits (slats extended) | +2 g / 0 g |
KEY NUMBERS
| Parameter | Value |
|---|---|
| MTOW | 153,000 kg (337,307 lbs) |
| Max Landing Weight | 124,000 kg (273,373 lbs) |
| Max Zero Fuel Weight | 114,000 kg (251,326 lbs) |
| Operating Empty Weight | 80,000 kg (176,370 lbs) |
| Max Fuel Quantity | 60,300 kg (132,940 lbs) |
| Max Total Payload | 35,440 kg (78,131 lbs) |
| Max Demonstrated Crosswind | 28 kts dry (37 kts computed) |
| Max Tailwind | 10 kts takeoff and landing |
| Max Runway Altitude | 8,500 ft AMSL |
| Mean Runway Slope | +/- 2% |
| Autoland limits | 20 kts head / 15 kts cross / 5 kts tail |
| Autoland | Not approved single-engine, not demonstrated above MLW |