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MSFS 2024 · Airliner
Inibuilds A380-800 Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| VLO | 250 kt / M 0.55 | Max gear operation, extension and retraction |
| VLE | 250 kt / M 0.55 | Max gear locked down |
| Max Tire Ground Speed | 204 kt | - |
| Max Wiper Operation | 250 kt | Windshield wiper |
| Rotation Target | 12.5 deg at 3 deg/sec | All engines operative; 10 deg is not used, follow SRS |
| Green Dot | Minimum clean speed | Speed target after flaps 0 on the takeoff schedule |
| VAPP | Approach phase target | Becomes the target when the approach phase activates |
| Reverser to Idle | 70 kt | - |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff (first stage) | RR 30 percent THR, EA 25 percent THR |
| Takeoff (second stage) | FLX or TOGA once the engines are stable |
| Thrust Reduction | CLIMB detent at the thrust reduction altitude |
| Climb (RR) | AUTO-DERATE or CLB |
| Climb (EA) | CLB 3 below 420 T, CLB 2 to 510 T, CLB 1 to 540 T, none above |
| Go-Around | TOGA, then FLC/MCT for MAN GA SOFT at +2000 fpm |
| Landing | REV IDLE or REV MAX, back to REV IDLE at 70 kt |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| CONF 1 | 263 kt | Holding. Slats 20, flaps 0 |
| CONF 1+F | 222 kt | Take-off. Slats 20, flaps 8, ailerons 5 |
| CONF 2 | 220 kt | Take-off and approach. Slats 20, flaps 17, ailerons 5 |
| CONF 3 | 196 kt | Take-off, approach and landing. Slats 23, flaps 26 |
| CONF FULL | 182 kt | Landing. Slats 23, flaps 32, ailerons 5 |
| Slats/flaps max FL | FL200 | Altitude limit for any extension |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engines (RR) | 4x Rolls-Royce Trent 972-84, 72,000 lb thrust |
| Engines (EA) | 4x Engine Alliance GP7270, 70,000 lb thrust |
| Spools | RR three shaft (N1/N2/N3), EA two shaft (N1/N2) |
| Idle N1 (after start) | ~20 percent |
| Idle N2 (after start) | ~50 percent |
| Idle N3 (after start, RR only) | ~60 percent |
| Idle EGT (after start) | ~400 degC |
| Idle Fuel Flow (after start) | ~600 kg/h (1,320 lb/hr) |
| Thrust Reversers | Inboard engines 2 and 3 only |
| Fire Extinguisher Bottles | Two per engine, one for the APU |
| APU Start Delay | 5 s between APU MASTER and APU START |
KEY NUMBERS
| Parameter | Value |
|---|---|
| Max Takeoff Weight | 572,000 kg (1,261,044 lb) |
| Max Landing Weight | 391,000 kg (862,007 lb) |
| Max Zero Fuel Weight | 366,000 kg (806,892 lb) |
| Operating Empty Weight | 284,856 kg (628,000 lb) |
| Max Fuel Capacity | 253,963 kg (573,600 lb) |
| Cruise Speed | 480 KTAS |
| Max Altitude | 43,100 ft |
| Range | 8,000 NM |
| Length / Wingspan | 72.7 m / 79.8 m |
| Max Tailwind (T/O and LDG) | 10 kt |
| Max Certified Crosswind (T/O and LDG) | 30 kt |
| Max Wind for Door Operation | 40 kt |
| Autoland Max Headwind | 38 kt |
| Autoland Max Crosswind | 30 kt |
| Autoland Max Tailwind | 10 kt |
| Autoland Max Altitude | 9,200 ft |
| Autoland Glide Slope | -2.5 to -3.5 degrees |
| g-Limits (clean) | +2.5 g / -1 g |
| g-Limits (slats extended) | +2 g / 0 g |
| Mean Runway Slope | +/- 2 percent |
| Minimum Runway Width | 148 ft |
| Max Normal Cabin Altitude | 7,500 ft |
| External Power Units | Minimum 2; connect in order EXT 2, 3, 1, 4 |
| Battery Charge After Reset | Below 60 A and decreasing |
| Brake Pressure Check | Above 3,500 PSI |
| Autobrake T/O | RTO |
| Flaps After Landing | Keep flaps 1 above 30 degC OAT |