THIS TOOL CALCULATES WEIGHT AND BALANCE, TAKEOFF AND LANDING PERFORMANCE FOR THE DIAMOND DA40 TDI. SELECT A PRE-CONFIGURED AIRCRAFT FROM THE DROPDOWN OR ENTER VALUES MANUALLY. ALL CALCULATIONS ARE BASED ON THE OFFICIAL DA40 TDI AIRCRAFT FLIGHT MANUAL.
Weights & Balance | ||
Weight (kg) | Moment (kgm) | |
Empty Weight | ||
Front Seat L | ||
Front Seat R | ||
Rear Seat L | ||
Rear Seat R | ||
Baggage(30kg) | ||
Zero Fuel Weight | ||
Fuel (l) | ||
Ramp weight | ||
Fuel allowance (l) | ||
Takeoff Weight | ||
Fuel burned (l) | ||
Landing Weight |
Aircraft Data | |
Aircraft Preset | |
Weight & Balance | |
T/O Dist. (m) | |
LDG Dist. (m) |
Environment | |
OAT (°C) | 15 |
QNH (hPa) | 1013 |
Elevation (ft) | 0 |
Headwind (kts) | 0 |
Pressure Alt. (ft) | |
Density Alt. (ft) |
General Tools | |||
Wind Components | |||
Wind | @ | Rwy | |
Xwind. | Hwind. | ||
Navigation | |||
Course | TAS | ||
Wind | @ | Var | |
Hdg | GS | ||
Std. Rate Turn | |||
GS | Bank | ||
Unit Conversions | |||
°C | °F | ||
NM/kts | SM/mph | ||
feet | m | ||
lb | kg | ||
US gal | l |