Engine
Lycoming IO-360-A3B6D
Power
200 HP
Empty Weight
1,925.3 lbs
MTOW
2,740 lbs
Useful Load
640 lbs
Fuel Capacity
64 gal
V-Speeds (Sea Level)
Vx
66 KIAS
Vy
88 KIAS
Vr
60 KIAS
V2
70 KIAS
Performance
ROC (SL)
900 fpm
Ceiling
20,000 ft
Max Cruise
175 kt
Normal Cruise
160 kt
Modelo Oficial
Dados baseados no POH do fabricante
Max: 2740 lbs
ISA: 15.0°C at this altitude
ISA +0.0°C
No HW/TW component
Runway Status
✓ Adequate
Required: 1,208 ft
Margin: +3,792 ft (76%)
Density Alt
0
feet
Ground Roll
683
ft · 208 m · ground roll (POH)
Vr / V2
60
KIAS rotation
Headwind
0
knots
Wind Speed
0 kt
Wind Direction
0°
Headwind Component
+0.0 kt
✓ Headwind - reduces takeoff distance
Crosswind Component
0.0 kt
✓ Within limit of 15 kt
Wind Impact
• Headwind reduces takeoff distance by ~5% per 10 knots
• Tailwind increases takeoff distance by ~10% per 5 knots
• Crosswind affects control authority and handling
Temperature
15°C
59.0°F
Pressure Altitude
0 ft
Density Altitude
0 ft
0 ft below field elevation
Performance Impact
Density altitude is favorable. Aircraft performance is near normal.
What is Density Altitude?
Density altitude is the altitude at which the air density equals the standard atmosphere. High temperatures and high elevations increase density altitude, reducing aircraft performance.
Available Length
5,000 ft / 1,524 m
Required Distance
1,208 ft / 368 m
hard
Safety Margin
+3,792 ft / +1,156 m
76% extra
Other Surface
1,425 ft / 434 m
grass
Recommendations
Factors Affecting Takeoff Distance
- • Higher density altitude increases required distance
- • Heavier aircraft requires longer distance
- • Tailwind increases required distance significantly
- • Grass/unprepared surfaces require ~18% more distance
- • Uphill slope increases required distance
Ground Roll (POH)
683 ft
208 m
Ground Roll (Grass)
806 ft
246 m · +18% for grass
Mooney M20J (Standard 2740 lbs)
MTOW: 2,740 lbs · Empty: 1,925.3 lbs
Performance Basis
POH (Pilot's Operating Handbook)
Important Notes
For planning only. Always verify with actual POH data.