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AROTA
Equations
Equations, formulas, and other rule of thumbs
Formula | Equation | Notes |
|---|---|---|
Moment | Weight x arm | |
C.G in % MAC | CG distance aft of LEMAC/MAC | LEMAC: Leading edge mean aerodynamic chord |
Center of gravity | Total moment/Total weight | |
Tire hydroplaning speed | 9 √ tire pressure(psi) | |
Radio range formula | R = 1.25√HT + √HR | HT = Height of transmitter, HR = Height of receiver |
Equal time point (distance) | ETP = (Total distance x inbound groundspeed)/(outbound groundspeed x inbound groundspeed) | |
Equal time point (time) | ETP distance/outbound groundpseed | |
Point of no return (distance) | Total endurance x (Outbound groundspeed x Return groundspeed)/(Outbound groundspeed/Return groundspeed) | |
Point of no return (time) | PNR distance / outbound groundspeed | |
Point of safe return (distance) | Endurance minus reserve x (Outbound groundspeed x Return groundspeed)/(Outbound groundspeed/Return groundspeed) | |
Point of safe return (time) | PSR distance / outbound groundspeed |
Radio navigation instruments, their frequencies, and range

Other rule of thumbs and useful info
Emergency frequencies | VHF 121.5, UHF 243, ELT 406 |
|---|---|
A headwind of 10% of your approach speed | decreases landing distance by 20% |
A 10% change in airspeed | causes 20% increase/decrease in stopping distance |
1000ft in field elevation | changes landing distance by 4% |
A narrow runway… | seems longer on approach |
A wider runway… | seems shorter on approach |
A narrow and uplsoping runway | creates an illusion that the aircraft seems higher on approach |
A wide and downsloping runway | creates an illusion that the aircraft seems lower on approach |
A wet runway | Increases landing distance by 50% |
Land on the 1st 1/3 of runway | Or go around |
Loss of 50% of thrust in a twin engine | Approx 80% loss of ROC |
10 - 25 degrees add more lift than drag | 25 - 40 degrees add more drag than lift |
Having a forward CG… | aircraft more stable and stall at higher speed |
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