PA-28-161 Landing Distance Calculator

Landing Distance Performance Calculator for Piper PA28-161 Cherokee Warrior II aircraft.

Always check and use the procedure and information that is described in the Pilot Operating Handbook/Flight Manual for your aircraft.

The following landing configuration is assumed:
Power off full stall touchdown
Maximum braking
Approach speed 63 kts IAS (Indicated Air Speed)
Gross weight (2325lbs)
Flaps 40degrees (full flaps)

Calculation limits are:
Sea-level to 3,000ft elevation
-20 to +40 degrees Centigrade
QNH 950 to 1050mb
Head/tailwind limit 40kts
Runway length up to 3000m
Downhill slope to 10 degrees
Result includes 43% safety factor increase
Yellow warning if >70% runway required