PA28-161 · Performance · 02 of 04
Takeoff and Climb Charts
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Takeoff and Climb Charts
The takeoff and climb charts are read against their associated conditions. Knowing those conditions tells you when a chart figure applies as printed and when it needs a correction.
At a glance
- Climb chart weight2440 LBS
- Climb chart speed79 KIAS
- Rate of climb reduction, wheel fairings removed40 FPM
Takeoff charts
There are two sets of takeoff charts, each giving the ground roll and the distance over a 50 ft barrier: one with 0° flaps and one with 25° flaps. Both assume a paved, level, dry runway and full power before brake release.
Climb performance chart
Weight — gross weight, 2440 LBS.
Power — full throttle, mixture leaned per Lycoming instructions.
Speed — 79 KIAS.
NOTE — Reduce the rate of climb by 40 FPM when the wheel fairings are removed.
Fuel, time and distance to climb
This chart assumes a weight of 2440 LBS, 0° flaps, full throttle, mixture leaned per Lycoming instructions, 79 KIAS and no wind.
Check yourself
What two distances do the takeoff charts give?
What runway and power conditions do the takeoff charts assume?
At what weight and speed is the climb chart drawn?
What correction applies to the rate of climb without wheel fairings?
Study aid — always fly your aircraft's current AFM/POH.
Source: Piper PA-28-161 Warrior II Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, Report VB-1180, p. 5-15..5-20, Rev. 9 (17 July 2015)
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