Power Settings

PA-46 Malibu · N9124Y

Assigned altitude (ft)

Altimeter (in Hg)

OAT (°C)

Desired performance

RPM —

Manifold pressure — in Hg

Adj. fuel flow — GPH

Expected airspeed — KTAS

For reference only. Verify against the POH.

Airspeed calibration

Adjust the Expected airspeed to match this airframe (e.g. "runs 3 kt slow"). Enter a percentage, or knots at a reference altitude — both are stored as a uniform percentage applied at every altitude.

%

kt at ft

How to use

Entering conditions

Set Assigned altitude, Altimeter, and OAT with the − / + buttons. Press and hold to change quickly.
Tap the Altimeter or OAT value to reset it to standard — 29.92 in Hg for the altimeter, and ISA temperature for the current altitude. A value is outlined in teal when it is at standard.
As you change altitude, OAT follows the standard lapse rate (−2 °C per 1,000 ft) from wherever you set it.

Flight levels (18,000 ft and up)

At or above 18,000 ft the altimeter locks to 29.92 (standard), and pressure altitude equals your assigned altitude.

Checking your airspeed

Tap the Expected airspeed to briefly see the estimated indicated airspeed (KIAS) — handy for checking your ASI.
Use the gear (⚙) to calibrate the Expected airspeed to this airframe.

Fuel flow: these values are per the POH and should yield 50° lean of peak if you have an accurate fuel-flow meter to set the fuel flow. Every few flights, use the standard lean-of-peak procedure to confirm your fuel meter is correct.

For reference only — always verify against your POH.