AIRCRAFT ____________________________________
MANIFOLD PRESSURE | RPM | PITCH SETTING | AIRSPEED | VSI | |
CLIMB | |||||
CRUISE | |||||
CRUISEDESCENT | |||||
APPROACH | |||||
APPROACH DESCENT | |||||
NON-PRECISION DESCENT |
ATTITUDE + POWER = PERFORMANCE
CONTROL INSTRUMENTSQ Attitude IndicatorQ RPM (or MP) | PERFORMANCE INSTRUMENTSQ AirspeedQ AltimeterQ Turn CoordinatorQ Vertical Speed Indicator |
PITCH – POWER – TRIM (Except When Descending: POWER – PITCH – TRIM)
UNUSUAL ATTITUDES
NOSE HIGH | NOSE LOW |
Power – ADD | Power – RETARD |
Pitch – LOWER | Wings – LEVEL |
Wings – LEVEL | Pitch – RAISE |
PARTIAL PANEL RECOVERY
Aircraft is level when ALTIMETER and VSI stop movement and reverse.