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.