Attitude plus power equals performance: the power-change rule of thumb
Attitude plus power equals performance. Instruments show airspeed, altitude, and rate of climb or descent. Attitude or power changes alter them.
- Same attitude gives different numbers per aircraft. Example: light aircraft at a nose-up attitude might climb 500 ft/min at 90 KT, gaining 2,500 ft in five minutes.
- Learn own aircraft's numbers.
Controls:
| Control | Sets |
|---|---|
| Elevators | Pitch attitude |
| Throttle | Power |
- Neither alone controls airspeed or altitude.
- In cruise attitude, changing airspeed needs throttle and elevator adjusted together.
Rule of thumb for a power change of one unit step (100 RPM, or 1 in Hg of manifold pressure):
| Flight | Held constant | Change per step |
|---|---|---|
| Level flight | Altitude | Airspeed about 5 KT |
| Climb or descent | Attitude | Rate about 100 ft/min |
Worked example:
- Level flight at 120 KT, 2,300 RPM.
- Slow to 100 KT (20 KT reduction): reduce power about 400 RPM, to 1,900 RPM.
Trap: two multipliers (5 KT vs 100 ft/min) for the same step; swapping the level and climb/descent figures is the classic mix-up.
Trap: holding altitude with power alone, or airspeed with elevator alone, instead of both together.
References
- TP 1102 Instrument Flying: Attitude Plus Power Equals Performance
- TP 1102 Instrument Flying: Power Control
- TP 1102 Ex.24 Climbing / Descending
- TP 1102 Ex.6 Straight-and-Level Flight (Attitude Plus Power Equals Performance)