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Tecnam P2010
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1
st
Edition, Rev. 0
Section 4 Normal procedures
CHECKLISTS
AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV4-20
5.6. TAKEOFF
For 5000ft density altitude and above, or high ambient temperatures, a FULL RICH mixt
may cause rough running of the engine or a loss of performance. The mixture may be
justed to obtain smooth engine operations.
Lean to maximum RPM at Full Throttle prior to take-off where airports are at 5000ft den
altitude or higher.
During climb, a rough method of correctly leaning is to slowly reduce mixture lever until
increase of appr.ly 50-100 RPM is noticed at constant IAS or EGT reaches 1375°F mark
1. Pitot HEAT: ON if required
2. Fuel pump: ON
3. Brakes: apply
4. Throttle: FULL and check approximately 2680

20 RPM
Engine proper performance at full throttle shall be checked early in the ground roll in
order to abandon take-off if necessary.
A rough engine, sluggish RPM increase or failure to reach take-off RPM are reasons for
abandoning the take-off. If the engine oil is cold, an oil pressure in the yellow sector is per-
missible
5. Engine instruments: check parameters within the limits
6. Brakes: Release
7. Rotation speed VR: 60 KIAS
8. Airspeed: 67 KIAS
Above a safe height:
1. Propeller lever: 2600 RPM
2. Landing lights: OFF

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