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Tecnam P2010 - Page 435

Tecnam P2010
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AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV3-19
Section 3 Emergency procedures
POWERPLANT EMERGENCIES
Ed. 1, Rev.0
6.10. DEFECTIVE ENGINE CONTROLS
Defective Mixture Control Cable
1. Maintain altitude to the nearest arfield
2. During descent, check engine behaviour to a higher power setting.
A lean mixture can lead to engine roughness and loss of power.
Landing approach must be planned accordingly.
Defective Throttle Control Cable
If power is sufficient to continue flight:
1. Approach nearest airfield, control engine power with Propeller lever
2. Perform landing with shut-down engine applying
Forced landing procedure. (See Para 11)
If power is not sufficient to continue flight:
1. Carry out Forced landing procedure. (See Para 11)
Defective Propeller Lever Control Cable
If power is sufficient to continue flight:
1. Approach nearest airfield, control engine power with throttle
2. Perform normal landing.
If power is not sufficient to continue flight:
1. Carry out Forced landing procedure. (See Para 11)
Go-around may then be impossible.
Go-around may then be impossible.

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