Tecnam P2010 2015 - Page 41

AFMS N' D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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13.2.2 NON ALTITUDE CRITICAL MODES (VS, VNAV, IAS)
When the airspeed trend vector (dedicated algorithm) reaches 65 +/- 2 KIAS a single aural
··AJRSPEFD will sound, alerting the pilot to the impending under- speed condillon. wluch
requm:s pilot action.
If the aircrafi is allowed 10 decelerate to an IAS below the mini 111u111 com111andable autopilot
airspeed (65 Kts for 1'2010), a red .. UN DERSPl' ELJ PROTECT ACTIVE ,. anuuncrntion appear
to the right of the vertical speed indicator
Vertical night director mode will change from active to armed, l'hght Director and autopilot
will comm,md the aircrafi to pitch down until reaching a pitch attitude at which IAS equals at ....)
ll:a~l the 111inimum commandable autopilot airspeed, a\oiding the development ofa stall condi-
tion.
HOG I +-AP VD I ALT 2000FT
When airspeed increases (as a result of adding power /thrust) to an IAS above 70 KIAS, U SP
will then disengage and the autopilot will command the aircrafi to pitch up until recapturing
the vertical reference (vertical vertical flight director mode will switch from white armed lo
green active).
Section 1 - General
AUTOPILOT FUNCTIONS
l~d 2, Rev. 0