Tecnam P2010 2015 - Section 4 - Normal Procedures; 1. Introduction; 2. IFR Flight: Training Pre-requisites and Incremental Exposition to G1000 Suite

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AFMS N'D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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13.2.1 ALTITUDE CRITICAL MODES (ALT, GS, GP, TO, GA, FLC)
When the airspeed trend vector (dedicated algorithm) reaches 65 +/ - 2 KIAS a single aural
''AIRSPEED" will sound, alerting the pilot to the impending undcr~pecd condition, which
requires pilot actmn.
If the aircraft decelerates to stall warning and a ~ peed of 65 K IA S is reached, th e la teral and
vertical night director modes will change from active to armed and the autopilot will provide
input causing the aircraft to pitch down and the wings to level.
The aural "AIRSPEED'' alert wi ll sound every five ~ c conds .
If aircrall is unintentionally decelerated to 65 Kli\S, a MINSPD annunciation posts above
the airspeed tape on PHJ in alternating amber and hlack text A red "UNDER'>l'EED PRO-
TECT ACTI VE " annunciation will appear to the right of the vertical speed indicator. USP
will drive the pitch down until the indicated airspeed increases above 70 K IAS or stall warning
turns ofT , plus two knots (whichever comes first).
When USP disengages, autopilot wi ll cause th e oircrafi to pitch up until recapturmg the vertical
reference (vertical and lateral fli g ht director modes will change from white armed to green ac-
tive).
Section 1 - General
AUTOPILOT FUNCTIONS
Ed 2, Rev.O