AFMS
N"D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
~TECNAM
~'1]@
Cl
&!J[i'@~
[?0~
~llilOO@O
11agcAPv1-211
To
enable or disable ESP:
I)
Tum the large
fMS
Knob
to
select the AUX Page Group.
2)
Tum
the small FMS Knob
to
select the System Sctup
Pa!'C.
3)
If
necessary, select the
~ETUP
2 SoOkcy to display the AUX-SYSTEM
SETUP 2 Page.If the AUX-SYSTEM SETUP 2
is
already displayed, pro-
ceed to step
4.
4) Press the FMS Knob to activate the cursor.
5)
Tum
the large FMS Knob to place cursor
in
the
STA131LITY
& PRU-
TFCTION field.
6)
Tum the small
I·
MS
Knob to select 'ENABLE' or 'DISABLE'
7)
Press the
FMS
Knoh to remove the cursor.
ESP
engagement
and
operation:
ESP
is
automatically enabled on system power up.
ESP unavailability and/or failure is indicated to the pilot
on PFD by the advisory
"F.SP
not available" nn alert
window.
ESP will
tum
OFF
upon loss
of
hoth GPS.
7l1e
ADl'SY
"ESP
OFF"
will appear
1111
the alert
wi11duw
i11
case
of
loss
of
both GPS
13.1.1
PITCH
MODE
Pilch alliludc boundaries arc scl based on P20 I 0 aircrafi performances. Smee pilch E P
augmcnls the natural aircrafi longitudinal stability,
no
special simbology
is
required.
Value llial have been set-up for the 1'20
IO
arc as follows:
Nose above lhc horizon:
Engagcmcnl low lhrcshold: + 15°
Engagcmcnl upper threshold: +
18°
Lower disengage lhreshold: + 12°
Nose below lhe horizon:
Engagement low lhrcshold: -15°
Engagement upper threshold: -20°
Lower disengage threshold: -13°
ESP ulilizes eleclronie lorque and speed commands lo augmcnl the aircrall's slability:
it
uses an Electronic Torque Limil (ETL) and an Electronic Speed Limit (ESL) to limit the
maximum authority
of
the ESP function. ESP
is
inaclive when the pitch attitude
is
within
the posilivc and negative engagemcnl limits defined
in
the certification gain file
Section
1 -
General
AUTOPILOT
FUNCTIONS
Ed.
2,
Rev.O
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