AFMS
N'D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
~TECNAM
[p~@'\]@
c
&f!IT'©~
rfO~@Ou{k
[iVA]t!}[fi)(!!]@O
Page
APVl-19
12.1
GDU
(MFD)
GOU
MFD
unit can display
a>
default engine parameters and movmg map information, along
with other mformauon that cun
be
selected by the pilot {see the first ligurc below), when revcrsion-
ary mode
I>
active it will display night param<!lers
(111
the form
of
l'FD
with the lefi strip engine
information, as can be seen
in
the second figure below).
It
is
the user interfact: for P2010 avion-
ics suite
GDt
l (l\H"D)
Reversionary
mode
:
In
the event
of
a single display failure the
sy;tcm
is
able to automatically
swnch
the
crll1cal inlormation
mduding
flight and engine parameters on the remaining displ.iy prc-
>enting them
in
a comp.ict view.
In
the event
of
a failun:
or
the automatic switch logic, the
pilot can
ea
~il)
force th.:
r~vcrs1onary
mode b) pressing the red button on the bottom
of
th.: audio
1>Jnd
thus gettmg both Hight and engine parameters mlormation, necessary for
co
nti11ucd
sali: flight, on the n:mami
ng
display.
NAV1
and
COM1
(provided
by
the
failed
PFD)
Flagged
Invalid
CD
U
{l\lfO)
in
rcversiunnry mode
Section
1 -
General
AUTOPILOT
DESCRIPTION
Ed.
2. Rev. I
To Next Page
Loading...
