Thales FMGS, Pilot'S Manual

Page: 180 / 703

FLIGHT PHASES
28 CLIMB
4.7. SCRATCHPAD MESSAGES
SPEED ERROR AT XXX
"SPD ERROR AT XXX" s-pad msg (white) is displayed when NAV mode
and SPD managed are engaged and the system predicts that a speed
constraint will be missed by more than 10 knots.
The message is cleared when the predicted discrepancy is reduced to
less than 5 knots.
In this example SPD is
selected 270 KT although
a SPD CSTR 250 KT exists
at TOU.
FROM THV001 {}
UTC SPD/ALT
T-P 2201 / FL60
(SPD) BRG356° 6
(LIM) 2207 * 270/ FL100
TRK339° 1
TOU 2207 * 270/ FL108
46
(T/C) 2215 270/ FL360
FIST5A 1 NM
FISTO 2215 .79/ "
DEST UTC DIST EFOB
EGLL27R 2327 525 4.2
SPD ERROR AT TOU £$
SPEED LIMIT EXCEEDED
"SPD LIMIT EXCEEDED" s-pad msg (white) is displayed in CLIMB,
CRUISE and DESCENT flight phases when:
− Speed exceeds SPEED LIMIT by 10 KT, and
− ALT is within 150 ft of SPEED LIMIT ALTITUDE.
Message is cleared when speed no
longer exceeds the SPEED LIMIT + 5 KT.
In this example SPD has been selected
at 270 KT although a SPD LIM 250 KT
exists below FL100.
FROM THV001 {}
UTC SPD/ALT
T-P 2201 / FL60
(SPD) BRG356° 6
(LIM) 2207 * 270/ FL100
TRK339° 1
TOU 2207 * 270/ FL108
46
(T/C) 2215 270/ FL360
FIST5A 1 NM
FISTO 2215 .79/ "
DEST UTC DIST EFOB
EGLL27R 2326 525 4.2
SPD LIM EXCEEDED £$
J43126AA 00
© THALES AVIONICS S.A.
AIRBUS A318/319/320/321