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engagement.
C - can be de-activated if the APPR
pushbutton is pressed.
TMUFM2004 LEVEL 3
EFFECTIVITY 22-81-00 Page 16
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 140
ALL
22 - AUTO FLIGHT SYSTEM
22-00-00 FLIGHT MODE ANNUNCIATOR
DESCRIPTION/OPERATION
CONTENTS:
General
Colours
A/THR Zone
AP/FD Vertical Zone
AP/FD Lateral Zone
Landing Category Zone
Engagement Status
Messages
Self Examination
TMUFGCR04 LEVEL 3
EFFECTIVITY 22-00-00 Page 1
Jan 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 141
ALL
FLIGHT MODE ANNUNCIATOR DESCRIPTION/OPERATION
GENERAL
Information about modes and engagement status of
guidance functions, plus some specific messages, are
displayed on the Flight Mode Annunciator located at
the top of each Primary Flight Display.
The Flight Mode Annunciator (FMA) is divided into fives
zones: A/THR information, vertical and lateral AP/FD
modes, landing capability, engagement status of
guidance functions. Message use the third line of the
second and third zones.
COLOURS
Five colors are used:
- GREEN: A/THR and AP/FD active modes.
- CYAN: AP/FD armed mode, A/THR engaged (not
active), V/S, FPA, FLX TEMP, MDA, MDH and DH
numeric values, selected Mach and speed.
- WHITE: Flight Guidance function engaged, A/THR
activated, landing categories, manual thrusts
(surrounded by boxes) which are held when A/THR
is not active, messages.
Mode change and guidance function engagement
make a white box appear for ten seconds.
- AMBER: Messages, boxes around certain thrust
modes.
- RED: MAN PITCH TRIM ONLY message.
A/THR ZONE
Here are all the possible displays in the autothrust
zone.
Autothrust function information:
- First line in green: SPEED, MACH, THR MCT, THR
CLB, THR IDLE, THR LVR.
- First line in green with a flashing amber box:
A.FLOOR, TOGA LK.
- First and second lines in white: MAN TOGA, MAN
FLXxx ,MAN THR, MAN MCT.
- Third line, flashing white: LVR CLB, LVR MCT.
Third line in amber: LVR ASYM.
NOTE: In MAN FLXxx, xx is the value of the selected
flexible take-off temperature in degrees Celsius
in cyan.
TMUFGCR04-T01 LEVEL 3
EFFECTIVITY 22-00-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 142
ALL
FLIGHT MODE ANNUNCIATOR DESCRIPTION/OPERATION
TMUFGCR04-P01 LEVEL 3
EFFECTIVITY 22-00-00 Page 3
Jan 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 143
ALL
FLIGHT MODE ANNUNCIATOR DESCRIPTION/OPERATION
AP/FD VERTICAL ZONE
Here is a list of the possible messages in the
autopilot/Flight Director vertical zone.
Vertical modes:
- First line in green: SRS, ALT*, ALT, ALT CRZ*,
ALT CRZ, ALT CST*, ALT CST, EXP CLB, EXP DES,
G/S*, G/S, OP CLB, OP DES, CLB, DES.
And common to vertical and lateral areas: LAND,
FLARE, ROLL OUT, FINAL APP.
- First line in green and cyan: FPA±xx°, V/S±xxxx.
- Second line in cyan: ALT, CLB, G/S, DES, OP
CLB, OP DES, FINAL and SPEED SEL:xxx, MACH
SEL:.xx which are seen in lateral and vertical
areas (xxx is a preset speed, .xx is a preset
Mach).
AP/FD LATERAL ZONE
Here is a list of possible messages in the
autopilot/flight director lateral zone.
Lateral modes:
- First line in green: RWY, RWY TRK, HDG, TRK,
LOC*, LOC, GA TRK, APP NAV, NAV.
And common to vertical and lateral areas: LAND,
FLARE, ROLL OUT, FINAL APP.
- Second line in cyan: NAV, LOC, APP NAV.
LANDING CATEGORY ZONE
Here is a list of the possible messages in the landing
category zone.
Landing categories:
- On the first and second lines, the possible
white displays are: CAT1, CAT2, CAT3 SINGLE,
CAT3 DUAL.
- On the third line, messages in white and numeric
values in cyan: DHxxx, NO DH, MDAxxxx, MDHxxxx.
NOTE: Information appears in this zone as soon as land
mode is armed or active.
TMUFGCR04-T01 LEVEL 3
EFFECTIVITY 22-00-00 Page 4
Jan 31/95
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 144
　
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