FL
390
370
350
330
310
290
280 and below
MAX SPD
252
265
278
290
305
315
320
— WHEN L/G DN : DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as well as in roll. NOTE: Use manual control of cabin pressurization (Refer to 3.02.21) :
— MODE SEL MAN
— MAN V/S CTL AS ROD
STATUS
MAX SPEED 320/.82
RUD WITH CARE ABV 160 KT
At slats' extension, full rudder travel authority is recovered.
APPR PROC :
* FOR L/G GRVTY EXTN (not on the ECAM) :
— GRVTY GEAR
EXTN handcrank . . . . PULL AND TURN
— L/G LEVER DOWN
WHEN L/G DN : DIRECT LAW
— FOR LDG USE FLAP 3
— GPWS LDG FLAP 3 ON
APPR SPD VREF + 10 KT
CAT 1 ONLY
INOP SYS ATT LIMIT
OVSP LIMIT ALPHA LIMIT ADR 1+2+3 WINDSHEAR DET RUD TRV LIM 1+2 A/THR
AP 1+2
GPWS
Other inop sys : See below
* DURING FINAL APPR
— V/S CTL FULL UP
LDG DIST X 1.2
NOTE 1 : In case of a go-around, respect maximum speed 215 knots in CONF 1+F due to the loss of flap auto retraction to CONF 1.
Other inoperative systems
CAB PR 1+2 ATC ALTI MODE TCAS <
L/G RETRACT
RAT automatic extension is lost.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.19
SEQ 200
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.20
SEQ 001
This procedure is not displayed on the ECAM. Only dual ADR warnings are displayed, in case of a triple ADR failure.
— ADR (all) OFF
— STBY INST (ALT + ASI) USE
NOTE : Disregard ECAM actions for AIR DATA SWTG and ATC, since these have no effect in case of a total loss of ADRs.
F/CTL ALTN LAW (PROT LOST)
NOTE : The STALL WARNING is lost.
— MAX SPEED 320/.82
See the following table for the IAS/M relationship for .82.
FL
390
370
350
330
310
290
280 and below
MAX SPD
252
265
278
290
305
315
320
— WHEN L/G DN : DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as well as in roll. NOTE: Use manual control of cabin pressurization (Refer to 3.02.21) :
— MODE SEL MAN
— MAN V/S CTL AS ROD
STATUS
MAX SPEED 320/.82
RUD WITH CARE ABV 160 KT
At slats' extension, full rudder travel authority is recovered.
APPR PROC :
* FOR L/G GRVTY EXTN (not on the ECAM) :
— GRVTY GEAR
EXTN handcrank . . . . PULL AND TURN
— L/G LEVER DOWN
WHEN L/G DN : DIRECT LAW
— FOR LDG USE FLAP 3
— GPWS LDG FLAP 3 ON
APPR SPD VREF + 10 KT
CAT 1 ONLY
INOP SYS ATT LIMIT
OVSP LIMIT ALPHA LIMIT ADR 1+2+3 WINDSHEAR DET RUD TRV LIM 1+2 A/THR
AP 1+2
GPWS
Other inop sys : See below
* DURING FINAL APPR
— V/S CTL FULL UP
LDG DIST X 1.2
NOTE 1 : In case of a go-around, respect maximum speed 215 knots in CONF 1+F due to the loss of flap auto retraction to CONF 1.
Other inoperative systems
CAB PR 1+2 ATC ALTI MODE TCAS <
L/G RETRACT
RAT automatic extension is lost.
A319/A320/A321
oniatTril.,,
ABNORMAL PROCEDURES
REV 36
2.21
SEQ 001
If IR alignment is lost, the navigation mode is inoperative (red ATT flag on the PFD, and red HDG flag on the ND(.
Aircraft attitude and heading may be recovered by applying the following procedure. The aircraft must stay level, with constant speed for 30 seconds.
— MODE SELECTOR ATT
ALIGN light on for 30 seconds. ATT MODE displayed on the CDU.
— LEVEL A/C ATTITUDE HOLD
— CONSTANT NC SPEED MAINTAIN
— DISPLAY SYS switch AFFECTED SYS
— DISPLAY DATA switch HDG
Depending on the CDU keyboard installed, an "H" may be written on the "5" key :
* If "H" is written on the "5" key :
— H KEY PRESS
Degree marker, 0 decimal point, ENT and CLR lights come on.
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