320系列机组课程自动飞行非正常操作

航空

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航空

AUTOFLIGHT MENU Abnormal operation 1/59
AUTOFLIGHT MENU
Abnormal operation 2/59
Both FMGC exchange data through a
cross-talk bus and are synchronized.
The FMGC which drives the
synchronization is called MASTER.
The master FMGC is automatically
determined by the engagement status of
the AP/FD:
- if AP1 is ON, FMGC1 is master,
- if AP2 is ON, FMGC2 is master,
- if AP1+2 and/or FD1+2 are ON,
FMGC1 is master.
The A/THR is driven by the master
FMGC.
When both FMGCs crosstalk, they
are in DUAL mode of operation.
Note: when FD1+2 are ON, each FMGC
drives its FD and FMA on its onside PFD.
FMGC 1 FMGC 2
AUTOFLIGHT MENU
Abnormal operation 3/59
If the cross talk is lost
between both FMGCs, each
FMGC operates independently.
This mode of operation is
called “INDEPENDENT mode”.
The crew is advised by a
message in the scratchpad
“INDEPENDENT OPERATION”.
FMGC 1 FMGC 2
AUTOFLIGHT MENU
Abnormal operation 4/59
FMGC 1 FMGC 2
In INDEPENDENT mode, each
FMGC drives its own FG
(AP/FD), its own EFIS (PFD/ND),
and its own MCDU.
The crew must make the
same entries on each MCDU in
order to have the same guidance
orders for both AP/FDs and the
same informations displayed on
EFIS, and on MCDU.
When the crosstalk is
recovered, the FMGCs revert
automatically to “DUAL Mode”.
AUTOFLIGHT MENU
Abnormal operation 5/59
FMGC 1 FMGC 2
Let’ review the failure of
one FMGC, FMGC1 for
example.
If AP1 was engaged,
AUTO FLT AP OFF warning
is triggered on ECAM, and
AP1 is actually OFF.
AP2/FD2 and A/THR are
available since FMGC2 is
working.
AUTOFLIGHT MENU
Abnormal operation 6/59
The MCDU1 is now a copy of the
other MCDU2 with the scratchpad
message:
OPP FMGC IN PROCESS
This mode of operation is called
“SINGLE mode”.
FMGC 1 FMGC 2
AUTOFLIGHT MENU
Abnormal operation 7/59
Both FMAs display 2FD2, indicating that FD bars on both PFDs are driven by FMGC2.
Additionally, only FMGC2 position is computed and FMGC2 tunes the offside
navaids.
AUTOFLIGHT MENU
Abnormal operation 8/59
As a consequence of “SINGLE Mode”, the ND1 displays “SET
OFFSIDE RNG/MODE” and “MAP NOT AVAIL”messages as long as ND1
range and mode are not set identical to the ND2 ones.
Here, the Captain’s ND has to be set to the same range as the First
Officer’s ND in order to be able to display navigation map.
Seelleecctt Caappttaaiinn’’ss ND rraannggee ttoo 8800..
AUTOFLIGHT MENU Abnormal operation 9/59
As a consequence of “SINGLE Mode”, the ND1 displays “SET
OFFSIDE RNG/MODE” and “MAP NOT AVAIL”messages as long as ND1
range and mode are not set identical to the ND2 ones.
Here, the Captain’s ND has to be set to the same range of the First
Officer’s ND in order to be able to display navigation map.
Noo,, sseelleecctt Caappttaaiinn’’ss ND rraannggee ttoo 8800..
AUTOFLIGHT MENU Abnormal operation 10/59
As a consequence of “SINGLE Mode”, the ND1 displays “SET
OFFSIDE RNG/MODE” and “MAP NOT AVAIL”messages as long as ND1
range and mode are not set identical to the ND2 ones.
Here, the Captain’s ND has to be set to the same range of the First
Officer’s ND in order to be able to display navigation map.
Noo,, sseelleecctt Caappttaaiinn’’ss ND rraannggee ttoo 8800..
AUTOFLIGHT MENU Abnormal operation 11/59
AUTOFLIGHT MENU
Abnormal operation 12/59
Let’s review a similar failure called FMGC RESET,
which is a temporary failure of one FMGC caused by a
software interruption.
During the time of the reset, the mode of operation
is ‘SINGLE mode” with slightly different effects.
You are in cruise, AP1 is ON, FD1+2 are ON in
managed mode.
Clliicckk oonn tthhee ffoorrwaarrdd aarrrroow ttoo aaccttiivvaattee tthhee ffaaiilluurree..
AUTOFLIGHT MENU Abnormal operation 13/59
AUTOFLIGHT MENU Abnormal operation 14/59
No, to extinguish the Master Warning light,
push the Master Warning pb sw.
AUTOFLIGHT MENU Abnormal operation 15/59
No, to extinguish the Master Warning light,
push the Master Warning pb sw.
AUTOFLIGHT MENU Abnormal operation 16/59
AUTOFLIGHT MENU
Abnormal operation 17/59
AP1 turns OFF.
On the ECAM E/WD, read the title of the failure.
The warning “AUTO FLT AP OFF” is displayed
on the E/WD.
AP2/FD2 and A/THR are available.
After review and confirmation from the PF...
Clleeaarr AUTTO FFLLTT..
AUTOFLIGHT MENU Abnormal operation 18/59
AP1 turns OFF.
On the ECAM E/WD, read the title of the failure.
The warning “AUTO FLT AP OFF” is displayed
on the E/WD.
AP2/FD2 and A/THR are available.
After review and confirmation from the PF...
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 19/59
AP1 turns OFF.
On the ECAM E/WD, read the title of the failure.
The warning “AUTO FLT AP OFF” is displayed
on the E/WD.
AP2/FD2 and A/THR are available.
After review and confirmation from the PF...
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 20/59
Observe that the FD has reverted to HDG-V/S
modes, and that AP1 is no more displayed on FMA.
Note: Depending on the AP modes initially engaged
and on the type of reset, AP loss and FD reversion may
or may not occur.
In this example, we are facing one of the most serious
case.
AUTOFLIGHT MENU Abnormal operation 21/59
During the time of the reset:
- ND1 displays “MAP NOT AVAIL” red message,
- both MCDUs display the A/C STATUS page with
“PLEASE WAIT” in the scratchpad,
- Auto tuning of Navaids may be lost on side 1.
Note: do not use the MCDU while “PLEASE WAIT”
message is displayed in order not to increase the reset
time.
AUTOFLIGHT MENU Abnormal operation 22/59
The reset is usually over after few seconds; all
functions are recovered.
This is indicated by the disappearance of the
“PLEASE WAIT” and the “MAP NOT AVAIL”
messages.
- Check your F-PLN and the tuned navaids.
- Reengage the AP1 and managed modes.
- Reselect the most convenient MCDU page.
AUTOFLIGHT MENU
Abnormal operation 23/59
We have studied an FMGC 1 reset .
We will now review a FCU fault. Suppose the a/c is in
descent. You are the PNF, AP 1 and A/THR are engaged...
Clliicckk oonn tthhee ffoorrwaarrdd aarrrroow ttoo aaccttiivvaattee tthhee ffaaiilluurree..
AUTOFLIGHT MENU
Abnormal operation 24/59
On the E/WD, read the title of the failure.
Note that FCU 1 failure has no consequence
on the FCU indications, since FCU 2 has
automatically taken over.
AUTOFLIGHT MENU
Abnormal operation 25/59
The PF will ask you to perform the ECAM actions.
Here, only the barometer reference has to be crosschecked
between both PFDs, both EFIS CTL panels and the standby
altimeter; indeed the baro reference on both PFDs is driven by the
only FCU2.
Note that the FCU2 drives the two PFDs.
AUTOFLIGHT MENU
Abnormal operation 26/59
Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......
Clleeaarr AUTTO FFLLTT..
AUTOFLIGHT MENU Abnormal operation 27/59
Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 28/59
Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 29/59
The STATUS page is displayed for review.
No system capability degradation is shown.
You can see, in the INOP SYS column, that FCU 1
is now inoperative.
Clleeaarr STTATTUS..
AUTOFLIGHT MENU Abnormal operation 30/59
The STATUS page is displayed for review.
No system capability degradation is shown.
You can see, in the INOP SYS column, that FCU 1
is now inoperative.
Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 31/59
The STATUS page is displayed for review.
No system capability degradation is shown.
You can see, in the INOP SYS column, that FCU 1
is now inoperative.
Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 32/59
ECAM action completed.
We will now review the unlikely double FCU
failure. AP 1 and A/THR are ON, you are the PNF.
AUTOFLIGHT MENU Abnormal operation 33/59
You hear the continuous chime and see both warning lights
on.
AUTOFLIGHT MENU Abnormal operation 34/59
You hear the continuous chime and see both warning lights
on.
No, to extinguish the Master Warning
light, push on the Master Warning pb sw
AUTOFLIGHT MENU Abnormal operation 35/59
You hear the continuous chime and see both warning lights
on.
No, to extinguish the Master Warning
light, push on the Master Warning pb sw
AUTOFLIGHT MENU Abnormal operation 36/59
TThheeMaasstteerrWaarrnniinngg lliigghhtt iiss eexxttiinngguuiisshheedd..
AUTOFLIGHT MENU Abnormal operation 37/59
TThheeMaasstteerrWaarrnniinngg lliigghhtt iiss eexxttiinngguuiisshheedd..
No, to extinguish the Master Caution
light, push on the Master Caution pb sw
AUTOFLIGHT MENU Abnormal operation 38/59
TThheeMaasstteerrWaarrnniinngg lliigghhtt iiss eexxttiinngguuiisshheedd..
No, to extinguish the Master Caution
light, push on the Master Caution pb sw
AUTOFLIGHT MENU Abnormal operation 39/59
AUTOFLIGHT MENU
Abnormal operation 40/59
On the ECAM E/WD, read the title of the failure.
The consequences of the FCU 1+2 failure are:
- both APs are lost,
- A/THR is lost and thrust is locked ( THR LK message on FMA ),
- all FCU controls and indications are lost, including the EFIS
control panel.
AUTOFLIGHT Abnormal operation 41/59
On the E/WD, an additional amber caution comes up:
AUTO FLT THRUST LOCKED is triggered every 5 seconds. The
procedure asks to move the thrust levers out of the CLB detent so as to
recover manual control of the thrust.
We will do it for you in order to cancel this ECAM caution.
The thrust is now manually adjusted by the PF.
MENU
AUTOFLIGHT MENU
Abnormal operation 42/59
Note on the PFD that :
- all targets (SPD,HDG,ALT) are lost and red flags are displayed,
- altitude alert is lost,
- baro reference changes to 1013 QNH,
- FPV is displayed,
- FMA indications are lost,
- ILS deviation scales are displayed,
- Mach number indication is lost.
AUTOFLIGHT MENU
Abnormal operation 43/59
On ND :
- Rose Nav mode 80 NM range is displayed, regardless of
the position of the range selectors on EFIS control panels,
- needle 1 VOR/ADF is related to VOR 1,
- needle 2 VOR/ADF is related to ADF 2,
- weather radar image is lost (red “WXR RNG” message).
AUTOFLIGHT MENU
Abnormal operation 44/59
The PF will ask you to perform the ECAM actions.
You will have to deal with the first failure AP OFF.
Clleeaarr AUTTO FFLLTT..
AUTOFLIGHT MENU Abnormal operation 45/59
The PF will ask you to perform the ECAM actions.
You will have to deal with the first failure AP OFF.
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 46/59
The PF will ask you to perform the ECAM actions.
You will have to deal with the first failure AP OFF.
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 47/59
Then you deal with the second failure :
AUTO FLT FCU 1+2 FAULT.
Check the PFD baro reference (automatically set to
QNH 1013) with the standby altimeter.
Once below the transition altitude, set the standby
altimeter reference to the actual QNH.
AUTOFLIGHT MENU
Abnormal operation 48/59
Once the procedure is achieved and
confirmed by the PF,...
Clleeaarr AUTTO FFLLTT..
AUTOFLIGHT MENU Abnormal operation 49/59
Once the procedure is achieved and
confirmed by the PF,...
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 50/59
Once the procedure is achieved and
confirmed by the PF,...
Noo,, pprreessss eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 51/59
The STATUS page is displayed for review.
As baro reference is 1013, you have to determine
the altitude correction to be applied to get the proper
altitude reading, as a function of ( QNH-1013),
The approach capability is degraded to CAT1.
AUTOFLIGHT MENU
Abnormal operation 52/59
You can see, in the INOP SYS column, that both
FCUs, both APs and the A/THR are now inoperative.
After review and confirmation from the PF...
Clleeaarr STTATTUS..
AUTOFLIGHT MENU Abnormal operation 53/59
You can see, in the INOP SYS column, that both
FCUs, both APs and the A/THR are now inoperative.
After review and confirmation from the PF...
Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU Abnormal operation 54/59
You can see, in the INOP SYS column, that both
FCUs, both APs and the A/THR are now inoperative.
After review and confirmation from the PF...
Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..
AUTOFLIGHT MENU
Abnormal operation 55/59
ECAMaaccttiioonn ccoompplleetteedd..
AUTOFLIGHT MENU
Abnormal operation 56/59
We will now review a possible MCDU
malfunction.
AUTOFLIGHT MENU
Abnormal operation 57/59
In case you cannot neither insert any
data into the scratchpad nor change any
MCDU page, the MCDU is “locked“.
Such a failure is not automatically
detected.
AUTOFLIGHT MENU
Abnormal operation 58/59
In order to unlock the MCDU, you will
have to reset a C/B.
For more detail, please refer to your
documentation, ( QRH ).
AUTOFLIGHT MENU Abnormal operation 59/59
The same procedure would
apply in case of an MCDU failure
indicated by the amber
annunciator “FAIL”on the MCDU
itself.
NEXT
MMoodduullee ccoommpplleetteedd
AUTOFLIGHT MENU Abnormal operation 60/59
LLIISSTTOOFFSSUUBBJJEECCTTSS
EXIT
AUDIO GLOSSARY FCOM
RETURN
FFMMGGCCAAUUTTOORREESSEETT
FFMMGGCC““IINNDDEEPPEENNDDEENNTTMMOODDEE””
FFMMGGCC““SSIINNGGLLEEMMOODDEE””
FFMMGGCC““DDUUAALLMMOODDEE””
FFAAIILLEEDDMMCCDDUU
““LLOOCCKKEEDD””MMCCDDUU
FFCCUU11++22FFAAUULLTT
FFCCUU11FFAAUULLTT

guanshyy

kkkkkkkkkkkkkkkkk

bocome

A320系列机组课程自动飞行非正常操作

tissle

好资料，学习了。。。

gordon525

谢谢辛苦了 收藏一下

wsinglejoke

66666666666666666666666

diguo

恩。好东西。好好学习一下。