AUTOFLT SYS AFS Flashcards

1
Q

AFS INCLUDES

A

FG
FLT GUIDANCE

FMS
FLT MGMT SYS

FE
FLT ENVELOPE

FCDC
FLT CONTROL DATA CONCENTRATOR

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2
Q

FG PROVIDES

A

LATERAL AND VERTICAL GUIDANCE

SPEED OR MACH CONTROL

IN ACCORDANCE WITH TARGETS

SEL BY FLT CREW
OR
MANAGED BY FMS

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3
Q

SELECTED TARGETS

A

FLT CREW SEL INPUT ON AFS CP

THESE INPUTS DIRECTLY TO FG FOR IMMEDIATE GUIDANCE RESPONSE

THIS IS CALLED SELECTED GUIDANCE

AFS CP IS SHORT TERM INTERFACE

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4
Q

MANAGED TARGETS

A

FLT CREW INSERTS THE FLT PLAN INTO MFD AHEAD OF TIME

FMS COMPUTES AND MANAGES THESE TARGETS FOR FG

THIS IS CALLED MANAGED GUIDANCE

MFD IS LONG TERM INTERFACE

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5
Q

LATERAL AND VERT GUIDANCE

A

EITHER SELECTED OR MANAGED INDEPENDENTLY OF EACH OTHER

HOWEVER MANAGED GUIDANCE NOT POSSIBLE WHEN SEL GUIDANCE USED

                                   LATERAL

                                      SEL.          MGD

                Selected.      YES.            YES VERTICAL
                Managed.      NO.              YES
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6
Q

VERT SPD

A

CAN ONLY BE SEL

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7
Q

FMS

A

PROVIDES LONG TERM GUIDANCE ALONG ACTIVE FLT PLAN

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8
Q

FE

A

USED BY FG AND FLT CONTROLS TO PREVENT THE AIRCRAFT FROM EXITING THE ENVELOPE

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9
Q

FCDC

A

DETERMINES THE AUTOLAND CAPABILITY FOR THE AFS

INTERFACES THE AP FD A/THR WITH FWS TO ALLOW ASSOC ALERTS TO BE TRIGGERED

GENERATES MAINT MSG FOR FG AND FE

FCDC ALSO PERFORMS FUNCTIONS FOR FLT CONTROLS

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10
Q

AFS ARCHITECTURE

A

3 PRIM
PRIMARY FLT CONTROL AND GUIDANCE COMP

2 FMS
FMS 1 and 2
EACH FMS OPERATED BY ONE OF 3 FMCS A,B,C

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11
Q

3 PRIMS CONTROL

A

FG ( AP FD A/THR)

FE

FLT CONTROLS

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12
Q

EACH PRIM CAN OPERATE

A

ONE OR BOTH AP

2 FD

A/THR

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13
Q

PRIM

MASTER AND SLAVE

A

ONE PRIM MASTER

2 SLAVES

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14
Q

MASTER PRIM

A

BEST OPERATIONAL CAPABILITY TAKING INTO ACCOUNT

MAN FLT CONTROL LAW CAPABILITY

FE AP AUTOLAND CAPABILITY

A/THR CAPABILITY

MASTER PRIM HAS PRIORITY TO OPERATE THE ENGAGED AP FD AND A/THR

IF ALL PRIMS HAVE SAME CAPABILITY PRIORITY PRIM 1,2,3

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15
Q

SLAVE PRIMS

A

SLAVE 1 and 2 PRIMS ARE IN STBY

READY TO CONTROL AP FD A/THR

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16
Q

MASTER PRIM LOST

A

IF MASTER PRIM LOSES BEST CAPABILITY

SLAVE 1 BECOMES MASTER PRIM

ALL ENGAGED AP FD A/THR TRANSFERRED

TWO OTHERS BECOME SLAVE 1,2

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17
Q

PRIM INTERFACES WITH

A
NAV AND POSN
FLT CTLS
LDG GEAR
BRAKES
STEERING
FUEL AND WT
ENGINES
FMS
AFS CP
MFDS
EWD
PFDS
THRUST LEVERS
FWS
SIDESTK DISCONNECT PB
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18
Q

FMS 1 and 2

A

FMS 1 CAPT SIDE FMC A

FMS 2 FO SIDE FMC B

FMC C STBY

AP1 FMC A MASTER B SLAVE

AP2 FMC B MASTER A SLAVE

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19
Q

FLT CREW INTERFACES AFS VIA

A
AFS CP
2 MFDS
2 KCCU
2 PFDS with FMA
2 NDS
2 EFIS CP
1 AP DISC PB SIDESTK
4 THRUST LEVERS WITH 2 A/THR INSTINCTIVE DISC PBSW
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20
Q

MFDS INTERFACE

A

INTERFACE WITH FMS

INFO ON FLT PLAN

AIRCRAFT POSN

FLT PERFORMANCE

FCU BACKUP

SURV

ATC

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21
Q

KCCU

A

NAVIGATE THROUGH FMS PG MFD

ENTER AND MODIFY DATA MFD

SOME LAT FLT PLAN REVISIONS ON MFD

22
Q

AFS CP FAILURE

A

MFD FCU BACKUP AUTO FLT PG

PROVIDES ALL AFS CP FUNCTIONS

23
Q

THRUST LEVER DETENTS

A

SENT TO PRIMS

A/THR THEN SENDS THRUST COMMANDS TO FADEC SYS

A PB CALLED INSTINCTIVE DISCONNECT PB LOCATED ON EACH SIDESTK DISENGAGES AP

24
Q

FG OVERVIEW

A

AP FD A/THR ALL INTEGRATED WITHIN FG

FG MODES ARE FMA

25
FMA
CAN DISPLAY 3 LINES EACH COLUMN ACTIVE MODES GREEN SECOND LINE BLUE MAGENTA FOR CONSTRAINTS 3RD LINE REMINDERS OR MESSAGES
26
SELECTED LAT MODES
HDG TRK
27
MGD LAT MODE
NAV
28
SEL VERT MODE
OP CLB VS FPA
29
MGD VERT MODE
DES
30
MGD LAT AND VERT MODE
LAND
31
AP FD VERT MODE DETERMINES
A/THR MODE AP FD VERT MODE CONTROLS SPD M A/THR CONTROLS THRUST AP FD VERT MODE CONTROLS TRAJ A/THR CONTROLS SPD M DURING ROLLOUT FLARE W AP ON A/THR MODE CONTROL THRUST IDLE
32
NO AP FD ENGAGES A/THR
A/THR ENGAGES IN SPEED OR | MACH IN ORDER TO CONTROL A SPD OR M TARGET
33
SPEED COLOURS
MANAGED MAGENTA SELECTED BLUE SELECTED HDG BLUE
34
FD
ONLY ONE PBSW FOR FD 1 and 2 FD 1 CAPT ADIRS 1 FD 2 FO ADIRS 2
35
EQUIP FOR FD
TO ENGAGE BOTH FDS FOLLOWING EQUIP REQD ``` 1 PRIM 2 ADRS 2 IRS AFS CP OR BACKUP PG NORMAL LAW (ALTN LAW IN SOME CASES) ```
36
FDS AUTO ENGAGE
AT AC POWER UP <30’ NO ROLL BAR REPLACED YAW BAR IF LOC AVAIL ROLL BAR LAT MODE ENGAGED PITCH BAR VERT MODE ENGAGED
37
YAW BAR
RWY FLARE ROLLOUT MODES ENGAGED ALONG W PITCH BAR RWY MODE ROLL AND PITCH IN FLARE ALONE IN ROLLOUT MODE
38
FD AUTO DISPLAYS
FD 1 and 2 AUTO DISPLAY IF GA ENGAGES
39
IF CREW SWITCH OFF FD PBSW
NO AP LAT AND VERT MODES DISENGAGE IF A/THR IN THRUST MODE REVERTS SPD M WITH AP LAT AND VERT MODES REMAIN ENGAGED
40
FD BARS AUTO DISAPPEAR
PITCH >13 DEG DOWN 25 DEG UP BANK ANGLE >45 DEG IN ROLLOUT MODE IF DIFF BETWEEN AC TRK AND RWY TRK >20DEG
41
FDS AUTO DISENGAGE
A/THR NOT ENGAGED AND AC SPD
42
FD FLASHES
PITCH AND OR ROLL BAR FLASH FOR 10 SECS ON BOTH PFDS INCASE REVERSION MODE PERMANENTLY FLASH ON RESPECTIVE PFD IF A FAILURE OCCURS IN ONE OF THE EQUIP USED FOR APP
43
RED FD FLAG PFD
PITCH ROLL AND YAW ORDERS NOT AVAIL WHEN FD ENGAGED RED FLAG PFD FLASHES THEN STEADY PFD WILL NOT SHOW BARS
44
DUAL ADR FAILURE
LOSS BOTH APS AND FDS
45
2 PRIM FAILURES
BOTH APS AND FDS REMAIN AVAIL
46
ONE FD LOST
1FD1 2FD2
47
AP WILL ENGAGE WHEN
FLT CREW PRESSES AP1 or AP2 IF AC IN FLT >5 SECS AC PITCH BANK AND SPD IN LIMITS
48
ENGAGING 2 AP
WHEN 1 ENGAGED PRESS OTHER AP ONCE APP MODE ARMED OR ACTIVE WHEN GA MODE ENGAGED WHEN BOTH AP ENGAGED AP1 ACTIVE AP2 STBY REGARDLESS OF ORDER OF ENGAGEMENT
49
AP DISENGAGEMENT
SIDESTK PB PRESSED AP PBSW AFS CP DESELECTED ANY SIDESTK OR RUDDER PEDAL MOVED
50
PRESS AP DISC PB TWICE
PRESSING ONCE AP OFF MEMO PFD AND EWD LOW VOLUME CAVALRY CHARGE MASTER WARN LT ILLUM