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113 Cards in this Set

  • Front
  • Back
LEVELS OF AUTOMATION
LOWEST- FLIGHT DIRECTORS
HIGHER- AUTOTHROTTLE TO CONTROL THRUST AUTOPILOT TO CONTROL PITCH AND ROLL
HIGHEST- FMC TO NAVIGATE

F/D DIRECTOR SWITCH ON DISPLAYS COMMAND BARS IF

COMMAND PITCH AND ROLL MODES ARE ENGAGED

WITH ONE OR BOTH A/P ENGAGED IN CMD
THE FCC FOR THE FIRST A/P IN CMD IS THE MASTER FCC REGARDLESS OF WHICH F/D TURNED ON FIRST
INDEPENDENT F/D OPERATION OCCURS WHEN NEITHER A/P ENGAGED IN CMD, BOTH F/D SWITCHES ARE ON AND ONE OF THE FOLLOWING MODE CONDITIONS EXISTS
-APP MODE ENGAGED WITH LOC AND G/S CAPTURED
-GA MODE ENGAGED BELOW 400 RA
-TO MODE ENGAGED BELOW 400 RA
INDEPENDENT F/D OPERATION IS INDICATED BY
ILLUMINATION OF BOTH MA LIGHTS
WHEN INDEPENDENT OPERATION TERMINATES
THE MA LIGHT EXTINGUISHES ON THE SLAVED SIDE
NEW AUTOFLIGHT MODES ARE SHOWN WITH A BOX FOR
10 SECONDS
IN CONTROL WHEEL STEERING, THE AUTOPILOT USES CONTROL WHEEL INPUTS
TO CHANGE PITCH AND ROLL
IF THE AUTOPILOT IN CWS MODE AND YOU RELEASE THE THE CONTROL WHEEL
WHEN THE BANK ANGLE IS LESS THEN 6 DEGREES THE AUTOPILOT COMMANDS WINGS LEVEL
ARM MODE
NO AUTOTHROTTLE MODE ENGAGED, THE THRUST LEVER AUTOTHROTTLE SERVOS ARE INHIBITED, THE PILOT CAN SET THRUST LEVERS MANUALLY ALSO MINIMUM SPEED PROTECTION
SPEED MODE ENGAGES MANUALLY BY PUSHING SPEED SWITCH. SPEED MODE ENGAGES AUTOMATICALLY WHEN
ALT ACQ
ALT HOLD
V/S
G/S CAPTURE
A/T DOES NOT SET THRUST ABOVE DISPLAYED N1 LIMIT, HOWEVER
A/T CAN EXCEED N1 VALUE MANUALLY SET BY N1 MANUAL SET KNOB
AUTOTHROTTLE DISENGAGEMENT
THRUST LEVERS BECAME SEPERATED MORE THAN 10 DEGREES
IF AN AUTOPILOT IS ENGAGED IN CMD, BUT NO ROLL MODE IS ENGAGED
THE AUTOPILOT USES CWSR
BANK ANGLE SELECTOR IS ACTIVE FOR HDG, VOR IS NOT ACTIVE FOR
LOC AND LNAV
IF THE AIRPLANE IS MORE THAN 3 MILES FROM THE ACTIVE ROUTE, LNAV ENGAGES ONLY
IF THE AIRPLANE IS ON A HEADING THAT INTERCEPTS THE ACTIVE ROUTE BEFORE THE ACTIVE WAYPOINT AT AN INTERCEPT ANGLE LESS THAN 90 DEGREES
IF THE AIRPLANE IS WITHIN 3 MILES OF AN ACTIVE ROUTE
LNAV CAN ENGAGE FROM ALL AIRPLANE HEADINGS
WHEN FCC-A IS THE MASTER FCC, THE AUTO FLIGHT SYSTEM USES DATA FROM
CAPTAINS BAROMETRIC ALTIMETER
WHEN FCC-B IS THE MASTER
THE FIRST OFFICERS ALTIMETER IS USED
ALTITUDE RANGE IS
0-50 000 FEET IN 100 FOOT INCREMENTS
ALTITUDE DISPLAY WHEN POWER FIRST APPLIED
DISPLAYS PREVIOUSLY SELECTED ALTITUDE
IN A LVL CHANGE CLIMB
THE AUTOTHROTTLE USES MAXIMUM THRUST
THRUST IS SET TO THE ACTIVE N1 LIMIT
N1 SHOWS IN THE A/T FIELD OF THE FMA
IN A LVL CHANGE DESCENT
THE AUTOTHROTTLE USES THE MINIMUM THRUST
LVL CHANGE IS BEST USED FOR
LARGE ALTITUDE CHANGES
VERTICAL SPEED RANGE IS
-7900 TO +6000 FPM
50 FPM < 1000 FPM
100 FPM > 1000 FPM
VERTICAL SPEED IS BEST FOR
SMALL ALTITUDE CHANGES
LATER CHANGES IN THE ALTIMETER BAROMETRIC SETTING
DO NOT MAKE THE AIRPLANE CLIMB OR DESCENT TO FOLLOW THE NEW INDICATED ALTITUDES
VNAV SPD
AFDS CONTROLS PITCH TO MAINTAIN FMC SPEED

VNAV PTH

AFDS CONTROLS PITCH TO MAINTAIN FMC ALTITUDE OR DESCENT PATH

IN A VNAV SPD DESCENT
THE AUTOTHROTLE SETS THE THRUST TO IDLE AND THE AUTOPILOT HOLDS THE FMC TARGET SPEED
IN A VNAV PTH DESCENT
THE A/P COMMANDS THE AIRPLANE TO FOLLOW THE FMC VERTICAL PATH. A/T HOLDS IDLE, BUT COMMAND THE FMC SPD MODE IF GROUND SPEED TO SLOW TO FOLLOW THE FMC VERTICAL PATH
DRAG REQUIRED
IF THE AIRSPEED INCREASES MORE THAN 10 KNOTS ABOVE FMC TARGET SPEED
IFF ALL ALTITUDE CONSTRAINS ARE REMOVED FROM A VNAV PTH DESCENT
THE FMC AUTOMATICALLY CHANGES TO A VNAV SPD DESCENT
N1 TO/GA TAKEOFF
THE FLIGHT DIRECTOR COMMAND BARS SHOW A 10 DEGREE NOSE DOWN PITCH AND THE AUTOTHROTTLE ADVANCES THE THRUST TO N1 LIMIT
AT 60 KNOTS
THE FLIGHT DIRECTOR COMMAND BARS MOVE TO SHOW 15 DEGREES NOSE UP PITCH
ABOVE 80 KNOTS
THE AUTOTHROTTLE MODE CHANGES TO THR HLD

AS THE CLIMB RATE INCREASES

THE PITCH BAR COMMANDS AN ATTIDUE TO HOLDS A SPEED V2+20

AT 400 RA
ENGAGE A ROLL MODE
AT 800 RA
THE A/T MODE CHANGES FROM THR HLD TO ARM
WHEN YOU REACH FLAP RETRACTION ALTITUDE AND YOU PUSH THE N1 SWITCH
THE THRUST REDUCED TO CLIMB THRUST
IF YOU ENGAGE A/P WHILE IN T/O MODE
THE PITCH MODE AUTOMATICALLY ENGAGES IN LVL CHG, ROLL MODE HDG SEL, CURSOR V2 TO V2+20
AFDS LEAVES T/O MODE
WHEN AN AUTOPLIOT IS SELECTED OR A PITCH MODE IS ENGAGED
APP THEN SECOND A/P
THIS ARMS THE SECOND A/P BUT DOES NOT ENGAGE IT
SINGLE CH
ONLY ONE A/P IS ENGAGED
AT G/S CAPTURE
G/S CHANGES FROM ARMED TO AN ACTIVE MODE, TMD DISPLAYS GA AS ACTIVE THRUST LIMIT
THE SECOND A/P ENGAGES WHEN THE AIRPLANE
BELOW 1500 RA SINGLE CH TO CMD, FLARE IS ARMED
A/P GO AROUND IS ARMED BUT NOT ANNUNCIATED

FOR A DUAL A/P APPROACH

SELECT SECOND A/P ABOVE 800 RA

AT 400 RA
AUTOPILOTS AUTOMATICALLY ADD AN ADITIOANAL AMOUNT OF STABILIZER NOSE UP TRIM
IF FLARE IS NOT ARMED BY 350 RA
AUTOPILOTS AUTOMATICALLY DISENGAGE
THE FLARE MANEUVER STARTS AT
50 RA FMA PITCH FIELD CHANGES TO FLARE
FLIGHT DIRECTOR COMMAND BARS ARE REMOVED
THE A/T REDUCES THRUST
BELOW 27 FEET FMA SHOWS RETARD
AUTOTHROTTLE AUTOMATICALLY DISENGAGES
AFTER TOUCHDOWN 2 SECONDS
MANUALLY DISENGAGE THE AUTOPILOT
WITH A SINGLE CHANNEL AUTOPILOT APP
AUTOPILOT MUST BE DISCONNECTED BEFORE 50 RA
F/D GA BELOW 2000 RA
COMMAND BARS AUTOMATICALLY POP UP IF F/D OFF
UNLESS FLARE IS ARMED ON A DUAL A/P APP
ALL AUTOPILOTS DISENGAGE WHEN PUSH TOGA
IF YOU ENGAGE A/P DURING A F/D GO AROUND
THE PITCH MODE ENGAGES IN LVL CHG AND ROLL MODE ENGAGES HDG SEL UNLESS A DIFFERENT ROLL MODE WAS ENGAGED FIRST
STAB OUT OF TRIM
STABILIZER HAS NOT BEEN TRIMMED CORRECTLY BY THE AUTOPILOT TRIM SYSTEM
IF THE STAB IS OUT OF TRIM BELOW 800 RA ON A DUAL A/P APP
A/P WARNING LIGHT ILLUMINATES STEADY RED
DUAL A/P GO AROUND; IF A/P CANNOT CHANGE TRIM SUFFICIENTLY
ALTITUDE ACQUIRE MODE INHIBITED
A/P WARNING LIGHT ILLUMINATES STEADY
ALTITUDE AQUIRE INHIBITS CAN OCCUR UNDER THESE CONDITIONS
LOW MISSED APP ALTITUDE
FULL GO AROUND THRUST
LIGHT WEIGHT
IF A RADIO ALTIMETER FAILS AFTER FLARE IS ARMED
THE A/Ps IGNORE THE FAILURE
UNDERSPEED LIMITING
FLASHING A
OVERSPEED LIMITING
FLASHING 8
IAS DISPLAYS ..... WHEN POWER FIRST APPLIED
100 KNOTS
IAS DISPLAY SETTING
100 KNOTS - VMO IN 1 KNOT
0,60 M - MMO IN 0,1 INCREMENT
N1 MODE LVL CHG CLIMB INHIBIT PERIOD
FOR 2 1/2 MINUTES AFTER LIFT OFF
VNAV TERMINATION
SELECTING ANOTHER PITCH MODE
GLIDE SLOPE CAPTURE
END OF LNAV ROUTE
INTERCEPT WAWPOINT TO G/S IF ARMED
LNAV ARMING CRITERIA ON THE GROUND
ORIGIN RUNWAY IN FLIGHT PLAN
ACTIVE ROUTE ENTERED IN FMC
TRACK OF FIRST LEG WITHIN 5 DEGREES OF RWY HDG
LNAV SELECTED PRIOR TO TO/GA
LNAV GUIDANCE BECOMES ACTIVE
AT 50 RA
LNAV TERMINATION CRITERIA
REACHING END OF ACTIVE ROUTE
REACHING A ROUTE DISCONTINUITY
INTERCEPTING A SELECTED APP COURSE
HDG SEL
LOSS OF CAPTURE CRITERIA
THE SELECTED COURSE CAN BE INTERCEPTED
LNAV
HDG SEL
CWSR IF AN AUTOPILOT ENGAGED IN CMD
LOCALIZER CAPTURE OCCURS
NOT LATER THAN 1/2 DOT DEVIATION
WHEN A LOC FREQUENCY SELECTED
VHF NAV RADIOS AUTOMATICALLY SWITCH FROM TAIL ANTENNA TO NOSE ANTENNA VORLOC IS ANNUNCIATED (ARMED OR ENGAGED) IF ANTENNA SWITCHING DOES NOT OCCUR LOC MODE IS INHIBITED
G/S CAPTURE OCCURS
2/5 DOT BELOW GLIDE SLOPE
APP SWITCH LIGHT EXTINGUISHES
AFTER LOC AND GLIDE SLOPE CAPTURE
AFTER LOC AND GLIDE SLOPE CAPTURE CWS..
CAN NOT BE ENGAGED BY MANUALLY OVERRIDING PITCH AND ROLL. MANUAL OVERRIDE OF AUTOPILOTS CAUSES AUTOPILOT DISENGAGEMENT
CMD ENGAGE SWITCH PUSH
CWS ENGAGES:
PITCH OR ROLL MODE NOT SELECTED
PITCH OR ROLL MODE DESELECTED
PITCH OR ROLL MODE MANUALLY OVERRIDEN WITH CONTROL COLUMN FORCE
WHEN APPROACHING A SELECTED ALTITUDE IN CWS PITCH
THE PITCH MODE ENGAGES IN ALT ACQ AND ALT HLD WHEN REACHING SELECTED ALTITUDE
IF PITCH IS MANUALLY OVERRIDEN WHILE IN ALT HOLD
AND CONTROL FORCE IS RELEASED WITHIN 250 FEET OF SELECTED ALTITTUDE, A/P PITCH MODE ENGAGES IN ALT ACQ AND RETURNS TO SELECTED ALTITUDE IN ALT HOLD MODE
DURING F/D ONLY OPERATION WHILE PITCH AND ROLL COMMANDS ARE MORE THAN 1/2 SCALE FROM CENTER PUSHING A CMD A OR B SWITCH
ENGAGES THE A/P IN CWS FOR PITC AND ROLL AND THE RELATED F/D BARS RETRACT
CWS HEADING HOLD FEATURE INHIBITED
BELOW 1500 RA WITH GEAR DOWN AFTER LOC CAPTURE IN APP MODE AFTER VOR CAPTURE WITH TAS 250 K OR LESS
A/P DISENGAGE LIGHT ILLUMINATED AMBER FLASHING
A/P AUTOMATICALLY REVERTS TO CWS PITCH OR ROLL MODE WHILE IN CMD
A/T DISENGAGE LIGHT ILLUMINATED AMBER FLASHING
IN FLIGHT
FLAPS NOT UP
AIRSPEED DIFFERS FROM COMMANDED VALUE BY + 10 OR -5 KNOTS AND IS NOT APPROACHING COMMANDED VALUE
STABILIZER OUT OF TRIM LIGHT OPERATES ONLY
WITH A/P ENGAGED. REMAIN EXTINGUISHED WITH A/P NOT ENGAGED
A/P ENGAGEMENT CRITERIA
NO FORCE IS BEING APPLIED TO THE CONTROL WHEEL
THE STAB TRIM AUTOPILOT CUT OUT SWITCH IS AT NORMAL
A/P DISENGAGEMENT
STAB TRIM A/P CUTOUT SWITCH TO CUTOUT
EITHER LEFT OR RIGHT IR SYSTEM FAILURE OR FAULT LIGHT ILLUMINATED
LOSS OF ELECTRICAL POWER
LOSS OF RESPECTIVE HYDRAULIC SYSTEM PRESSURE
DUAL CHANNEL A/P OPERATION IS POSSIBLE
ONLY WHEN TWO GENERATORS ARE POWERING THE BUSSES
WITH A RADIO ALT INOPERATIVE
THE A/P WILL DISCONNECT TWO SECONDS AFTER LOC AND G/S CAPTURE
1CH/SINGLE CH FOR SINGLE A/P ILS APP
ANNUNCIATES AFTER LOCALIZER CAPTURE AND REMAINS ON FOR ENTIRE APP
1CH/SINGLE CH FOR DUAL A/P ILS APP
ANNUNCIATES AFTER LOCALIZER CAPTURE AND EXTINGUSHES AFTER PITCH MONITOR CONFIDENCE TEST IS SUC. COMPLETE
VNAV ARMED IS DISPLAYED WHEN VNAV IS ARMED PRIOR TO TAKEOFF
AFTER TAKEOFF VNAV AUTOMATICALLY ENGAGES 400 RA
LNAV ARMED IS DISPLAYED PRIOR TO TAKEOFF
AFTER TAKEOFF ENGAGE AT 50 RA
IN NORMAL OPERATION FMC PROVIDES THE A/T SYSTEM
WITH FMC N1 LIMIT VALUES
DURING A/T OPEARTION IT IS RECOMMENDED THAT
BOTH EEC ON OR BOTH BE IN ALT AS THIS PROVIDES MINIMUM THRUST LEVER SEPERATION
MOVING THE A/T ARM SWICH TO ARM
ARMS THE A/T FOR ENGAGEMENT IN THE
N1
MCP SPD
FMC SPD

THE AUTOTHROTTLE DISENGAGES

THRUST LEVERS BECOME SEPERATED MORE THAN 10 DEGREES DURING A DUAL CHANNEL APPROACH AFTER FLARE ARMED IS ANNUNCIATED

THE A/T DISENGAGE LIGHTS DO NOT ILLUMINATE
WHEN THE A/T AUTOMATICALLY DISENGAGES AFTER TOUCHDOWN
THE F/D CAN ALSO BE ENGAGED IN THE TAKEOFF MODE WITH THE F/D SWITCHES OFF
IF A TO/GA SWITCH IS PUSHED AFTER 80 KNOTS
BELOW 2000 FEET AGL
PRIOR TO 150 SECONDS AFTER LIFTOFF
AUTOMATIC THRUST REDUCTION IS INHIBITED
WHEN ENGAGING LVL CHG OR V/S MODES UNTIL 2 1/2 MINUTES AFTER LIFT OFF
TO TERMINATE THE TAKEOFF MODE BELOW 400 RA
BOTH F/D SWITCHES MUST BE TURNED OFF
TO TERMINATE THE TAKEOFF MODE ABOVE 400 RA
SELECT ANOTHER PITCH MODE
BEFORE THE APP MODE CAN BE SELECTED
ONE VHF NAV RECIEVER MUST BE TUNED TO ILS FREQUENCY
G/S CAPTURE IS INHIBITED
PRIOR TO LCALIZER CAPTURE

THE A/P GA MODE REQUIRES DUAL A/P OPERATION AND IS AVAILABLE

AFTER FLARE ARMED ANF PRIOR TO THE A/P SENSING TOUCHDOWN

IF THE GO AROUND MODE IS SELECTED AFTER TOUCHDOWN AND PRIOR TO A/P DISENGAGEMENT
THE A/P DISENGAGE AND THE A/T MAY COMMAND GA THRUST (DUAL A/P)
DUAL A/P GO AROUND THE PITCH MODE CAN NOT BE CHANGED FROM TO/GA
UNTIL SUFFICIENT NOSE DOWN TRIM HAS BEEN INPUT TO ALLOW SINGLE CHANEL A/P OPERATION
GA MODE TERMINATED WHEN
ANOTHER PITCH MODE SELECTED
ALT ACQ ANNUNCIATES
SINGLE ENGINE F/D GO AROUND
F/D PITCH COMMANDS 13 DEGREES NOSE UP
AS CLIMB RATE INCREASES F/D PITCH COMMANDS MAINTAIN A TARGET SPEED
SPEEDS GREATER THAN VMO/MMO CANNOT BE SELECTED FROM MCP. SPEEDS CAN BE SELECTED WHICH
EXCEED FLAP AND GEAR PLACARDS
OR ARE LESS THAN MIN SPEED
MINIMUM SPEED
IS BASED ON ANGLE OF ATTACK AND IS APP 1.3 VS FOR THE CURRENT FLAP POSITION. IT IS SENSED BY THE ANGLE OF ATTACK VANES, ONE EITHER SIDE OF THE FORWARD FUSELAGE
TO REMOVE THE UNDERSPEED LIMITING SYMBOL
A SPEED OF 15 KNOTS GREATER THAN THE MIN SPEED MUST BE SELECTED
VMO/MMO ONLY, IF THE A/T ENGAGED IN A SPEED MODE AND THE THRUST LEVERS AT IDLE
THE AFDS, IF IN V/S MODE WILL AUTOMATICALLY ENGAGE TO LVL CHG MODE
MINIMUM SPEED REVERSION IS NOT AVAILABLE
WHEN A/T IS OFF