IPT LEARNINGS Flashcards
CONSIDERATIONS ARMING APP
CLEARED FOR APP
HEADING TO INT
ILS GLS TUNED AND IDENTIFIED
POINTERS
SPD WINDOWS OPEN
G/S and GP INHIBITED UNTIL LOC FAC CAPTURE
WHERE ARE PBN PROC LOCATED
QRH
FCOM SUPP PROC
WHAT PROC NEED TO BE COMPLETED PRIOR RNP AR APCH
IAN OR VNAV OR VS OR FPA
TALQS
TERRAIN VSD
ANP < RNP
LNAV VNAV PTH OR VNAV ALT
QNH + TEMP
SPD WINDOW OPEN
ALSO NEED COLD WX CORRECTIONS AND CHK WAYPT TRK/ DIST
WHAT ALERTS WILL FLT CREW RECEIVE IF ANP EXCEEDS RNP
IF ANP > RNP, ANP BARS TOUCH AT CENTER OF SCALE ANP BARS TURN AMBER, DEVIATION POINTERS FLASH FOR 10 SECS EICAS NAV UNABLE RNP
WHAT LATERAL AND VERTICAL MODES CAN BE USED TO FLY RNP APCH
LNAV
VNAV PTH IAN VS OR FPA
WHEN CAN WE USE DELAYED FLAP APP
VMC
OR GLS ILS OR CODED FMS APP
BASICALLY ALL APP EXCEPT 2D
MCP ALT SETTING PROC INSTRU APP USING IAN
APPROACHING GP 2NM TO DESCENT PT
MISSED APP ALT GP CAPTURE
MCP ALT SETTING INSTRU APP USING VNAV
SET MDA
300’ < MISSED APP ALT SET MISSED APP ALT
MCP ALT SETTING INSTRU APP USING VS OR FPA
SET ALT CONSTRAINTS TO MDA
SET 100’ BELOW CONSTRAINT IF NEEDED EXCEPT LOWER THAN MDA
300’ > MDA SET MISSED APP ALT
LOW VIS APP CALLS
SAME AS INSTRU PROC EXCEPT
CONFIGURED
LAND 3 AUTOLAND
APP MINIMUMS 80’ TO MINIMA
@100’ RA CONTINUE
STABLE APP POLICY
LDG CONFIG BY 1000’ RA
WITHIN TOLERANCES
NORMAL CHECKLISTS BY 500’ RA
NEW GA POLICY
IF ACFT TOUCHES DOWN NEED TO MANUALLY INCREASE THRUST
IF TOGA PRESSED AND NO THRUST INCREASE PF DOES MANUALLY
BRIEF ON DESCENT POSSIBLY MANUAL THR FOR GA
NEW CALL FOR PM
GO AROUND PROC
PUSH TOGA
VERIFY THR INCREASES
MAY NEED MANUAL THR IF TOUCHDOWN OCCURS
FLAPS 20
VERIFY ROTATION GA ALT
PM CALL THRUST SET
POSITIVE RATE GEAR UP
@400’ RA ROLL MODE
PM VERIFY MISSED APP ALT
VERIFY MISSED APP TRACKING
@ ACCEL HT SET FLAPS MAN SPEED
FLAP AS REQD
AT PLANNED FLAP MAN SPD
FLCH OR VNAV VERIFY CLB THR
MISSED APP ALT
AFTER TAKEOFF CHKLIST
GS FROM ABOVE PROC
SELECT APP MODE
VERIFY GS ARMED
FINAL LANDING CONFIG
SET MCP ALT 1000’ AFE
VS -1000 to -1500 FPM
USE VSD AND GREEN ARC TO ASSIST
WHEN IS MAX THR REQD
WHICH ABRK SETTING?
4 OR MORE
INSTRU APP USING IAN OR VNAV WHAT MUST BE CHECKED
PUBLISHED GP ANGLE LEGS PG
RWXX BEFORE END RWY
MISSED APP PT BEFORE APP END RWY
PRIOR 2 NM
TALQS CHECK
FIX PG PUT 2NM RING AROUND DESCENT PT
INSTRU APP USING IAN OR VNAV OR VS OR FPA
WHEN MUST AP BE DISC BY
135’ AGL
WHEN TO DO VREF CHECK ON DEP
AFTER LOADING PERF INIT PRIOR THRUST LIMS
DO OPT
CONFIRM WITH OTHER PILOT
F5 …
CHECK VREF LOAD THRUST LIMS ETC
FINISH PROC
AFTER SEATBELT SECURE
CHECK ROUTE
PDC READBACK
PDC READBACK
SID INCLUDING RWY AND TRANS
SQUAWK
ADDITIONAL REQ IN PDC
CURRENT POSN BAY
WHAT IS ANNUNCIATED CHKLIST
NON NORMAL FOR AN EICAS MSG
WHAT IS AN UNANNUNICATED CHKLIST
NON NORMAL FOR CONDITION WITHOUT EICAS MSG
LEVELS OF EICAS MSG
WARNING
CAUTION
ADVISORY
IN WHAT ORDER DO ALERTS APPEAR ON THE EICAS
ORDER OF PRIOIRITY
AND
ORDER OF OCCURRENCE
PRIORITY OF SEQUENCING NORMAL VS NNC
NNC THEN NORMAL CHKLIST
WHAT MUST BE READ ON NNC USING ECL
TITLE
OBJECTIVE STATEMENT IF NEEDED TO UNDERSTAND
WHAT IS DIFFERENCE IN AREA OF RESP WHEN STATIONARY ON GND PRIOR TO TAXIING UNDER POWER VERSUS AFTER COMMENCING TAXI UNDER OWN POWER OR INFLT
STATIONARY ON GND PRIOR TAXI
CAPT AND FO
ACFT IN FLT OR TAXIING
PF PM AREAS OF RESP
WHEN WOULD FLT CREW START CHECKLIST WITHOUT AN ICON
UNANNUNCIATED CHECKLIST
AS NEEDED MOST COVERED BY NNC
QRH PROC
MOST NNC
RAMATE
RECOGNISE and ANNOUNCE NON NORMAL SITUATION
ACKNOWLEDGE
MAINTAIN AIRPLANE CONTROL
ANALYSE THE SITUATION
TAKE PROPER ACTION
EVALUATE NEED TO LAND DIVERT OR CONTINUE
QRH PROC
ANALYSE THE SITUATION
EXPANDED
REVIEW ALL EICAS
PRIORITISE AND RECOMMEND COURSE OF ACTION
PF CONFIRMS
THEN TAKE THE PROPER ACTION
QRH PROC
TAKE THE PROPER ACTION
EXPANDED
DO NNC MEM ITEMS BASED ON AREAS OF RESP
PF CALL NNC
PM DO NNC
REVIEW ALL EICAS ALERT MSG AND DO OTHER NNC AS NEEDED
THEN EVALUATE
AIRSPEED UNRELIABLE
KABUKI PROC
PM
AIRSPEED UNRELIABLE
PF
AIRSPEED UNRELIABLE CONFIRMED
AIRSPEED UNRELIABLE MEMORY ITEMS
AP DISC SW PUSH
ATHR ARM SW BOTH OFF PM DOES
FD SW BOTH OFF PM DOES
SET PITCH ATTIT AND THR SETTING AS APPROP PM VERIFIES
MEMORY ITEMS COMPLETE
AT APPROP TIME
AIRSPEED UNRELIABLE NNC
ENG SEV DAMAGE SEP
KABUKI PROC
PM ABNORMAL ENG INDICATION OR ENGINE PROBLEM
ASSESS ENG PARAMETERS AND ANNOUNCE DIAGNOSIS STATES ENGINE SEVERE DAMAGE RIGHT
PF ENGINE SEV DAMAGE RIGHT CONFIRMED
ENGINE SEVERE DAMAGE RIGHT MEM ITEMS
ATHR ARM SW R (POINTS TO)
PM CONFIRM
PF TURNS SW OFF STATES OFF
THR LEVER RIGHT POINTS TO
PM CONFIRM
PF CLOSES THR LEVER STATES IDLE
PM FUEL CONTROL SW R POINTS TO
PF CONFIRM
PM FUEL CONTROL SW R CUTOFF STATES CUTOFF
PM ENGINE FIRE SW R POINTS TO
PF CONFIRM
PM PULLS ENG FIRE SW STATES PULL
PF MEMORY ITEMS COMPLETE
AT APPROP TIME ENGINE SEVERE DAMAGE SEP R NNC
CAPT LOADSHEET CHECK
NORMAL STUFF UP TOP
CHECK ZFW
CHECK CDU FUEL CALC AGREES EICAS
VERIFY FUEL SUFFICIENT FOR FLT
GR WT ON CDU AND FINAL AGREE
RWY VERIFICATION
ND
FMC RWY ON TAKEOFF REF PG
DO U NEED TO SLEW HDG BUG
YES MF
WHEN MUST PF GUARD FLT CONTROLS
FLAPS OUT OF UP
AND
ATHR WHEN MAKING LARGE CHANGES ON APP AND LDG
WHEN MUST PM GUARD FLT CONTROLS
GUARD RUDDER PEDALS DURING TAKEOFF
AND
LANDING
AND
PARKING
WHAT IS MINIMUM MANOEUVRE SPEED
TOP AMBER BAR
1.3 G MANOEUVERING TO STICK SHAKER < FL200.
1.3 G > FL200 TO LOW SPD BUFFET
1.3 G = 40 DEG AOB LVL TURN
REFERENCES AOA
EICAS
AIRSPEED LOW
BOX AROUND PFD AMBER WHEN IAS BELOW MIN MAN SPEED
WHAT IS FLAP MAN SPEED
1.3 G MANOEUVERING
ALLOWS 40 DEG AOB
FOR EXTENSION/ RETRACTION NOT SHOWN TO IF <\ 4 KTS VREF
REFERENCES WT
WHAT IS MINIMUM SPD
BOTTOM YELLOW
TOP ZIPPER
WHERE STICK SHAKER ACTIVATES
3 FLT CONTROL MODES
NORMAL
SECONDARY
DIRECT
WHAT IS FLT ENVELOPE PROTECTION
PREVENT STALL AND OVERSPEED
WHAT FLT ENVELOPE PROTECTIONS ARE AVAIL TO US IN THE NORMAL FLT CONTROL MODE
OVERSPEED
FLAPS UP OR ALL FLT MODES EXCEPT G/S
FLAP OUT OF UP ONLY FLCH OR TOGA
WHAT ARE INDICATIONS THAT FLT ENVELOPE PROTECTION IS ACTIVE
EICAS AUTOPILOT
AMBER LINE PITCH / ROLL MODE
WHAT PROTECTIONS IN NORMAL FLT MODE
BANK ANGLE PROTECTION - CAN OVERRIDE WITH AP DISENGAGE BAR
OVERSPEED PROTECTION
STALL PROTECTION
OVERSPEED PROTECTION
CANT TRIM NOSE DOWN
SMALL PITCH UP INDUCED
STALL PROTECTION
CAN APPLY NOSE UP TRIM
IF ATHR ARMED ATHR ACTIVATES TO MIN MAN SPEED OR SPD SET IN WINDOW
SECONDARY MODE
WHAT DO WE LOSE?
NO AP
AUTO SB
ENVELOPE PROTECTION
GUST SUPPRESSION
PITCH COMPENSATION
ROLL/ YAW ASSY COMPENSATION
TAIL STRIKE PROTECTION
APPROACH TO STALL
MEM ITEMS
RCB
NOSE DOWN PITCH CONTROL REDUCE AOA UNTIL BUFFET STICK SHAKER STOPS
ROLL SHORTEST DIRECTION WINGS LEVEL
ADV THR AS NEEDED
RETRACT SB
DO NOT CHANGE GEAR OR FLAP
DURING LIFTOFF IF FLAP UP FLAP 1
CHECK SPD AND THR
ESTABLISH PITCH ATTIT
RETURN DESIRED FLT PATH
REENGAGE AP AND ATHR
TCAS TA
MEM ITEMS
LOOK FOR TFC
CALLING OUT CONFLICTING TFC
IF TFC SIGHTED MAN AS REQD
TCAS RA
WHICH ONE DONT WE FOLLOW
DESCEND RA < 1000’ RA
TCAS RA
EXCEPT CLB LDG CONFIG
MEM ITEMS
IF MAN REQD DISENGAGE AP AND ATHR
SMOOTH ADJ PITCH FOR RA COMMAND
FOLLOW LATERAL TRACK
ATTEMPT VIS CONTACT
TCAS RA
CLB RA IN LDG CONFIG
DISENGAGE AP AND ATHR
ADV THR FWD MAX THR FLAP 20
SMOOTHLY ADJ PITCH FOR RA COMMAND
FOLLOW LATERAL PATH UNLESS VIS DIFFERS
POSITIVE RATE GEAR UP
ATTEMPT VIS CONTACT
WHICH CHECKLIST SHOUKDNT WE OVERRIDE
FUEL IMBALANCE
OPCS OEI GA
FUEL
POSSIBILITY OF OEI GA THEN ON SUBSEQUENT APP FUEL IMBALANCE SITUATION
IF NEAR RUNWAY CONSIDER LANDING AND MENTION IN EVENT OF GA WILL RUN FUEL IMBALANCE NNC
MAINTAIN AIRPLANE CONTROL
FMAs
CONSIDER HT FOR DRIFTDOWN
ENG FAIL > TAKEOFF
ONCE ALL EICAS MSG COVERED
PRESS CANCEL
OPEN LOOP
SENSED BY ACFT
CLOSED LOOP
CHOICE MADE BY PILOT
WHAT ACTIONS MUST BE CONFIRMED
AUTHTHROTTLE ARM SW
THRUST LEVEL
FUEL CONTROL SW
FIRE SW
GEN DRIVE DISCONNECT
CAN SB BE USED WITH FLAP
FCTM SAYS NOT WITH FLAP 5 OR MORE
DRIFTDOWN PROC
DUDU
DOWN
VNAV EO PG
UP
SET ENG OUT ALT
DOWN
EXECUTE
UP
PUSH ALT KNOB
HOW MANY UNANNUNCIATED CHECKLISTS?
30
LIST UNANNUNCIATED CHECKLISTS
ABORTED ENGINE START
ALTIMETER ERROR
BOMB ON BOARD
CABIN TEMP COLD
CABIN TEMP HOT
CHEMICAL BIO THREAT OR HAZMAT DG THREAT
DITCHING
DUAL ENG FAIL STALL
ENG INFLT START
ENG SEV DAMAGE SEP
EVACUATION
FIRE ENG ON GROUND
FIRE ENG TAILPIPE
FLAP LEVER INOPERATIVE
FLAPS AND SLATS FAIL
FUEL JETTISON
FUEL LEAK
GEAR LEVER LOCKED DOWN
ICE CRYSTAL ICIING
ISFD USE
JAMMED FLIGHT CONTROLS
LOSS OF ALL DISPLAYS
OVERWT LANDING
RADIO ALT UNRELIABLE
SMOKE OR FUMES REMOVAL
SMOKE FIRE OR FUMES
TAIL STRIKE
VOLCANIC ASH
WINDOW DAMAGE FWD L R
WINDOW DAMAGE SIDE L R
STANDARD LIST OF ITEMS FOR NON NORMAL PROCEDURE
MANOEUVRE
MEM ITEMS
ATC
NNC
DURING NON NORMAL SITUATION
VERBAL CONFIRMATION IS REQD BEFORE ACTIONING WHICH ITEMS
ATHROTTLE ARM SW
THRUST LEVER
FUEL CONTROL SW
ANY FIRE SW
GEN DRIVE DISC
WHO ACTIONS ITEMS ON MCP DURING AIRSPEED UNRELIABLE MEM ITEMS
PM AS PF MANUAL FLYING
WHO OWNS TRIM CUTOUT SW INFLT
PM
WHAT LGTS ARE REQD DURING EMERG DESCENT
ALL EXT LGTS
WHEN SHOULD CREW PERFORM A DRIFT DOWN
EF > EO MAX ALT
HOW CAN CREW PERFORM A DRIFTDOWN USING VNAV
DUDU
DOWN
VNAV EO PG SEL
UP
MCP ALT TO EO MAX
DOWN
PRESS EXEC
UP
MCP ALT KNOB PRESS TO MAKE VNAV CRZ ALT
CABIN ALT
PM > MEM ITEMS
TURN ON EXT LGTS
ATC
SQ 7700
CHK LSALT
PA ATTENTION CABIN CREW EMERGENCY DESCENT
CABIN ALT
MANOEUVRE
ANNOUNCE DESCENT
TURN HDG SEL
LOWER ALT MCP
FLCH
CLOSE THR LEVERS EXT SB
FINESSE MCP
ADJ ALT AND SPD DAMAGE?
ACCEL MMO VMO
ATC AND QNH
CALL-OUT 2000’ and 1000’ TO GO
2000’ TO GO SET 300 KTS
1000’ TO GO STOW SB
@14k CABIN CREW CARRY OUT FOLLOW UP DUTIES
LEVEL LSALT OR 10K
RNP APP
CAUTION RE IAN USE
MAY BE DIFFICULT TO CAPTURE FAC ON FINAL
IF SO GP INHIBITED UNTIL FAC CAPTURE MAY END UP HIGH
CAN USE LNAV VNAV INTIALLY WITH APP ARMED AND THEN IAN
DESCENT PROC
AFTER SETTING UP FMC
RECALL CHECK NOTES
4 CORNERS OF FMC
INIT REF CHECK WT
NAV RAD
PROG PG 4 CHECK RNP
VNAV FOR DES SPD
AIRSPEED UNRELIABLE
MEM ITEMS
DISENGAGE AP
DISCONNECT ATHR
FDS BOTH OFF
SET FOLLOWING PITCH AND THR
FLAPS EXT 10/85
FLAPS UP 4/70
STABILIZER
MEM ITEMS
STABILIZER SW BOTH CUTOUT
DO NOT EXCEED CURRENT AIRSPEED
CABIN ALTITUDE
MEM ITEMS
DON THE OXY MASKS
ESTABLISH CREW COMMS
CHECK CABIN ALT AND RATE
IF CABIN ALTITUDE UNCONTROLLABLE
PASS OXY SW PUSH TO ON AND HOLD FOR ONE SEC
WITHOUT DELAY DESCEND TO LSALT OR 10k WHICHEVER IS HIGHER
TO DESCENT
MOVE THR LEVERS TO IDLE
EXT SB
IF STRUCTUAL INTEG IS IN DOUBT AVOID HIGH MAN LOADS
DESCEND VMO MMO
HOW ARE SUPP PROC ACCOMPLISHED
AS NEEDED READ AND DO
COMMON SUPP PROCS CAN BE DONE FROM MEMORY
ACCORDING TO POLICY
WHEN SHOULD APU BE STARTED ON DEP
AS LATE AS POSSIBLE
KEEP 10-27 DEG IN CABIN
WITH PAX ONBOARD DONT EXCEED 20 MINS WITHOUT AIR COND
ALSO CHECK RMS FOR LOCAL REQMTS
WHEN WOULD GND AIR COND BE USED
APU INOP
OR STRICT LOCAL PROC
NO INDICATION THAT ITS ON
MAYBE PACKS OFF AND LOWER RECIRC OFF WHEN WE COME ONBOARD COULD SHOW ENG HAVE SET IT UP
WHAT SOURCES OF POWER CAN BE USED TO START ENGINES
EXT PWR NEED AT LEAST 2
APU
CONSIDERATIONS WHEN STARTING ON GND POWER
NEED 2 SOURCE EXT PWR
AFT EXT POWER ONLY REDUCES LOAD SHEDDING
FO SIDE LOTS LOAD SHEDDING
ADVISE CABIN THAT CABIN ITEMS WILL BE LOADSHED
START ONE ENG THEN DISC EXT PWR
USE CROSSTART PROC FOR OTHER ENGINE
NORMALLY START R ENG FIRST AS FWD EXT POWER L SIDE
WHAT ARE ICIING CONDS
TAT 10 DEG C OR LESS
AND
VISIBLE MOISTURE
OR
SLUSH STANDING WATER DURING TAXI
WHEN SHOULD TAKEOFF CHANGE CONSIDERATIONS CHECKLIST BE REFERENCED
ANY TIME RWY CHANGE OR POSSIBLY EVEN FOR CHANGE IN TEMP ETC AND NEEDING RECALC
IF FLAP CHANGES AND NOT CHANGED IN FMC WILL NOT BE DIFF SO MUST CHECK
CAPT ACTIONS FOR RTO
CALL STOP
SIMULT CLOSE THR LEVERS AND DISC ATHR
VERIFY RTO BRAKING OR MAX MANUAL BRAKING
MAX USE AVAIL REV THR
VERIFY SB
STOPPING ASSURED STOW REV
SET PB
FO ACTIONS FOR RTO
MONITOR ACTIONS CALL ANY OMISSIONS
CANCEL ALERT
CHECK THR LEVERS CLOSED
ATHR DISC
MAX BRAKING
CALL SB UP OR NOT UP
REV NORMAL
60 KTS
ADVISE TWR STOPPING AND ALERT PA
WHAT LEVEL IS ALERT IF ENG FAIL L OR R DURING TAKEOFF ROLL PRIOR TO V1
RED ENG FAIL PFD
ENG FAIL ON HUD
>65 KTS IF ENG NOT PRODUCING THR OR RATE OF THR INSUFF
HOW DOES ACFT MONITOR FOR POTENTIAL FUEL LEAK
FMC COMPARES ACTUAL FUEL FLOW FROM EECS WITH PREDICTED FUEL FLOW PERF TABLES EICAS FUEL FLOW DISAGREE
EICAS FUEL DISAGREE
FMC CALCULATES LARGE DIFF BETWEEN TOTALISER (FQIS) AND CALCULATED
FMC MSG
INSUFFICIENT FUEL
IF FUEL AT DEST < FUEL RES
CHANGES FOR TAKEOFF PERF
WHEN TO RECALC
USING ATM
CG FWD SELECTED RANGE
ANY INCREASE TWC
HWC REDUCE 5 KTS
OAT PLUS 2 DEG
QNH MINUS 2 QNH
FOR NON ATM
ANY DETERIORATION IN ENTERED ENVIRONMENTAL CONDS
SHUTDOWN CHECK FOR FO
TX
STANDBY
AND
CODE 3000 IN AUST 2000 OVERSEAS
EICAS QTY LOW
<1.6 T MAIN TANK
DESCENT PROC
FIRST STEP
RECALL CHECK NOTES
LIST FIRE DET SYS
APU
CARGO COMPT
ENGINES
LAVATORIES
MAIN GEAR WHEEL
OVERHEAD FLT CREW REST
OVERHEAD CABIN CREW REST
LIST FIRE EXTINGUISH SYS
APU
CARGO COMPT
ENGINES
LAVATORIES
WHERE IS OVERHEAT DET
ENGINES
INDICATIONS OF AN ANNUNCIATED ENGINE FIRE
FIRE BELL
MASTER WARN
EICAS FIRE ENG L/R
ENG FIRE LT
ENG FIRE SW UNLOCKS
FUEL CONTROL SW FIRE LT
WHICH CHKLIST SHOULD BE REFERENCED FOR AN OBSERVED ENG FIRE WITH NO ANNUNICATED INDICATIONS ON FLT DECK
ON GND
USE FIRE ON GND L/R QRH CHECKLIST
BACK QRH
CAN USE FOR ANNUNCIATED FIRE ENG EICAS ALSO ON GND
WHEN RUNNING UNANNUNCIATED FIRE ENG ON GND L/R and ANNUNCIATED EICAS ALERT FIRE ENG L/R SHOWS ARE CREW REQD TO STOP AND CHANGE CHECKLIST?
NO
AS BOTH SAME CHECKLIST AND REFER C AND FO
MAKE COMMENT THAT NO MEM ITEMS APPLICABLE AS ON GND
DIFF PRIORITIES ON GND VERSUS INFLT. INFLT EXT FIRE THE PRIORITY ON GND NEED COMMS TO PREVENT PAX/ CABIN CREW EVAC
ENG FIRES
WHICH ACTION HAS MOST EFFECT
FUEL CONTROL SW
CLOSES FUEL SPAR VALVE AND PREVENTS FUEL FLOWING TO FIRE
FIRST BOTTLE REMOVES OXY AND COOLS HOT SECTION WITHIN FIRE ZONE
IF FIRST BOTTLE HASNT WORKED SECOND ONE UNLIKELY TO
INDICATIONS OF CARGO FIRE
FIRE BELL
MASTER WARN
EICAS CARGO FIRE FWD/AFT
CARGO FIRE LT
CARGO FIRE SUPPRESSION FOR HOW MANY MINS
330 MINS
MOST LIMITING CARGO FIRE SUPPRESSION SYSTEM TIME
300 MINS
EDTO BASED ON OEI
ASSUMES AEO SO FASTER TIME AND NOT LIMITING EDTO
WHY DOES CARGO FIRE AFT OR FWD CHECKLIST CONTAIN THE LINE PLAN TO LAND AT NEAREST AVAIL APT
SUPPRESSION VERSUS EXTINGUISHING
FIRE MAY BE CONTAINED BUT STILL BURNING
WHICH SW REQUIRE VERBAL CONFIRMATION FROM CREW BEFORE ACTIONING
ATHROTTLE ARM SW
THRUST LEVEL
FUEL CONTROL SW
ANY FIRE SW
GEN DISC SW
R HYD SYS POWERS
FLT CONTROLS
R THR REVERSER
R AND L WING SPOILERS
L HYD SYS POWERS
IDENTICAL TO R
FLT CONTROL
L THR REVERSER
R AND L WING SPOILERS
C HYD SYS POWERS
FLT CONTROLS
LDG GEAR ACTUATION
LE SLATS
NOSE GEAR STEERING
R AND L WING SPOILERS
TE FLAPS
CONSIDERATIONS FOR APP AND LDG WITH INOP HYD SYS
FOR C HYD SYS SLOWER FLAP MOVEMENT
MORE TIME REQUIRED
GEAR REMAINS DOWN
SECONDARY FLAP MODE DONT REDUCE SPD UNTIL FLAP IN GIVEN POSN
CHECK LDR
OVERALL FOR L AND R HYD SYS MINIMAL DEGRADATION
C HYD SYS DEF NEEDS MGMT
CARGO COMPT
BOTTLE DISCHARGE
7 BOTTLES
2 BOTTLES IMMEDIATELY HDR
>15 MINS 5 BOTTLES AT REDUCED RATE
IF LDG WITHIN 15 MINS DELAY ONLY 1 BOTTLE AT REDUCED RATE ON TOUCHDOWN
ON GND 3 BOTTLES SIMULT INTO SELECTED COMPT THIRD BOTTLE AT REDUCED RATE
LAND AT NEAREST AVAIL APT
QRH
NNC PLAN TO LAND AT NEAREST AVAIL APT
FIRE OR SMOKE CONTINUES
ONLY 2 AC POWER SOURCES REMAIN (2 MAIN ENG GEN OR ONE MAIN GEN AND 2 APU GEN)
ANY OTHER SITUATION DETERMINED BY FLT CREW TO HAVE SIGNIFICANT ADVERSE EFFECT ON SAFETY IF FLT IS CONTINUED
RAT
5000 PSI SOME ELEC POWER
ONLY HYD POWER TO C HYD SYS PRIMARY FLT CONTROLS
AUTO DEPLOYS
BOTH ENG FAILED
ALL 3 HYD SYS PRESS LOW
LOSS ALL ELEC POWER TO CAPT AND FO FLT INSTRU
LOSS OF ALL 4 EMPS AND FAULTS IN FLT CONTROL SYS ON APP
LOSS OF ALL 4 EMPS AND ENG FAIL ON TAKEOFF OR LANDING
C HYD SYS ISOL VALVES
NOSE GEAR ISOL VALVE
RESERVE STEERING ISOL VALVE
ALTERNATE EXTEND ISOLATION VALVE AND A RESERVOIR STAND PIPE
ENSURES FLT CREW CAN LOWER LDG GEAR AND THAT NOSE WHEEL STEERING IS OPERATIONAL FOR LDG, ROLLOUT AND TAXI
ISOL VALVES OPERATE AUTOMATICALLY AND CANNOT BE CONTROLLED BY THE CREW
SMOKE FIRE OR FUMES
TIPS
USE REMOVAL CHECKLIST IF SITUATION DETERIORATES
CAN CHANGE ANSWER GO BACK AND CHANGE ON ECL, CHKLST RESET AND OPTION BUT RESETS ALL OPTIONS
USE OF THE TERM
IDENTIFY THE PROBLEM
NOT REQD FOR ONE EICAS MSG
WHAT PROCS MUST BE COMPLETED PRIOR TO DEP WHEN FLYING RNP AR DEP
TERRAIN VSD
VERIFY RNP
ANP < RNP
LNAV ARMED
REQD EQUIP SERVICEABLE
RWY FLAP MATCH OPT
BRANCH PT ON FIX PG
FMC EO SID DOESNT NEED TO BE CHECKED
WHERE CAN CREW CHECK CURRENT RNP VALUE
POS REF PG 2
Or
PROG PG 4
APP RNP BOTTOM PROG PG
ENSURE SMALL FONT SO ACFT CAN CHANGE AS REQD
WHAT ARE INDICATIONS WHEN ANP EXCEEDS RNP
EICAS UNABLE RNP
NPS NAVIGATION PERFORMANCE SCALES AMBER BARS FLASH
WHAT TRIGGERS EO SID
VALID N2 LESS THAN IDLE FOR 1 SEC
FLAPS OUT OF UP
OR THR LEVER AT IDLE
FLAPS OUT OF UP
WHAT IS BRANCH PT
HOW TO LOCATE ON CHART
PT WHERE DECISION OCCURS ON CDP
SHOWN UP TOP OF CDP
PLACE ON FIX PG 2 NM RING?
INDICATIONS OF ENG SEVERE DAMAGE
CONDITIONS STATEMENT IN QRH
AIRFRAME VIBRATION AND ABNORMAL ENG INDICATIONS
OR ENG SEPARATION
IE ONLY ENG VIBRATION MAYBE NOT ENOUGH FOR MEM ITEMS
ENG FIRE ON TAKEOFF
V1
ENGINE PROBLEM
@200’ AGL AP ON
@400’ IDENTIFY THE PROBLEM
FIRE ENG R
FIRE ENG R MEM ITEMS
FIRE ENG R MEM ITEMS COMPLETE
IF AT ACCEL ALT CLEANUP
DISCUSS FIRE ENG R REF ITEM FOR SECOND BOTTLE
THEN HOLD CHECKLIST UNTIL CESSNA PROC
INDICATIONS OF VOLCANIC ASH
ODOUR
ST ELMOS FIRE
UNREL AIRSPEED
ENG SURGE
VOLCANIC ASH
SYS EFFECTED
ENG POSS DUAL ENG FAIL
PITOT STATIC SYS
WINDSCREEN
PRESSURISATION
VOLCANIC ASH
PROC
180 DEG DESCENDING TURN
USE HDG SEL FLCH FOR IDLE THR
CREW MAY NEED OXY
ATHR OFF
REDUCE THR IF POSS
CONT IGNITION
FOR ENG FLAMEOUT/ STALL ATTEMPT RESTART
EAI ON WAI ON PACKS ON
START APU
MONITOR EGT
MONITOR SPD AND ALT MAY NEED UNREL AIRSPEED WITHOUT PITCH AND THR
DIVERT FOR AUTOLAND? FWD VIS MAY BE MINIMAL
ENG SEVERE DAMAGE
MEM ITEMS
ATHROTTLE ARM SW CONFIRM OFF
THR LEVER CONFIRM IDLE
FUEL CONTROL SW CONFIRM CUTOFF
ENG FIRE SW CONFIRM PULL
DUAL ENG FAIL/ STALL
MEM ITEMS
FUEL CONTROL SW BOTH CUTOFF THEN RUN
RAT SW PUSH AND HOLD FOR ONE SEC
> 270 KTS
HIGHER PROB OF START AFTER FAILURE AT HIGH RPM
ENG SURGE AND ENG LIMIT EXCEED
MEM ITEMS
ATHROTTLE ARM SW CONFIRM OFF
THRUST LEVER CONFIRM RETARD UNTIL MSG BLANKS OR THR LEVER AT IDLE
SENSED EF
<EO ACCEL ALT AND <THR RED ALT
VNAV REMAINS VNAV SPD V2 - V2 + 15. ATHR THR REF THRUST LIM TO
@ACCEL HT
VNAV ACCELS FLAPS UP MAN SPD FMC MSG ADVISING ENG FAIL. ACFT AT FLAPS UP MAN SPD THR LIM TO CON
SENSED EF
> EO ACCEL HT >THR RES
CURRENT CLIMB THR MAINTAINED
PRESS CON FOR EXTRA THR FOR ENG FAIL
EO SID
INFLT
EO SENSED AND FLAPS EXTENDED AND EO SID IN DATABASE CAN BE EXECUTED OR ERASED
FOR ENG FAIL AND FLAPS UP NEED TO GO TO DEP ARR PG AND LAST PG EOSID IF AVAIL FOR APT
EF IN CRZ
MAY NEED TO DESCEND IMMEDIATELY IF IN COFFIN CORNER
DUDU
VNAV EO PG
MCP SET ALT
VNAV EXEC
MCP PRESS ALT CHECK CRZ ALT
EO SPD IS SLOWER SPD IF TIME NEEDED AT ALT
V1 CUT
PROC
ON GND WHATEVER RUDDER NEEDED TO KEEP ACFT STRAIGHT
AIRBORNE WILL HEAR AUDIBLE CLOCK ABRK RELAX RUDDER INPUT
SLIGHTLY LOWER PITCH 10-11 DEG
@200’ AP ON DECLARE PAN
@400’ IDENTIFY THE PROBLEM
FOR ENG FAIL CONTINUE TO CLEANUP
MEM ITEMS IF REQD
CONSIDER KEEPING ACFT CLIMBING WHILST MEM ITEMS PERFORMED
@1000’ OR EO ACCEL HT CLEANUP
AT FLAPS UP CESSNA
CON
EO VNAV PG EXEC
SPD WINDOW
SA
NNC
AFTER TAKEOFF CHKLIST
SCEL WHY DIFF FLAPS SETTINGS OPT
FLAP SETTING BASED ON TURN DECREMENTS
MAY ALSO BE DIFF EO ACCEL HT
DONT USE OPTIMUM FLAP. HARD TUNE SO CAN DO OPTIMUM THEN HARD TUNE FLAP AND RWY SELECTION
THRUST ASSY PROTECTION
TRIGGERS <V2 ON TAKEOFF
AND
GA < VREF
REDUCES THR FOR CONTROLLABILITY
AUTORELIGHT
SHOWN IN WHITE ABOVE N2
SHOWS ENG FAIL AND EEC ATTEMPTING RELIGHT
TAKEOFF
PRACTICAL FLYING
WHEN STABILISING THRUST
PUSH FWD CONTROL COLUMN
LIGHT FWD PRESS INITIALLY
