FFS LEARNINGS Flashcards
1
Q
MTOW
A
254 692 KG
2
Q
MLW
A
192 776 KG
3
Q
PITCH TRIM SW
A
ON GND
MOVES STABILIZER
IN AIR
NORMAL MODE CHANGES TRIM REFERENCE SPD
IN SEC AND DIRECT MODES DIRECTLY MOVES STABILIZER
4
Q
TRIM REFERENCE SPEED
A
SPEED WHERE ACFT EVENTUALLY STABILISE IF NO CONTROL COLUMN INPUTS
5
Q
EFFECT PILOT TRIM INPUTS
A
PFC MOVES ELEV TO ACHIEVE TRIM CHANGE, THEN MOVES STABILIZER TO STREAMLINE THE ELEV
6
Q
NORMAL FLT CONTROL MODE VERSUS DIRECT MODE
A
DIRECT MODE
NO AUTO PITCH COMPENSATION FOR CHANGES
FLAP SPDBRK
GEAR
THR CHANGES
TURNS TO 30 DEG AOB
TURBULENCE
NO ROLL PROTECTION
NO LATERAL AND VERTICAL GUST SUPPRESSION
7
Q
OXY TEST
A
ADVISE GND OXY TEST
PRESS ENSURE HOURGLASS
PRESS EMERG FOR OXY FLOW INT TEST
RELEASE AND HOURGLASS REMOVED
100% SEL
CHECK OXY PRESS 1300/ 1600 EUR
8
Q
TAXI SPEED REQMTS
A
10 KTS FOR TURNS
BRAKING ONE LONG APPLICATION DO NOT RIDE BRAKES
30 KTS LONG STRAIGHT TAXIWAY CAUTION USING TILLER > 20 KTS
GS SHOWN ND AND HUD
NEED 38.6 M FOR 180 DEG TURN USING FULL TILLER 5-10 KTS FOR TURN
9
Q
PRESS TOGA ON GND
A
<50 KTS FLAPS EXT THR REF @ THR LIM PG
IF NOT PUSHED <50 KTS ATHR INHIBITED TO 400’
PUSHING >80 KTS DISARMS LNAV VNAV
10
Q
POSN OF NOSE WHEEL AND MAIN GEAR
A
NOSE WHEEL
2.7 M BEHIND
MAIN GEAR
28.6 M BEHIND
11
Q
ACFT WINGSPAN
A
60.1 M
12
Q
NWS AND VEERING
A
NWS ELECTRONIC SIGNALS
RELEASE TILLER RETURNS TO CENTER
CAUTION DONT RELEASE IN TURN
70 DEG/ 8 DEG RUDDER
TAKE NOTE OF ‘0’ POSN TILLER
VEERING REQ >1.5 UNITS RUDDER TRIM REPORT TO MAINT
HANDOVER TO OTHER PILOT WITH ACFT STRAIGHT NOT IN TURN
13
Q
ENTERING HUD TAKEOFF
WHAT PROC IF RWY CHANGE
A
ENSURE IRS ALIGNED
ON DEP ARR PG
FOR RWY CHANGE FD OFF SEL HUD TAKEOFF AND EXEC FD ON
14
Q
DEFINE STABILISED THRUST
A
MAIN THING IS SYMMETRICAL
<2 SECS OTHERWISE MAY REDUCE TAKEOFF DIST AVAIL
15
Q
WHEN DOES RUDDER BECOME EFFECTIVE
A
40-60 KTS
16
Q
CONSIDERATIONS FOR LIGHT TOW WITH AFT CG
A
LIGHT FWD PRESS TO 80 KTS
INCREASES NWS EFFECTIVENESS
17
Q
IF LNAV VNAV NOT USED FOR DEP WHAT ROLL PITCH MODE WOULD U USE
A
TOGA TOGA
@400’ HDG SEL
@1000’ FLCH
18
Q
ROTATION TECH
PITCH RATE
TARGET PITCH ATTIT
A
2-2.5 DEG SEC
TO AETA
1-2 DEG LOWER UNTIL GEAR UP
THEN TOGA REF LINE
19
Q
ON TAKEOFF
SECOND PUSH TOGA AIRBORNE
A
REMOVES TO AND CLB DERATES
50-400’ TOGA ROLL MODE
>400’ TOGA ROLL AND PITCH
20
Q
HOW DOES ROTATION TECH VARY WITH DIFF FLAP SETTINGS
A
NO CHANGE
21
Q
EFFECT ON TAKEOFF PERF OF SLOW LATE ROTATION
A
REDUCES PERF
INCREASED TIRE SPEED
22
Q
BENCH SYMBOL ON HUD
SQUARE—————SQUARE
A
AOA LIMIT SYMBOL
AOA FOR STICK SHAKER
23
Q
TAILSTRIKE PROTECTION
NORMAL MODE
A
DECREASES ELEV DEFLECTION
NO FEEDBACK TO CONTROL COLUMN
PILOT CAN OVERRIDE
24
Q
XWIND TAKEOFF PROC
A
ROLLING TAKEOFF XWC >20 TWC >5
RUDDER FOR CENTRELINE
START CONTROL COLUMN NEUTRAL AS ACFT ACCEL INTO WIND AILERON KEEP WINGS LEVEL
NEUTRALISE RUDDER AILERON AIRBORNE
25
HUD FAILURE DURING TAKEOFF
COMMUNICATE TO OTHER CREW
SWITCH TO PFD
REMEMBER SMALL MOVEMENTS ON PFD
TRANSITION FROM OUTSIDE TO PFD
26
CONSIDER THREATS OF MULTIPLE FLAP SETTINGS
THOROUGH BRIEFING
PIECE OF PAPER ON FLAP LEVER
MITIGATE VERIFYING OPT VERSUS FMC VERSUS ACTUAL FLAP SETTING
27
AFTER TAKEOFF
LEAVING GND EFFECT
EFFECT ON PERF
NOSE DOWN PITCH
REDUCES ROC
28
LIST FLAP LIMIT SPEEDS
1 260
5 240
10 230
15 220
17 215
18 215
20 210
25 190
30 180
29
QRH
PERF INFLT
CLB
FLAPS UP CLB THR
> TAKEOFF 11 DEG 3500 FPM
> 10K 9 DEG 3000 FPM
30
BEST ROC
VREF 30 PLUS 140
OR
UP PLUS 60
31
WHAT ATHR FMA MODE FOR FLCH CLIMB
THR FLCH SPD
@ LEVEL OFF
SPD ALT
32
WHAT WILL HAPPEN TO ATHR MODE IN FLCH CLIMB OR DESCENT IF THR LEVERS ARE MANUALLY OVERRIDDEN
CHANGE TO HOLD
33
WHAT SPEED PROTECTION IS AVAIL FOR VARIOUS AUTOFLT MODES
OVERSPEED AND LOW SPEED
ATHR ARM SW MUST BE ON
ATHR WAKE UP FOR LOW SPEED WILL KEEP SPD ABOVE MIN MAN SPD
NOSE UP TRIM INHIBIT
34
HOW WILL FLAP RETRACTION VARY WITH DIFFERENT TAKEOFF FLAP SETTINGS
@ 10, 15 17 18 20
FLAPS 5
35
ANY EFFECT ON TAIL CLEARANCE MARGINS WITH DIFFERENT FLAP SETTINGS
NO
36
DURING LEVEL FLT DOES A THR CHANGE NEED TO BE COUNTERED BY A CONTROL INPUT? WHAT ABOUT SPDBRK AND FLAP CHANGES
AUTO STABILISATION FOR STAB AND ELEV FOR THR AND CONFIG CHANGES
NO NEED TO TRIM ONLY FOR AIRSPEED CHANGE
37
HOW DO U EXPECT THE FBW ENVELOPE AND AFDS PROTECTIONS TO RESPOND APPROACHING VMO/ MMO
NOSE DOWN TRIM INHIBITED
CONTROL COLUMN FORCE DOUBLES TO LOWER THE NOSE
38
REVIEW AP OVERRIDE PARAMETERS
IF PILOT OVERRIDE AP DISCONNECTS
39
WILL FLAPS EXT >260 KTS? OR ABOVE 20k?
NO
INHIBITED IN PRI AND SEC MODES
LOAD RELIEF SHOWN WHERE FLAP POSN WOULD BE
40
REVIEW
NNC PRI FLIGHT COMPUTERS
FLT CONTROLS DIRECT MODE (ATTEMPTS RESET)
41
HOW CAN U MAINTAIN YOUR SCAN DISCIPLINE AND ESTABLISH RELIABLE MONITORING BEHAVIOURS
PRACTICE
ARMCHAIR FLYING
42
BANK ANGLE PROTECTIONS
WHEN DO THEY BECOME ACTIVE
APPROX 35 DEG
CAN BE OVERRIDDEN
AP DISENGAGE BAR INHIBITS
PFD AMBER BANK ANGLE INDICATOR >35 DEG
GPWS ‘BANK ANGLE’ 35 40 45
43
NEED BACK PRESS FOR STEEP TURNS?
NEED BP > 30 DEG AOB
44
HOW TO USE HUD FPV AND FLT PATH ACCEL SYMBOL FOR STEEP TURN
KEEP LEVEL
AND
CONSTANT SPEED
45
HOW DO U EXPECT THE STALL SPD TO DO WITH INCREASING AOB? HOW WOULD THIS BE DISPLAYED ON SPEED TAPE
STALL SPEED INCREASE
ZIPPER MOVES HIGHER CLOSE TO MIN MAN SPD
46
INPUT SOURCES FOR THE STBY INSTRU
INDEPENDENT SOURCE OF ATTITUDE AIRSPEED ALTITUDE
CENTER PITOT AND STATIC
ATTIT FROM INTERNAL INERTIAL SENSORS
47
HOW LONG WILL STBY INSTRU REMAIN POWERED AFTER LOSS OF ALL MAIN AC BUSSES. DO U EXPECT RAT TO DEPLOY
10 MIN ON MAIN BATT
THEN RAT WILL DEPLOY TO POWER STBY SYS
48
WHAT AUTO MANUAL DISPLAY SWITCHING IS AVAILABLE IN THE EVENT OF A DISPLAY FAILURE
PFD MFD SELECTOR
49
LIST TOLERANCES DURING APPROACH
<1000 FPM BELOW 1000’ AGL
ANY SIGN DEVIATION PAPI
ON CENTRELINE
TARGET SPD -5 to +10 <500’ RA
THRUST FOR CONDS
LLZ >300’ RA 1 DOT LLZ OR WITHIN EXPANDED SCALE
LLZ <300’ RA 1/2 DOT LLZ OR WITHIN EXPANDED SCALE
LLZ APP MINIMUMS 1/2 EXPANDED SCALE
GLIDESLOPE 1 DOT
50
IN APP MODE
CAN U CAPTURE GS BEFORE LLZ
NO SYS LOGIC
GS CAPT INHIBITED UNTIL LLZ CAPT
51
HOW CAN APP MODE BE DESELECTED
WHAT ABOUT ABOVE 1500’
>1500’ PRESS APP
<1500 IF LOC ONLY USE HDG/TRK SEL OR HDG/TRK HOLD
IF LOC AND GS PRESS TOGA
52
APPROACHING MINIMUMS
CALLOUT
80’ ABOVE MINIMA
53
WHAT IS MAX DIST FROM APT A GLS CAN BE USED
RANGE LISTED IN ERSA
YSSY 23 NM
54
DURING AN APPROACH USING INSTRU PROC IF PM CALLS VISUAL PRIOR TO MINIMA WHAT IS THE CORRECT RESPONSE FROM PF
LOOK UP ASSESS
CONTINUE
OR
STANDARD PROCS
55
PM RESPONSIBILITIES REGARDING DEVELOPMENT VISUAL SEGMENT
ENSURE REQD VIS MET
AERODROME FEATURES CAN BE SEEN
ENSURE CAN REMAIN VISUAL
56
STATE CONDS FOR CREW TO CONDUCT MANDATORY GA OR MISSED APP
OUTSIDE TOLERANCE
NOT STABLE
NOT VISUAL
ATC INSTRUCTION
NOT CONFIGURED
57
DURING ILS GLS TO NON AUTOLAND RWY WHAT IS LOWEST ALT BY WHICH AFDS MUST BE DISENGAGED
135’ RA
58
REQMTS FOR STABLE APP
CONFIGURED BY 1000’
NORMAO CHKLISTS BY 500’
WITHIN TOLERANCES
59
USING HUD FOR AIM PT DURING LANDING
GS REF LINE ON AIM PT MARKINGS ON RWY
60
QRH
PERF INFLT
FOR APP
FLAP 20 MLW
0.5 DEG 49% N1 166 KTS
61
WHERE IS VISUAL AIM PT 787
1000’-2000’
62
RMS TDZ AIM PT MARKINGS
AUST AIM PT 1312’
FAA 1000’
ICAO VARIES 1200-1400’
MEL RWY16 1837’
63
SCAN FOR STABLE APP
HUD
FPV ON GS REF LINE
SPD ATTIT ROD CENTRELINE
KEEP AIM PT SAME POSN WINDSCREEN
64
PF USING IDLE REV FOR LDG
PF CALL
IDLE REVERSE
65
WHAT IS THE RELATIONSHIP BETWEEN HUD FPV AND GLIDESLOPE REF LINE? HIW CAN THESE BE USED TO CORRECT VERTICAL PROFILE
HIGH OR LOW
ADJ FPV ABOVE OR BELOW GS REF LINE
THEN FPV ON GS REF LINE WHEN BACK ON PROFILE
66
PAPI
ALIGNED FOR TOUCHDOWN WHERE
NORMALLY 1000’-1500’
67
JEPP TCH
787 TCH?
CROSS THRESHOLD AT 50’
68
HOW DO U CALC ROD FOR APP
5 TIMES GROUNDSPD
69
WHERE DO U COMMENCE FLARE
ENSURE ACFT SPD CORRECT
FLARE APPROX 30’
FOCUS END RWY HOLD NOSE CONSTANT POSN
THEN LOWER NOSE TO RWY
70
WHAT COMMAND SPEED DO U SET?
WOULD THIS CHANGE IN WINDY OR GUSTY CONDITIONS OR IF ATHR NOT USED?
VREF + 5 NORMAL ATHR ON
GUSTY VREF + 10 ATHR ON
ATHR OFF
ADD 1/2 HWC AND FULL GUST UP TO MAX VREF + 15
TWC NO ADDITIVE JUST VREF + 5
71
IF ATHR ENGAGED WHEN WILL IT REDUCE THR FOR LANDING? NO ATHR WHEN WILL U REDUCE THR
25’ RA
MANUALLY AS PART OF FLARE
72
WHAT EFFECT WILL THR REDUCTION HAVE ON THE PITCHING MOMENT OF THE ACFT? HOW WILL U FLY THE NOSEWHEEL ONTO THE RWY?
NOSE DROP
HOLD BACK PRESS
MAIN WHEELS ON SLOWLY LOWER THE NOSE
73
WHERE SHOULD U PLACE YOURSELF IN RELATION TO CENTRELINE
CENTRELINE INSIDE LEFT LEG?
SIT ON R SIDE SO SLIGHTLY R OF CENTRELINE
74
HOW TO DESELECT REV THR
IF USING IDLE REV PF CALLS IDLE REVERSE
FOR FULL REV REDUCE TO IDLE BY 60 KTS TAKES SIGN TIME TO IDLE (LOW 20%) BEFORE STOWING
75
PM CALLS FOR THR REV DEPLOYMENT
REVERSERS NORMAL
NO REV L/R
NO REVERSERS
76
HOW TO DISCONNECT ABRK
STOW SPDBRK
BRAKE PEDAL TO DISARM BRAKES
PF ORDER PM ABRK TO OFF
77
POTENTIAL CONSEQUENCES OF SHORT AND LONG LANDINGS
SHORT OBSTACLE ISSUES AND LANDING SHORT OF RWY
LONG POTENTIAL OVERRUN
78
CUES THAT INDICATE CORRECT VERSUS INCORRECT FLARE TECHNIQUE
EASY IF ACFT STARTS IN CORRECT SPOT
AIM PT RETENTION
MISJUDGED COMMENCEMENT HT
79
CROSSWIND TAKEOFF LIMIT
40 KTS DEPENDS ON VARIETY OF FACTORS
80
WHY IS ROLLING TAKEOFF ADVISED FOR SETTING TAKEOFF THR IN STRONG CROSSWINDS
>20 KTS
REDUCES RISK FOD DAMAGE
AND ENG SURGE/ STALL
81
CONSIDERATIONS FOR TAKEOFF IN GUSTY WIND IR STRONG CROSSWIND CONDS
HIGHER THRUST SETTING TO MINIMISE GND ROLL
INCREASE VR TO MAX VR + 20 USE V SPEEDS FOR ACTUAL WT
FWD PRESS TO 80 KTS INCREASE NWS EFFEFTIVENESS
82
XWIND TAKEOFF
HOW TO MAINTAIN CENTRELINE
RUDDER FOR CENTRELINE
CONTROL COLUMN INTO WIND TO KEEP WINGS LEVEL
SKY POINTER
83
HOW TO MAINTAIN WINGS LEVEL FOR TAKEOFF
WHAT HUD INDICATIONS COULD HELP?
KEEP RWY HEADING
PITCH BAR LEVEL?
TRK ON ND
SKY POINTER
KEEP FPV UNDER HDG BUG
DIFFICULT IN STRONG XWC AS ITS GHOSTED
84
LARGE CONTROL WHEEL INPUTS WILL CAUSE SPOILER RISE. WHAT EFFECT WILL THIS HAVE
INCREASED DRAG AND REDUCED TAKEOFF PERF
85
AT ROTATION NOSE WHEEL LIFTS OFF NOSE WHEEL STEERING LOST.
HOW WILL THIS AFFECT ACFT AND HOW CAN U COMPENSATE?
ACFT SHOULD NATURALLY TURN INTO WIND
NEUTRALISE CONTROLS
86
WHAT WOULD YOUR ACTIONS BE IF U THINK TAIL STRIKE ON TAKEOFF OR LANDING
WHAT WILL AID U IN THIS ASSESSMENT
IS THERE ANY PROTECTIONS
STOP PULLING BACK
NOT SURE?
TAILSTRIKE PROTECTION REDUCES ELEV DEFLECTION BUT PILOT CAN OVERRIDE
87
HUD FPV MAY BE GHOSTED WITH HIGHER CROSSWINDS FROM WHERE CAN U DETERMINE YOUR TRACKING INFO AND HOW WILL THIS AFFECT YOUR SCAN AND WORKLOAD
HIGHER WORKLOAD AS DIFF SCAN REQD
USE ND FOR TRK
88
CROSSWIND LIMITS FOR LANDING
RCAM 5/6 40 KTS
89
SOME NNC WILL REDUCE CROSSWIND LIMIT WHAT ARE THEY
ASSY THR
RUDDER RATIO
FLT CONTROLS NOT NORMAL MODE?
90
DESCRIBE EFFECT XWC ON RWY PERSPECTIVE
FLT DECK UPWIND SIDE
91
DOES 787 HAVE RUNWAY ALIGN MODE
IF 5-10 DEG CRAB ALIGNS 500’ AND 200’
>10 DEG CRAB ALIGN 500’ 5 DEG CRAB ON TOUCHDOWN
<5 DEG CRAB JUST 200’
92
CONSIDERING RWY ALIGN MODE WHEN SHOULD AP BE DISC FOR MANUAL LANDING
PRIOR TO 500’ AGL
93
ON INSTRU APP WHEN TRANSITIONING FROM INSTRU TO VISUAL TENDENCY TO TURN ACFT
HOW CAN THIS BE AVOIDED
KEEP SCAN GOING
USE INSTRU MORE THAN VISUAL PICTURE
94
SPECIFIC CROSSWIND LANDING TECH
DECRAB DURING FLARE
RUDDER TO STRAIGHTEN IN FLARE AILERON FOR WINGS LEVEL
FLARE NORMALLY
RUDDER STRAIGHTEN ACFT
AILERON WINGS LEVEL
95
HOW DO U MAINTAIN CENTRELINE TRACKING AND WINGS LEVEL DURING LANDING ROLL
RUDDER FOR CENTRELINE
AILERON TO KEEP WINGS LEVEL SHOUKD REDUCE AS ACFT SLOWS
96
SLIPPERY RUNWAY
POSS LOSS DIRECTIONAL CONTROL
COULD TOUCHDOWN IN CRAB
PERMITS RAPID OPERATION OF SPOILERS AND AUTOBRK
USE DIFFERENTIAL BRAKING/ REV THR FOR DIRECTIONAL CONTROL
97
PILOT SEAT
98
FUEL TANKS TOTAL
101.4 T
COULD BE 98-102 DEPENDING ON SG
99
L AND R MAIN TANK
EACH
16 776 KG
100
CENTER TANK
FUEL
67 889 KG
101
FUEL IMBALANCE
NOT AN ISSUE
EXCEPT FOR LONG TERM STRUCTURAL IMBALANCE
ACFT CONTROLLABLE WITH ALL FUEL ON ONE SIDE
102
PROV LOADSHEET
PANTRY
NO NEED CHECK NUMBERS
EXCEPT
CHECK CITY PAIRING
103
FINAL LOADSHEET
SHOULD BE RECEIVED WITHIN 3 MINS DOOR CLOSED
104
TAKEOFF PERF
WINDSHEAR
FULL THRUST AND FLAP 20
V1 VR FOR WINDSHEAR
ROTATE AT FASTER VR
105
FWD CG MOVEMENT
IF ON BORDERLINE CHOOSE MORE FWD POSN REDUCES NEED FOR RECALC
106
DEST APT RWY CONTAMINATED
NEED CHECK LDR PREFLT
107
AFTER LDG DIST CALC
BTV?
SEND OUTPUT
TO FD PRO CHANGE TO UNFACTORED LDG DIST ASSESS ABRK AND TAXIWAY TO USE
108
CRS
YES
NO
R
YES 330 MINS
NO 60 MINS
R RESTRICTED
109
HOLDING IN ICIING
FLAP 1 ONLY NO FLAP JUST SLATS
110
UPRT
RCB
AS L AND R PFD IDENTICAL MAY NEED TO INCLUDE ISFD
HAPPY PLACE
FD OFF
FD ON
PRESS ALT
AP ON
MCP SPEED
ATHR ARM ON
ATHR SPD
FMA FMA
111
PF
THRUST SETTING REQD
ALT + 50
IE FL330 = 83% N1
112
RANGE FOR DISPLAYING APT MAP
0.5, 1, 2 or 5 NM
113
EICAS
HUD TAKEOFF
FOR TAKEOFF GUIDANCE FAILURE NOT COMPLETE HUD FAILURE
114
DERATES CLB 1 CLB 2
TO1 TO2
CLB 1 5%
CLB 2 15%
>25000’ DERATE REDUCES TO CLB BY 33k
TO1 5%
TO2 15%
115
CLB/ CON MCP SW
ON GND AND <400’ SW INOP
AEO CHANGES FMC SEL CLB THR
OEI CON
116
MAX ROC
VREF 30 + 140
OR
UP + 60 TO M0.82
117
IF SPD REDUCES TO STICK SHAKER
ATHR ACTIVATES IN SPD TO MIN MAN SPD OR MCP SPD WHICHEVER IS HIGHER
118
DESCENT IN VNAV SPD
STALL PROTECTION
IN HOLD
ATHR WILL ACTIVATE FOR STALL PROTECTION
THR LEVERS WILL NOT MOVE
119
ATHR WILL NOT ACTIVATE
ATHR NOT ARMED
IF PITCH MODE TOGA OR FLCH SPD
IN HOLD WONT SUPPORT STALL PROTECTION EXCEPT VNAV SPD
120
EICAS
FLIGHT CONTROL MODE
FLT CONTROLS
SECONDARY MODE
121
EICAS
PRI FLIGHT COMPUTERS
FLT CONTROLS
DIRECT MODE
122
MISSED APP PROC
PF CALL GO AROUND PUSH TOGA
CONSIDER FLAPS FLAP 20/ FLAP 5 OEI/ FLAP MAINTAIN CLOSE TO GND
ROTATE GA ATTITUDE
VERIFY OR ADJ THR
PM THRUST SET
POSITIVE RATE GEAR UP
FMA FMA
@400’ ROLL MODE
PM VERIFY MISSED APP ALT
@1000’ MCP SET FLAP SPD
RETRACT FLAP
AT FINAL FLAP SPD
VNAV FLCH
VERIFY CLB CON
AFTER TAKEOFF CHECKLIST
123
GA
FMA
THR TOGA TOGA
FOR 2000 FPM
THR REF TOGA TOGA
FULL CHARGE
LNAV @ 50’ MANUAL FLYING
LNAV @ 200’ AP ON
124
TRACKING AND HT REQMTS FOR GA INSTRU APP VERSUS VISUAL APP
INSTRU APP FOLLOW CHARTED GA
VISUAL APP TURN TOWARDS RWY CENTRELINE
125
MISSED APP FROM 2000’
WILL FD ALWAYS PROVIDE GUIDANCE?
FIRSTLY NO RUSH
BOTH PILOTS READY
CALL GO AROUND THEN QUICKLY FLCH OR VNAV
THEN GA PROC
126
FMA CALLOUT REQMT
FOR GA
FMA REQD TO BE CALLED
MANUAL AND AP ON
127
DESCENDING MISSED APP USING AFDS
>1500’ PRESS APP DISARMS APP OR USE LOC VS
<1500’ LOC ONLY PRESS VS
<1500’ LOC GS NEED PRESS TOGA
128
BALKED LANDING
DISENGAGE AP
DISC ATHR
MAINTAIN LDG CONFIG
MAN ADVANCE THR
ROTATE AT VREF
15 DEG PITCH AIRBORNE
THEN GA PROC AWAY FROM GND
129
IF GA INITIATED AFTER TOUCHDOWN AND TOGA SEL WHAT HAPPENS TO SPDBRK AND ABRK
AUTO STOWS
130
ROLE OF PM IN APPROACH MONITORING
CALL DEVIATIONS
GUIDANCE ON TRENDS
131
CONSIDER MCP ALTITUDE SETTING WITH CONDITIONAL CLIMB DO U SET LOWER ALT
SET HIGHER ALT WILL BE IN VNAV BY THEN
132
2 WAYS CLB CAN BE SEL ON MCP
FLCH
CLB BUTTON
VNAV?
133
WHAT IS A BALKED LDG
TOUCHDOWN OCCURS WITHOUT REV THR SEL
134
KEY TO EARLY RECOGNITION PILOT INCAPACITATION
SOPS
80 KT CALL
TELL OTHER PILOT IF FEELING UNWELL
CROSSCHECKING
CHECKLIST RESPONSES
135
INCAPACITATION
WHEN MUST PAN BE DECLARED
CAPT OR FO INCAPACITATED
136
WOULD U TAXI TO GATE
CAPT INCAPACITATED
YES ID TAXI TO GATE
CAPT REQMT A QF THING
137
WHAT FEATURES DO PILOT SEATS HAVE TO ASSIST WITH INCAPACITATION
LOCK SEATBELT
REMOVE PILOT FROM CONTROL ELECTRONICALLY OR MANUALLY
138
CONSIDERATIONS
ATC KEEPS ACFT HIGH ON APP
CONFIGURE EARLY
SLOWER SPD AND HIGHER DRAG
CONSIDER WHERE FAF IS
USE VSD OR ALT ARC TO DETERMINE WHETHER STABLE APP CAN BE MET
139
GS FROM ABOVE
PROC
PRESS APP
ON LOC CHECK GS ARMED
SET 1000’ ALT WINDOW
FULLY CONFIGURED
VS -1500 FPM
VISUAL BY 1000’
IMC BY FAF
140
WHY IS FLCH NOT PREFERRED PITCH MODE WHEN INT GS FROM ABOVE
WILL PITCH FOR SPD
120 SECS FOR ALT COULD BE HIGH ROD
COMPANY ROD LIMIT MAY BE REACHED
141
FLCH
ANY RESTRICTIONS?
NOT BELOW 1000’ AFE
142
FAM
APPROACH SLOPE GUIDANCE
NEEDS TO BE SERVICEABLE WITHIN 7 DAYS
NOT FOR 787 WITH HUD
CAPT CAN MAKE APP USING HUD WITH NO SLOPE GUIDANCE
MUST HAVE DONE ONE WITHIN 12 MTHS
143
TOOLS TO ASSIST WITH CCTS
FIX PG RWY END AND ABEAM
XTK ERROR UNDER ACFT TRIANGLE ON ND
144
CCT
BANK ANGLE FOR UPWIND TURN
20 DEG AOB
+/- 5 DEG PER 15KTS
145
CCT
DWIND SPACING
2-2.5 NM
146
CCT
PITCH CHANGES WITH CONFIG CHANGES?
YES
WILL NEED TO TRIM FOR SPD CHANGES
147
CCT
WHEN DO U TURN BASE
40 SECS FROM ABEAM
25 DEG AOB LEVEL TURN
FPV JUST UNDER HZN 200-300 FPM DESCENT UNTIL INT 3 DEG PATH
148
CCT
HOW DO U ANTICIPATE TURNING FINAL
USE ND EXT CENTRELINE
TREND VECTOR ACCOUNTS FOR WIND
149
CCT
TRAINEES ROLE DURING TOUCH AND GO
KEEP ACFT STRAIGHT
SET GA THR
INSTRUCTOR SETS FLAP AND STAB TRIM
MAYBE ABRK?
150
CCT
AFTER TAKEOFF CHECKLIST
FLAPS REMAINING AT 5
WILL NEED TO OVERRIDE FLAPS ITEM OVERRIDE
151
LAHSO
CONDITIONS
UP TO CAT C
BRAKING ACTION GOOD
PILOTS PLAN GA
FOLLOW ANY TCAS RA
WX
20 KTS XWC
5 KTS TWC DRY NIL WET
8K vis
787 HAS EXEMPTION FOR LAHSO OPS IN AUST
152
ACTIVE AND PASSIVE
LAHSO
ACTIVE
ARRIVAL RWY WITH HOLD SHORT INSTRUCTION
PASSIVE
FULL LENGTH AVAIL GIVEN INFO ABOUT CROSSING ACFT
153
ACFT UNABLE LAHSO
ATC
NEGATIVE ACTIVE OR PASSIVE LAHSO
154
FLAPS
COMMAND SPD TO SET
UP VREF 30 + 80
1 VREF 30 + 60
5 VREF 30 + 40
10/15/17/18/20 VREF 30 + 20
25 VREF 25
30 VREF 30
155
DIFF BETWEEN MIN MAN SPD AND FLAP MAN SPD
MIN MAN SPD BASED AOA
FLAP MAN SPD BASED ON WT
156
MIN MAN SPD
BASED ON AOA AND CURRENT SPD
PROVIDES 1.3 G 40 DEG AOB
FULL MANOEVERABILITY UP TO 20k TO STICK SHAKER ABOVE 20K TO LOW SPD BUFFET
TOP OF AMBER BAND DOES NOT VARY WITH G LOADING
157
FLAP MAN SPD
BASED ON ACFT WT
158
WHAT EFFECTS MAN MARGIN TO STICK SHAKER
IE ZIPPER
GROSS WT
ALTITUDE
LDG GEAR
SPDBRKS
ENG FAIL
159
PM CALLS DURING STALL RECOVERY
AIRSPEED TREND
ANY TREND TOWARDS TERRAIN
160
ANTIICE SYS
STALL WARNING LOGIC
ADJUSTS STICK SHAKER TO LOWER AOA
THIS RESULTS IN HIGHER STICK SHAKER SPEED AND HIGHER MIN MAN SPD
161
ROLL PROTECTION
BANK ANGLE PROTECTION
SAME THING
>35 DEG AOB OPPOSING FORCES BUT CAN BE OVERRIDEN
PFD POINTER TURNS AMBER
RELEASE BANK ACFT WILL REDUCE AOB UNDER 10 DEG
WILL NEED BP > 30 DEG AOB
AP DISENGAGE BAR STOPS BANK ANGLE PROTECTION
GPWS BANK ANGLE 35/40/45
IN DIRECT MODE NEED BP FOR ALL TURNS LIKE NORMAL ACFT
162
HIGH SPEED PROTECTION
@ VMO MMO
NOSE DOWN TRIM INHIBITED
NEED DOUBLE FORCE TO PUSH CONTROL COLUMN FORWARD
USE SB TO REDUCE SPD KEEP AP ON
163
LOW SPEED PROTECTION
@ MIN MAN SPD
INHIBITS NOSE UP TRIM
PILOT NEEDS MORE FORCE TO RAISE NOSE
HALFWAY THROUGH AMBER BAND EICAS AIRSPEED LOW
ATHR ARMED AND NOT ACTIVE ATHR WAKE-UP TO KEEP SPEED > MIN MAN SPD OR BACK TO MCP SPD
ATHR NOT ARMED DOES NOT FUNCTION
164
APPROACH TO STALL
MEM ITEMS
RCB
DISENGAGE AP DISC ATHR
NOSE DOWN ELEV TO REDUCE AOA OR STICK SHAKER STOPS
ROLL SHORTEST DIRECTION TO WINGS LEVEL
ADV THR AS NEEDED
RETRACT SB
DO NOT CHANGE CONFIG EXCEPT DURING LIFTOFF IF FLAPS UP SET FLAP1
CHECK AIRSPEED AND THR
ESTABLISH PITCH ATTIT
RETURN DESIRED FLT PATH
165
HAPPY PLACE PROC
WHEELS ON HZN
THR SET
ACFT TRIMMED
REESTABLISH AUTOMATION
FD OFF
FD ON
PRESS ALT
AP ON
MCP SPD SET
ATHR ARMED
ATHR ENGAGED
FMA FMA
166
CCT
UPWIND PROC
@400’
TRK SEL 160
@1000’
F5 SET F5 SPD
FD OFF
@1500’
LEVEL OFF
SET DWIND TRK
20 DEG AOB
+/- 5 DEG PER 15 KTS WIND
167
CCT
CROSSWIND PROC
CONTINUOUS TURN UPWIND TO DWIND
AFTER TAKEOFF CHECKLIST OVERRIDE FLAPS
DESCENT PROCS
PM DEP ARR LOAD ILS INTC DIR RWY EXEC
168
CCT
DWIND
2-2.5 NM SPACING
ONCE PM SETUP
BRIEF
DESCENT AND APP CHKLISTS
ABEAM THRESHOLD START CLOCK CALL 20/40 SECS +/- 1 SEC PER 2 KTS
@20 SECS GEAR DOWN F20 ARM SB SET F20 SPEED
@40 SECS SET RWY TRK
BASE TURN
169
CCT
BASE
25 DEG AOB TURN
FPV JUST BELOW HZN
200-300 FPM UNTIL INT 3 DEG PATH
INT PROFILE
F 25/30 SET F25/30 SPD
LANDING CHKLIST
DECLUTTER HUD
TREND VECTOR FOR FINAL TURN
170
LHR MISSED APP
INTERMED CLIMB
SET LOWER ALT FIRST
CONSERVATIVE
171
APPROACH VIEW
MAL BURNS PIC
172
UPRT RECOVERY
RCB
DONT TOUCH CONTROLS DURING
173
RADALT DURING FLARE
8 GOOD
3 KEEP FLARING
RADALT ON HUD UNDER ACFT SYMBOL
174
MAIN WHEELS TOUCHDOWN
LITTLE BIT MORE BP
HIGHER ABRK = MORE BP REQD
175
STALL INDICATIONS
PFD
BLUE BENEATH WHEELS
5 DEG PITCH WHY ARE WE HERE
PLIs APPEAR
EICAS AIRSPEED LOW
EICAS AUTOPILOT AND PITCH MODE AMBER BAR THROUGH
176
STALL RECOVERY
VIDEO
IF AP RESPONSE NOT APPROP
DISCONNECT AP
NOSE DOWN PITCH CONTROL APPLY
THRUST AS REQD AND SPD BRAKE DOWN
LINK THESE TWO THINGS
IF TERR NOT A THREAT
ONCE RECOVERED HAPPY PLACE
177
UPRT
RECOVERY PROC
PUSH
ROLL
POWER INCL THRUST AND SPDBRK
RECOVER
178
MISSED APP
MAN FLYING
FMAS ONCE CLEAR OF GND
AND CONFIG CHANGES
179
MAX DEMONSTRATED XWC
TAKEOFF 29 KTS
LANDING 35 KTS
QF USES TALPA TABLE
180
WHAT IS WINDSHEAR
DIFFERENCE IN WIND SPEED AND DIRECTION OVER A RELATIVELY SHORT DIST IN THE ATMOSPHERE
181
ROLLING START
EFFECT ON XWC
REDUCE BY 5 KTS
ROLLING START REDUCES ENGINE STRESS/ SURGE MAY SEE THRUST RAMPING WITH HIGH XWINDS
182
FBW FOR XWIND TAKEOFF
ATTEMPT ZERO YAW RATE
PEDALS DONT MOVE
183
WINDSHEAR PROC
ON RWY
< V1 REJECT
>V1 WINDSHEAR ESCAPE PROC
@Vr AND AIRSPEED SUDDENLY DECREASES ROTATE 2000’ TO END RWY MAY NEED HIGHER ATTIT TO LIFTOFF ENSURE MAX THR SET
184
HUD
TOGA REF LINE
DISPLAYS FOR
TAKEOFF
GA
WS
185
NORMAL PITCH ATTIT RANGE
+5
-2.5
186
WINDSHEAR
PRIOR BEGINNING TAKEOFF
FULL THR
FLAP 20
LONGEST RWY CLEAR WS
INCREASE VR UP TO VR + 20
SET VSPDS ACTUAL WT
DO NOT EXCEED PLI
187
WINDSHEAR
PRIOR TO APP AND LANDING
F25/30
STABLE APP
SUITABLE RWY AWAY FROM WINDSHEAR
MANUAL THR?
188
WINDSHEAR
LIGHT
MOD
STRONG
SEV
LIGHT
MINOR EXCURSIONS
MOD
SIGN EFFECT ON CONTROL OF ACFT
STRONG
DIFFICULTY IN KEEPING ACFT ON FLT PATH AND OR AIRSPEED
SEVERE
HAZARDOUS EFFECTS TO CONTROLLABILITY
189
WINDSHEAR ESCAPE MAN
MANUAL FLT
DISC AP
PUSH TOGA
AGGRESSIVELY MAX THR
DISC ATHR
SIMULT ROLL WINGS LEVEL AND PITCH 15 DEG
VERIFY SB RETRACTED
FOLLOW FD TOGA
AP
PUSH TOGA
VERIFY TOGA FMA
VERIFY GA THR
VERIFY SB RETRACTED
MONITOR SYS PERF
BOTH
DO NOT CHANGE CONFIG
WINGS LEVEL INCREASES CLB GRADIENT
MONITOR VERT SPD AND ALT
DO NOT ATTEMPT REGAIN AIRSPEED UNTIL WS NO LONGER A FACTOR
190
WS MAN
WHY DISC ATHR
SO THR ISNT REDUCED
191
WHAT CLUES MAY INDICATE WS ON INTENDED FLT PATH
ATIS
TS
PILOT REPORTS
VIRGA
192
FOR WS ESCAPE MAN
INITIAL PITCH ATTIT
WHAT WILL U SEE ON HUD
15 DEG
PARK BENCH
FPV NEEDS TO BE BELOW
ACFT SYMBOL TOGA REF LINE
193
CAN U CONTINUE APP IF U RECEIVE WS WARN
NO SHOULD ABORT OR PRIOR TO V1 ON TAKEOFF
PWS CAN DO NORMAL GA VERSUS WS MAN
194
ROLE PM DURING WS MAN
VERIFY MAX THR
ATHR DISC
PITCH
NO CHANGE CONFIG
MONITOR ACTIONS
CALL OMISSIONS
ANY TREND TOWARDS TERR
195
INDICATIONS OF WS
<1000’ AGL
15 KTS IAS
500 FPM
5 DEG PITCH
1 DOT GS
UNUSUAL THR LEVER POSN
196
HUD WS SYMBOLOGY
FPV FILLS IN
PARK BENCH APPEARS AOA LIMIT TO STICK SHAKER
197
ACTIONS REQD WHEN WS EVENT FINISHED
CLEAR WS
DO GO AROUND PROC
198
DURING TAKEOFF ROLL
HOW WOULD U DEFINE AND RECOGNISE WS
FLUCTUATIONS IN AIRSPEED
SLOW ACCEL
199
PM
RADIO CALL WS
WINDSHEAR ESCAPE
CLEAR OF WS RETURNING TO …
200
DETERMINE TRACK OFF HUD
HUD IS HEADING UP DISPLAY
FPV ON COMPASS ROSE IS TRK
201
SOME NNC REDUCE CROSSWIND LIMIT
WHAT ARE THEY
FLTS CONTROLS 20 KTS
ROLL LEFT AUTHORITY 10 KTS
ROLL RIGHT AUTHORITY 10 KTS
HYD PRESS SYS L+C 20 KTS
HYD PRESS SYS L+R 20 KTS
HYD PRESS SYS R+C 20 KTS
202
DESCRIBE POSN NOSE GEAR IN RELATION TO LLZ ANTENNA FOR LDG
LOC ANTENNA NOSE OF ACFT
MAIN GEAR DOWNWIND FROM LLZ IN XWC
203
FMC WIND ACCURATE IN SIDESLIP FOR LDG?
NO USE TOWER WIND
204
APPROACHING MINS
WHICH EFIS
CAPT EFIS CONTROL PANEL
205
UPRT RECOVERY
PITCH RATE
2.5 DEG/ SEC
206
STALL INDICATIONS
NOSE HIGH
BLUE UNDER WHEELS
PLI APPEARING OR PARK BENCH
AMBER IAS BOX
AIRSPEED LOW EICAS
AUTOPILOT EICAS
INCREASING BUFFET
STICK SHAKER
LACK PITCH AUTHORITY
LACK ROLL CONTROL
INABILITY TO ARREST ROD
207
PREDICTIVE VERSUS REACTIVE WS WARN
PREDICTIVE PWS
DETECTED AHEAD OF ACFT
REACTIVE WS GPWS
EXCESSIVE DOWNDRAFT OR TAILWIND OCCURING
208
PWS
PICTURE
209
PWS ALERT
OCCUR ON TAKEOFF EVEN IF WXR NOT SEL
WXR SEL - SCANS - ENABLED AFTER 12 SECS - <2300’ RA, ALERTS < 1200’ RA
WXR NOT SEL - SCANS WHEN THR LEVERS ADVANCED FOR TAKEOFF <2300’ RA, ALERTS <1200’ RA
IF ND MAP/CENTRE PWS ALERT AUTO SHOWS
210
PWS AURAL ALERTS
WARNING
GO AROUND WINDSHEAR AHEAD
WINDSHEAR AHEAD WINDSHEAR AHEAD
CAUTION
MONITOR RADAR DISPLAY
211
GPWS AURAL ALERTS
WINDSHEAR WINDSHEAR WINDSHEAR
<1500’ RA
DETECTION BEGINS AT ROTATION
GPWS INHIBITS PWS AS ACFT ACTUALLY IN WS
212
PWS INHIBITS ON TAKEOFF
WARNING
100 KTS TO 50’
CAUTION
80 KTS TO 400’
213
WINDSHEAR
HOW TO FLY INCREASED VR
SET HIGHER VR MAX ACTUAL VR + 20
OTHER V SPDS FOR ACTUAL WT
INCREASED VR RESULTS IN INCREASED STALL MARGIN AND MEETS TAKEOFF PERF
IF WS ENCOUNTERED AT ACTUAL GROSS WT VR DO NOT ATTEMPT TO ACCEL TO THE INCREASED VR BUT ROTATE WITHOUT HESITATION
214
N1 IDLE
10k 35k
10k
30
35k
47
215
N1 MAX THR
10k 35k
10k
99.1
35k
101
216
SPOOL UP TIME
IDLE TO MAX
10k 35k
10k
12 SECS
35k
22 SECS
217
N1 280 KTS
10k 35k
10k
62 %
35k
85 %
INDICATOR OF EXCESS THR AVAIL FOR ACCEL
218
FUEL FLOW AT 280 KTS
10k 35k
10k
2.5 T
35k
2.7 T
219
FUEL FLOW AT MAX THR
10k 35k
10k
8.6 T
35k
4.2 T
INDICATOR OF ABILITY FOR FUEL TO ACCEL KINETIC ENERGY OF FUEL
220
280 - 300 KTS
TIME TO ACCEL
10k 35k
10k
13 SECS
35k
90 SECS 1:30
221
WINDSHEAR
ON TAKEOFF
BRIEF THAT U WILL CALL VR AND ROTATE AT THE AMBER VR
WINDSHEAR MUST PRESS TOGA
WHEN CLEAR AFTER TAKEOFF USE FLCH AS IT OPENS SPD WINDOW
MAY NEED HIGH ALT THAN CLEARED
222
TCAS CLEAR OF CONFLICT
FLCH ENGAGES ATHR
AND
AP BACK TO CLEARED ALT
223
ILS GLS BREAKOUT MAN
PF
DISC APP AND TURN BREAKOUT HDG
IF REQD INITIATE CLIMB DESCENT
PM
BOTH FD OFF
SET BREAKOUT HDG MCP
SET ALT MCP
AS SOON AS PRACTICAL
PM
ACKNOWLEDGE ATC
PM FD ON
HDG SEL AND VS OR FLCH
WHEN SEL MODES ON PM FD
PF FD ON
AFTER ACFT ON BREAKOUT HDG
REENGAGE AP AS REQD
PF CALL FOR GR AND FLAP
MAX ROD 1000 FPM
FOR CLIMB UP TO GA THR
224
UNANNUN CHKLST
RADIO ALT UNRELIABLE
VREF 30 and F30 LDG
USE AFTER GA IF CAPT AND FO RA DIFF
OR IF RA NOT SHOWING PFD HUD AS EXPECTED
225
FMC NNC
LNAV VNAV INOP
ALL MAPS INOP
ALL CDU PGS INOP
ALL NAV RAD EXCEPT ILS GLS
ALL NAV FUNCTIONS EXCEPT TCP ALTN NAV
ONLY USE CAPT ILS GLS POINTERS
226
RADIO ALTIMETER L + R
NNC
FD AND APP ILS MODES MAY BE INOP
DO NOT ARM SB
MANUALLY EXT SB AFTER LDG
CONFIG GEAR EICAS POSSIBLE
MAN THR APP LDG GA
SOME OR ALL TCAS GPWS ALERTS MAY NOT BE AVAILABLE. TCAS GPWS ALERTS THAT OCCUR ARE VALID
NO ALT MINIMUMS CALL-OUTS DURING APP NOT AVAIL
227
PRM APP
WHERE
AUST AND USA APPROVED
MAINLY SYD
228
SYD PRM BRIEF
PRM ON ATIS
R16R 3000’ 6 NM TO URDEN
34R 2000’ < ENDEV
TCAS TA RA
DUAL VHF REQMT
ONE TWR ONE PRM FREQ
TRANSMIT ON TOWER
DEVIATIONS RETURN TO FINAL COURSE
BREAKOUT INSTRUCTION HAND FLY
229
FLYING A BREAKOUT
WAIT UNTIL FULL BREAKOUT INSTRUCTION RECEIVED SO AP DISC DOESNT DROWN OUT INSTRUCTIONS
USE 25 DEG AOB BE POSITIVE
IF TCAS OCCURS FOLLOW LATERAL BREAKOUT INSTRUCTION VERTICAL FOLLOW TCAS
ATC SEP 1000’ OR 3 NM EXPECT LONGER CCT MORE TRACK MILES
230
FLT CONTROL MODES
NORMAL
SECONDARY
DIRECT
231
HOW CAN FLT CONTROLS DEGRADE TO SECONDARY OR DIRECT MODES
SECONDARY
INTERTIAL OR AIR DATA IS INSUFF OR WHEN ALL FLAP AND SLAT POSN DATA UNAVAIL
DIRECT
FAILURE OF ALL 3 PFCs OR LOSE COMMS WITH THE PFCs. MAN SEL PRI FLT COMP DISC
232
SEC AND DIRECT MODES
WHAT PROTECTIONS ARE LOST
NO AP
NO AUTO SB
ENVELOPE PROT
GUST SUPPRESSION
PITCH COMPENSATION
ROLL YAW ASSY COMPENSATION
TAIL STRIKE PROT
233
HOW WILL DIRECT MODE CHANGE STAB TRIM FUNCTIONALITY
NONE BECOMES NORMAL ACFT
NEED BP FOR FLAP AND SB
TURNS TO 30 DEG AOB
GEAR CONFIG
THR CHANGES
TURBULENCE
234
WHAT AUTOFLT MODES AVAIL TO FLY NON ILS APP
IAN
LNAV VNAV
LNAV VS
LNAV FPA
235
NDB VOR APP TOL
+/- 5 DEG
236
HOW MUST APP BE CODED TO ALLOW USE IAN OR VNAV
GP ANGLE LEGS PG
RWXX WAYPT
MXXX MISSED APP PT
237
2D APP SETTING MCP
SET ALL ALTS TO MDA
USE VSD
300’ TO MDA SET MISSED APP ALT
238
2D APP
FD USE AT MINIMA
BOTH FDs OFF
PM FD ON
239
CIRCLING AREA FOR 787
5.28 NM FIX PG?
240
WHICH ITEMS IN YOUR SCAN WILL U PRIORITISE ON FINAL FOR STABLE APP
GS
GS REF LINE
ROD
PAPI
241
RNP AR APP
WHAT MODES
LNAV VNAV
242
WHY MUST TERR VSD BE DISPLAYED ON ONE ND
INCASE TOTAL FMC FAILURE
243
WHEN ARE VERTICAL NPS FIRST DISPLAYED ON ARR
ON DESCENT
VNAV PTH
244
WHAT HAPPENS ON VERTICAL OR LATERAL NPS WHEN ANP EXCEEDS RNP
WHITE BARS TOUCH
THEY TOUCH AND TURN AMBER AND FLASH FOR 10 SECS
245
WHY SPD INTERVENE ON VNAV PTH
ON APPROACH LOGIC. SPD WILL OTHERWISE REDUCE POSS < FLAP MAN SPD
246
MCP ALT CAPT DURING APP
IN VNAV SET LOWER ALT AND PRESS ALT FOR ALTITUDE INTERVENTION
IN VS SET LOWER ALT AND RESELECT VS OR FPA AS APPLICABLE
247
MISSED APP REQD FOR RNP APP
FULL SCALE LAT OR VERT NPS
EICAS NAV UNABLE RNP OR FMC VERIFY POSN MSG
OR VIS REF NOT ESTABLISHED
VISUAL REF
RWY ENVIRONMENT
APP LGTS
TDZ
RWY END LGTS
248
TCAS TA
MEM ITEMS
TCAS I HAVE CONTROL
TA
LOOK FOR TFC
249
TCAS RA
MEM ITEMS
RA EXCEPT CLIMB LDG CONFIG
IF MAN REQD DISENGAGE AP AND ATHR
SMOOTHLY ADJ PITCH AND THR TO SATISFY RA
FOLLOW LATERAL PATH
ATTEMPT VISUAL CONTACT
RA CLIMB LDG CONFIG
DISENGAGE AP AND ATHR
ADV THR LEVERS FORWARD TO ENSURE MAX THR ATTAINED
F20 SMOOTHLY ADJ PITCH FOR RA COMMAND
FOLLOW LATERAL PATH
ATTEMPT VISUAL CONTACT
POSITIVE RATE OF CLIMB GEAR UP
250
TCAS
HUD SYMBOLOGY
251
TCAS
TIMING FOR RECOVERY
5 SECS/ 2.5 SECS
252
TCAS
RADIO CALLS
TCAS RA
UNABLE TCAS RA
CLEAR OF CONFLICT RETURNING TO …
CLEAR OF CONFLICT FL… RESUMED
253
TCAS TA OR RA
SO AS PF
CAPT OR FO MUST TAKEOVER
254
VSD USE
ALLOWS CHECK QNH VERSUS RWY
GIVES VISUAL INDICATION OF FPA CONSTRAINTS AND QNH ERRORS
255
TCAS INHIBITS TAKEOFF
TCAS TA ON GND TO 600’ RA
TCAS RA ON GND TO 1000’ RA
TCAS DESCEND RA ON GND 1200’ RA
256
TCAS INHIBITS LANDING
ALL TCAS RA 1000’ RA ENDS GA 900’ RA
INCREASE DESCENT RA 1450’ RA ENDS GA 1650’ RA
DESCEND RA 1000’ RA ENDS GA 1200’ RA
257
TA
RA
TIME TO COLLISION
TA 20-48 SECS
RA 15-35 SECS
5 SECS 0.25G
2.5 SECS 0.35G
258
HOW MANY FMC?
3
MASTER
SLAVE
BACKUP
259
APPROACHING GLIDEPATH CALL
2NM TO DESCENT PT
2D APP GR DOWN F20 ARM SB
AT DESCENT PT F30 LDG CHKLST
260
GLIDESLOPE ALERT ON IAN APP OTHER THAN ILS GLS
DUE BAROMETRIC ALTIMETER INDICATION VARIATIONS
INCORRECT ALT SETTING
WARMER THAN STD OAT
261
NOSE HIGH
RECOVERY
RCB
DISC AP AND ATHR
NOSE DOWN ELEV TO OBTAIN NOSE DOWN PITCH RATE
NOSE DOWN TRIM
REDUCE THR
ROLL TO INDUCE NOSE DOWN PITCH RATE
COMPLETE RECOVERY
HAPPY PLACE
REENGAGE AUTOMATION
262
NOSE LOW
RECOVERY
RCB
DISC AP AND ATHR
RECOVER FROM STALL IF NEEDED
ROLL SHORTEST DIRECTION TO WINGS LEVEL
COMPLETE RECOVERY
NOSE UP ELEV
NOSE UP TRIM IF NEEDED
HAPPY PLACE
REENGAGE AUTOMATIONQ
263
ILS RAW DATA
HUD CAN USE CAT I MINIMIA
NO HUD NEED 1200 M VIS
264
PRIOR TO ARMING APP
CHIPS
CLEAR TO INT APP
HEADING TO INT
ILS GLS IDENTIFIED
POINTERS IN VIEW
SPD WINDOW OPEN
265
NNC INSTRUCTIONS
RAMATE
RECOCNISE AND ANNOUNCE
MAINTAIN ACFT CONTROL
ANALYSE THE EICAS
TAKE THE PROPER ACTION
EVALUATE THE NEED TO LAND
266
WHAT IS THE SIGNIFICANCE OF THE COLOUR OF THE CHECKLIST TITLE IN AN ECL CHECKLIST
WHITE VS AMBER
SITUATION NO LONGER PRESENT
267
IF A CHECKLIST IS OPENED IN ECL FOR REVIEW OR IN ERROR WHAT IS FLT CREW ACTION REQD
CHECKLIST OVERRIDE
268
WHAT EICAS INDICATIONS FOR WINDMILLING START OR X START
WINDMILLING
MAX FL OR SPEED FOR CURRENT FL
SHOWS IF FUEL CONTROL SW CUTOFF OR N2 < IDLE
X START
UNDER N2
CURRENT ALT AND OR AIRSPEED OUTSIDE WINDMILLING ENVELOPE. STARTER ASSIST IS RECOMMENDED FOR INFLT START
269
HOW WILL FBW SYS RESPOND TO A THR ASYMMETRY IN NORMAL MODE? WILL RUDDER PEDALS MOVE
> 60 KTS MAINTAIN ZERO YAW RATE
RUDDER PEDALS MOVE
270
IS AUTO RELIGHT PROTECTION PROVIDED
YES
FOR FLAMEOUT AND SUB IDLE STALL RECOVERY
AUTOSTART SHOWN ABOVE N2
271
HOW DO U MANAGE VARIOUS TASKS THAT NEED TO BE COMPLETED IN ORDER TO MANAGE ENG FAIL IN CRUISE
GAP TO MIN MAN SPEED = TIME OR URGENCY FOR DESCENT
272
WHICH PG FMC WOULD U FIND DRIFT DOWN SCHEDULE AND MAX OPERATING ALT
VNAV EO PG
273
WHAT ARE DIFFERENCES WITH DRIFTDOWN UNDER EDTO PROCEDURES
OEI OFF OFP
BETWEEN BEST L/D AND VMO MMO
274
PREFERRED AFDS MODES FOR DRIFTDOWN
DUDU
DOWN VNAV EO PG
UP SET MAX ALT MCP ALT
DOWN PRESS EXEC
UP PRESS ALT TO BEGIN DESCENT IN VNAV
275
OTHER CONSIDERATIONS FOR DRIFTDOWN FOR PM
CLEARANCE
VOICE OR CPDLC
LIGHTS
CALL ON 123.45
TCAS BELOW
276
CONTINGENCY PROC
OTHER THAN WEATHER SITUATIONS
FOR DESCENT
OFFSET 45 DEG AND 15 NM
277
DRIFTDOWN LEVEL OFF
WHAT SPEED
ETOPS CONSIDER OFP SPEED
WILL DEPEND ON LOCATION AND PRIORITY IF DIVERTING AND DIST TO GO
278
ENG FAIL CRUISE FLT
DOES CREW HAVE TO LAND NEAREST AVAIL APT
IF CAT C CAN CONTINUE CAT A OR B
DEPENDS ON WEATHER, FAMILIARITY WILL APT AND DIST TO GO TO PREFERRED ALTN
279
CAN FUEL BE JETTISONED FROM ALL TANKS
YES
AUTO SETS MLW
280
WHERE DO U OBSERVE CALC JETTISON TIME
FUEL SYNOPTIC BOTTOM RIGHT
281
SOME OPERATIONAL CONSIDERATIONS PRIOR TO JETTISONING FUEL
ATC CLR
PREFERRED ALT > 6000’?
AWAY FROM HOUSES ETC
282
CONSIDER OVERWT LANDING VERSUS FUEL JETT
GENERALLY CAN LAND IF CAN TAKEOFF
IF F25 MAX APP SPEED 185 KTS GIVES 5 KTS TO PLACARD SPD
FUEL JETTISON FOR REDUCING LDR
AUTOLAND NOT RECOMMENDED NOT CERTIFIED NEED MANUAL LANDING
TIME TO GET ACFT ON GND IE PRIORITY VERSUS TIME TO JETTISON OR IF NEEDED FOR LANDING PERF CALC
CAPT CAN USE UNFACTORED DATA IN EMERG
283
REVIEW OVERWT LANDING CHECKLIST IN ECL
UNANNUN
284
REVIEW TAP
WHAT WILL U EXPECT EEC TO DO IF AIRSPEED REDUCES BELOW V2 AFTER TAKEOFF OR VREF ON APP? WHAT WILL EEC DO ONCE AIRSPEED REGAINED?
REDUCES THR TO ALLOW RUDDER FOR DIRECTIONAL CONTROL
INCREASES THR ONCE AIRSPEED >V2 VREF
TAP ENHANCES SECOND SEGMENT
285
IF AIRSPEED REDUCES TOWARDS THRUST ASYMMETRY MINIMUM SPEED TAMS WHAT WOULD U EXPECT IN THE WAY OF VISUAL AND AURAL ALERTS?
HOW IS TAMS SHOWN ON SPEED TAPE
< TAMS
AIRSPEED AIRSPEED AURAL
MASTER WARN
SHOWN IN RED RECTANGULAR BOX
RELATED TO MINIMUM CONTROL SPEED
286
DIVERSION AND DECISION MAKING STRATEGIES
NON EDTO 60 MINS
EDTO 330 MINS
TIME STRATEGY
FUEL STRATEGY
OBSTACLE STRATEGY
287
WHAT IS AN EDTO ALTN
ADEQ APT
CAT A B C
WX FORECAST AVAIL
SERVICES FACILITIES EG LGTS
LDA < LDR
AT LEAST ONE INSTRU APP
288
WHAT IS EDTO PLANNING MINIMA
DEFINED WX CRITERIA USED TO DETERMINE SUITABILITY OF ADEQ APT
SHOWN EFF MSG
289
WHAT SPECIFIC REQMTS NEED TO BE CONSIDERED FOR EDTO ALTN PREFLT STAGE
RFF
30 MIN CALL-OUT CAT 4 OUTSIDE AUST
IN AUST NIL
ATC
AVAIL 30 MINS NOTICE OUTSIDE AUST
IN AUST NIL
290
EDTO WX ASSESSMENT
BETWEEN EARLIEST AND LATEST ARRIVAL TIME
FORECAST CEILING AND VIS
XWC INCL GUST OEI WIND COMP
PROB < 40% DISREGARD
INTER TEMPO CONSIDERED
291
CAN FLT DEPART WITHOUT FORECAST FOR EDTO ALTN
YES PROVIDED ONE RECEIVED WHEN APT RELIED UPON
292
TECH LOG REQMTS FOR EDTO FLT
YES 330 MINS
NO 60 MINS
RESTRICTED VARIES
NEW E LOGBOOK SHOWS CLEARLY
293
SPECIFIC INFLT REQMTS PRIOR TO EEP
2 WAY COMMS WITH ATC AND FLT DISPATCH
INFLT FUEL REQMTS
ACFT STATUS OK
NOTAMS
EDTO ALTN WX ABOVE LDG MINIMA
294
WHAT ARE SIGNIFICANT SYS FAILURES
NNC
PLAN TO LAND AT NEAREST AVAIL APT
295
WHAT ARE TIME LIMITED SYS
LIMITATION SPECIFIED ACFT FLT MANUAL
296
ACTIONS WITH A SIGNIFICANT SYS FAILURE BETWEEN EEP AND EXP
IF EDTO ALTN CAT C CAN CONTINUE TO CAT A B
SPEED DEPENDS ON PRIOIRITIES
297
REVIEW CPE FUEL REQMTS
DOES IT NEED TO BE PROTECTED INFLT
NO PREFLT REQMT
298
RTO
REASONS
<80 KTS
MASTER WARN CAUTION
TYRE FAILURE
UNUSUAL NOISE OR VIBRATION
SLOW ACCEL
ANY FIRE WARN
PWS
ENG FAIL
ACFT UNSAFE UNABLE TO FLY
TAKEOFF CONFIG
>80 KTS
ENG FAIL
ANY FIRE
PWS
ACFT UNSAFE UNABLE TO FLY
299
RTO
ACTIONS CAPT
CALL STOP
SIMULT CLOSE THR LEVERS AND DISC ATHR
MAX BRAKING OR VERIFY RTO
FULL AVAIL REV THR
SB
ONCE ACFT STOPPING IN AVAIL DIST STOW REVERSERS
300
RTO
ACTIONS FO
MONITOR ACTIONS
CALL OMISSION
ENSURE THR LEVERS CLOSE
ATHR DISC
SB UP NOT UP
REVERSERS NORMAL NO REVERSERS
60 KTS
ONCE ACFT STOPPED
ADVISE ATC
ALERT PA
PAPER QRH OR ECL AS REQD
301
WITH RTO SEL
WHEN WOULD BRAKES BE APPLIED
ACFT ON GND
GROUNDSPEED > 85 KTS
BOTH THR LEVERS IDLE
302
TAKEOFF INHIBITS
MASTER WARN CAUTION
MASTER WARN
V1 OR ROTATION TO 400’ OR 25 SECS AFTER INHIBIT
CAUTION
80 KTS TO 400’ OR 20 SECS AIRBORNE
303
INDICATIONS OF INCAPACITATION ON TAKEOFF
THRUST SET MISSED
POOR CENTRELINE TRACKING
80 KTS CALL MISSED OR NO REPLY
304
WHAT INFO ON HUD IS AVAIL TO ASSIST WITH RTO BRAKING
GND DECEL SCALE > 50 KTS AND REMOVED < 25 KTS
305
EVAC PROC
PAPER QRH
READ AND DO
306
THRUST LOSS DURING TAKEOFF ROLL
WHERE TO LOOK FOR TRACKING
USE HUD
FPV VERSUS HDG BUG
307
OEI INITIAL PITCH FOR TAKEOFF
APPROX 10 DEG
ROTATE 1.5- 2 DEG
308
V1 CUT
WHEN SHOULD U ASK PM TO IDENTIFY THE PROBLEM
> 400’ AND ACFT UNDER CONTROL
309
ENG SEV DAMAGE
ACFT INDICATIONS
NEED AIRFRAME VIBRATION
310
V1 CUT
WHEN IS FLAP RETRACTION
MEM ITEMS COMPLETE IF REQD
> EO ACCEL ALT OR 1000’ AGL
311
V1 CUT
PROC
CONTROL ACFT ON RUNWAY
RELEASE RUDDER WHEN ABRK CLICKS AIRBORNE
MAINTAIN V2 TO V2 + 15
@200’ AP ON
@400’ IDENTIFY THE PROBLEM
MEM ITEMS IF REQD
@ EO ACCEL ALT
VNAV SET FLAPS UP MAN SPD AND RETRACT FLAP
NO VNAV KEEP TOGA PITCH SET FLAPS UP MAN SPD AND RETRACT FLAP THEN FLCH
CESSNA ONCE ACFT CLEAN
312
V1 CUT
AFTER FLAPS UP CESSNA
AFTER FLAPS UP
CON VERIFY
ENG OUT PG EXEC
SA
SPD WINDOW OPEN
NNC
AFTER TAKEOFF CHECKLIST
313
V1 CUT
CURVED DEP WHAT MAX ANGLE OF BANK WOULD YOU USE
WILL AFDS ROLL MODE SEL AUTO LIMIT BANK ANGLE
AFDS LIMITS BANK TO 15 DEG UNTIL V2 + 10
BANK LIMIT 25 DEG @ V2 + 20 IN LNAV OR HDG/ TRK SEL IN AUTO
314
OEI
FLYING THE APP
AS PER NORMAL
F 20 OR F30 DEPENDING ON PERF?
315
OEI
TARGET THR SETTING FOR APP
NOT SURE
HUD SPEED TREND VECTOR EXCELLENT FOR MAN THR
KEEP ATHR ENGAGED
APPROX 65%
316
ENG LIMIT EXCEED
MEM ITEMS
ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM RETARD UNTIL ENG LIMIT EXCEED MSG BLANKS OR THR LEVER AT IDLE
317
ENG SURGE
MEM ITEMS
ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM RETARD UNTIL ENG SURGE MSG BLANKS OR THR LEVER IDLE
318
ENG SEV DAMAGE
MEM ITEMS
NEED ACFT VIBRATION
ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM IDLE
FUEL CONTROL SW CONFIRM CUTOFF
ENG FIRE SW CONFIRM PULL
319
EXTRA THRUST AVAIL
V1 CUT
ONLY IF USING TO THRUST AND ATM
TO 1 OR TO 2 NO EXTRA THR AVAILABLE
320
WHEN TO DECLUTTER HUD
SEL LDG FLAP
321
OEI LAND 2/3
AP CONTROLS RUDDER
MANUAL TRIM INHIBITED
322
OEI
AUTOLAND XWC
25 KTS
AUTOLAND APPROVED OEI
323
OVERWT LANDING
FLAP EXT AND COMMAND SPD
CAN REDUCE AIRSPEED BY AS MUCH AS 20 KTS UNDER NORMAL MAN SPDS BEFORE EXT NEXT FLAP
DOES NOT ALLOW 15 DEG OVERSHOOT FOR TURNS
324
787 VERTICAL OFFSET
USE MINIMAL VS
HARD TO GO DOWN AND SLOW DOWN
USING HIGHER DESCENT SPEED MAY NOT HELP REGAIN PROFILE AS WING TOO GOOD
UNLESS
USE FULL SB
OR GEAR DOWN F20
325
ISFD USE ON BASE
SAME AS JUMBO
PICKS UP GLIDESLOPE EARLIER THAN HUD
326
EDTO
TS CONSIDERED?
NO NOT BY THEMSELVES
UNLESS CEILING VIS LESS THAN ADEQ MIN
327
OEI CRUISE LEVELS
MAX WT FL180s
LGT WTS FL330
DURING FLT LIKELY MID FL200s
328
DRIFTDOWN
AFDS MODES
NORMALLY VNAV
BASIC MODES AS BACKUP IE FLCH AND HOLD THR AT MAX
329
FAM ALLOWS ONE CB WE CAN RESET
FLT DECK IPAD CHARGER
2 STEP PROC AS NEED TO CONFIRM IN FLT
330
ALTERNATE GA PROC
NOT FOR F30 ONLY F25
PF GO AROUND FLAPS 5
BASED ON RTL PERFORMANCE
RETURN TO LAND
CERTAIN CONDITIONS 787 CANNOT MEET OEI CLIMB GRADIENT WITH F20
TAKEOFF AND RETURN EF ON APP AND LDG MAY NOT MEET CLIMB GRADIENT @ F20
CALLED FUEL JETT/ LIMIT WEIGHT
LDG F25GAF5 FAOR ALLOWS 4T INCREASE TAKEOFF WT
MAINLY HIGH ALT APTS AND HIGH TEMP
ANYTIME RTL F25/GAF5 USED NO MATTER TAKEOFF WT DO OVERWT LANDING CHKLST IF RETURN DEP APT
ICIING NEEDS CONSIDERATION AS IT DEGRADES GA PERF
331
V1 CUT
TARGET ATT
ROTATION RATE
DEPENDS ON OPT
APPROX 11 DEG
ROTATE SLOWLY TO 9 DEG UNTIL GEAR UP THEN HIGHER
ENSURES ACFT ALWAYS ABOVE V2
332
OVERWT LDG
DIFF FLARE?
IF F20 THINK ABOUT FLARING BUT VERY MINIMAL
333
CAN 787 AUTOLAND OVERWT?
NO NOT CERTIFIED
NEED MANUAL LDG
334
OEI
TARGET THR SETTING ON APP
APPROX 65%
DEPENDS ON WT AND CONFIG
335
OEI
GA PROC
PF GO AROUND FLAPS 5
PRESS TOGA
ENSURE GA THR SET
PM THRUST SET
POSITIVE RATE GEAR UP
FMA FMA FMA FMA FMA FMA
@400’ ROLL MODE
@1000’ SET FLAPS UP SPD OR EO ACCEL
CLEANUP
CON
ENG OUT PG
SA
SPD WINDOW
NNC
AFTER TAKEOFF CHECKLIST
336
NNC
NAV AIRSPEED DATA
NO MEM ITEMS
SYS DETERMINES PITOT ISSUE
SIGNIFICANT DIFFERENCE BETWEEN 3 PITOTS AND NO 2 PITOT THE SAME
THE VOTED PITOT TOTAL IS DECLARED INVALID
AIRSPD INDICATION CHANGES TO SYNTHETIC AIRSPEED (AOA SPD)
FLT CONTROLS SEC MODE
AP DISC
ATHR DISC
VMO REDUCES 300 KTS
337
VHHH
NOTES
090-230 WINDS > 15 KTS CAN EXPECT SIGN WS AND TURB
MICROBURSTS > 30 KTS AND FUEL CAV
LOCAL DETECTION TO 3 NM
338
VHHH
ALERTS
MICROBURST ALERT
WIND SPD LOSS >/ 30 KTS AND RAIN
WINDSHEAR ALERT
WIND SPD LOSS 15-29 KTS OR GAIN >/ 15 KTS
TURBULENCE ALERT
TURB MOD SEVERE (FOR HVY ACFT)
339
EICAS MSG GROUPING
GROUPED BY PRIORITY LEVEL
WITHIN EACH LEVEL SHOWN IN ORDER THEY APPEARED
NEWEST AT TOP OF LIST
340
AOA SPD HAS LIMITATIONS
ERRATIC DURING CONFIG CHANGES
INACCURATE AT HIGH SPEEDS
341
SEC MODE
2 MODES FOR ELEV FEEL
FOR FLAPS UP AND EXT
PITCH SENSITIVITY INCREASED SO AVOID ABRUPT CONTROL INPUTS AND HIGH MAN LOADS
342
1 ST SEGMENT
TO 35’
POSITIVE
343
2ND SEGMENT
35’ TO 400’
2.4%
344
3RD SEGMENT
ACCEL @ 400’
1.2%
345
4TH SEGMENT
CLEAN ENROUTE CLIMB
1.2%
346
TAKEOFF SEGMENT
SUMMARY
POSITIVE
2.4%
1.2%
1.2%
THESE ARE GROSS GRADIENTS
NET CAN BE REDUCED BY 0.8%
347
APPROACH CLIMB PERF
OEI @ 1.5 Vs
2.1 % GRADIENT
348
LANDING CLIMB PERF
AEO @ 1.3 Vs
CLIMB GRADIENT 3.2%
349
AIRSPEED UNRELIABLE
MEM ITEMS
AP DISCONNECT SW PUSH
ATHR ARM SW OFF
FD SW BOTH OFF
SET FOLLOWING GEAR UP PITCH AND THR SETTINGS
FLAPS EXT 10 DEG 85% N1
FLAPS UP 4 DEG 70% N1
350
AOA SPD
DERIVED
BASED AOA AND INERTIAL SYSTEM INPUTS
WHEN PITOT AND OR STATIC PRESS ERRONEOUS OR NOT AVAIL
VMO REDUCED FROM 360/ M0.9 to 300/ M0.85
351
GPS ALT
BACKUP ALT FROM GPS DATA
352
2D APP PROC
FULLY CONFIGURED FOR FINAL DESCENT
MDA + 50’
LNAV TRK SEL VS OR FPA
FPA START DESCENT 0.3 NM EARLY
2NM TO DESCENT PT (FIX PG)
APPROACHING GLIDEPATH
GEAR DOWN F20 ARM SB
F25/30
START DESCENT
LDG CHECKLIST
PUSH VS/ FPA
SET CONSTRAINTS USE VSD 300’ TO MINIMA SET MISSED APP ALT
DISENGAGE AP BY 135’ FD OFF PM FD ON
353
AIRSPEED UNRELIABLE
WHAT FLT MODE
EICAS FLIGHT CONTROL MODE
IS SEC MODE
354
IF AOA SPD UNREL
MAY SEE ISFD SPD
USES C PITOT
355
TURB PENETRATION SPEED
290 < 25k
310/ .84 WHICHEVER LOWER >/ 25k
356
WHICH PORTS DONT HAVE HEATING ON 787
STATIC PORTS NO HEATING
357
AIRSPEED UNRELIABLE
EXPLAIN SYSTEMS
NO FAULTS DETECTED AIR DATA SYS
BUT
FLT CONTROLS COMPUTERS DETECT DISAGREEMENT BETWEEN AIR DATA BEING REPORTED AND SYNTHETIC AIRSPEED BEING CALCULATED USING AOA
PFDs WONT AUTO SW AND NNC GUIDES THE CREW TO USE MORE ACCURATE SOURCE OF DATA (AIR DATA OR SYNTHETIC DATA)
3 FAULTS RESULT IN AIRSPEED UNRELIABLE
SIMULT AND TOTAL BLOCKAGE OF 2 OR 3 PITOT
COMPLETE AND TOTAL BLOCKAGE 2 OR 3 STATIC PORTS
SIMULT SEIZURE OF BOTH AOA VANES IN SAME POSN
358
AIRSPEED UNRELIABLE SUMMARY
IN NORMAL OPS WITH AIR DATA SEL AUTO THE L AND R ASI AND ALTITUDE INDICATIONS ARE THE SAME AS THEY ARE A VOTED OUTPUT OF THE ADRS
PITOT DISAGREE SWITCH TO AOA SPD AND NAV AIRSPEED DATA EICAS
STATIC INPUTS DISAGREE SW TO AOA SPD AND GPS ALT AND NAV AIR DATA SYS EICAS
IF ADRS AIRSPEED AND AOA SPD DISAGREE NO AUTO SWITCHING AND AIRSPEED UNRELIABLE EICAS
MEM ITEMS MUST BE COMPLETED
359
507
ICAO HOLD SPEEDS
0-14 230
14-20 240
20-34 265
>34 .83
360
507
AUST HOLD SPEEDS
0-14 230
14-20 240
>20 265
361
507
FAA HOLD SPEEDS
0-6000 200
6-14 230
>14 265
362
507
HOLD TIMINGS
<14 k 1 MIN
>14 k 1.5 MINS
363
507
FMC HOLDING
CONSTANT RADIUS TURN BASED ON CURRENT WIND AND FMC COMMANDED AIRSPD
IN LNAV 30 DEG AOB
>ICAO FAA AIRSPDS ACFT MAY BE OUTSIDE PROTECTED AIRSPACE
SECTOR ENTRY BASED ON TRK TEARDROP 40 DEG OFFSET
ACTIVE HOLD PATTERN MAGENTA ND
PRESS HOLD CAN ENTER WAYPT LEGS PG ON R6 PPOS
364
507
HOLD PG TERMS
EFC
EXPECT FURTHER CLEARANCE UPDATES DOWNTRACK ETA AND FUEL
HOLD AVAIL
HOLD TIME BEFORE NEEDING FUEL RESERVES
365
507
WHEN HOLDING IN ALT OR VNAV ALT WHAT ACTION IS REQD TO PERMIT VNAV PTH DESCENT AFTER EXITING HOLD
250 KTS VNAV DES PG
INBOUND LAST HOLD DCT TO HOLD FIX AND EXEC
REMOVES HOLD AND CHANGES VNAV ACT DES PG
ALSO CHECK CRZ ALT
366
WHY MUST TERR OR VSD BE DISPLAYED ON AT LEAST ONE ND DURING RNP AR APCH
BACKUP TOTAL FMC FAILURE AND LOSS LNAV TRACKING
367
WHY IS IT ESSENTIAL TO CHECK FOR SIGN WX ON THE FULL EXTENT OF AN RNP AR APCH FOR ARRIVAL BOTH THE APP AND MISSED APP TRKS
CANT TRACK AROUND THE WX MAY NEED DIFF APP?
368
WHEN IS VERTICAL NPS FIRST DISPLAYED ON ARR
TOD WITH VALID VNAV PTH
369
WHEN IS LATERAL NPS FIRST SHOWN ON DEP
LNAV @ 50’
370
WHAT HAPPENS ON LATERAL OR VERTICAL NPS WHEN ANP EXCEEDS RNP
ANP BARS OVERLAP AND TURN FROM WHITE TO AMBER > 5 SECS
IF NPS POINTER IN ANP > 5 SECS NPS POINTER FLASHES 10 SECS AND ANP BARS AMBER
371
WHAT ALT CAN AP BE ENGAGED TO ON AN RNP AR APCH
135’ AGL
372
WHAT IS THE DIFF BETWEEN A PROPRIETARY RNP AR AND ICAO RNP AR
DIFFERENT CRITERIA
373
WHAT IS THE DEFAULT DME AND VOR UPDATING IN 787 FMC
HOW IS THIS RELEVANT TO RNP AR APCH OPS
VOR DME OFF UPDATING
DME DME AS NEEDED
374
CAN ANY MODIFICATIONS BE MADE TO RNP AR APCH PROCEDURE LOADED FROM FMC DATABASE
ONLY SPD PROVIDED NOT ABOVE MAX SPD ON CHART
CAN CHANGE FAF TO AT ALT IF CODED AT OR ABOVE
375
WHAT APP CAN IAN BE USED FOR
ALL APP
EXCEPT
ILS GLS RNP AR APCH
376
HOW LONG IS AWIS QNH VALID FOR WHEN OPERATING TO A CTAF R APT AND CONDUCTING RNP AR APCH
15 MINS FROM RECEIPT
377
CALC TIME FOR A HOLD PATTERN
<20 k 2 MIN TURNS
PLUS
2 * LEG TIME
SO APPROX 6 MINS
378
WHY DOES RNP LNAV OR LNAV VNAV PROCEDURAL CHECKLIST IN QRH REQUIRE TRK DIST TO BE CHECKED FOR ALL LEGS
WHAT SHOULD BE CHECKED FOR RNP AR APCH
AR APP HAS INTEGRITY CHECKING PRIOR LOADING FMC NAV DATABASE OTHER APPs DONT
RNP AR ALSO TRK TO FIX, RADIUS TO FIX OR OTHERS
379
WHAT IS THE BASIS FOR OBSTACLE CLEARANCE DURING RNP AR INSTRU APP PROC
VERTICAL NAVIGATION BUDGET
380
RNP AR
LARGE FONT SPD
LARGE FONT SPD ON LEGS PG IS LIMIT FOR RADIUS OF TURN DO NOT EXCEED (RARE NORMAL SPD)
381
WHAT IS ON APPROACH LOGIC
MCP CAN BE SET 300’ ABOVE AND REMAIN VNAV
SPD PRIOR FROM VNAV PTH TO VNAV SPD IF FAST AND HIGH
382
HOW TO GET FMC OUT OF ON APPROACH LOGIC
TOGA
LANDING
OR >MAPT
383
HOW CAN ISSUE OF MISSET QNH BE MITIGATED DURING PBN APP
CHECK VSD
384
WHY DOES RNP AR APCH HAVE CHARTED TEMP LIMITS
CHART VALID FOR ALL TEMPS WITHIN
385
ARE COLD WX CORRECTIONS APPLIED TO DA FOR RNP AR APCH
WHAT ABOUT MSA?
NO ONLY FOR MSA
386
WHAT DIRECT TO TRACKING REQMTS APPLICABLE TO RNP AR APCH? WHAT ABOUT CLASS G AIRSPACE
WITHIN 30 DEG INT LIP
LATEST INTERCEPT POINT
387
WHEN ARE YOU ON APPROACH LOGIC
DESCENT PHASE AND FLAPS OUT OF UP
PAST FIRST WAYPT OF APP
DIRECT TO ACTIVE WAYPT < 12 NM
MAPT ACTIVE WAYPT AND DIST < 25 NM
388
MISSED APP REQMTS FOR PBN APP
OUTSIDE NPS LIMITS
NAV UNABLE RNP EICAS
FMC VERIFY POSITION
389
OBSTACLE CLEARANCE FOR MISSED APP
AUST
2.5% 100’ IF CLIMBING 152’/ NM
HIGHER GRADIENT LISTED ON CHART
TERPS IN USA
3.3%
390
WHAT IS THE DEFINITION OF DAY OR NIGHT VISUAL APP REQMTS IN QRH PBN PROC GEN
IF NAV INTEGRITY IN DOUBT BUT VISUAL REF IN CIRCLING AREA CAN CONTINUE WITHOUT MAKING MISSED APP
391
GPWS
TIME TO IMPACT
CAUTION
40-60 SECS
WARNING
20-30 SECS
392
GPWS WS ALERT
OVERRIDES ALL PWS TCAS OTHER GPWS WARN
393
WHAT DIFFERENTIATES GPWS CAUTION AND WARNING
PULL UP
394
WHAT ARE TARGET PERF PARAMETERS FOR GPWS MAN
MAX THR
PITCH 20 DEG
WINGS LEVEL
SB RETRACT
395
DIFF BETWEEN GPWS AND WS MAN
PITCH 20 DEG VERSUS 15 DEG
396
DOES TOGA GUIDANCE PROVIDE GUIDANCE FOR GPWS RESPONSE
NO WE DONT PRESS TOGA
397
WHEN CAN A GPWS CAUTION OR WARN BE REGARDED AS CAUTIONARY? IS THERE ANY DIFF BETWEEN THE CRITERIA FOR CONTINUING AN APP WITH A CAUTION VERSUS A WARN
IF POSITIVE VISUAL VERIFICATION IS MADE THAT NO TERRAIN OR OBSTACLE HAZARD EXISTS UNDER DAYLIGHT VMC PRIOR TO TERR/ OBST WARN ALERT CAN BE DISREGARDED
IF WARNING DURING LOW RNP OPS REESTABLISH GND TRK WHILE EXECUTING MAN
SO FOR WARN NEED TO HAVE SEEN TERR PRIOR TO WARN OTHERWISE MUST FOLLOW
398
OPT FLAP SETTING SCEL
DONT USE OPTIMUM
HARD WIRE FLAP SEL
399
SCEL
HOW DO U IDENTIFY BRANCH PT FMC
TOP CDP
DECISION PT
PUT ON FIX PG
400
SCEL
HOW WILL U ALTER RNP REQD FOR DEP
WONT TOUCH AEO
WILL NEED TO VERIFY IN EVENT OF OEI
USE ND AS NO GUIDANCE FOR WHICH PG TO LOOK AT
401
WHAT ARE TRAPS WITH ENTERING LOWER RNP
REMAINS IN LARGE FONT UNTIL DELETED
402
CRITERIA FOR EO SID LOADING
WHERE IS IT LOCATED
WE DONT LOAD OR CHECK
LOCATED DEP ARR LAST PG
403
SCEL
REQMTS FOR OEI BEFORE AND AFTER BRANCH PT
BEFORE FOLLOW EO SID
AFTER AS PER CDP
404
SCEL
WHEN CAN EO SID BE DISCONTINUED?
AS PER CDP
ABOVE MSA?
405
SCEL
WHEN TO EXEC EO SID
IMPORTANT ONCE ACFT UNDER CONTROL
EXEC PRIOR TO BRANCH PT
406
FIRE ENG
MEM ITEMS ON GND
NOT REQD
EITHER ECL OR QRH
407
WHEN IS THE SECOND BOTTLE DISCHARGED FOR AN ENG FIRE WHEN ON THE GND
PART EVAC CHECKLIST
408
ALTN PG
DIVERT NOW
CHANGES RTE DEST APT
INCLUDES RTE MOD IN ACTIVE FLT PLAN
DELETES ALL PARTS OF ORIGINAL RTE NOT PART OF DIVERSION
IF DES PTH REMOVES ALL CONSTRAINTS
409
NPS
NAVIGATION PERFORMANCE SCALES
PRESENT A REAL TIME DISPLAY OF THE LOCATION OF THE LNAV AND VNAV PTH RELATIVE TO THE ACFT
VERT NPS VALID DESCENT PATH
LAT NPS LNAV @ 50’
410
RNP AR OBST CLR
INITIAL (NORMAL) 1000’
INITIAL (TERRAIN) 2000’
INTERMED 500’
411
RNP AR
CONTAINMENT
RNP AR APP USES LINEAR CONTAINMENT AT 2 * RNP FOR OBSTACLE PROTECTION - THEREFORE WITH LOWER RNP THE FINAL APP SEGMENT (FAS) IS NARROWER + POTENTIALLY EXCLUDES MORE OBSTACLES
412
EQUIP NEEDED RNP AR APCH
ALL ON ONE SIDE
1 * FMC
1 * CDU
1 * PFD + ND
1 * FD
413
GPWS CALL-OUTS
2500’
1000’
VERIFY AGAINST ALT
ARE THEY REASONABLE?
414
WX RADAR USE
CRZ
DURING CRZ
IF RADAR TOO SENSITIVE TURN GAIN DOWN -2 RETURN TO CAL AFTER ASSESSMENT
IN CENTRAL PACIFIC CONSIDER +1 AS SMALL CELLS LESS REFLECTIVE
415
WX RADAR USE
DES
IN CRZ ONLY SCANS 6000’ BELOW
SWITCH TO MANUAL PRIOR DESCENT AND SCAN LOWER
NO WX BACK TO AUTO
IF WX SHOWN MAINTAIN MANUAL TO 22K
THEN AUTO AS AUTO SHOWS ALL WX < 22k
416
FO IMPACT DRILL
LAND
COMPLETE CHECKLIST
TAKE TORCH NOTOC LOADSHEET
PROCEED TO CABIN AND RELAY EVAC COMMAND
EVAC FIRST AVAILABLE EXIT
REPORT TO EMERG SERVICES IF AVAIL
417
FO IMPACT DRILL
DITCH
COMPLETE CHECKLIST
FIT LJ AND TAKE TORCH
PROCEED TO CABIN OR AS DIRECTED BY CAPT
WHEN ALL ASSISTANCE RENDERED EVACUATE
418
RNP AR
PROC
BRIEF FROM QRH
DELAYED FLAP APP
2NM DESCENT PT APPROACHING GLIDEPATH
TERR VSD
ANP < RNP
LNAV
QNH AND TEMP
SPD WINDOW OPEN
LNAV VNAV
SET DA
300 < MISSED APP ALT SET MISSED APP ALT
DISENGAGE AP BY 135’ RA
FD ON TO LDG
419
GPWS
QRH MAN
CAUTION
CORRECT FLT PATH OR ACFT CONFIG
WARNING PULL UP
DISC AP
DISC ATHR
AGRESSIVELY MAX THR
SIMULT ROLL WINGS LEVEL AND PITCH 20 DEG
VERIFY SB RETRACTED
IF TERR REMAINS A THREAT PITCH PLI OR STICK SHAKER OR INITIAL BUFFET
DO NOT CHANGE GEAR OR FLAP CONFIG
MONITOR RA FOR TERR SEP
WHEN CLEAR TERR SLOWLY DECREASE PITCH ATTIT AND ACCEL
PM
VERIFY MAX THR
CALL OMISSIONS
MONITOR VERT SPD AND ALT
CALL ANY TREND TOWARDS TERRAIN
420
V1 CUT
300’
PAN CALL
MIN 300 FPM IF LESS MAY HAVE LEFT WHEELS DOWN
CESSNA192
MLW 192776
421
V1 CUT
400’
IDENTIFY THE PROBLEM
EITHER MEM ITEMS OR NO MEM ITEMS
CONSIDER CDP OR EO SID
422
JETT RATE
APPROX 1000 KG PER MIN
423
USING OPT FOR LANDING DIST CALC WITH A NON NORMAL AND GRADIENT
ENTERING NON NORMAL CANT SELECT GRADIENT
NEED TO CHECK WITHOUT NON NORMAL WHICH U CAN THEN SEE IF GRADIENT CAN BE MET OEI WHICH IS CONSIDERED MORE RESTRICTIVE THAN ANY OTHER NON NORMAL
424
2D APP
WHICH ALT TO SET
SET TO FAF
THEN SET MINIMA
300’ TO MINIMA SET MISSED APP ALT
425
CDP
DO U NEED TO CLEANUP TO FLAPS UP
YES
AS CDP PREDICATED ON FLAPS UP
IE NORMAL OEI GA CAN CLEANUP TO FLAPS 5 IF CLIMB GRADIENT AN ISSUE AND NEED TO FOLLOW CDP MUST CLEANUP TO FLAPS UP
426
WS
WHY ONLY ONE PRESS TOGA
AS ATHR ATTEMPTS TO GIVE U 2000 FPM
IF DESCENDING WILL END UP FULL THR IN AN ATTEMPT TO ACHIEVE 2000 FPM
427
AIRSPEED UNRELIABLE
MEM ITEMS
NOTE
GEAR UP PITCH ATTIT AND THRUST
GEAR UP ONLY
MAY NEED TO SEL GEAR UP IF AIRSPEED UNRELIABLE ON FINAL?
428
AIRSPEED UNRELIABLE
MEM ITEMS
NOTE
GEAR UP PITCH ATTIT AND THRUST
GEAR UP ONLY
MAY NEED TO SEL GEAR UP IF AIRSPEED UNRELIABLE ON FINAL?
429
CONTAINMENT CDP
STAY IN CONTAINMENT AREA UNTIL ABOVE MSA
430
508
STANDBY POWER
INOP ITEMS
AUOTHROTTLE
LNAV VNAV
FMC PREDICTIONS
FMC THR LIMITS
TAP
FLAPS SLATS
STAB TRIM
THR REV
AUTO SBDBRK
PACKS
HUD HF
TCAS GPWS TX WX RADAR EXTERNAL LGTS
WIPS WINDOW HEAT
431
508
CAT
NOT SENSED BY RADAR
JUNE TO AUG IN AUST > FL200
NEAR JETSTREAMS AND MOUNTAIN WAVES NEAR TROPOPAUSE
NEAR CORE OF JETSTREAM
432
508
INFLT START ENVELOPE
CERTIFIED AND GUARANTEED START
433
508
TURB PENETRATION SPEED
290 < 25k
310/.84 WHICHEVER IS LOWER >/ 25k
434
508
HOW TO MAKE CABIN PA WITHOUT DISTURBING CREW REST
PRESS 40
PA TO PAX AREA ONLY
435
508
DEFINE VARIOUS INTENSITY DESCRIPTIONS YOU WOULD USE WHEN REPORTING TURB
LIGHT
MODERATE
SEVERE UNCONTROLLABLE
436
508
CAN ATHR AND AP REMAIN ENGAGED DURING FLT THROUGH TURBULENCE
YES VS RECOMMENDED CLIMB DESCENT
VNAV AND ALT HOLD IN CRZ KEEPS SPD ON ATHR
437
508
HOW IS ACFT FLOWN DURING SEVERE TURBULENCE
AP AND ATHR ON
MAY NEED MANUAL THRUST IF EXCESSIVE THRUST CHANGES OCCURRING
WORSE CASE MAY NEED TO HAND FLY DONT CHASE SPEED TRY AND MAINTAIN A PITCH ATTIT
438
508
DUAL ENG FAIL STALL
MEM ITEMS
FUEL CONTROL SW BOTH CUTOFF THEN RUN
RAT SW PUSH AND HOLD FOR ONE SEC
439
DUAL ENG FAIL STALL
INDICATIONS FOR X START
IDEAL AIRSPEED
ENVELOPE AND X START BELOW N2
SPD > 270 KTS
MEM ITEMS AS SOON AS POSSIBLE TO TAKE ADVANTAGE OF HIGH ENGINE WINDMILL RPM
440
WILL APU AUTO START FOR DUAL ENG FAIL
YES
AS APU AUTO STARTS WHEN 3 OR MORE GENs OFFLINE
441
DUAL ENG FAIL
FOR STABILIZER MSG DO WE DO MEM ITEMS?
STAB LOSES POWER PART OF CONDITION STATEMENT SO YES DO MEM ITEMS
Check this
442
PARAMETERS TO DEFINE AIRPLANE UPSET
>25 DEG NOSE UP
>10 DEG NOSE DOWN
>45 DEG AOB
LESS THAN ABOVE BUT INAPPROP AIRSPEED FOR CONDS
OUTSIDE NORMAL PARAMETER +5/ -2.5
443
HUD UA SYMBOLOGY
MINIMISES AND POINTS TO HORIZON
ALWAYS ROLL TOWARDS SKY POINTER
PITCH -20 to +35 DEG
OR ROLL > 55 DEG AOB
444
GUIDELINES TO USING RUDDER
UA
GENERALLY SPEAKING DONT USE
USE MINIMAL IF NEEDED
MAY BE NEEDED TO INDUCE ROLL UA
445
RAPID DESCENT
PM DUTIES
EXT LGTS
ATC EMERG DESCENT
SQ 7700
CHK LSALT
1000/ 2000 TO GO
CABIN PA ATTENTION CABIN CREW EMERGENCY DESCENT
446
WHAT IS THE IMPORTANCE OF RCB
STOP REFLEX ACTION
ENSURE CORRECT ACTION TAKEN
447
UA
CORRECT PITCH RATE TO ENSURE G LIMITS ARE RESPECTED AND TO AVOID PAX INJURY
2.5 DEG PER SEC
448
INDICATIONS IN THE EVENT THAT THE CABIN PRESSURE CONTROL SYSTEM CPCS ENTERS DEGRADED MODE
EICAS LANDING ALT
449
FCTM
RAPID DESCENT
PF
MEM ITEMS
HDG TRK SEL
LOWER ALT MCP
FLCH
CLOSE THR LEVERS EXT SB
2ND GO FINESSE MCP
IF STRUCTUAL INTEGRITY IN DOUBT LIMIT AIRSPEED AND AVOID HIGH MAN LOADS
TARGET VMO MMO OR CURRENT SPD
NOTIFY ATC
2000 TO GO REDUCE SPD
1000 TO GO STOW SB
LRC OR 300 KTS
450
HOW WOULD A CABIN ALTITUDE VERSUS CABIN ALTITUDE AUTO PROC BE MANAGED
LOSS CABIN CONTROL VERSUS OUTFLOW VALVES MANUAL
451
RAPID DESCENT
WHAT PAs REQD
ONCE DESCENT STARTED
ATTENTION CABIN CREW EMERG DESCENT
@14k
FOLLOW UP DUTIES
452
WHAT ASSUMPTIONS ARE USED IN CALC DPD CPE
14k TO LIMIT OXY ENDURANCE (78 MINS) THEN 10k
453
IF U OBSERVE VOLCANIC ACTIVITY WHAT IS THE REPORT CALLED
PIREP
454
POTENTIAL SIGNS OF VOLCANIC ASH ENCOUNTER
ACRID ODOUR
AIRSPEED ISSUES
ENG SURGE
ST ELMOS
HAZE
PRESSURISATION
STATIC DISCHARGE
455
WHAT ACTIONS SHOULD BE TAKEN UPON RECOGNISING A VOLCANIC ASH ENCOUNTER
180 DEG DESCENDING TURN
REDUCE THR IF POSSIBLE
VOLCANIC ASH CHKLST
OXY IF REQD
ATHR OFF
START APU
MONITOR EGT
MONITOR AIRSPEED AND PITCH ATTIT
MAY NEED AUTOLAND DEPENDING FWD VIS FROM WINDSCREEN
456
WHAT OTHER SYS MAY BE IMPACTED BY VOLCANIC ASH
EQUIP COOLING
AIRSPEED ERROR
457
ENG FLAMEOUT
WITH
AIRSPEED UNRELIABLE
4 DEG PITCH 70%
NO THR ATTITUDE WOULD BE VERY DIFFERENT
458
CABIN ALTITUDE
MEM ITEMS
DON THE OXY MASKS
ESTABLISH CREW COMMS
CHECK CABIN ALT AND RATE
IF CABIN ALT UNCONTROLLABLE
PASS OXY SW PUSH TO ON AND HOLD FOR ONE SEC
WITHOUT DELAY DESCEND TO LSALT OR 10k WHICHEVER IS LOWER
TO DESCEND
THR LEVERS IDLE
EXT SB
IF STRUCTURAL INTEGRITY IS IN DOUBT LIMIT AIRSPEED AND AVOID HIGH MAN LOADS
DESCEND VMO MMO
459
NOSE HIGH
PROC
RCB
DISCONNECT AP AND ATHR
PUSH NOSE DOWN
ROLL WINGS LEVEL
POWER THR AND SPDBRK DOWN
RECOVER HAPPY PLACE
TRIM AND THRUST
REESTABLISH AUTOMATION
460
NOSE LOW
PROC
RCB
DISCONNECT AP AND ATHR
PUSH RECOVER FROM STALL IF NEEDED
ROLL
POWER THR IDLE AND SPDBRK AS REQD
RECOVER
HAPPY PLACE
THRUST AND TRIM
REESTABLISH AUTOMATION
461
HIGH ALT EFFECT ON ENG RELIGHT TIME
SLOW
APPROX 2-2.5 MINS
462
DUAL ENG FAIL
PACKS
PACKS INOP UNTIL APU STARTS AND APU GENs COME ONLINE
463
STABILIZER
MEM ITEMS
PM AREA OF RESP
STAB CUTOUT SW BOTH CUTOUT
DO NOT EXCEED CURRENT AIRSPEED
464
STABILIZER
MEM ITEMS COMPLETE
PITCH TRIM AVAIL?
IN NORMAL MODE YES
STAB DOESNT MOVE BUT PITCH TRIM FOR ELEV
465
NON NORMAL
HOW TO SET VREF 30 + 20
DO TOGETHER AS A CREW
SEL FLAP 20 AND ADD 20 NEED TO INSERT MANUALLY
466
SHORT SECTOR TIPS
RTE 2
USE RTE 2
CANT LOAD ARR RTE 1 LOAD RTE 2 AND BRIEF ON GROUND
BRIEF ANY CHANGES AIRBORNE
467
HOW TO SET REMINDERS
COMM MENU
COMPANY
CAN SET ALT/ TIMES AND ATTACH REASONS
468
HOW MANY FIX PGs?
4
CAN PUT ALT AND TIMES ALSO
469
AIP
TIMINGS
HOLDING AT FIX
CAN BE ONE MIN EARLY NOT LATE
ETA AT FIX
CAN BE 30 SECS EARLY NOT LATE
470
FIRE ON GND
ANNUN VS UNANNUN
ANNUN USE ECL
UNANNUN USE QRH
ALSO CONDITION STATEMENT
ENG FIRE IS FIRE DETECTED
FIRE ON GND IS FIRE IS DETECTED OR OBSERVED
471
EVAC CHECKLIST
READ AND DO ALL
WILL GET DARK STORM LGT ON
472
EO SID
OK TO LOOK AT
TAKE BRANCH PT OFF LEGS AND PUT ON FIX PG
473
SPDs ON LEGS PG
NEED TO BE MAGENTA TO BE ACTIVE
474
OEI GA
PROC
IF NOT FOLLOWING CDP DO NOT NEED TO CLEANUP
DO CESSNA
AFTER FINAL FLAP COVERS POSS FUEL IMBALANCE CHECKLIST
475
ISFD
PFD
WHEN DO THEY PICKUP GS
ISFD WITHIN 110 DEG
PFD WITHIN 90 DEG
476
R35L R EO SID
SCEL
TIPS
LONG CDP
MSA 20k
CONSIDER LOOKING AT R35 LR APPROACHES AND FIND POSN TO HOLD
ALLOWS LESS TRACKING AND LOWER ALT TO HOLD APPROX 6000’ INCASE UNCONTROLLABLE FIRE
477
TR TIP
VISUAL APP
ATC RWY INSIGHT
HINT TO GET READY FOR TURN
F5 AND REDUCE SPD
LOOK AT GLS AND LOAD APP AND GET HEIGHT TO AIM FOR
VS TO THAT HEIGHT USE ISFD FOR GS INFO AND TURN FINAL ARM APP
AND LAND 30 KTS XWIND FOCUS
478
CLEARED TO TAXI
PF
SEL WX
CURSOR OVER VNAV
LINING UP
HUD UP
RANGE UP
479
RNP AR APP
FIX PG
IAF ON FIX PG
2 NM RING
APP GLIDEPATH CALL PF SET DH
TALQS CHECK
480
GPWS
AFTER RECOVERY
GIVE YOURSELF 2000’ ABOVE CURRENT ALT
LEVEL OUT MANAGE THE HIGH INERTIA
GET ON SAME PG USE GA PROC
GA FLAPS 20
THRUST SET POSITIVE RATE GEAR UP
FMA FMA
ROLL MODE
SET HIGHER SPD AND CLEANUP
FLCH OR VNAV CHECK CLB THR
481
507 LDG
GOOD SESSION
LAST LDG POOR
ACFT SETUP PERFECTLY
WORK HARDER SCANNING END RWY
FLARE RATE TOO SLOW
482
DUAL ENG FAIL
FUEL CONTROL SW
L AND R TO CUTOFF
WAIT 2 SECS
THEN L AND R TO RUN
483
UPSET RECOVERY
NOSE HIGH TIPS
KEEP NOSE BELOW HZN LONGER
USE ALT IF AVAILABLE TO ACCEL
INSTEAD OF WHEELS ON HZN AND SLOW ACCEL RATE
484
UPSET RECOVERY
NOSE LOW TIPS
DONT NEED SB UNLESS FAR INTO OVERSPEED BAND
MINOR EXCURSIONS INTO OVERSPEED ARE OK
IN RECOVERY ENSURE SB STOWED
485
DUAL ENG FAIL
VOLCANIC ASH
TIPS
LEFT SEAT WILL BECOME PF
CRM BE SLOW AND METHODICAL STAY PATIENT
486
VNAV CLB PG ON DEP
FOR CLIMB AT HEAVY WT
SOME DISCREPANCY BETWEEJ VREF 30 + 80 AND MAX ANGLE ON VNAV CLB PG
USE MAX ANGLE AS LIKELY TO BE BETTER MIN MAN MARGIN
487
SEL CLB THR HOW
ON CLIMB
INIT REF WILL BE FIRST PG
488
PA
TO AVOID CREW REST
46?
PRESS CAB WAIT FOR DIAL TONE THEN DIAL ON CAB PG TCP NORMALLY USE OBS TCP
489
DUAL ENG FAIL
STABILIZER MEM ITEMS
SUGGESTED NOT TO DO
CHECKLIST CORRECTS CONFIG IF REQD
490
VOR APP
ENSURE USING DME
491
UPRT
PUSH
ROLL
POWER
RECOVER
492
AIRBUS HINTS FOR 787
LET GO OF CONTROLS
SEE IF ITS TRIMMED
RELAX HANDS IF TENSE
493
LOSS ALL HYD
RAT FLT CONTROLS
ELEC ACTUATED STABILIZER AND 2 SPOILER PAIRS ALLOW PILOT CONTROL OF PITCH AND ROLL USING THE PRIMARY PITCH TRIM SW, ALTERNATE PITCH TRIM SW AND CONTROL WHEEL
FLAPS DRIVE VREF 30 + 40 LDG MLW AB 4 3080 M REQD
SLATS DRIVE VREF 30 + 40 LDG MLW AB 4 2893 M REQD
494
L/ R HYD SYS
FLT CONTROLS
THR REV
R AND L WING SPOILERS
495
C HYD SYS
FLT CONTROL
LDG GEAR ACTUATION
LE SLATS
NOSE GEAR STEERING
L AND R WING SPOILERS
TE FLAPS
496
IDENTIFY HYD NON NORMALS WITH CROSSWIND LIMITATIONS
DOUBLE HYD FAIL
ALL 20 KTS XWC
497
CONSIDER THE EFFECTS OF LOSING THE PRIMARY HYD PUMPS IN L OR R SYS
WOULD ALL SYSTEMS OPERATE NORMALLY?
WHAT ABOUT C HYD?
ELEC DEMAND PUMPS
OPERATE IN HIGH WORKLOAD TO ASSIST ENG PUMPS
C SYS ONE PRIMARY ELEC ONE DEMAND ELEC PUMP
498
INCREASED LDG DIST MAY RESULT FROM HYD FAIL
IS LDR FROM OPT FACTORED
YES FACTORED
499
IF NOSE WHEEL STEERING IS AFFECTED WHAT ADDITIONAL FACTORS NEED CONSIDERATION? CAN ACFT BE TAXIIED?
POSSIBLY DUE TO NOSE GEAR ISOLATION VALVE
ID SUGGEST HAVE TUG READY JUST INCASE
500
IF LDG GEAR IS EXTENDED USING ALTN GEAR EXT CAN IT BE RAISED
NO UNLESS C HYD PRESS
501
IF FLAPS EXT USING SECONDARY DRIVE SYS CAN THEY BE RETRACTED?
WHEN WOULD U BEGIN FLAP EXT
EARLY
F UP TO F20 2.5 MINS
YES RETRACTED USING SEC MODE AND FLAP LEVER
502
ETOPS
WHICH HYD FAIL REQUIRES LAND NEAREST AVAIL APT
DUAL HYD FAIL
SINGLE IS OK
503
DESCRIBE WHAT HAPPENS WHEN ALTN LDG GEAR SYS IS USED TO EXT GEAR.
WILL DOORS CLOSE?
IS THERE MAIN GEAR TILT?
DEDICATED DC POWERED ELEC HYD PUMP AND C HYD SYS FLUID TO EXT LDG GEAR
ALTERNATE EXTEND ISOLATION VALVE
SEL DOWN ON ALTN GEAR SW RELEASES ALL DOORS AND UPLOCKS
LDG GEAR LEVER HAS NO EFFECT
DOORS REMAIN OPEN
NO GEAR TILT
504
HOW ARE FLAPS AND SLATS POSITIONED IN PRIMARY MODE? WHAT ABOUT SEC MODE?
FLAP LEVER FOR BOTH
505
HOW ARE ALTN SLATS FLAPS POWERED?
ELEC WHEN NNC DIRECT USE
506
WHAT FAILURES CAN CAUSE THE FLAPS AND SLATS MODES TO ENGAGE IN SEC MODE
WHAT EICAS WOULD U EXPECT TO SEE
C HYD SYS FAIL
CONTROL SURFACES <50% NORMAL HYD RATE
FLAP OR SLAT DISAGREE
UNCOMMANDED FLAP OR SLAT MOTION
FLAP OR SLAT PRIMARY CONTROL FAILURE
PRIMARY MODE FAILS TO MOVE FLAPS AND SLATS
507
WHAT IS THE DIFF BETWEEN SLAT AUTO GAP AND SLAT PRE GAP
AUTO GAP PRIMARY MODE
PRE GAP SEC MODE
508
WHAT DOES A MAGENTA FLAP SEL NUMBER AND LINE MEAN? WHAT ABOUT GREEN?
MAGENTA IN TRANSIT TO SEL POSN
GREEN SLATS/ FLAPS IN COMMANDED POSN
509
CAN AP AND ATHR BE USED FOR ALL FLAP NON NORMALS?
YES EXCEPT FOR FLAPS AND SLATS FAIL NEED MAN THR
DONT SET NEW COMMAND SPEED UNTIL FLAPS ACTUALLY IN POSN
510
SLAT AUTO GAP
PRIMARY MODE
WHEN SLATS MIDDLE POSN AND AIRSPEED < 240 KTS @ HIGH AOA AUTO GAP FULLY EXTEND THE SLATS TO INCREASE WING CAMBER THUS INCREASING LIFT AND MARGIN TO STALL
SLATS RETURN TO MIDDLE POSN AFTER AOA DECREASES
AUTOGAP TRIP THRESHOLD A FUNCTION OF AOA/ AIRSPEED AND FLAP POSN
511
SLAT PREGAP
SEC MODE
AS SYS TOO SLOW FOR AUTOGAP REQUEST. SLATS AUTO MOVE FULLY EXT POSN FROM MIDDLE POSN WHEN FLAP LEVER IS NOT UP AND AIRSPEED <240 KTS
SLATS REMAIN IN EXT POSN UNTIL FLAP LEVER IS IN UP POSN OR AIRSPEED >240 KTS
512
FLAP PRIMARY MODE
AUTOGAP
AND
FLAP LOAD RELIEF
513
FLAP SEC MODE
SLATS AND FLAPS CONTROLLED SEPARATELY AND CAN BE POSITIONED BY HYD OR ELEC MOTORS
IF SLATS HYD CONTROL FAILS FLAPS STILL DRIVEN HYD BUT SLATS NOW POWERED ELEC
SEC MODE USES FLAP LEVER MAX F20
514
ALTN FLAP
3 POSN ALTN FLAPS EXT AND RETRACTS SLATS AND FLAPS
FLAPS AND SLATS EXT SIMULTANEOUSLY BUT SLAT RETRACTION INHIBITED UNTIL FLAPS ARE UP
ALTN LIMITED SLATS MIDDLE POSN AND F20
ASYMMETRY AND UNCOMMANDED MOTION PROTECTION/ SLAT AUTO GAP AND PRE GAP/ FLAP AND SLAT LOAD RELIEF NOT AVAIL ALTN MODE
515
FLAPS ONE
SLAT EXT MID RANGE POSN
NO FLAP
516
FLAPS 5-20
SLATS REMAIN MID POSN
FLAP EXT SEL POSN
517
F25
SLATS FULLY EXT
FLAPS DO NOT MOVE
518
F30
SLATS REMAIN FULLY EXT
FLAPS EXT TO 30
519
AIRSPEED UNREL
MEM ITEMS
AP DISC SW PUSH
ATHR ARM SW BOTH OFF
FD SW BOTH OFF
SET FOLLOWING GEAR UP PITCH ATTIT AND THR
FLAPS EXT 10 DEG 85% N1
FLAPS UP 4 DEG 70% N1
520
AIRSPEED UNREL
WHAT HAPPENS TO FLT CONTROL MODE
SEC OR DIRECT MODE
521
INDICATIONS OF A CARGO FIRE
FIRE BELL
MASTER WARN
EICAS
CARGO FIRE WARN LGTS
522
HOW MANY CARGO FIRE EXT ARE THERE?
7 BOTTLES
2 HIGH SPEED AND 5 SLOW
523
CARGO FIRE BOTTLE
DISCHARGE SEQ?
IN FLT
2 IMMEDIATELY THEN > 15 MINS 5 AT METERED RATE
IF LANDING WITHIN 15 MINS 1 BOTTLE ON LDG
ON GND
3 BOTTLES 3RD SLOWER RATE
524
HOW LONG SHOULD CARGO FIRE SUPP LAST?
EDTO 330 MINS
MOST LIMITING CARGO FIRE SUPPRESSION SYS TIME IS 300 MINS
525
ONCE ACFT HAS LANDED WHAT SHOUKD BE DONE BEFORE ANY CARGO DOOR IS OPENED
ALL PAX AND CREW OFF
FIRE FIGHTING EQUIP NEARBY
526
HOW IS EVAC SIGNAL SIREN CANCELLED ON THE FLT DECK?
PRESS MASTER WARN
527
FO IMPACT DRILLS
LAND
COMPLETE CHECKLIST
TAKE TORCH NOTOC LOADSHEET
PROCEED TO CABIN AND RELAY EVAC COMMAND
EXIT FIRST AVAILABLE EXIT
REPORT TO EMERG SERVICES IF AVAIL
528
FO IMPACT DRILLS
DITCH
COMPLETE CHECKLIST
FIT LJ AND TAKE TORCH
PROCEED TO CABIN OR AS DIRECTED BY CAPT
WHEN ALL ASSISTANCE RENDERED EVACUATE
529
TAKEOFF DISPATCH
LANDING DISPATCH
NEED TO USE ACTUAL CONTAMINANT AND DEPTH INFO
530
RWY CONTAMINATION DEST AND OR ALTN
ON DEP NEED TO DO LANDING DISPATCH CALC
WET * 1.92 DRY * 1.67
LANDING ENROUTE * 1.15
USE RWY COND 2 TO ASSESS
NOT GROOVED OR PFC ANY RAIN MOD+ TREAT AS CONTAMINATED
LANDING ENROUTE CAN USE UNFACTORED FOR NON NORMALS
531
SKR CREDIT
SKID RESISTANT FUNCTIONALITY
NOTAM MAY NEGATE
MAY NEED SEL NOTAMS - GROOVED RWY - NO CREDIT
532
PRE FLT
DEST AND OR ALTN CONTAMINATED
LDG DISPATCH AND LDG ENROUTE CALC
TAKE LOWEST LDG WT
IF PREDICTED LW ABOVE AND FORECAST TO BE CONTAMINATED NEED HOLDING OR ALTN FUEL
533
LANDING
SLIPPERY WHEN WET
RCAM 3
534
GROOVED HEAVY RAIN
NON GROOVED NON PFC MOD OR MORE RAIN
RCAM 2
535
CONTAMINATED RWY
TAKEOFF NOT RECOMMENDED
>15 MM SLUSH/ STANDING WATER
> 30 MM WET SNOW
> 100 MM LOOSE DRY SNOW
IF RWY CONTAMINATED CAN USE FIXED DERATE BUT NO ATM
RCAM ONLY USED INFLT LANDING ENROUTE CALC
536
CONSIDER COMMS THAT WOULD BE RELEVANT BETWEEN FLT CREW AND CABIN CREW IN NON ROUTINE DISEMBARKATION OR EVAC
ALERT PA
POSS UPGRADE TO EVAC PA
NITS BRIEF
NATURE EMERG
INTENTIONS
TIME AVAIL
SPECIAL CONSIDERATIONS OR REQMTS
537
WHAT ARE THE POTENTIAL THREATS OF AN EVACUATION WITH A CREW MEMBER INCAPACITATED AND HOW COULD THIS BE MANAGED?
TASKS MISSED
BE SLOW AND METHODICAL
DO BOTH ROLES
VERBALISE AS NORMAL
538
510
PREFLT PROC
MAKE YELLOW
539
510
MEL ITEMS
A
B
C
D
A SPECIFIED
B 3 DAYS
C 10 DAYS
D 120 DAYS
540
510
DEP SFO HNL LAX
DEPARTING OVER WATER AFTER 12 NM CAN ACCEL NORMAL ECON CLB SPD
OVER LAND CAN ACCEL MIN SAFE SPEED > 250 KTS < 10k ADVISE ATC ‘MINIMUM SAFE SPEED 260 KTS’
541
510
WHEN IS WAKE TURB HEAVY REQD IN RADIO TRANS
USA
UNDER RADAR AND ALL TERMINAL FREQS
542
USA
PDC PROCEDURES
VIA ACARS NO READBACK
VOICE READBACK TX CODE AND ALT RESTR
543
USA
SIDE STEP APP COMPANY REQMTS
NOT LESS THAN 1500’ UNLESS CHARTED AS SUCH
PROGRAM RTE 2
ENSURE GOOD FLT PATH MGMT
ENSURE MISSED APP PROC UNDERSTOOD
BE PREPARED TO DECLINE IF WORKLOAD IS HIGH/ LDA INSUFF/ STABLE APP PARAMETERS UNABLE TO BE MET
WILL LOSE 500’ ACTIVATING RTE2
544
USA
UNIQUE RADIO PHRASEOLOGY
CLEARED RYDRR ARRIVAL CAN SET LOWEST ALT
545
USA
UNIQUE RADIO PHRASEOLOGY
CLEARED RYDRR ARRIVAL CAN SET LOWEST ALT
546
USA
TERPS DIFF
CIRCLING AREA 4 NM RADIUS OBSTACLE CLR 400’ MAX 165 KTS
MISSED APP GRADIENT 3.3 % 200’/ NM
TERPS BOTTOM LEFT JEPP CHART 185 KTS FOR TURN MISSED APP
547
MEL 49-11-01
APU INOP
EDTO REDUCED TO 180 MINS
NIL POLAR OPS
AGCU APU GEN CONTROL UNIT
VFSG VARIABLE FREQ ENG STARTER GENERATOR
548
FUEL BURN FOR 787
HOW MUCH FOR 15 MIN HOLDING?
APPROX 5T AN HOUR
1.3 T FOR 15 MIN HOLDING
549
MIN OIL QTY FOR DEP
12 L PLUS 0.25L PER FLT HOUR
550
ANY RESTR ON MIXING JET A AND JET A1 FUEL
NORMALLY ENGINEERING FUNCTION
USE -40 DEG C FREEZE PT CONSERVATIVE
551
TAXI SPEED
20 KTS STRAIGHT
10 KTS TURNS
MAX 30 KTS LONG STRAIGHT TAXIWAYS
552
TAXI
PAVEMENT WIDTH
WHEEL TRACK 9.8 M WIDE
MIN WIDTH 23 M?
553
TAXI
WINGSPAN
60.1 M
198 FT
554
STERILE FLT DECK FOR DEP
DOOR CLOSED TO SEATBELT SIGN OFF
NO CONTACT
TAKEOFF THRUST TO GEAR UP
555
SHARED MENTAL MODEL FOR TAXI
PM BRIEF CLEARED TAXI ROUTE
PF CONFIRM AND EXPLAIN THEIR INTENTIONS
556
REVIEW TAKEOFF CHANGE CONSIDERATIONS CHECKLIST AND HOW TO MANAGE IT
STOP ACFT OUT OF THE WAY
CAPT BECOMES PF
FOLLOW CHECKLIST
RESET FD
FO LOADS FMC AS PER PREFLT
557
REVIEW BRAKING TECHNIQUE
DONT RIDE BRAKES
ONE LONG APPLICATION
558
HOW COULD YOU USE CLIMB THR SELECTION TO IMPROVE THE CLIMB RATE WHEN IN TURB AFTER TAKEOFF
INIT REF
FIRST PG THR LIM
SEL CLB THR AND MAX RATE UP + 60 TO GET ABOVE TURB
559
CONSIDER HOW U MIGHT RESPOND TO AN EICAS STATUS MSG. WHAT EFFECT WILL THIS HAVE ON THE FLT?
NO EFFECT LET MAINT KNOW AT DEST
STATUS INHIBITED LIFTOFF PLUS 30 MINS
560
HOW CAN U CALC BEST ANGLE AND BEST RATE OF CLIMB? ARE THEY SELECTABLE?
MAX ANGLE VNAV CLB PG
BEST RATE VREF 30 + 140 OR UP + 60
561
CONSIDER ACTIONS IN RESPONSE TO NON NORMAL DURING CLIMB
DEPENDING ON NATURE OF PROBLEM CONSIDER EARLIER LEVEL OFF AND NOT ACCEL ACFT
562
TURB PENETRATION SUPP PROC
290 < 25k
310/.84 WHICHEVER LOWER >/ 25k
KEEP ACFT CLEAN AS ACFT CAN HANDLE HIGHER GUST LOADS
CLIMB DESCENT CONSIDER VS
CRZ VNAV PTH AND ALT USE SPD ON ATHR
DISC ATHR FOR LARGE THRUST CHANGES
SEVERE TURB IF MAN FLT REQD DONT CHASE ALTITUDE SET ATTIT AND TRIM TURB SPD
563
TURB PENETRATION SPDS
WHY WERE THESE SPEEDS CHOSEN?
SPEEDS PROVIDE AMPLE PROTECTION FROM STALL AND HIGH SPD BUFFET WHILE ALSO PROVIDING PROTECTION FROM EXCEEDING STRUCTURAL LIMIT
564
WHEN DO U AND DONT U EXPECT CALLBACK FROM TURBULENCE PA
AFTER CABIN PREP PA NOT REQD
FOR TURB PA MAY NOT GET CALLBACK IF CSM CSS WEDGED THEMSELVES IN SOMEWHERE
565
TOC DUTIES
PM
VERIFY RNP AS NEEDED
> 10k CPDLC LOGON
SEATBELT SIGNS AS NEEDED
BOTH
QNH AT TRANSITION ALT
PM
FUEL IN CENTER MSG TURN CENTER PUMPS ON
WHEN FUEL LOW CENTER TURN PUMPS OFF
CHECK CARGO TEMP FOR LIVE ANIMALS 20 DEG
BEFORE TOD MODIFY ACTIVE ROUTE FOR ARR AND APP
566
PREFERRED OPTION FOR DEALING WITH OVERSPEED DURING CRZ
USE SB
567
FAM DESCENT SPEEDS
ECON 280-310 KTS
+/- 10 KTS
250 < 5000’ AGL
568
HOW WOULD U DEAL WITH AN ACFT APPROACHING VMO MMO ON DESCENT
USE SB
REDUCE ROD
569
STERILE FLT DECK REQMTS FOR LANDING
CABIN PREP PA TO TERMINAL
NO CONTACT
GEAR DOWN TO ACFT STOPPED OR TURNS OFF RWY
CABIN PREP 20K AGL START CLOCK GIVE CABIN 10 MINS
570
AFDS MODES FOR DESCENT
VNAV SPD
IDLE THR AND PITCH FOR SPEED
VNAV PTH
PITCH FOR PATH MAY NEED USE SB OR INCREASE THR
787 MAINTAINS 10 KTS ABOVE SEL SPD
571
WHAT IS YOUR DECISION MAKING PROCESS DEALING WITH REQ FROM ATC ON DESCENT
TRY AND ACHIEVE
IF UNABLE SAY NO
572
WHAT DESCENT PROFILE AND GATES DO U USE
4 * HT
10k 40 NM
20k 80 NM
573
HOW MUCH FUEL DO U EXPECT TO BURN ON DESCENT
MINIMAL 500 KG
574
WHAT GATES WILL YOU USE FOR CONFIGURING THE ACFT ON APP
FLAPS 5 OR 10 INT LOC FOR <185 KTS
RAD ALT ALIVE GR DOWN F20 ARM SB
@2000’ AGL LDG FLAP
575
REQMTS OF DELAYED FLAP APP
ALL EXCEPT 2D OR NON NORMALS
576
ENG OUT TAXI IN AFTER LANDING PROC
APU MUST BE OPERATING
3 MIN COOLDOWN STARTS ON LANDING FOR IDLE REV OR OUT REV
CONSIDER MAN OR UPHILL ETC
APU IS RUNNING AND BOTH APU GEN OPERATIONAL
FLT CONTROL TEST COMPLETE (45 SECS AFTER SB AND FLAP RETRACTION)
THR LEVER CLOSE
FUEL CONTROL SW CUTOFF
IF ACFT STOPS AND HIGH BREAKAWAY THRUST CONSIDER REQ A TOW
577
MEL APPLICATION
CAPT
WIEN ACCEPTING MEL CAPT MUST CONSIDER IMPLICATIONS OF INCREASED WORKLOAD AND WX CONDS FOR DEP/ ENROUTE AND DEST
578
APPLICATION MEL
DEFECTS PREFLT
CONSULT ENG
579
APPLICATION MEL
DEFECTS AFTER DOOR CLOSED
AFTER DOORS CLOSED AND BEFORE TAKEOFF
CREW COMPLETE NNC
CONSULT MEL TO DETERMINE IF DISPATCH RELIEF AVAIL
IF NOT LISTED IN MEL TAKEOFF PROHIBITED
AT NON MAINT PORTS CAPT CAN APPLY MEL AT ANY TIME DURING TRANSIT
AT MAINT PORT CAPT MAY APPLY MEL AFTER DOORS CLOSED. MEL CAN ONLY BE APPLIED IF NO SPECIFIC M PROC. IF CAPT DOES APPLY MEL ANY PLACARD REQMTS AND APPLICABLE PROC MUST BE ACTIONED BEFORE TAKEOFF
580
PROC WHEN FLT CREW APPLY MEL
NOT FOR M ITEMS
CONTACT MOC AND CHECK WHICH MEL AND MOC AUTHORITY NUMBER
E LOG
ENSURE MEL PROVISOS COMPLIED WITH
PLACARD
ENSURE MOC AUTHORITY NUMBER RECEIVED
581
GND POWER ENG START
POSS SIGN LOAD SHEDDING FO SIDE
ASVISE CABIN CREW CABIN ITEMS LOADSHED
582
ENG CROSS START
OPERATING ENG N2 5% > IDLE
IF N2 ON RUNNING ENG >81% ONE STARTER AND INCREASED START TIME
583
KUSA
DEP LAX DFW JFK SFO
LOGON KUSA DURING PREFLT NORMALLY ACTIVE ETD -30
CHECK UPLINK AND LOAD FMC ANY SID DELETED
584
VISUAL APP
MISSED APP
TURN TOWARDS RUNWAY
FOR SYD
FOLLOW MISSED APP INSTRU APP
585
SIDE STEP APP
MUST BE ON REQD VIS APP PATH BY 1000’
MAN COMPLETED BY 500’
<1500’ DONT ACCEPT
CONSIDER WHICH MISSED APP YOU WOULD FOLLOW
586
VISUAL APP
USA VERSUS AUST
USA CIRCLING AREA 4 NM
AUST 5.28 NM
587
VISUAL APP
NGT
WITHIN 30 NM
5K VIS
CLEAR OF CLOUD
IN SIGHT OF GND OR WATER
NOT BELOW LSALT MSA UNTIL
5 NM (7NM ILS GLS) ON CENTRELINE AND NOT BELOW ON SLOPE PAPI
10 NM (14 NM 16L 34L SYD) NOT BELOW ILS GLS GLIDEPATH WITH LESS THAN FULL AZIMUTH DEFLECTION
588
VISUAL APP
DAY
WITHIN 30 NM
5K VIS
CLEAR OF CLOUD
IN SIGHT GND OR WATER
CAN DESCEND 500’ NON POP OR 1000’ POP
589
USA
SPD FOR MISSED APP
185 KTS
FOR TURNING DEP AND TURNING MISSED APP
WORKS WELL FOR POTENTIAL HOLDING <6k HOLD SPEED MAX 200 KTS
590
USA
CLEARED FOR APP
DESCEND VIA ARR
CLEARED VIA APP IS FOR LATERAL TRACKING NOT VERTICAL
DESCEND VIA INCLUDES DESCENT ALT CLEARANCE
591
USA
ON FINAL ATC REQ TO SIGHT TRAFFIC
CAUTION IF U SIGHT TFC MAY THEN HAVE OWN SEP MAYBE DONT SAY SIGHTED
592
INTO HNL
LAHSO
TO ATC UNABLE LAHSO
593
USA METAR
LOOKUP DECODE
594
USA
110 W
DEPRESS ROUTE ESCAPE
595
USA
LOW VIS OPS
800’ / 2 SM
596
QRH
APP SUMMARY
DO EVERY APP
597
USA
GA FROM SIDESTEP
DONT USE RTE2
NEED TO FOLLOW ORIGINAL MISSED APP
DISC AND HAND FLY USE HUD
598
TOC PROC
TROUSER
TCAS BELOW
RADAR PF +1 PM 0
OVERHEAD PANEL
UPLINK WINDS AND FDA
SYS REVIEW
EDTO WX + FIX
REMINDERS CREW REST
599
SHORT TRIP CHARTS FOR FUEL TO DIVERSIONS QRH
WILL CALC FUEL LESS THAN DIVERSION DATA
MAY PREVENT DIVERSION
600
TAXIING
PF
VISUAL CUES
R TURN
CENTRELINE TOP L IPAD
L TURN
CENTRELINE HDG BUG
STRAIGHT INSIDE LEFT KNEE
601
PM
LDG CHECKLIST
WHEN SEL LDG FLAP
BRING UP LDG CHECKLIST STRAIGHT AWAY
602
XWC LANDING
REMEMBER FLARE FIRST
THEN STRAIGHTEN ACFT
603
STALL RECOVERY BEYOND CRIT AOA
PUSH
ROLL
POWER THR AND SB
RECOVER
KEEP NOSE BELOW HZN
AS SPEED INCREASES 1/2 WAY THROUGH AMBER BAND INCREASE THR
WHEN LOTS MARGIN HAPPY PLACE
THR AND TRIM
REENGAGE AUTOMATION
604
STALL
APP CONFIG YBCS
PUSH
ROLL
POWER THR AND SB
RECOVER
HAPPY PLACE
MAYBE TERR AND NEED TURN
PITCH 10 DEG THR 85%
THEN HAPPY PLACE ONCE CLEAR TERR
REENGAGE AUTOMATION
605
SMOKE/ FIRE AND FUMES
GO TO REMOVAL AT ANY TIME FIRE/ SMOKE BECOMES GREATEST THREAT
ECL PROCEEDS TO TURN OFF EQUIP TO POSS STOP CAUSE SMOKE ETC
606
SMOKE/ FIRE AND FUMES
OXY MASK USE
ANY SIGN OF SMOKE OR FUMES IN COCKPIT
TO PURGE SMOKE/ FUMES USE 100% OXY UNDER POSITIVE PRESS
607
QUESTIONS TO ASK CABIN CREW
SMOKE/ FIRE AND FUMES
LOCATION FWD OR AFT OF WING
SMELL
HOW MANY ROWS AFFECTED?
PIECE OF EQUIP?
608
WHAT IS AN IMMEDIATE LANDING?
IMMEDIATE DIVERSION TO A RUNWAY
SEVERE SITUATION - OVERWEIGHT LANDING/ TAILWIND LANDING/ OFF AIRPORT LANDING OR DITCHING
609
UNCONTROLLABLE FIRE OR FUMES WHAT ALT DO U DESCEND TO
POSS LSALT MSA
DIVERT TO A RUNWAY OR DITCH?
LOCATION AND INTENSITY OF FIRE A CONSIDERATION
DESCEND AND REASSESS CABIN REGULARLY TO SEE NEED FOR IMMEDIATE LANDING
610
NNC DITCHING
JETTISON FUEL TO REDUCE WT WHICH REDUCES VREF
= LOWER TOUCHDOWN SPEED
<5000’ DEPRESS ACFT
GPWS OVERRIDE
611
AEPM DITCHING
NITS BRIEF CSM
COORDINATION WITH CABIN
CAPTS PA FROM QRH
612
UNCONTROLLABLE FIRE
CABIN CREW
REMEMBER BASIC FIRE DRILL AEPM
MAY NEED TO GET CABIN CREW TO ARRANGE FOR ALL CREW TO FIGHT FIRE
WAKE-UP CREW
ALL AVAIL FIRE EXT
SHORT TIMEFRAME TO CONTAIN FIRE
613
STICK SHAKER
5-7 % < STALL
614
COLD WX COREECTIONS
IN WX APP
USE FOR POLAR OPS TO ADJ GRID MORAS
615
FAM
DIGITAL TERRAIN METHOD
VALID 8NM
ONLY IN LNAV THOU SO ON TRK IN HDG SEL NOT VALID
616
VNAV
EO ALTS
HVY WTS OPT ALT -14
LGT WTS OPT ALT -13
EO SPD
AMBER + 10
