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787 > FFS LEARNINGS > Flashcards

FFS LEARNINGS Flashcards

1
Q

MTOW

A

254 692 KG

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2
Q

MLW

A

192 776 KG

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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

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4
Q

TRIM REFERENCE SPEED

A

SPEED WHERE ACFT EVENTUALLY STABILISE IF NO CONTROL COLUMN INPUTS

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5
Q

EFFECT PILOT TRIM INPUTS

A

PFC MOVES ELEV TO ACHIEVE TRIM CHANGE, THEN MOVES STABILIZER TO STREAMLINE THE ELEV

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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

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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

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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

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9
Q

OPTIMUM EYE POSITION AND RUDDER PEDAL CONTROL

A

EYE BOX FOR HUD
RUDDER PEDAL WHERE U CAN APPLY FULL RUDDER AND MAX BRAKING

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10
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

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11
Q

POSN OF NOSE WHEEL AND MAIN GEAR

A

NOSE WHEEL
2.7 M BEHIND

MAIN GEAR
28.6 M BEHIND

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12
Q

ACFT WINGSPAN

A

60.1 M

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13
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

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14
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

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15
Q

DEFINE STABILISED THRUST

A

MAIN THING IS SYMMETRICAL
<2 SECS OTHERWISE MAY REDUCE TAKEOFF DIST AVAIL

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16
Q

WHEN DOES RUDDER BECOME EFFECTIVE

A

40-60 KTS

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17
Q

CONSIDERATIONS FOR LIGHT TOW WITH AFT CG

A

LIGHT FWD PRESS TO 80 KTS
INCREASES NWS EFFECTIVENESS

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18
Q

IF LNAV VNAV NOT USED FOR DEP WHAT ROLL PITCH MODE WOULD U USE

A

TOGA TOGA
@400’ HDG SEL
@1000’ FLCH

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19
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

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20
Q

ON TAKEOFF

SECOND PUSH TOGA AIRBORNE

A

REMOVES TO AND CLB DERATES
50-400’ TOGA ROLL MODE
>400’ TOGA ROLL AND PITCH

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21
Q

HOW DOES ROTATION TECH VARY WITH DIFF FLAP SETTINGS

A

NO CHANGE

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22
Q

EFFECT ON TAKEOFF PERF OF SLOW LATE ROTATION

A

REDUCES PERF
INCREASED TIRE SPEED

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23
Q

BENCH SYMBOL ON HUD

SQUARE—————SQUARE

A

AOA LIMIT SYMBOL
AOA FOR STICK SHAKER

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24
Q

TAILSTRIKE PROTECTION

NORMAL MODE

A

DECREASES ELEV DEFLECTION
NO FEEDBACK TO CONTROL COLUMN
PILOT CAN OVERRIDE

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25
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

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26
Q

HUD FAILURE DURING TAKEOFF

A

COMMUNICATE TO OTHER CREW
SWITCH TO PFD
REMEMBER SMALL MOVEMENTS ON PFD
TRANSITION FROM OUTSIDE TO PFD

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27
Q

CONSIDER THREATS OF MULTIPLE FLAP SETTINGS

A

THOROUGH BRIEFING
PIECE OF PAPER ON FLAP LEVER
MITIGATE VERIFYING OPT VERSUS FMC VERSUS ACTUAL FLAP SETTING

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28
Q

AFTER TAKEOFF
LEAVING GND EFFECT
EFFECT ON PERF

A

NOSE DOWN PITCH
REDUCES ROC

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29
Q

LIST FLAP LIMIT SPEEDS

A

1 260
5 240
10 230
15 220
17 215
18 215
20 210
25 190
30 180

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30
Q

QRH
PERF INFLT
CLB

A

FLAPS UP CLB THR
> TAKEOFF 11 DEG 3500 FPM
> 10K 9 DEG 3000 FPM

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31
Q

BEST ROC

A

VREF 30 PLUS 140
OR
UP PLUS 60

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32
Q

WHAT ATHR FMA MODE FOR FLCH CLIMB

A

THR FLCH SPD

@ LEVEL OFF
SPD ALT

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33
Q

WHAT WILL HAPPEN TO ATHR MODE IN FLCH CLIMB OR DESCENT IF THR LEVERS ARE MANUALLY OVERRIDDEN

A

CHANGE TO HOLD

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34
Q

WHAT SPEED PROTECTION IS AVAIL FOR VARIOUS AUTOFLT MODES

A

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

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35
Q

HOW WILL FLAP RETRACTION VARY WITH DIFFERENT TAKEOFF FLAP SETTINGS

A

@ 10, 15 17 18 20
FLAPS 5

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36
Q

ANY EFFECT ON TAIL CLEARANCE MARGINS WITH DIFFERENT FLAP SETTINGS

A

NO

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37
Q

DURING LEVEL FLT DOES A THR CHANGE NEED TO BE COUNTERED BY A CONTROL INPUT? WHAT ABOUT SPDBRK AND FLAP CHANGES

A

AUTO STABILISATION FOR STAB AND ELEV FOR THR AND CONFIG CHANGES

NO NEED TO TRIM ONLY FOR AIRSPEED CHANGE

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38
Q

HOW DO U EXPECT THE FBW ENVELOPE AND AFDS PROTECTIONS TO RESPOND APPROACHING VMO/ MMO

A

NOSE DOWN TRIM INHIBITED
CONTROL COLUMN FORCE DOUBLES TO LOWER THE NOSE

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39
Q

REVIEW AP OVERRIDE PARAMETERS

A

IF PILOT OVERRIDE AP DISCONNECTS

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40
Q

WILL FLAPS EXT >260 KTS? OR ABOVE 20k?

A

NO
INHIBITED IN PRI AND SEC MODES

LOAD RELIEF SHOWN WHERE FLAP POSN WOULD BE

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41
Q

REVIEW
NNC PRI FLIGHT COMPUTERS

A

FLT CONTROLS DIRECT MODE (ATTEMPTS RESET)

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42
Q

HOW CAN U MAINTAIN YOUR SCAN DISCIPLINE AND ESTABLISH RELIABLE MONITORING BEHAVIOURS

A

PRACTICE
ARMCHAIR FLYING

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43
Q

BANK ANGLE PROTECTIONS
WHEN DO THEY BECOME ACTIVE

A

APPROX 35 DEG
CAN BE OVERRIDDEN
AP DISENGAGE BAR INHIBITS
PFD AMBER BANK ANGLE INDICATOR >35 DEG

GPWS ‘BANK ANGLE’ 35 40 45

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44
Q

NEED BACK PRESS FOR STEEP TURNS?

A

NEED BP > 30 DEG AOB

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45
Q

HOW TO USE HUD FPV AND FLT PATH ACCEL SYMBOL FOR STEEP TURN

A

KEEP LEVEL
AND
CONSTANT SPEED

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46
Q

HOW DO U EXPECT THE STALL SPD TO DO WITH INCREASING AOB? HOW WOULD THIS BE DISPLAYED ON SPEED TAPE

A

STALL SPEED INCREASE
ZIPPER MOVES HIGHER CLOSE TO MIN MAN SPD

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47
Q

INPUT SOURCES FOR THE STBY INSTRU

A

INDEPENDENT SOURCE OF ATTITUDE AIRSPEED ALTITUDE
CENTER PITOT AND STATIC
ATTIT FROM INTERNAL INERTIAL SENSORS

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48
Q

HOW LONG WILL STBY INSTRU REMAIN POWERED AFTER LOSS OF ALL MAIN AC BUSSES. DO U EXPECT RAT TO DEPLOY

A

10 MIN ON MAIN BATT
THEN RAT WILL DEPLOY TO POWER STBY SYS

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49
Q

WHAT AUTO MANUAL DISPLAY SWITCHING IS AVAILABLE IN THE EVENT OF A DISPLAY FAILURE

A

PFD MFD SELECTOR

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50
Q

LIST TOLERANCES DURING APPROACH

A

<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

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51
Q

IN APP MODE
CAN U CAPTURE GS BEFORE LLZ

A

NO SYS LOGIC
GS CAPT INHIBITED UNTIL LLZ CAPT

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52
Q

HOW CAN APP MODE BE DESELECTED

WHAT ABOUT ABOVE 1500’

A

> 1500’ PRESS APP

<1500 IF LOC ONLY USE HDG/TRK SEL OR HDG/TRK HOLD
IF LOC AND GS PRESS TOGA

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53
Q

APPROACHING MINIMUMS
CALLOUT

A

80’ ABOVE MINIMA

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54
Q

WHAT IS MAX DIST FROM APT A GLS CAN BE USED

A

RANGE LISTED IN ERSA
YSSY 23 NM

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55
Q

DURING AN APPROACH USING INSTRU PROC IF PM CALLS VISUAL PRIOR TO MINIMA WHAT IS THE CORRECT RESPONSE FROM PF

A

LOOK UP ASSESS
CONTINUE
OR
STANDARD PROCS

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56
Q

PM RESPONSIBILITIES REGARDING DEVELOPMENT VISUAL SEGMENT

A

ENSURE REQD VIS MET
AERODROME FEATURES CAN BE SEEN
ENSURE CAN REMAIN VISUAL

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57
Q

STATE CONDS FOR CREW TO CONDUCT MANDATORY GA OR MISSED APP

A

OUTSIDE TOLERANCE
NOT STABLE
NOT VISUAL
ATC INSTRUCTION
NOT CONFIGURED

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58
Q

DURING ILS GLS TO NON AUTOLAND RWY WHAT IS LOWEST ALT BY WHICH AFDS MUST BE DISENGAGED

A

135’ RA

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59
Q

REQMTS FOR STABLE APP

A

CONFIGURED BY 1000’
NORMAO CHKLISTS BY 500’
WITHIN TOLERANCES

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60
Q

USING HUD FOR AIM PT DURING LANDING

A

GS REF LINE ON AIM PT MARKINGS ON RWY

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61
Q

QRH
PERF INFLT
FOR APP

A

FLAP 20 MLW
0.5 DEG 49% N1 166 KTS

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62
Q

WHERE IS VISUAL AIM PT 787

A

1000’-2000’

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63
Q

RMS TDZ AIM PT MARKINGS

A

AUST AIM PT 1312’
FAA 1000’
ICAO VARIES 1200-1400’
MEL RWY16 1837’

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64
Q

SCAN FOR STABLE APP

A

HUD
FPV ON GS REF LINE
SPD ATTIT ROD CENTRELINE
KEEP AIM PT SAME POSN WINDSCREEN

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65
Q

PF USING IDLE REV FOR LDG

A

PF CALL
IDLE REVERSE

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66
Q

WHAT IS THE RELATIONSHIP BETWEEN HUD FPV AND GLIDESLOPE REF LINE? HIW CAN THESE BE USED TO CORRECT VERTICAL PROFILE

A

HIGH OR LOW
ADJ FPV ABOVE OR BELOW GS REF LINE
THEN FPV ON GS REF LINE WHEN BACK ON PROFILE

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67
Q

PAPI
ALIGNED FOR TOUCHDOWN WHERE

A

NORMALLY 1000’-1500’

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68
Q

JEPP TCH

A

787 TCH?
CROSS THRESHOLD AT 50’

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69
Q

HOW DO U CALC ROD FOR APP

A

5 TIMES GROUNDSPD

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70
Q

WHERE DO U COMMENCE FLARE

A

ENSURE ACFT SPD CORRECT
FLARE APPROX 30’
FOCUS END RWY HOLD NOSE CONSTANT POSN
THEN LOWER NOSE TO RWY

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71
Q

WHAT COMMAND SPEED DO U SET?

WOULD THIS CHANGE IN WINDY OR GUSTY CONDITIONS OR IF ATHR NOT USED?

A

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

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72
Q

IF ATHR ENGAGED WHEN WILL IT REDUCE THR FOR LANDING? NO ATHR WHEN WILL U REDUCE THR

A

25’ RA

MANUALLY AS PART OF FLARE

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73
Q

WHAT EFFECT WILL THR REDUCTION HAVE ON THE PITCHING MOMENT OF THE ACFT? HOW WILL U FLY THE NOSEWHEEL ONTO THE RWY?

A

NOSE DROP
HOLD BACK PRESS
MAIN WHEELS ON SLOWLY LOWER THE NOSE

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74
Q

WHERE SHOULD U PLACE YOURSELF IN RELATION TO CENTRELINE

A

CENTRELINE INSIDE LEFT LEG?
SIT ON R SIDE SO SLIGHTLY R OF CENTRELINE

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75
Q

HOW TO DESELECT REV THR

A

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

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76
Q

PM CALLS FOR THR REV DEPLOYMENT

A

REVERSERS NORMAL
NO REV L/R
NO REVERSERS

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77
Q

HOW TO DISCONNECT ABRK

A

STOW SPDBRK
BRAKE PEDAL TO DISARM BRAKES
PF ORDER PM ABRK TO OFF

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78
Q

POTENTIAL CONSEQUENCES OF SHORT AND LONG LANDINGS

A

SHORT OBSTACLE ISSUES AND LANDING SHORT OF RWY

LONG POTENTIAL OVERRUN

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79
Q

CUES THAT INDICATE CORRECT VERSUS INCORRECT FLARE TECHNIQUE

A

EASY IF ACFT STARTS IN CORRECT SPOT
AIM PT RETENTION
MISJUDGED COMMENCEMENT HT

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80
Q

CROSSWIND TAKEOFF LIMIT

A

40 KTS DEPENDS ON VARIETY OF FACTORS

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81
Q

WHY IS ROLLING TAKEOFF ADVISED FOR SETTING TAKEOFF THR IN STRONG CROSSWINDS

A

> 20 KTS
REDUCES RISK FOD DAMAGE
AND ENG SURGE/ STALL

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82
Q

CONSIDERATIONS FOR TAKEOFF IN GUSTY WIND IR STRONG CROSSWIND CONDS

A

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

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83
Q

XWIND TAKEOFF
HOW TO MAINTAIN CENTRELINE

A

RUDDER FOR CENTRELINE
CONTROL COLUMN INTO WIND TO KEEP WINGS LEVEL

SKY POINTER

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84
Q

HOW TO MAINTAIN WINGS LEVEL FOR TAKEOFF
WHAT HUD INDICATIONS COULD HELP?

A

KEEP RWY HEADING
PITCH BAR LEVEL?

TRK ON ND

SKY POINTER

KEEP FPV UNDER HDG BUG
DIFFICULT IN STRONG XWC AS ITS GHOSTED

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85
Q

LARGE CONTROL WHEEL INPUTS WILL CAUSE SPOILER RISE. WHAT EFFECT WILL THIS HAVE

A

INCREASED DRAG AND REDUCED TAKEOFF PERF

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86
Q

AT ROTATION NOSE WHEEL LIFTS OFF NOSE WHEEL STEERING LOST.

HOW WILL THIS AFFECT ACFT AND HOW CAN U COMPENSATE?

A

ACFT SHOULD NATURALLY TURN INTO WIND
NEUTRALISE CONTROLS

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87
Q

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

A

STOP PULLING BACK
NOT SURE?
TAILSTRIKE PROTECTION REDUCES ELEV DEFLECTION BUT PILOT CAN OVERRIDE

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88
Q

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

A

HIGHER WORKLOAD AS DIFF SCAN REQD
USE ND FOR TRK

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89
Q

CROSSWIND LIMITS FOR LANDING

A

RCAM 5/6 40 KTS

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90
Q

SOME NNC WILL REDUCE CROSSWIND LIMIT WHAT ARE THEY

A

ASSY THR
RUDDER RATIO
FLT CONTROLS NOT NORMAL MODE?

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91
Q

DESCRIBE EFFECT XWC ON RWY PERSPECTIVE

A

FLT DECK UPWIND SIDE

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92
Q

DOES 787 HAVE RUNWAY ALIGN MODE

A

IF 5-10 DEG CRAB ALIGNS 500’ AND 200’
>10 DEG CRAB ALIGN 500’ 5 DEG CRAB ON TOUCHDOWN
<5 DEG CRAB JUST 200’

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93
Q

CONSIDERING RWY ALIGN MODE WHEN SHOULD AP BE DISC FOR MANUAL LANDING

A

PRIOR TO 500’ AGL

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94
Q

ON INSTRU APP WHEN TRANSITIONING FROM INSTRU TO VISUAL TENDENCY TO TURN ACFT

HOW CAN THIS BE AVOIDED

A

KEEP SCAN GOING
USE INSTRU MORE THAN VISUAL PICTURE

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95
Q

SPECIFIC CROSSWIND LANDING TECH

A

DECRAB DURING FLARE
RUDDER TO STRAIGHTEN IN FLARE AILERON FOR WINGS LEVEL

TOUCHDOWN IN CRAB

SIDESLIP (WING LOW) PRIOR TO FLARE STRAIGHTEN ACFT

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96
Q

HOW DO U MAINTAIN CENTRELINE TRACKING AND WINGS LEVEL DURING LANDING ROLL

A

RUDDER FOR CENTRELINE
AILERON TO KEEP WINGS LEVEL SHOUKD REDUCE AS ACFT SLOWS

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97
Q

SLIPPERY RUNWAY
POSS LOSS DIRECTIONAL CONTROL

A

COULD TOUCHDOWN IN CRAB
PERMITS RAPID OPERATION OF SPOILERS AND AUTOBRK
USE DIFFERENTIAL BRAKING/ REV THR FOR DIRECTIONAL CONTROL

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98
Q

PILOT SEAT

A
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99
Q

FUEL TANKS TOTAL

A

101.4 T

COULD BE 98-102 DEPENDING ON SG

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100
Q

L AND R MAIN TANK

EACH

A

16 776 KG

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101
Q

CENTER TANK

FUEL

A

67 889 KG

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102
Q

FUEL IMBALANCE

A

NOT AN ISSUE
EXCEPT FOR LONG TERM STRUCTURAL IMBALANCE
ACFT CONTROLLABLE WITH ALL FUEL ON ONE SIDE

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103
Q

PROV LOADSHEET

PANTRY

A

NO NEED CHECK NUMBERS
EXCEPT
CHECK CITY PAIRING

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104
Q

FINAL LOADSHEET

A

SHOULD BE RECEIVED WITHIN 3 MINS DOOR CLOSED

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105
Q

TAKEOFF PERF

WINDSHEAR

A

FULL THRUST AND FLAP 20

V1 VR FOR WINDSHEAR
ROTATE AT FASTER VR

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106
Q

FWD CG MOVEMENT

A

IF ON BORDERLINE CHOOSE MORE FWD POSN REDUCES NEED FOR RECALC

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107
Q

DEST APT RWY CONTAMINATED

A

NEED CHECK LDR PREFLT

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108
Q

AFTER LDG DIST CALC

BTV?

A

SEND OUTPUT
TO FD PRO CHANGE TO UNFACTORED LDG DIST ASSESS ABRK AND TAXIWAY TO USE

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109
Q

CRS

YES
NO
R

A

YES 330 MINS
NO 60 MINS
R RESTRICTED

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110
Q

HOLDING IN ICIING

A

FLAP 1 ONLY NO FLAP JUST SLATS

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111
Q

UPRT

A

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

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112
Q

PF

THRUST SETTING REQD

A

ALT + 50

IE FL330 = 83% N1

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113
Q

RANGE FOR DISPLAYING APT MAP

A

0.5, 1, 2 or 5 NM

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114
Q

EICAS
HUD TAKEOFF

A

FOR TAKEOFF GUIDANCE FAILURE NOT COMPLETE HUD FAILURE

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115
Q

DERATES CLB 1 CLB 2

TO1 TO2

A

CLB 1 5%
CLB 2 15%

> 25000’ DERATE REDUCES TO CLB BY 33k

TO1 5%
TO2 15%

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116
Q

CLB/ CON MCP SW

A

ON GND AND <400’ SW INOP
AEO CHANGES FMC SEL CLB THR
OEI CON

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117
Q

MAX ROC

A

VREF 30 + 140
OR
UP + 60 TO M0.82

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118
Q

IF SPD REDUCES TO STICK SHAKER

A

ATHR ACTIVATES IN SPD TO MIN MAN SPD OR MCP SPD WHICHEVER IS HIGHER

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119
Q

DESCENT IN VNAV SPD
STALL PROTECTION

A

IN HOLD
ATHR WILL ACTIVATE FOR STALL PROTECTION
THR LEVERS WILL NOT MOVE

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120
Q

ATHR WILL NOT ACTIVATE

A

ATHR NOT ARMED
IF PITCH MODE TOGA OR FLCH SPD
IN HOLD WONT SUPPORT STALL PROTECTION EXCEPT VNAV SPD

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121
Q

EICAS
FLIGHT CONTROL MODE

A

FLT CONTROLS
SECONDARY MODE

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122
Q

EICAS
PRI FLIGHT COMPUTERS

A

FLT CONTROLS
DIRECT MODE

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123
Q

MISSED APP PROC

A

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

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124
Q

GA

FMA

A

THR TOGA TOGA
FOR 2000 FPM

THR REF TOGA TOGA
FULL CHARGE

LNAV @ 50’ MANUAL FLYING
LNAV @ 200’ AP ON

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125
Q

TRACKING AND HT REQMTS FOR GA INSTRU APP VERSUS VISUAL APP

A

INSTRU APP FOLLOW CHARTED GA

VISUAL APP TURN TOWARDS RWY CENTRELINE

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126
Q

MISSED APP FROM 2000’

WILL FD ALWAYS PROVIDE GUIDANCE?

A

FIRSTLY NO RUSH
BOTH PILOTS READY
CALL GO AROUND THEN QUICKLY FLCH OR VNAV
THEN GA PROC

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127
Q

FMA CALLOUT REQMT

FOR GA

A

FMA REQD TO BE CALLED
MANUAL AND AP ON

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128
Q

DESCENDING MISSED APP USING AFDS

A

> 1500’ PRESS APP DISARMS APP OR USE LOC VS
<1500’ LOC ONLY PRESS VS
<1500’ LOC GS NEED PRESS TOGA

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129
Q

BALKED LANDING

A

DISENGAGE AP
DISC ATHR
MAINTAIN LDG CONFIG
MAN ADVANCE THR
ROTATE AT VREF
15 DEG PITCH AIRBORNE
THEN GA PROC AWAY FROM GND

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130
Q

IF GA INITIATED AFTER TOUCHDOWN AND TOGA SEL WHAT HAPPENS TO SPDBRK AND ABRK

A

AUTO STOWS

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131
Q

ROLE OF PM IN APPROACH MONITORING

A

CALL DEVIATIONS
GUIDANCE ON TRENDS

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132
Q

CONSIDER MCP ALTITUDE SETTING WITH CONDITIONAL CLIMB DO U SET LOWER ALT

A

SET HIGHER ALT WILL BE IN VNAV BY THEN

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133
Q

2 WAYS CLB CAN BE SEL ON MCP

A

FLCH
CLB BUTTON
VNAV?

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134
Q

WHAT IS A BALKED LDG

A

TOUCHDOWN OCCURS WITHOUT REV THR SEL

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135
Q

KEY TO EARLY RECOGNITION PILOT INCAPACITATION

A

SOPS
80 KT CALL
TELL OTHER PILOT IF FEELING UNWELL
CROSSCHECKING
CHECKLIST RESPONSES

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136
Q

INCAPACITATION

WHEN MUST PAN BE DECLARED

A

CAPT OR FO INCAPACITATED

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137
Q

WOULD U TAXI TO GATE

CAPT INCAPACITATED

A

YES ID TAXI TO GATE
CAPT REQMT A QF THING

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138
Q

WHAT FEATURES DO PILOT SEATS HAVE TO ASSIST WITH INCAPACITATION

A

LOCK SEATBELT
REMOVE PILOT FROM CONTROL ELECTRONICALLY OR MANUALLY

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139
Q

CONSIDERATIONS

ATC KEEPS ACFT HIGH ON APP

A

CONFIGURE EARLY
SLOWER SPD AND HIGHER DRAG
CONSIDER WHERE FAF IS
USE VSD OR ALT ARC TO DETERMINE WHETHER STABLE APP CAN BE MET

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140
Q

GS FROM ABOVE

PROC

A

PRESS APP
ON LOC CHECK GS ARMED
SET 1000’ ALT WINDOW
FULLY CONFIGURED
VS -1500 FPM

VISUAL BY 1000’
IMC BY FAF

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141
Q

WHY IS FLCH NOT PREFERRED PITCH MODE WHEN INT GS FROM ABOVE

A

WILL PITCH FOR SPD
120 SECS FOR ALT COULD BE HIGH ROD
COMPANY ROD LIMIT MAY BE REACHED

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142
Q

FLCH

ANY RESTRICTIONS?

A

NOT BELOW 1000’ AFE

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143
Q

FAM

APPROACH SLOPE GUIDANCE

A

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

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144
Q

TOOLS TO ASSIST WITH CCTS

A

FIX PG RWY END AND ABEAM

XTK ERROR UNDER ACFT TRIANGLE ON ND

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145
Q

CCT

BANK ANGLE FOR UPWIND TURN

A

20 DEG AOB
+/- 5 DEG PER 15KTS

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146
Q

CCT

DWIND SPACING

A

2-2.5 NM

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147
Q

CCT

PITCH CHANGES WITH CONFIG CHANGES?

A

YES

WILL NEED TO TRIM FOR SPD CHANGES

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148
Q

CCT

WHEN DO U TURN BASE

A

40 SECS FROM ABEAM

25 DEG AOB LEVEL TURN
FPV JUST UNDER HZN 200-300 FPM DESCENT UNTIL INT 3 DEG PATH

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149
Q

CCT

HOW DO U ANTICIPATE TURNING FINAL

A

USE ND EXT CENTRELINE
TREND VECTOR ACCOUNTS FOR WIND

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150
Q

CCT

TRAINEES ROLE DURING TOUCH AND GO

A

KEEP ACFT STRAIGHT
SET GA THR

INSTRUCTOR SETS FLAP AND STAB TRIM
MAYBE ABRK?

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151
Q

CCT

AFTER TAKEOFF CHECKLIST

A

FLAPS REMAINING AT 5
WILL NEED TO OVERRIDE FLAPS ITEM OVERRIDE

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152
Q

LAHSO

CONDITIONS

A

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

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153
Q

ACTIVE AND PASSIVE

LAHSO

A

ACTIVE
ARRIVAL RWY WITH HOLD SHORT INSTRUCTION

PASSIVE
FULL LENGTH AVAIL GIVEN INFO ABOUT CROSSING ACFT

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154
Q

ACFT UNABLE LAHSO

A

ATC
NEGATIVE ACTIVE OR PASSIVE LAHSO

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155
Q

FLAPS

COMMAND SPD TO SET

A

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

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156
Q

DIFF BETWEEN MIN MAN SPD AND FLAP MAN SPD

A

MIN MAN SPD BASED AOA

FLAP MAN SPD BASED ON WT

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157
Q

MIN MAN SPD

A

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

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158
Q

FLAP MAN SPD

A

BASED ON ACFT WT

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159
Q

WHAT EFFECTS MAN MARGIN TO STICK SHAKER

IE ZIPPER

A

GROSS WT
ALTITUDE
LDG GEAR
SPDBRKS
ENG FAIL

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160
Q

PM CALLS DURING STALL RECOVERY

A

AIRSPEED TREND
ANY TREND TOWARDS TERRAIN

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161
Q

ANTIICE SYS

STALL WARNING LOGIC

A

ADJUSTS STICK SHAKER TO LOWER AOA
THIS RESULTS IN HIGHER STICK SHAKER SPEED AND HIGHER MIN MAN SPD

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162
Q

ROLL PROTECTION

BANK ANGLE PROTECTION

A

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

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163
Q

HIGH SPEED PROTECTION

A

@ VMO MMO
NOSE DOWN TRIM INHIBITED
NEED DOUBLE FORCE TO PUSH CONTROL COLUMN FORWARD
USE SB TO REDUCE SPD KEEP AP ON

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164
Q

LOW SPEED PROTECTION

A

@ 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

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165
Q

APPROACH TO STALL

MEM ITEMS

A

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

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166
Q

HAPPY PLACE PROC

A

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

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167
Q

CCT

UPWIND PROC

A

@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

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168
Q

CCT

CROSSWIND PROC

A

CONTINUOUS TURN UPWIND TO DWIND
AFTER TAKEOFF CHECKLIST OVERRIDE FLAPS
DESCENT PROCS
PM DEP ARR LOAD ILS INTC DIR RWY EXEC

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169
Q

CCT

DWIND

A

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

170
Q

CCT

BASE

A

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

171
Q

LHR MISSED APP

INTERMED CLIMB

A

SET LOWER ALT FIRST

CONSERVATIVE

172
Q

APPROACH VIEW

MAL BURNS PIC

A
173
Q

UPRT RECOVERY

RCB

A

DONT TOUCH CONTROLS DURING

174
Q

RADALT DURING FLARE

A

8 GOOD
3 KEEP FLARING

RADALT ON HUD UNDER ACFT SYMBOL

175
Q

MAIN WHEELS TOUCHDOWN

A

LITTLE BIT MORE BP

HIGHER ABRK = MORE BP REQD

176
Q

STALL INDICATIONS

PFD

A

BLUE BENEATH WHEELS
5 DEG PITCH WHY ARE WE HERE
PLIs APPEAR
EICAS AIRSPEED LOW
EICAS AUTOPILOT AND PITCH MODE AMBER BAR THROUGH

177
Q

STALL RECOVERY

VIDEO

A

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

178
Q

UPRT

RECOVERY PROC

A

PUSH
ROLL
POWER INCL THRUST AND SPDBRK
RECOVER

179
Q

MISSED APP

MAN FLYING

A

FMAS ONCE CLEAR OF GND
AND CONFIG CHANGES

180
Q

MAX DEMONSTRATED XWC

A

TAKEOFF 29 KTS

LANDING 35 KTS

QF USES TALPA TABLE

181
Q

WHAT IS WINDSHEAR

A

DIFFERENCE IN WIND SPEED AND DIRECTION OVER A RELATIVELY SHORT DIST IN THE ATMOSPHERE

182
Q

ROLLING START

EFFECT ON XWC

A

REDUCE BY 5 KTS

ROLLING START REDUCES ENGINE STRESS/ SURGE MAY SEE THRUST RAMPING WITH HIGH XWINDS

183
Q

FBW FOR XWIND TAKEOFF

A

ATTEMPT ZERO YAW RATE
PEDALS DONT MOVE

184
Q

WINDSHEAR PROC

ON RWY

A

< 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

185
Q

HUD

TOGA REF LINE

A

DISPLAYS FOR

TAKEOFF
GA
WS

186
Q

NORMAL PITCH ATTIT RANGE

A

+5
-2.5

187
Q

WINDSHEAR

PRIOR BEGINNING TAKEOFF

A

FULL THR
FLAP 20
LONGEST RWY CLEAR WS
INCREASE VR UP TO VR + 20
SET VSPDS ACTUAL WT
DO NOT EXCEED PLI

188
Q

WINDSHEAR

PRIOR TO APP AND LANDING

A

F25/30
STABLE APP
SUITABLE RWY AWAY FROM WINDSHEAR
MANUAL THR?

189
Q

WINDSHEAR

LIGHT
MOD
STRONG
SEV

A

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

190
Q

WINDSHEAR ESCAPE MAN

A

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

191
Q

WS MAN

WHY DISC ATHR

A

SO THR ISNT REDUCED

192
Q

WHAT CLUES MAY INDICATE WS ON INTENDED FLT PATH

A

ATIS
TS
PILOT REPORTS
VIRGA

193
Q

FOR WS ESCAPE MAN

INITIAL PITCH ATTIT

WHAT WILL U SEE ON HUD

A

15 DEG

PARK BENCH
FPV NEEDS TO BE BELOW

ACFT SYMBOL TOGA REF LINE

194
Q

CAN U CONTINUE APP IF U RECEIVE WS WARN

A

NO SHOULD ABORT OR PRIOR TO V1 ON TAKEOFF

PWS CAN DO NORMAL GA VERSUS WS MAN

195
Q

ROLE PM DURING WS MAN

A

VERIFY MAX THR
ATHR DISC
PITCH
NO CHANGE CONFIG
MONITOR ACTIONS
CALL OMISSIONS
ANY TREND TOWARDS TERR

196
Q

INDICATIONS OF WS

A

<1000’ AGL

15 KTS IAS
500 FPM
5 DEG PITCH
1 DOT GS
UNUSUAL THR LEVER POSN

197
Q

HUD WS SYMBOLOGY

A

FPV FILLS IN
PARK BENCH APPEARS AOA LIMIT TO STICK SHAKER

198
Q

ACTIONS REQD WHEN WS EVENT FINISHED

A

CLEAR WS
DO GO AROUND PROC

199
Q

DURING TAKEOFF ROLL

HOW WOULD U DEFINE AND RECOGNISE WS

A

FLUCTUATIONS IN AIRSPEED
SLOW ACCEL

200
Q

PM

RADIO CALL WS

A

WINDSHEAR ESCAPE
CLEAR OF WS RETURNING TO …

201
Q

DETERMINE TRACK OFF HUD

A

HUD IS HEADING UP DISPLAY

FPV ON COMPASS ROSE IS TRK

202
Q

SOME NNC REDUCE CROSSWIND LIMIT

WHAT ARE THEY

A

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

203
Q

DESCRIBE POSN NOSE GEAR IN RELATION TO LLZ ANTENNA FOR LDG

A

LOC ANTENNA NOSE OF ACFT
MAIN GEAR DOWNWIND FROM LLZ IN XWC

204
Q

FMC WIND ACCURATE IN SIDESLIP FOR LDG?

A

NO USE TOWER WIND

205
Q

APPROACHING MINS

WHICH EFIS

A

CAPT EFIS CONTROL PANEL

206
Q

UPRT RECOVERY

PITCH RATE

A

2.5 DEG/ SEC

207
Q

STALL INDICATIONS

A

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

208
Q

PREDICTIVE VERSUS REACTIVE WS WARN

A

PREDICTIVE PWS
DETECTED AHEAD OF ACFT

REACTIVE WS GPWS
EXCESSIVE DOWNDRAFT OR TAILWIND OCCURING

209
Q

PWS

PICTURE

A
210
Q

PWS ALERT

A

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

211
Q

PWS AURAL ALERTS

A

WARNING
GO AROUND WINDSHEAR AHEAD
WINDSHEAR AHEAD WINDSHEAR AHEAD

CAUTION
MONITOR RADAR DISPLAY

212
Q

GPWS AURAL ALERTS

A

WINDSHEAR WINDSHEAR WINDSHEAR

<1500’ RA

DETECTION BEGINS AT ROTATION
GPWS INHIBITS PWS AS ACFT ACTUALLY IN WS

213
Q

PWS INHIBITS ON TAKEOFF

A

WARNING
100 KTS TO 50’

CAUTION
80 KTS TO 400’

214
Q

WINDSHEAR

HOW TO FLY INCREASED VR

A

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

215
Q

N1 IDLE

10k 35k

A

10k
30

35k
47

216
Q

N1 MAX THR

10k 35k

A

10k
99.1

35k
101

217
Q

SPOOL UP TIME

IDLE TO MAX

10k 35k

A

10k
12 SECS

35k
22 SECS

218
Q

N1 280 KTS

10k 35k

A

10k
62 %

35k
85 %

INDICATOR OF EXCESS THR AVAIL FOR ACCEL

219
Q

FUEL FLOW AT 280 KTS

10k 35k

A

10k
2.5 T

35k
2.7 T

220
Q

FUEL FLOW AT MAX THR

10k 35k

A

10k
8.6 T

35k
4.2 T

INDICATOR OF ABILITY FOR FUEL TO ACCEL KINETIC ENERGY OF FUEL

221
Q

280 - 300 KTS

TIME TO ACCEL

10k 35k

A

10k
13 SECS

35k
90 SECS 1:30

222
Q

WINDSHEAR

ON TAKEOFF

A

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

223
Q

TCAS CLEAR OF CONFLICT

A

FLCH ENGAGES ATHR
AND
AP BACK TO CLEARED ALT

224
Q

ILS GLS BREAKOUT MAN

A

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

225
Q

UNANNUN CHKLST

RADIO ALT UNRELIABLE

A

VREF 30 and F30 LDG
USE AFTER GA IF CAPT AND FO RA DIFF
OR IF RA NOT SHOWING PFD HUD AS EXPECTED

226
Q

FMC NNC

A

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

227
Q

RADIO ALTIMETER L + R

NNC

A

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

228
Q

PRM APP

WHERE

A

AUST AND USA APPROVED
MAINLY SYD

229
Q

SYD PRM BRIEF

A

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

230
Q

FLYING A BREAKOUT

A

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

231
Q

FLT CONTROL MODES

A

NORMAL
SECONDARY
DIRECT

232
Q

HOW CAN FLT CONTROLS DEGRADE TO SECONDARY OR DIRECT MODES

A

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

233
Q

SEC AND DIRECT MODES

WHAT PROTECTIONS ARE LOST

A

NO AP
NO AUTO SB
ENVELOPE PROT
GUST SUPPRESSION
PITCH COMPENSATION
ROLL YAW ASSY COMPENSATION
TAIL STRIKE PROT

234
Q

HOW WILL DIRECT MODE CHANGE STAB TRIM FUNCTIONALITY

A

NONE BECOMES NORMAL ACFT
NEED BP FOR FLAP AND SB
TURNS TO 30 DEG AOB
GEAR CONFIG
THR CHANGES
TURBULENCE

235
Q

WHAT AUTOFLT MODES AVAIL TO FLY NON ILS APP

A

IAN
LNAV VNAV
LNAV VS
LNAV FPA

236
Q

NDB VOR APP TOL

A

+/- 5 DEG

237
Q

HOW MUST APP BE CODED TO ALLOW USE IAN OR VNAV

A

GP ANGLE LEGS PG
RWXX WAYPT
MXXX MISSED APP PT

238
Q

2D APP SETTING MCP

A

SET ALL ALTS TO MDA
USE VSD
300’ TO MDA SET MISSED APP ALT

239
Q

2D APP

FD USE AT MINIMA

A

BOTH FDs OFF
PM FD ON

240
Q

CIRCLING AREA FOR 787

A

5.28 NM FIX PG?

241
Q

WHICH ITEMS IN YOUR SCAN WILL U PRIORITISE ON FINAL FOR STABLE APP

A

GS
GS REF LINE
ROD
PAPI

242
Q

RNP AR APP

WHAT MODES

A

LNAV VNAV

243
Q

WHY MUST TERR VSD BE DISPLAYED ON ONE ND

A

INCASE TOTAL FMC FAILURE

244
Q

WHEN ARE VERTICAL NPS FIRST DISPLAYED ON ARR

A

ON DESCENT
VNAV PTH

245
Q

WHAT HAPPENS ON VERTICAL OR LATERAL NPS WHEN ANP EXCEEDS RNP

A

WHITE BARS TOUCH
THEY TOUCH AND TURN AMBER AND FLASH FOR 10 SECS

246
Q

WHY SPD INTERVENE ON VNAV PTH

A

ON APPROACH LOGIC. SPD WILL OTHERWISE REDUCE POSS < FLAP MAN SPD

247
Q

MCP ALT CAPT DURING APP

A

IN VNAV SET LOWER ALT AND PRESS ALT FOR ALTITUDE INTERVENTION

IN VS SET LOWER ALT AND RESELECT VS OR FPA AS APPLICABLE

248
Q

MISSED APP REQD FOR RNP APP

A

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

249
Q

TCAS TA

MEM ITEMS

A

TCAS I HAVE CONTROL

TA
LOOK FOR TFC

250
Q

TCAS RA

MEM ITEMS

A

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

251
Q

TCAS

HUD SYMBOLOGY

A
252
Q

TCAS

TIMING FOR RECOVERY

A

5 SECS/ 2.5 SECS

253
Q

TCAS

RADIO CALLS

A

TCAS RA
UNABLE TCAS RA
CLEAR OF CONFLICT RETURNING TO …
CLEAR OF CONFLICT FL… RESUMED

254
Q

TCAS TA OR RA

SO AS PF

A

CAPT OR FO MUST TAKEOVER

255
Q

VSD USE

A

ALLOWS CHECK QNH VERSUS RWY
GIVES VISUAL INDICATION OF FPA CONSTRAINTS AND QNH ERRORS

256
Q

TCAS INHIBITS TAKEOFF

A

TCAS TA ON GND TO 600’ RA
TCAS RA ON GND TO 1000’ RA
TCAS DESCEND RA ON GND 1200’ RA

257
Q

TCAS INHIBITS LANDING

A

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

258
Q

TA
RA
TIME TO COLLISION

A

TA 20-48 SECS
RA 15-35 SECS

5 SECS 0.25G
2.5 SECS 0.35G

259
Q

HOW MANY FMC?

A

3
MASTER
SLAVE
BACKUP

260
Q

APPROACHING GLIDEPATH CALL

A

2NM TO DESCENT PT
2D APP GR DOWN F20 ARM SB
AT DESCENT PT F30 LDG CHKLST

261
Q

GLIDESLOPE ALERT ON IAN APP OTHER THAN ILS GLS

A

DUE BAROMETRIC ALTIMETER INDICATION VARIATIONS
INCORRECT ALT SETTING
WARMER THAN STD OAT

262
Q

NOSE HIGH

RECOVERY

A

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

263
Q

NOSE LOW

RECOVERY

A

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

264
Q

ILS RAW DATA

A

HUD CAN USE CAT I MINIMIA
NO HUD NEED 1200 M VIS

265
Q

PRIOR TO ARMING APP

A

CHIPS

CLEAR TO INT APP
HEADING TO INT
ILS GLS IDENTIFIED
POINTERS IN VIEW
SPD WINDOW OPEN

266
Q

NNC INSTRUCTIONS

A

RAMATE

RECOCNISE AND ANNOUNCE
MAINTAIN ACFT CONTROL
ANALYSE THE EICAS
TAKE THE PROPER ACTION
EVALUATE THE NEED TO LAND

267
Q

WHAT IS THE SIGNIFICANCE OF THE COLOUR OF THE CHECKLIST TITLE IN AN ECL CHECKLIST

WHITE VS AMBER

A

SITUATION NO LONGER PRESENT

268
Q

IF A CHECKLIST IS OPENED IN ECL FOR REVIEW OR IN ERROR WHAT IS FLT CREW ACTION REQD

A

CHECKLIST OVERRIDE

269
Q

WHAT EICAS INDICATIONS FOR WINDMILLING START OR X START

A

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

270
Q

HOW WILL FBW SYS RESPOND TO A THR ASYMMETRY IN NORMAL MODE? WILL RUDDER PEDALS MOVE

A

> 60 KTS MAINTAIN ZERO YAW RATE
RUDDER PEDALS MOVE

271
Q

IS AUTO RELIGHT PROTECTION PROVIDED

A

YES
FOR FLAMEOUT AND SUB IDLE STALL RECOVERY
AUTOSTART SHOWN ABOVE N2

272
Q

HOW DO U MANAGE VARIOUS TASKS THAT NEED TO BE COMPLETED IN ORDER TO MANAGE ENG FAIL IN CRUISE

A

GAP TO MIN MAN SPEED = TIME OR URGENCY FOR DESCENT

273
Q

WHICH PG FMC WOULD U FIND DRIFT DOWN SCHEDULE AND MAX OPERATING ALT

A

VNAV EO PG

274
Q

WHAT ARE DIFFERENCES WITH DRIFTDOWN UNDER EDTO PROCEDURES

A

OEI OFF OFP
BETWEEN BEST L/D AND VMO MMO

275
Q

PREFERRED AFDS MODES FOR DRIFTDOWN

A

DUDU

DOWN VNAV EO PG
UP SET MAX ALT MCP ALT
DOWN PRESS EXEC
UP PRESS ALT TO BEGIN DESCENT IN VNAV

276
Q

OTHER CONSIDERATIONS FOR DRIFTDOWN FOR PM

A

CLEARANCE
VOICE OR CPDLC
LIGHTS
CALL ON 123.45
TCAS BELOW

277
Q

CONTINGENCY PROC

OTHER THAN WEATHER SITUATIONS

A

FOR DESCENT
OFFSET 45 DEG AND 15 NM

278
Q

DRIFTDOWN LEVEL OFF

WHAT SPEED

A

ETOPS CONSIDER OFP SPEED
WILL DEPEND ON LOCATION AND PRIORITY IF DIVERTING AND DIST TO GO

279
Q

ENG FAIL CRUISE FLT

DOES CREW HAVE TO LAND NEAREST AVAIL APT

A

IF CAT C CAN CONTINUE CAT A OR B
DEPENDS ON WEATHER, FAMILIARITY WILL APT AND DIST TO GO TO PREFERRED ALTN

280
Q

CAN FUEL BE JETTISONED FROM ALL TANKS

A

YES
AUTO SETS MLW

281
Q

WHERE DO U OBSERVE CALC JETTISON TIME

A

FUEL SYNOPTIC BOTTOM RIGHT

282
Q

SOME OPERATIONAL CONSIDERATIONS PRIOR TO JETTISONING FUEL

A

ATC CLR
PREFERRED ALT > 6000’?
AWAY FROM HOUSES ETC

283
Q

CONSIDER OVERWT LANDING VERSUS FUEL JETT

A

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

284
Q

REVIEW OVERWT LANDING CHECKLIST IN ECL

A

UNANNUN

285
Q

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?

A

REDUCES THR TO ALLOW RUDDER FOR DIRECTIONAL CONTROL
INCREASES THR ONCE AIRSPEED >V2 VREF

TAP ENHANCES SECOND SEGMENT

286
Q

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

A

< TAMS
AIRSPEED AIRSPEED AURAL
MASTER WARN

SHOWN IN RED RECTANGULAR BOX

RELATED TO MINIMUM CONTROL SPEED

287
Q

DIVERSION AND DECISION MAKING STRATEGIES

A

NON EDTO 60 MINS
EDTO 330 MINS

TIME STRATEGY
FUEL STRATEGY
OBSTACLE STRATEGY

288
Q

WHAT IS AN EDTO ALTN

A

ADEQ APT

CAT A B C
WX FORECAST AVAIL
SERVICES FACILITIES EG LGTS
LDA < LDR
AT LEAST ONE INSTRU APP

289
Q

WHAT IS EDTO PLANNING MINIMA

A

DEFINED WX CRITERIA USED TO DETERMINE SUITABILITY OF ADEQ APT

SHOWN EFF MSG

290
Q

WHAT SPECIFIC REQMTS NEED TO BE CONSIDERED FOR EDTO ALTN PREFLT STAGE

A

RFF
30 MIN CALL-OUT CAT 4 OUTSIDE AUST
IN AUST NIL

ATC
AVAIL 30 MINS NOTICE OUTSIDE AUST
IN AUST NIL

291
Q

EDTO WX ASSESSMENT

A

BETWEEN EARLIEST AND LATEST ARRIVAL TIME
FORECAST CEILING AND VIS
XWC INCL GUST OEI WIND COMP
PROB < 40% DISREGARD
INTER TEMPO CONSIDERED

292
Q

CAN FLT DEPART WITHOUT FORECAST FOR EDTO ALTN

A

YES PROVIDED ONE RECEIVED WHEN APT RELIED UPON

293
Q

TECH LOG REQMTS FOR EDTO FLT

A

YES 330 MINS
NO 60 MINS
RESTRICTED VARIES

NEW E LOGBOOK SHOWS CLEARLY

294
Q

SPECIFIC INFLT REQMTS PRIOR TO EEP

A

2 WAY COMMS WITH ATC AND FLT DISPATCH
INFLT FUEL REQMTS
ACFT STATUS OK
NOTAMS
EDTO ALTN WX ABOVE LDG MINIMA

295
Q

WHAT ARE SIGNIFICANT SYS FAILURES

A

NNC
PLAN TO LAND AT NEAREST AVAIL APT

296
Q

WHAT ARE TIME LIMITED SYS

A

LIMITATION SPECIFIED ACFT FLT MANUAL

297
Q

ACTIONS WITH A SIGNIFICANT SYS FAILURE BETWEEN EEP AND EXP

A

IF EDTO ALTN CAT C CAN CONTINUE TO CAT A B

SPEED DEPENDS ON PRIOIRITIES

298
Q

REVIEW CPE FUEL REQMTS

DOES IT NEED TO BE PROTECTED INFLT

A

NO PREFLT REQMT

299
Q

RTO

REASONS

A

<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

300
Q

RTO

ACTIONS CAPT

A

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

301
Q

RTO

ACTIONS FO

A

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

302
Q

WITH RTO SEL

WHEN WOULD BRAKES BE APPLIED

A

ACFT ON GND
GROUNDSPEED > 85 KTS
BOTH THR LEVERS IDLE

303
Q

TAKEOFF INHIBITS

MASTER WARN CAUTION

A

MASTER WARN
V1 OR ROTATION TO 400’ OR 25 SECS AFTER INHIBIT

CAUTION
80 KTS TO 400’ OR 20 SECS AIRBORNE

304
Q

INDICATIONS OF INCAPACITATION ON TAKEOFF

A

THRUST SET MISSED
POOR CENTRELINE TRACKING
80 KTS CALL MISSED OR NO REPLY

305
Q

WHAT INFO ON HUD IS AVAIL TO ASSIST WITH RTO BRAKING

A

GND DECEL SCALE > 50 KTS AND REMOVED < 25 KTS

306
Q

EVAC PROC

A

PAPER QRH
READ AND DO

307
Q

THRUST LOSS DURING TAKEOFF ROLL

WHERE TO LOOK FOR TRACKING

A

USE HUD
FPV VERSUS HDG BUG

308
Q

OEI INITIAL PITCH FOR TAKEOFF

A

APPROX 10 DEG
ROTATE 1.5- 2 DEG

309
Q

V1 CUT

WHEN SHOULD U ASK PM TO IDENTIFY THE PROBLEM

A

> 400’ AND ACFT UNDER CONTROL

310
Q

ENG SEV DAMAGE

ACFT INDICATIONS

A

NEED AIRFRAME VIBRATION

311
Q

V1 CUT

WHEN IS FLAP RETRACTION

A

MEM ITEMS COMPLETE IF REQD
> EO ACCEL ALT OR 1000’ AGL

312
Q

V1 CUT

PROC

A

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

313
Q

V1 CUT

AFTER FLAPS UP CESSNA

A

AFTER FLAPS UP

CON VERIFY
ENG OUT PG EXEC
SA
SPD WINDOW OPEN
NNC
AFTER TAKEOFF CHECKLIST

314
Q

V1 CUT

CURVED DEP WHAT MAX ANGLE OF BANK WOULD YOU USE

WILL AFDS ROLL MODE SEL AUTO LIMIT BANK ANGLE

A

AFDS LIMITS BANK TO 15 DEG UNTIL V2 + 10
BANK LIMIT 25 DEG @ V2 + 20 IN LNAV OR HDG/ TRK SEL IN AUTO

315
Q

OEI

FLYING THE APP

A

AS PER NORMAL

F 20 OR F30 DEPENDING ON PERF?

316
Q

OEI

TARGET THR SETTING FOR APP

A

NOT SURE
HUD SPEED TREND VECTOR EXCELLENT FOR MAN THR
POSSIBLY KEEP ATHR ENGAGED?

317
Q

ENG LIMIT EXCEED

MEM ITEMS

A

ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM RETARD UNTIL ENG LIMIT EXCEED MSG BLANKS OR THR LEVER AT IDLE

318
Q

ENG SURGE

MEM ITEMS

A

ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM RETARD UNTIL ENG SURGE MSG BLANKS OR THR LEVER IDLE

319
Q

ENG SEV DAMAGE

MEM ITEMS

A

NEED ACFT VIBRATION

ATHR ARM SW CONFIRM OFF
THRUST LEVER CONFIRM IDLE
FUEL CONTROL SW CONFIRM CUTOFF
ENG FIRE SW CONFIRM PULL

320
Q

EXTRA THRUST AVAIL

V1 CUT

A

ONLY IF USING TO THRUST AND ATM

TO 1 OR TO 2 NO EXTRA THR AVAILABLE

321
Q

WHEN TO DECLUTTER HUD

A

SEL LDG FLAP

322
Q

OEI LAND 2/3

A

AP CONTROLS RUDDER
MANUAL TRIM INHIBITED

323
Q

OEI

AUTOLAND XWC

A

25 KTS
AUTOLAND APPROVED OEI

324
Q

OVERWT LANDING

FLAP EXT AND COMMAND SPD

A

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

325
Q

787 VERTICAL OFFSET

A

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

326
Q

ISFD USE ON BASE

A

SAME AS JUMBO
PICKS UP GLIDESLOPE EARLIER THAN HUD

327
Q

EDTO

TS CONSIDERED?

A

NO NOT BY THEMSELVES
UNLESS CEILING VIS LESS THAN ADEQ MIN

328
Q

OEI CRUISE LEVELS

A

MAX WT FL180s
LGT WTS FL330

DURING FLT LIKELY MID FL200s

329
Q

DRIFTDOWN

AFDS MODES

A

NORMALLY VNAV
BASIC MODES AS BACKUP IE FLCH AND HOLD THR AT MAX

330
Q

FAM ALLOWS ONE CB WE CAN RESET

A

FLT DECK IPAD CHARGER
2 STEP PROC AS NEED TO CONFIRM IN FLT

331
Q

ALTERNATE GA PROC

A

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

332
Q

V1 CUT

TARGET ATT
ROTATION RATE

A

DEPENDS ON OPT
APPROX 11 DEG
ROTATE SLOWLY TO 9 DEG UNTIL GEAR UP THEN HIGHER
ENSURES ACFT ALWAYS ABOVE V2

333
Q

OVERWT LDG

DIFF FLARE?

A

IF F20 THINK ABOUT FLARING BUT VERY MINIMAL

334
Q

CAN 787 AUTOLAND OVERWT?

A

NO NOT CERTIFIED
NEED MANUAL LDG

335
Q

OEI

TARGET THR SETTING ON APP

A

APPROX 65%
DEPENDS ON WT AND CONFIG

336
Q

OEI

GA PROC

A

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

337
Q

NNC

NAV AIRSPEED DATA

A

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

338
Q

VHHH

NOTES

A

090-230 WINDS > 15 KTS CAN EXPECT SIGN WS AND TURB
MICROBURSTS > 30 KTS AND FUEL CAV
LOCAL DETECTION TO 3 NM

339
Q

VHHH

ALERTS

A

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)

340
Q

EICAS MSG GROUPING

A

GROUPED BY PRIORITY LEVEL
WITHIN EACH LEVEL SHOWN IN ORDER THEY APPEARED
NEWEST AT TOP OF LIST

341
Q

AOA SPD HAS LIMITATIONS

A

ERRATIC DURING CONFIG CHANGES
INACCURATE AT HIGH SPEEDS

342
Q

SEC MODE

2 MODES FOR ELEV FEEL

A

FOR FLAPS UP AND EXT

PITCH SENSITIVITY INCREASED SO AVOID ABRUPT CONTROL INPUTS AND HIGH MAN LOADS

343
Q

1 ST SEGMENT

A

TO 35’

POSITIVE

344
Q

2ND SEGMENT

A

35’ TO 400’

2.4%

345
Q

3RD SEGMENT

A

ACCEL @ 400’

1.2%

346
Q

4TH SEGMENT

A

CLEAN ENROUTE CLIMB

1.2%

347
Q

TAKEOFF SEGMENT

SUMMARY

A

POSITIVE
2.4%
1.2%
1.2%

THESE ARE GROSS GRADIENTS
NET CAN BE REDUCED BY 0.8%

348
Q

APPROACH CLIMB PERF

A

OEI @ 1.5 Vs
2.1 % GRADIENT

349
Q

LANDING CLIMB PERF

A

AEO @ 1.3 Vs
CLIMB GRADIENT 3.2%

350
Q

AIRSPEED UNRELIABLE

MEM ITEMS

A

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

351
Q

AOA SPD

DERIVED

A

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

352
Q

GPS ALT

A

BACKUP ALT FROM GPS DATA

353
Q

2D APP PROC

A

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

354
Q

AIRSPEED UNRELIABLE

WHAT FLT MODE

A

EICAS FLIGHT CONTROL MODE
IS SEC MODE

355
Q

IF AOA SPD UNREL

A

MAY SEE ISFD SPD
USES C PITOT

356
Q

TURB PENETRATION SPEED

A

290 < 25k
310/ .84 WHICHEVER LOWER >/ 25k

357
Q

WHICH PORTS DONT HAVE HEATING ON 787

A

STATIC PORTS NO HEATING

358
Q

AIRSPEED UNRELIABLE

EXPLAIN SYSTEMS

A

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

359
Q

AIRSPEED UNRELIABLE SUMMARY

A

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

360
Q

507

ICAO HOLD SPEEDS

A

0-14 230
14-20 240
20-34 265
>34 .83

361
Q

507

AUST HOLD SPEEDS

A

0-14 230
14-20 240
>20 265

362
Q

507

FAA HOLD SPEEDS

A

0-6000 200
6-14 230
>14 265

363
Q

507

HOLD TIMINGS

A

<14 k 1 MIN
>14 k 1.5 MINS

364
Q

507

FMC HOLDING

A

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 L6 PPOS

365
Q

507

HOLD PG TERMS

A

EFC
EXPECT FURTHER CLEARANCE UPDATES DOWNTRACK ETA AND FUEL

HOLD AVAIL
HOLD TIME BEFORE NEEDING FUEL RESERVES

366
Q

507

WHEN HOLDING IN ALT OR VNAV ALT WHAT ACTION IS REQD TO PERMIT VNAV PTH DESCENT AFTER EXITING HOLD

A

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

367
Q

WHY MUST TERR OR VSD BE DISPLAYED ON AT LEAST ONE ND DURING RNP AR APCH

A

BACKUP TOTAL FMC FAILURE AND LOSS LNAV TRACKING

368
Q

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

A

CANT TRACK AROUND THE WX MAY NEED DIFF APP?

369
Q

WHEN IS VERTICAL NPS FIRST DISPLAYED ON ARR

A

TOD WITH VALID VNAV PTH

370
Q

WHEN IS LATERAL NPS FIRST SHOWN ON DEP

A

LNAV @ 50’

371
Q

WHAT HAPPENS ON LATERAL OR VERTICAL NPS WHEN ANP EXCEEDS RNP

A

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

372
Q

WHAT ALT CAN AP BE ENGAGED TO ON AN RNP AR APCH

A

135’ AGL

373
Q

WHAT IS THE DIFF BETWEEN A PROPRIETARY RNP AR AND ICAO RNP AR

A

DIFFERENT CRITERIA

374
Q

WHAT IS THE DEFAULT DME AND VOR UPDATING IN 787 FMC

HOW IS THIS RELEVANT TO RNP AR APCH OPS

A

VOR DME OFF UPDATING
DME DME AS NEEDED

375
Q

CAN ANY MODIFICATIONS BE MADE TO RNP AR APCH PROCEDURE LOADED FROM FMC DATABASE

A

ONLY SPD PROVIDED NOT ABOVE MAX SPD ON CHART
CAN CHANGE FAF TO AT ALT IF CODED AT OR ABOVE

376
Q

WHAT APP CAN IAN BE USED FOR

A

ALL APP
EXCEPT
ILS GLS RNP AR APCH

377
Q

HOW LONG IS AWIS QNH VALID FOR WHEN OPERATING TO A CTAF R APT AND CONDUCTING RNP AR APCH

A

15 MINS FROM RECEIPT

378
Q

CALC TIME FOR A HOLD PATTERN

A

<20 k 2 MIN TURNS
PLUS
2 * LEG TIME

SO APPROX 6 MINS

379
Q

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

A

AR APP HAS INTEGRITY CHECKING PRIOR LOADING FMC NAV DATABASE OTHER APPs DONT

RNP AR ALSO TRK TO FIX, RADIUS TO FIX OR OTHERS

380
Q

WHAT IS THE BASIS FOR OBSTACLE CLEARANCE DURING RNP AR INSTRU APP PROC

A

VERTICAL NAVIGATION BUDGET

381
Q

RNP AR

LARGE FONT SPD

A

LARGE FONT SPD ON LEGS PG IS LIMIT FOR RADIUS OF TURN DO NOT EXCEED (RARE NORMAL SPD)

382
Q

WHAT IS ON APPROACH LOGIC

A

MCP CAN BE SET 300’ ABOVE AND REMAIN VNAV
SPD PRIOR FROM VNAV PTH TO VNAV SPD IF FAST AND HIGH

383
Q

HOW TO GET FMC OUT OF ON APPROACH LOGIC

A

TOGA
LANDING
OR >MAPT

384
Q

HOW CAN ISSUE OF MISSET QNH BE MITIGATED DURING PBN APP

A

CHECK VSD

385
Q

WHY DOES RNP AR APCH HAVE CHARTED TEMP LIMITS

A

CHART VALID FOR ALL TEMPS WITHIN

386
Q

ARE COLD WX CORRECTIONS APPLIED TO DA FOR RNP AR APCH

WHAT ABOUT MSA?

A

NO ONLY FOR MSA

387
Q

WHAT DIRECT TO TRACKING REQMTS APPLICABLE TO RNP AR APCH? WHAT ABOUT CLASS G AIRSPACE

A

WITHIN 30 DEG INT LIP
LATEST INTERCEPT POINT

388
Q

WHEN ARE YOU ON APPROACH LOGIC

A

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

389
Q

MISSED APP REQMTS FOR PBN APP

A

OUTSIDE NPS LIMITS
NAV UNABLE RNP EICAS
FMC VERIFY POSITION

390
Q

OBSTACLE CLEARANCE FOR MISSED APP

A

AUST
2.5% 100’ IF CLIMBING 152’/ NM
HIGHER GRADIENT LISTED ON CHART

TERPS IN USA
3.3%

391
Q

WHAT IS THE DEFINITION OF DAY OR NIGHT VISUAL APP REQMTS IN QRH PBN PROC GEN

A

IF NAV INTEGRITY IN DOUBT BUT VISUAL REF IN CIRCLING AREA CAN CONTINUE WITHOUT MAKING MISSED APP

392
Q

GPWS

TIME TO IMPACT

A

CAUTION
40-60 SECS

WARNING
20-30 SECS

393
Q

GPWS WS ALERT

A

OVERRIDES ALL PWS TCAS OTHER GPWS WARN

394
Q

WHAT DIFFERENTIATES GPWS CAUTION AND WARNING

A

PULL UP

395
Q

WHAT ARE TARGET PERF PARAMETERS FOR GPWS MAN

A

MAX THR
PITCH 20 DEG
WINGS LEVEL
SB RETRACT

396
Q

DIFF BETWEEN GPWS AND WS MAN

A

PITCH 20 DEG VERSUS 15 DEG

397
Q

DOES TOGA GUIDANCE PROVIDE GUIDANCE FOR GPWS RESPONSE

A

NO WE DONT PRESS TOGA

398
Q

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

A

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

399
Q

OPT FLAP SETTING SCEL

A

DONT USE OPTIMUM
HARD WIRE FLAP SEL

400
Q

SCEL

HOW DO U IDENTIFY BRANCH PT FMC

A

TOP CDP
DECISION PT
PUT ON FIX PG

401
Q

SCEL

HOW WILL U ALTER RNP REQD FOR DEP

A

WONT TOUCH AEO
WILL NEED TO VERIFY IN EVENT OF OEI
USE ND AS NO GUIDANCE FOR WHICH PG TO LOOK AT

402
Q

WHAT ARE TRAPS WITH ENTERING LOWER RNP

A

REMAINS IN LARGE FONT UNTIL DELETED

403
Q

CRITERIA FOR EO SID LOADING

WHERE IS IT LOCATED

A

WE DONT LOAD OR CHECK
LOCATED DEP ARR LAST PG

404
Q

SCEL

REQMTS FOR OEI BEFORE AND AFTER BRANCH PT

A

BEFORE FOLLOW EO SID
AFTER AS PER CDP

405
Q

SCEL

WHEN CAN EO SID BE DISCONTINUED?

A

AS PER CDP
ABOVE MSA?

406
Q

SCEL

WHEN TO EXEC EO SID

A

IMPORTANT ONCE ACFT UNDER CONTROL
EXEC PRIOR TO BRANCH PT

407
Q

FIRE ENG

MEM ITEMS ON GND

A

NOT REQD
EITHER ECL OR QRH

408
Q

WHEN IS THE SECOND BOTTLE DISCHARGED FOR AN ENG FIRE WHEN ON THE GND

A

PART EVAC CHECKLIST

409
Q

ALTN PG

DIVERT NOW

A

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

410
Q

NPS

A

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’

411
Q

RNP AR OBST CLR

A

INITIAL (NORMAL) 1000’
INITIAL (TERRAIN) 2000’
INTERMED 500’

412
Q

RNP AR

CONTAINMENT

A

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

413
Q

EQUIP NEEDED RNP AR APCH

ALL ON ONE SIDE

A

1 * FMC
1 * CDU
1 * PFD + ND
1 * FD

414
Q

GPWS CALL-OUTS

2500’
1000’

A

VERIFY AGAINST ALT
ARE THEY REASONABLE?

415
Q

WX RADAR USE

CRZ

A

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

416
Q

WX RADAR USE

DES

A

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

417
Q

FO IMPACT DRILL

LAND

A

COMPLETE CHECKLIST
TAKE TORCH NOTOC LOADSHEET
PROCEED TO CABIN AND RELAY EVAC COMMAND
EVAC FIRST AVAILABLE EXIT
REPORT TO EMERG SERVICES IF AVAIL

418
Q

FO IMPACT DRILL

DITCH

A

COMPLETE CHECKLIST
FIT LJ AND TAKE TORCH
PROCEED TO CABIN OR AS DIRECTED BY CAPT
WHEN ALL ASSISTANCE RENDERED EVACUATE

419
Q

RNP AR

PROC

A

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

420
Q

GPWS

QRH MAN

A

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

787 (33 decks)

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