Pack B Flashcards
What pitch is tail strike possible
8’ take off
9.5 landing
Define narrow runway
Less than 4.5 m exists either side of the main gear when the nose is on the taxiway centreline
(Air 2.1.1(5))
Considerations for taxi in snow
Engine anti ice on
Flaps up
Taxi speed
Taxi spacing behind aircraft
Type of tire
And limitations
Bias tire
Limited to 20kts for taxi distance above 5 km
Cargo overheat light indicate
Cargo temp above 32’
Shutoff valve signaled closed
Autopilot logic from 1500 feet
1500
Land 2 ASFlare rollout armed
Multi A/p and rudder control engaged
500
Runway align
2 degree slip and 5’ crab max
200 No land 3 uninhibited Electrical system isolated Left Ap - left ac bus Centre ap - batt/standby bus Right Ap - right Ac bus
100 with land 2 only
Nose up trim
50 Flare engaged 15 Idle 5 Rollout Slip removed 5' + 2 seconds Nose lowered to runway
Fire detection and extinguishing is available in the lavatory
Smoke detection only
Aural sound in lavatory and cabin
No cockpit indications of lavatory fire
Automatic fire extinguishing (located in waste cabinet)
What is PSU and how does it work
Passenger service units
Uses an oxygen generator to supply oxygen to the entire PSU when any one of these hanging masks are pulled
Last 22 minutes
Flight deck door
Locks when electric power available (removed when lost)
Locking deadbolt from cockpit prevents key entry
Key pad
Red door locked
Amber -correct emergency code entered(45)
Green- door is unlocked (5)
1 then enter will sound flight deck chime
Flight deck door in event of depressurisation
Cabin depress
Two hinged decompression panels open to equialize pressure
They contain a security grill to prevent access
Flight deck depress
The door is unlocked
Flight deck door deny
How long to prevent access
30 minutes
How can a fuel imbalance be identified
Fuel quantity gauges
Acars
Fuel config message
Mel categories and is it possible to extend MEL
A - repeat interval listed PROVISO
B within 3 days
C within 10 days
B/C can be extended for unusual circumstances (reversion, weather, delay)
Difference between tcas 7 and 7.1
‘Adjust vertical speed’ replaced with ‘level off’
TCAS 7.1 decal is placed under the flight number reminder
PLI
Pitch limit indicator
Provided at low speeds or when flaps extended
Stick shakes activation point.
Six principal concepts
Task sharing - PF/PM areas of responsibility
Crew coordination - checklist/confirmed actions
Crew Communication - stand response, call outs, briefings
Monitor and cross check - FMa annunciation a, scan, instrument monitor
Workload management - use of autopilot
Discipline - adherence to SOPs
BASIC policy
Captain and dispatcher shall secure safety of operation, maximum efficiency, maintain schedule and maximise passenger comfort.
The captain and dispatcher shall follow this policy
Disagreement between captain and dispatcher the safer option is adopted
Captain will have final responsibility
Flight dispatcher shall support the captain
Flight shall not be undertaken if crew members are unfit for duty.
4 principal concepts
Fly first
Secured and reliable operation
Effective and efficient operation
Promote standardised and uniform operation
What can indicate wind shear
Thunderstorm activity
Virgo
PIPERS
LLEAS
PWS
Two types of wind shear and when are they reported
Wind shear
Headwind 20kts
Tailwind 20-30kts
Microburst
Tailwind exceeding 30 kts
Alerts provided on initial contact and when detected
LIDAR and Doppler radar
LIDAR (only at HND and NRT)
Able to detect wind shear with precipitation
Doppler
Can perceive air current and microburst activity around the airport but requires precipitation
PWS
Area it covers?
Inhibited?
How long before it operates after turned on?
PWS function of the wx radar
Covers 25’ either side 3 nm - warning are 0.5 nm beam 3nm ground 1.5 air
12 seconds after turned on
Inhibited
warnings 100 kts to 50’
cautions 80kts to 400
Overridden by egpws wind shear /terrain
Requires visible moisture
Definition of wind shear
+- 15 kts
+- 500 fpm
5’ pitch
1 dot g/s displacement
What is maneuvering speed
Minimum speed the allow 25’ AoB with 15’ overshoot without engaging stick shaker
Autopilot limitations
Take off
200’
Wind autoland
25kts head and crosswind
Aileron trim with autoland engaged is prohibited
ACARS fuel imbalance warning
Difference is at or above 1000 lbs for 25 seconds
Above 5000 ft
Precaution system is inhited for 45 minutes after imbalance is detected and can only provide two per flight
Difference between
Windshear windshear
Windshear ahead
Go around Windshear ahead
Windshear
Egpws requires escape maneuver
Windshear ahead / go around windshear ahead
PWS warning
Takeoff - caution
Go around unless no danger is judged
Most stick shaker activations occur
Flaps up +80 to 95
Speed brake extended or in AoB
During rough air and wake turbulence
Windshear escape maneuver
Disengage AP Press GA Max thrust Disconnect AT Wings level and 15' pitch Speed brake down Follow FD
Do not change config
Do not attempt to recover lost airspeed
EGPWS
Disengage AP Disconnect AT Max thrust Wings level and 15' pitch Speed brake down Continue pitch to PLI stick shaker or initial buffet if terrain remains a threat
Do not change config
Monitor RA
Speed margin from stick shaker to stall speed
5-8 kts
RAT
Deploys automatically in dual engine failure or manually with loss both AC buses
Cannot be stowed in flight
Minimum speed 130kts
System pressure low light remains illuminated if RAT is the only source of hydraulic power
Aircraft dimensions
Height 15.85 m
Wingspan 50.88 winglets
47.57 no winglets
Length 54.94
Main gear to nose gear 22.76
Main gear to main gear 9.3
Pilot to nose gear 2.3EGPWS warnings
Mode 7 - windshear
Mode 1 - severe descent rate
Mode 2 - severe terrain closure rate
Look ahead terrain (20-30 second from impact)
Look ahead obstacle (20-30 seconds from impact)
PWS windshear warning
Items to be carried in an emergency evacuation
Captain Crash axe Megaphone Flashlight ELT(freighter) First aid kit (freighter)
First officer Signal kit Flashlight ELT (freighter) Emergency food (international and freighter)
3 GA mean
Thrust GA 2000 fpm rate of climb Pitch GA Maintain existing speed or MCP speed, higher Roll GA Maintain runway ground track
If less than flap 20, thrust mode other than GA can be selected
RTO considerations
Pax
Evacuation required?
PA address
Brake temperature
Brake cooling cart required?
Influence of taxi speed and time
Use of park brake
Mechanics
Risk of tire bursting
Information required for brake energy calculation
When is seat belt signs illuminated when selected to auto
Cabin alt above 10000
Landing gear not up and locked
Flap lever not up
Passenger oxygen on
3 levels of crm assertion
Enquire
Advocate
Assert
What is alpha mode
An airspeed below the maximum angle of attract or minimum airspeed has been commanded
IRS NAV ONLY mean
The fmc has been without radio or gps for a predetermined time
Max thrust prohibited and required?
Prohibited Antiskid inoperative Any one wheel brake inoperative Thrust reverser inoperative Runway is short (2000m) and contaminated and max tables not processed then takeoff weight must be reduced by 14000lbs
Required
Windshear encounter
What is an upset
10’ nose down
25’ nose up
45 degrees angle of bank
Inappropriate airspeed
When is HF radio use prohibited
During refuelling
What classified as significant deviations below 1000’
30' AoB \+10 -5 airspeed 1 dot on glide slope 5' 1 dot on VOT \+100ft -50ft on VNAV path
Besides equipment failure what will prevent RVSM operations
Turbulence greater than moderate
Low speed RTO
AT disconnect (enters hold 80kts)
Thrust IDLE
Manual braking (RTO arms 85kts)
Verify speedbrake up
Equipment required for rnav1 operation
1 FMS
1 IRS
1 DME/GPS
What is the psi in the Brake accumulator with the right hydraulic system failed, how is it charged
1000 psi
Gas change is maintained by maintenance
Times of useful consciousness
350
400
350 - 30 seconds
400- 12 seconds
Time of useful consciousness can be 1/3rd with Rapid decompression
What is PES
Pitch enhancement system use a hydraulic motor in the right hydraulic system and trapped system hydraulic fluid in the left system to power the stab trim during a failure of the left and centre hydraulic systems
Only electric trim will be available and it’s operation will be at 1/4 rate
When is a landing configuration warning generated
The aircraft is in flight with any gear not down and locked and
Flaps in landing position
Or
Thrust lever idle below 800 ft
What alerts cannot be cancelled using a recall button
Warning and communication
What lakers cannot be silenced to the master warning/caution resist switches
Landing config
Autopilot disconnect
TO config
Overspeed warning
When does the 750 start limit display
From when the fuel switch is in Cutoff until 10 seconds after N2 has reached 60%
Maximum speed commanded by VNAV
Econ speed vmo -16kts
Pilot entered greater than vmo -11 kts
What actions are required in the event of a tail strike
Un-annunciated checklist
Don’t pressurise
Plan to land at nearest suitable airport
ATT DISAGREE eicas
When captain/copilot symbol generations disagree by 3 degrees in pitch or roll or more for greater than 2 seconds
Max alt with CoG
Max alt reduces as cog moves forward
FMS max alt based on 25% cog, if forward of this, max alt reduced
FCC FAILURE cockpit indications
Left failure
No left FD
No land 3
Right
No right FD
No land 3
Centre with AP C command
Autopilot disconnect
Symbol generator failure
AD and HSI blank
Loss of ILS receiver
Loss of RA
Both pilots on alt, INSTR SWITCH EICAS message will display
FMC failure
No speed
Cdu blank
L FMC FAIL EICAS
note - RNAV1 not available
IRS failure
No attitude or heading info
No VSI
RMI flags
ADC failure
No ASI ALT VSI
RVSM not available
Dual FMC failure
What climb and cruise speed should be used
250 (below 10), 290/0.78)
Alt disagree
Airspeed disagree
200 ft
5 kts
Takeoff warning generated
Takeoff config warning is generated when thrust lever is advanced to the takeoff range (75%)
Warning covers
Flaps and slats Stabiliser outside green range Speed brake lever not down Parking brake valve closed Main cargo door (bcf)
Definition of first flight of the day
Domestic
True first flight of the day is JST that departs from a domestic airport
International
The flight after a planned ground stay of 3 or more hours
Go around callout criteria
Go around is PIC discretion but is strongly advised in the following conditions
- speed not withheld in Vref- Vref +20 around threshold
What parts of a/c is frost permitted prior to takeoff
Lower surface of wings
Upper part of fuselage
When is pre takeoff runups require and what is the procedure
Required
Engine anti is required and temp below 3
Procedure
Run engine up to N1 60% for 30 seconds
Check engine stability
GA logic for a multiple autopilot approach
GA is armed when flaps are out of up or GS capture
GA disarmed
Ap - 5ft plus 2 seconds
AT - aircraft is on the ground
If GA pushed when aircraft at 5 ft for greater Than 2 seconds without touching down
AT will engage in GA
AP will remain in Flare
If GA pushed when air has been below 5 ft for less than 2 seconds and on the ground
AT will remain idle
AP will engage GA
9 items on the batt bus
Emergency Fire bottle Evacuation signals IRS emergency power RAT manual deploy
Fuel
Spar fuel valves, APU fuel valve
Fuelling system
Clock
Park brake valve
FD turned on in flight what will be default mode
Alt hold if level or VS if climbing descending
HDG hold if bank less than 5’ or attitude if greater than 5’
Main batt located
E and E compartment aft of nose gear
APU batt located
Aft cargo hold, just aft of door
When does standby instrument display activate
AC power loss
Eicas fail
CRT fail
What rate does fuel jettison system jettison fuel
2600 lbs
How can fuel leak be varieties
Progress page 2
Acars
Visual
What slat are heating with engine bleed with wing anti ice on
3 outboard slats
CDL repair time and affect it has?
Not specified- but restoration should be made as soon as parts, facilities, personnel and time becomes available
Multiply cdls cannot be applied to same system
Performance penalties are cumulative
Each negligible item that exceeds 3, shall incur a 100 lb weight penalty per item.
Tcas RA
Initial
Reversal TA RA time
Initial
+/- .25 g within 5 seconds
Reversal */- .35 g with 2.5 seconds
TA - 20 -48 seconds
RA - 15 - 35 seconds
Variable with altitude (minimum is low alt)
TCAS inhibited
1450 increase Descent RA
1100 Descent RA
1000 all RA
Stabilised approach
Attitude and position correct Engine thrust appropriate \+10/-5 kts Below 5000ft - 2500 fpm 1000-2000 ft - 1500 fpm Below 1000 - 1000fpm
Exception due ATC - NAHA requires a long approach at 1000’
Items still available if APU automatically shuts down prior to engine start
Emergency evacuation system Park brake PA Interphone Left VHF Light - aisle- main panel - standby instrument Emergency cabin lighting
What unavoidable reasons can you diaper a main maintenance base or international operation with an MEL
Lack of Spare Facitlites Personnel Time
What failures necessitate an emergency Descent
Dual pax off
Cab alt
Rapid depress
Cargo fire (bcf) or main deck cargo fire (f) when within 60 nm of arrival airport
Minimum oxygen for ETOPS and what usage rate?
2 crew - 850 3 crew - 1200 4 crew - 1500 UQI (Mongolia) - 1250 Oxygen is used at 7.5 psi per person per minute
Key figures for 280,000 lbs
Dual AC bus failure-7700 ft C hydraulic failure - 4700 ft Normal land ab 3 - 6400 ft Normal to 30' - 5960 Max alt gear down - 31200 Gear down increase fuel flow - 50% Gear down speed is reduced by 20%
Electric load shedding
Single generator ops and hydraulic pump on
Both utility buses
During start
Both utility buses
Thrust levers are advance into takeoff range with engines shut down
Both utility buses
Engine shutdown in flight
Both utility buses
Respective centre fuel pump
Cabin ceiling lights
Why C1 on prior to start
To provide hydraulic power to stab trim
C1 because C2 is shed during start
What is HDG KVA
5 KVA
The HDG is not powered by the RAT so the RAT produces no electrical power (flight controls only)
RVSM requirement
Equipment 2 individual altitude systems (40' each other, 75' FE, 200' airborne) One altitude control system (AP) with alt hold One altitude alert system One mode C transponder
Aircraft not overshoot by 150’
ATC notified if greater than moderate turbulence
Onboard documents
Logs and documents folder
Airworthiness certificate Designation for operating limitations Aircraft registration certificate Aircraft station radio licence Aircraft earth radio station licence Fuel carnet card
Manuals
AOM 1,2,3 QRH MEL/CDL Operations policy manual volume 2 FPDM
Logs and documents seal broken?
Cap check each document and report it to maintenance
If docs accounted for flight can depart
If missing or damaged documents the cap shall report it to ground personnel
How much contingency fuel is required to be carried
5% of burn off or 15 minutes holding at 1500’ at destination
When is a second alternate required
Wx at destination are forecast to be below landing minima unless ceiling and vis at the alternate is 1500’ and 5000m
Approach ban
An instrument approach may not continue if the weather is below company minimums or any RVR is less than 200’
Approach ban is assessed at the following in order of priority
FAF
Outer marker
1000’
Hell what approaches can CMV be used
Only when RVR is not available
CAT 1 straight in ILS
Straight in NPA
What wx conditions will approach not be able to continue due to approach ban on a CAT 1 ILS
Ceiling VIS or RVR is below company minima
Any RVR below 200’
Is missed approach always required if loss airborne or ground equipment
No not if aircraft has required visual reference and is stable
Recognise 2000’ remaining during takeoff
Runway edge lighting change from white to amber
Solid touch down marking will be the next visible touch down markings
Runway distance markers
What does RA read during taxi either fuel in the tank, is it permitted to reset the fuel pump?
There are no battles in the centre fuel tank so sloshing during taxi may move fuel away from the inlets. Fuel pumps can be reset only once.
During climb if L/R pump EICAS message is displayed select pumps off, on once again in cruise.
What is map shift
Map shift occurs when adequate position is no available and may result in the aircraft flying with safe margins.
Errors can be detected using gps or raw data on approach
Some map services do not use wgs-84 and this may cause nuisance egpws warning in china
Largest recorded was 800m enrojte to Dalian China
Fuel config message on short final? What about during missed
Check for fuel leak page prog 2/2
If no crossfeed req continue to land
If time permits or during missed approach conduct checklist
Fuel imbalance limitations do not apply for TO and Landing
Why are FDs 8’ pitch up for TO
Minimum possible pitch angle for a tail strike
What are confirmed items, is confirmed required on the ground
Thrust lever Fuel control switches Engine, APU fire switches Cargo fire arm switch Generate drive disconnect
Does not apply during dual engine failure
Inflight only, but in the interest of safety, confirmed action will be carried out on the ground under most circumstances
Why C autopilot
Redundancy - failure of left or centre stab trim aileron lockout module (SAM), stab trim control will be automatically switched to the operating module
Cross check - left and right FCCs provide AFDS information to their respective ADI with C engaged a cross check is available across all three FCC
Rain repellent used on the windscreen?
Has been removed due to environmental concerns.
Can be used on request on R1 and L1 windows when rain is forecast
VOR Auto and Manual
Auto
Allows FMC to auto tune Nav aids
Position updating
Manual
To provide raw data cross check
To ensure correct aid is timed at all times
What quantity of hydraulic fluid is reserved with standpipe in he centre system
14%
Sim is 8%
ANA touch down zone
750’ to 2000’
Turning radius of 767
46.3m
Hydroplanning 3 types
Dynamic 2.6 mm of water film Hydroplanning speed 9 x square root of psi Nose- 160psi-114kts Main- 200psi-126kts
Viscous
With dyanamic hydroplanning or locked wheel condition
Rubber reversion
Locked wheel condition
Cannot occur in a grooved runway
Rainfall in excess of 30mm/he will cause hydroplanning condition
When should emergency landing be declared
A single hydraulic source remains
A single electric source remains
Engine fire/failure
Smoke/fire/fumes on board that cannot be controlled
Altimeters are unreliable
Checklist ‘ plan to land at nearest suitable airport’
Other condition effecting the safety of flight
How do you apply cmv conversion
CMV is a substitute for RVR when RVR is not available
It can only be used for straight in approaches
CMV cannot be used in the flight planning phase
Night/day time is sunrise/sunset as determined by PIC
At what RVR does RVR bus reporting begin
Begins at 1800 m
What are the two ANA Cat 1 classes
550m/200’
Max crosswind 10kts captain must be CAT 1/2/3 qualifies and FO must be CAT 1
1200m/200’
AOM crosswind limitation
Only a basic qualification applies
What is the required equipment onboard required for RVSM
2 independent altimeter measuring systems
Altitude height monitoring and alerting system
Autopilot with altitude hold capability
Mode C or S transponder
What is the required equipment onboard required for RNP
GPS
What is the required equipment onboard required for Rnav 1/2
GPS
DME/DME
DME/DME/IRU
What is the required equipment onboard required for rnav 5
GPS
DME/DME
VOR/DME
Ins or IRS
What is the required equipment onboard required for rnav 10
GPS
INS OR IRS
Monitor 121.5
Unavoidable situation
Using for other coms
Workload
Only one comm
Capt communication in emergency
Close contact with
ATC
Search and rescue personal
Flight dispatcher
And give sufficient consideration to advice
Eicas?
Engine indicating and crew alerting system
IRS
Align
Navigation
Magnetic track
Align
78.2 NS
Nav
87 NS
Magnetic
73 N
60S
Go around windshear ahead
On approach and landing
Perform windshear escape or normal go around
However when judged no danger, no necessary to follow.
Gpws mode 7 active takeoff
Rotation to 1500 ft
Windshear alert
Microburst alert
Windshear
Headwind 20 +
Tailwind 20-30
Mircobust
Tailwind 30+
Fail operational
Fail passive
Operational
Level of Redundancy is such that a single fault cannot prevent autoland
Passive
Level of redundancy such that a single fault cannot cause significant flight path deviation
When do deviation calls commence in approach
VOR- final Descent (for left/right) Vnav - final Descent - glidepath Bank over 30 - bank Sink rate speed loc g/s - below 1000ft Alt deviation exceed 50 ft mda - altitude
Tailskid eicas message indicate a tail strike?
It indicates tailskid position disagrees with the land gear lever position (may help determine one he occurred)
When does auto relight occur
When n2 drops below idle only with fadec
Anti ice on the ground?
10’ or below with visible moisture
(Clouds, fog With vis of 1mile, rain or snow)
10’ or below snow ice standing water slush
No mel applied leaving Haneda( main maintenance base)
And international flights leaving Japan? True?
Yes Unless unavoidable circumstances Lack of spares Time Personal
Which mel can’t be extended
Due article 60 and 61 Weather radar TCAS Flight deck door Cvr Fdr VOR/adf
4 policies
Fly first
Assure safe and reliable operations
Achieve effect and efficient operations
Promote standardised and uniform operations
9 decals
Under standby alt
300 bcf
Pws
Under gear
Winglet
HDG
LAS
Alternate L/R ADC
Wifi
Ife/cab
Maintainence panel
AvOd
FMC resync
15 seconds - 1minute
Don’t touch cdu
Useful consciousness
350 - 45 seconds
400 - 30 seconds
1/3 rapid depress
Cabin alt light
Mask drop
Outflow value auto close/open
Cabin alt light
Above 10,000
Goes out below 8,500
Mask drop
14,000
Outflow value auto close/open
11,000
9,500
Rnav 1
5
10
Fig
FMS
IRS
GPS/DME
Same except
GPS/ or DME/VOR
GPS
Ins
Cat speeds
141-165
185-250
130-185
185/265
205
Weights
International 401 400 320 288
Short international 347 345 320 288
Domestic 290.7 288.7 288.7 288 (winglets 291.3)
Take off thrust selections
Domestic
2000m + d2 f5
1999m - d1 f15
Snow/slush/flooded d1 f15
International
370+ max f5
330-370 d1 f5
330 - d2 f5
Snow etc
300 + max f15
300 - d1 f15
How captain may use other ratings due mel/cdl/runway condition/tailwind any other reason
Taxi engine fuel flow
APU
And icing
47 Ilbs/min total
APU 4 Ilbs/min
Engine anti ice 240 ibs/hour
Wing and engine 300ibs/hour
Speed using for alternate planning
LRC
99% best range
