pf pnf taxi & before t/o...pf pnf a330/a340-300 flight controls check rudder check “full up”...
TRANSCRIPT
PFPF PNFPNFA330/A340-300
TAXI & BEFORE T/O
LR - Version 03b
PFPF PNFPNFA330/A340-3001. TAXI INITIATION
When Taxi clearance obtained:
NOSE LIGHT..………………………..………TAXI
PARKING BRAKE...............…………...……OFF
THRUST LEVERS……………………..AS RQRD
ANNOUNCE………………….”BRAKE CHECK”
BRAKE PEDAL……………………………PRESS
FLT CTL……………………………………CHECK
TAXI CLEARANCE..………………….…..OBTAIN
ELAPSED TIME ..............……….…..…AS RQRD
BRAKE PRESSURE......……….....CHECK ZERO
ANNOUNCE………………..”PRESSURE ZERO”
FLT CTL……………………………….….…CHECK
Before Taxiing:
NW STRG DISC……..CHECK not displayed onright ECAM MEMO
Observe ECAM MEMO :
PARKING BRAKE release
( Slight residual pressure may beindicated for a short period of time )
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
PFPF PNFPNFA330/A340-3003. TAXI CHECKS
CABIN REPORT…………………RECEIVE (CM1)
FCU ALT……..………………………………CHECK
If ATC requests to maintain runway heading or incase of a radar vector procedure :
HDG…………………………………………..…..SET
FLIGHT INSTRUMENTS….…………….….CHECK
T/O BRIEFING……………………………CONFIRM
FLIGHT INSTRUMENTS…………………..….…CHECK
BEFORE T/O C/L down to the line
PFPF PNFPNFA330/A340-300
If brake fans running:
BRAKE TEMP BELOW 150°C…….CHECK
BRAKE FANS……………………………OFF
TAKEOFF/LINE UP CLEARANCE………OBTAIN
ENGINE START SEL…………………....AS RQRD
TCAS…………………………………..TA or TA/RA
PACKS 1 + 2………………………….….AS RQRD
SLIDING TABLE………………………...…..STOW
4. BEFORE TAKE OFF
minimize bird strike hazardduring take-off
APPROACH PATH CLEAR OF TRAFFIC.…CHECK
CABIN CREW………………………………….ADVISE
EXTERIOR LIGHTS………………………………..SET
SLIDING TABLE………………………………...STOW
BEFORE T/O C/L below the line
PFPF PNFPNF………………
THE END...THE END...
PFPF PNFPNFA330/A340-300
FLIGHT CONTROLS CHECK
Rudder check
“FULL UP”
“FULL DOWN”
“NEUTRAL”
“FULL LEFT”
“FULL RIGHT”
“NEUTRAL”
“FULL LEFT”
“FULL RIGHT”
“NEUTRAL”
PF moves the flight controls
PNF announces :
Bothelevators
ailerons
PF checks that PNF calls are in accordancewith the sidestick orders
PNF applies full sidestick deflections andsilently checks full travels and correct sense
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. TO CONFIG……………………………...PRESS
5. TO MEMO…………………..CHECK NO BLUE
1 2
3
4
5
FMGS updatesTAKEOFF DATA updates
- Gross Weight and CG on FUEL PRED- F-PLN (runway in use)- Flaps levers (Take-off position)- V1,VR,V2 (reinsert)- FLEX T/O temperature (reinsert)
If takeoff data / ATC clearance has changed, (or in case of RWY change)…
…update takeoff data and FMGS :
- F-PLN- Initial climb and speed limit
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
If use of radar is required, consider selecting theradar display on the PF side, and TERR ON NDon the PNF side only.
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
Switch the Radar ON and the PWS to AUTO aslate as possible to avoid hazardous emissions toground staff
Switch the Radar ON and the PWS to AUTO aslate as possible to avoid hazardous emissions toground staff
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
Set the appropriate ATC configuration for takeoff:
ATC: AUTOALT RPTG: ONATC code setTCAS: TA or TA/RATraffic sel: ABV
Set the appropriate ATC configuration for takeoff:
ATC: AUTOALT RPTG: ONATC code setTCAS: TA or TA/RATraffic sel: ABV
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
Autobrake may be armed with PARKING BRK ON.
Autobrake may be armed with PARKING BRK ON.
AUTO BRKMAX
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ECAM WHEEL page
PFPF PNFPNFA330/A340-3002. TAXI : CLEARANCE CONFIRMATION
When ATC clearance obtained: ATC CLEARANCE……………………..CONFIRM
TERR ON ND……………………………AS RQRD
1. RADAR / PWS……………………...ON / AUTO
2. ATC…………………………………………..SET
3. AUTOBRAKE………………………………MAX
4. T/O CONFIG..…………………………...PRESS
5. T/O MEMO……..…………..CHECK NO BLUE
TCAS STBY
1 2
3
4
5
Check that ECAM upper display shows“T.O CONFIG NORMAL”
Check that ECAM upper display shows“T.O CONFIG NORMAL”
PFPF PNFPNFA330/A340-300
This disarms NAV mode.
Then RWY TRK will engage at 30 ft RA and will keep the aircraft on the current TRK.
This disarms NAV mode.
Then RWY TRK will engage at 30 ft RA and will keep the aircraft on the current TRK.
HEADING PRESET
Usual case :
If HDG preset :
CLB NAV
OP CLB
FMA
PFPF PNFPNFA330/A340-300Address any changes in the clearance
Make as extensive use as possible of the displays
T/O BRIEFING CONFIRMATION FLOW
Address any changes in the clearance
Make as extensive use as possible of the displays
T/O BRIEFING CONFIRMATION FLOW
TO BRIEFING CONFIRMATION
PERFpage
F-PLNpage
4
7 RWY/SIDGW
CONF
FLXSel ALT
V1
V2
VR( optional)
3
56
21
PFPF PNFPNFA330/A340-300limitation: 300°C
auto ignition temperature of the hydraulic fluid
BRAKE TEMPERATURE LIMITATION
Without brake fan: Rely on HOT BRAKE ECAM caution (triggered at 300°C)
With brake fans running:
The fans blow on the temperature sensor, and modifies the indication
The crew cannot rely on the ECAM caution (linked to indicated value).
Brake temperature must be checked
If indicated value is above 150°C: delay takeoff
Indication on ECAM : 150° CActual Brake temperature :300° C
PFPF PNFPNFA330/A340-300
If brake fans running:
BRAKE TEMP BELOW 150°C…….CHECK
BRAKE FANS……………………………OFF
TAKEOFF/LINE UP CLEARANCE………OBTAIN
ENGINE START SEL…………………....AS RQRD
TCAS…………………………………..TA or TA/RA
PACKS 1 + 2………………………….….AS RQRD
SLIDING TABLE………………………...…..STOW
4. BEFORE TAKE OFF
minimize bird strike hazardduring take-off
APPROACH PATH CLEAR OF TRAFFIC.…CHECK
CABIN CREW………………………………….ADVISE
EXTERIOR LIGHTS………………………………..SET
SLIDING TABLE………………………………...STOW
BEFORE T/O C/L below the line
Conditions for selecting IGN/START prior to takeoff :
Consider igniter’s wear in case of continuous ignition
Conditions for selecting IGN/START prior to takeoff :
Consider igniter’s wear in case of continuous ignition
ONENG ANTI ICE (not valid for RR and CFM engines)automatically
Heavy rain or severe turbulencesexpected after takeoff
Runway with standing water
CFMGEPWRR
PFPF PNFPNFA330/A340-300
If brake fans running:
BRAKE TEMP BELOW 150°C…….CHECK
BRAKE FANS……………………………OFF
TAKEOFF/LINE UP CLEARANCE………OBTAIN
ENGINE START SEL…………………....AS RQRD
TCAS…………………………………..TA or TA/RA
PACKS 1 + 2………………………….….AS RQRD
SLIDING TABLE………………………...…..STOW
4. BEFORE TAKE OFF
minimize bird strike hazardduring take-off
APPROACH PATH CLEAR OF TRAFFIC.…CHECK
CABIN CREW………………………………….ADVISE
EXTERIOR LIGHTS………………………………..SET
SLIDING TABLE………………………………...STOW
BEFORE T/O C/L below the lineKnown nearby traffic, in visual contact
Significant potential for unwanted or inappropriateresolution advisories
The FAA recommendsselecting TA mode
PFPF PNFPNFA330/A340-300
If brake fans running:
BRAKE TEMP BELOW 150°C…….CHECK
BRAKE FANS……………………………OFF
TAKEOFF/LINE UP CLEARANCE………OBTAIN
ENGINE START SEL…………………....AS RQRD
TCAS…………………………………..TA or TA/RA
PACKS 1 + 2………………………….….AS RQRD
SLIDING TABLE………………………...…..STOW
4. BEFORE TAKE OFF
minimize bird strike hazardduring take-off
APPROACH PATH CLEAR OF TRAFFIC.…CHECK
CABIN CREW………………………………….ADVISE
EXTERIOR LIGHTS………………………………..SET
SLIDING TABLE………………………………...STOW
BEFORE T/O C/L below the lineConsider selecting packsOFF or APU bleed ON
Improved performance(TOGA)
Reduced EGT (FLEX)
Use of APU bleed is not allowed, if wing anti-ice is to be used.
To avoid the ENG THRUST LOST ECAM warning :
t
APUbleed ON
Takeoff powerapplication
At least 20 sec.
Note: Select Packs OFF at least 20sbefore applying takeoff thrust.