a320-npa approach (selected)
DESCRIPTION
A320 procedure for Non PrecisionApproachTRANSCRIPT
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PFPF PNFPNFNON PRECISION APPROACH (SELECTED)
MDA/H
FLYING REF : TRACK/FPA (FPD)
A320 - Version 03a
FAF
Final APPInterm. APP
IAF
Initial APP
D
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PFPF PNFPNF1.a. INITIAL APPROACH
SEAT BELTS.......ON/AUTO ENG MODE sel .........AS RQRD
NAV ACCURACY ..........MONITOR
When cleared to 3700 ft :DESCENT .........INITIATE
LS P/B is OFF except for LOC only approaches.
BARO REF : QNHAPPROACH C/L
VAPP SPEED CSTR AT FAF..INSERT
FMA
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PFPF PNFPNF1.b. INITIAL APPROACH
When ATC gives radar vectorHDG SELECT
Manual Approach phase activation on the PERF page
FMAApprox 15 NM from touchdown :APPR PHASE....ACTIVATEPOSITIONING....MONITORMANAGED SPEEDCHECKSPEEDBRAKES.AS RQRD
ND MODE RANGE.AS RQRD ND MODE RANGE AS RQRD
APPRphase
NO AUTOACTIVATION :
For Lateral positioning properly monitor F-PLN sequencing
For Vertical positioning : Use the Energy Circle
D
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PFPF PNFPNF2. INTERMEDIATE APPROACH
When cleared for approach :TRK/FPASET
TCASTA or TA/RA
RADAR TILT..............ADJUST
FLAPS 1At green dot speed below VFE next :
DECEL TOWARDS S SPEED....CHECK
FLAPS 2At S speed, below VFE next :
DECEL TOWARDS F SPEED.CHECK
ECAM WHEEL PAGE...CHECK
GROUND SPOILERS.ARM
AUTO BRAKECONFIRM
GEAR DOWNWhen FLAPS 2 :
When L/G down, below VFE next FLAPS 3FLAPS FULLWhen FLAPS 3, below VFE next :
DECEL TOWARDS VAPP CHECK
FMA
TRK FPA
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PFPF PNFPNF3.a. FINAL APPROACH
Check that the A/C is actually on the descent path : Slope gradient () calculation :
FMA
GO AROUND ALTITUDE...SET
ANNOUNCE..GA ALT xx FT SET
A/THR...CHECK SPEED MODE
0.3 NM before the FAF :FPA TO FINAL APPROACH PATH...SET AND PULL
After the FAF :
ANNOUNCESET GA ALT xx FT
Bird below the horizon
Consistent V/S
() =(%) x 0.6
PNF Xchecks Altitudes and Distances withLanding charts
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PFPF PNFPNF3.b. FINAL APPROACH
SLIDING TABLESTOW
WING A. ICE (if not required)..OFF
EXTERIOR LIGHTSSET
SLIDING TABLE.STOW
LDG MEMO .......CHECK NO BLUE
CABIN REPORT..OBTAIN (CM1)
CABIN CREWADVISE
FLT PARAMETERS...CHECK
LANDING C/L
OBSERVE ECAM MEMO
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PFPF PNFPNF3.c. FINAL APPROACH
At MDA/H +100 ft :
MONITOR OR ANNOUNCE..ONE HUNDREDABOVE
MONITOR OR ANNOUNCE..MINIMUMAt MDA/H :
ANNOUNCE ....LANDINGor GO AROUND/FLAPS
MDA/H
AP offFDs offSet Runway Track
LANDING
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PFPF PNFPNF1.a. INITIAL APPROACH
SEAT BELTS.......ON/AUTO ENG MODE sel .........AS RQRD
NAV ACCURACY ..........MONITOR
When cleared to 3700 ft :DESCENT .........INITIATE
LS P/B is OFF except for LOC only approaches.
BARO REF : QNHAPPROACH C/L
VAPP SPEED CSTR AT FAF..INSERT
FMA
NAV ACCURACY
When GPS PRIMARY avail No NAV ACCURACY required
When GPS PRIMARY lost Use raw data to checkNAV ACCURACY
+
PROG
If the FMGS detects low NAV ACCURACY, then theenhanced modes of the EGPWS are automaticallydeactivated
If check is negative use Selected guidancefor ILS interception
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PFPF PNFPNF1.a. INITIAL APPROACH
SEAT BELTS.......ON/AUTO ENG MODE sel .........AS RQRD
NAV ACCURACY ..........MONITOR
When cleared to 3700 ft :DESCENT .........INITIATE
LS P/B is OFF except for LOC only approaches.
BARO REF : QNHAPPROACH C/L
VAPP SPEED CSTR AT FAF..INSERT
FMA
STABILIZED APPROACH
Entering VAPP as SPEED CONSTRAINT at FAF ...
will displace the upstreamD
D.
F-PLN Apage ND
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PFPF PNFPNF1.b. INITIAL APPROACH
When ATC gives radar vectorHDG SELECT
Manual Approach phase activation on the PERF page
FMAApprox 15 NM from touchdown :APPR PHASE....ACTIVATEPOSITIONING....MONITORMANAGED SPEEDCHECKSPEEDBRAKES.AS RQRD
ND MODE RANGE.AS RQRD ND MODE RANGE AS RQRD
APPRphase
NO AUTOACTIVATION :
For Lateral positioning properly monitor F-PLN sequencing
For Vertical positioning : Use the Energy Circle
D
with navaid raw data
ROSE VOR ARC, or..
PFPF PNFPNF
NM
NM
:
NM
GS TAS /
NM
NM
:
NM
GS TAS/
ROSENAV
ROSE VOR,or
NM
NM
:
NM
GS TAS /
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PFPF PNFPNF1.b. INITIAL APPROACH
When ATC gives radar vectorHDG SELECT
Manual Approach phase activation on the PERF page
FMAApprox 15 NM from touchdown :APPR PHASE....ACTIVATEPOSITIONING....MONITORMANAGED SPEEDCHECKSPEEDBRAKES.AS RQRD
ND MODE RANGE.AS RQRD ND MODE RANGE AS RQRD
APPRphase
NO AUTOACTIVATION :
For Lateral positioning properly monitor F-PLN sequencing
For Vertical positioning : Use the Energy Circle
D
F-PLN SEQUENCING
F-PLAN is automatically sequenced in case of radial inbound
FAF
CQFU
IN BND
INTCP
No NAV mode
NO SEQUENCING
FAFC
B
A
TOGA
SEQUENCING
FAF
NAV mode
GO AROUND mode :
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PFPF PNFPNF2. INTERMEDIATE APPROACH
When cleared for approach :TRK/FPASET
TCASTA or TA/RA
RADAR TILT..............ADJUST
FLAPS 1At green dot speed below VFE next :
DECEL TOWARDS S SPEED....CHECK
FLAPS 2At S speed, below VFE next :
DECEL TOWARDS F SPEED.CHECK
ECAM WHEEL PAGE...CHECK
GROUND SPOILERS.ARM
AUTO BRAKECONFIRM
GEAR DOWNWhen FLAPS 2 :
When L/G down, below VFE next FLAPS 3FLAPS FULLWhen FLAPS 3, below VFE next :
DECEL TOWARDS VAPP CHECK
FMA
TRK FPA
It is recommended to select FLAPS FULL atVFE next - 15 knots to minimize flaps wear.It is recommended to select FLAPS FULL atVFE next - 15 knots to minimize flaps wear.
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PFPF PNFPNF3.a. FINAL APPROACH
Check that the A/C is actually on the descent path : Slope gradient () calculation :
FMA
GO AROUND ALTITUDE...SET
ANNOUNCE..GA ALT xx FT SET
A/THR...CHECK SPEED MODE
0.3 NM before the FAF :FPA TO FINAL APPROACH PATH...SET AND PULL
After the FAF :
ANNOUNCESET GA ALT xx FT
Bird below the horizon
Consistent V/S
() =(%) x 0.6
PNF Xchecks Altitudes and Distances withLanding charts
GO AROUND ALTITUDE
In some cases the G/A ALT is under the current altitude of the A/C
The pilot should delay the G/A ALT selection below G/A ALT
G/A ALT
GO AROUND ALT ................SET
GO AROUND ALT ................SET
Delay it
If the GO AROUND setting is not done correctly ALT * will engage
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PFPF PNFPNF3.b. FINAL APPROACH
SLIDING TABLESTOW
WING A. ICE (if not required)..OFF
EXTERIOR LIGHTSSET
SLIDING TABLE.STOW
LDG MEMO .......CHECK NO BLUE
CABIN REPORT..OBTAIN (CM1)
CABIN CREWADVISE
FLT PARAMETERS...CHECK
LANDING C/L
OBSERVE ECAM MEMO
FLT PARAMETERS
10
SINK RATESPD
Speed Target+10 ktVAPP - 5kt
Vapp
10 10
PITCH10 10
+10
-2.5
BANK
1010
7
1000 ft/min
&
Vapp
Announce any deviation in excess of FLT PARAMETERS :
_ FT HIGH or LOW
At altitude check points
COURSE
1/2 dot(VOR)
5 ADF