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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
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
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 SPEED……………………………CHECKSPEEDBRAKES…………………………….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
PFPF PNFPNF2. INTERMEDIATE APPROACH
When cleared for approach :TRK/FPA………………………………………SET
TCAS……………………………………TA 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 BRAKE……………………………CONFIRM
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
PFPF PNFPNF3.a. FINAL APPROACH
Check that the A/C is actually on the descent path : Slope gradient (θ) 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 :
ANNOUNCE……………”SET GA ALT xx FT”
Bird below the horizon
Consistent V/S
θ(°) = θ(%) x 0.6
PNF Xchecks Altitudes and Distances withLanding charts
PFPF PNFPNF3.b. FINAL APPROACH
SLIDING TABLE………………………………STOW
WING A. ICE (if not required)…………………..OFF
EXTERIOR LIGHTS………………………………SET
SLIDING TABLE……………………………….STOW
LDG MEMO ……..…….....………CHECK NO BLUE
CABIN REPORT………..OBTAIN (CM1)
CABIN CREW……………………ADVISE
FLT PARAMETERS…………………….…..CHECK
LANDING C/L
OBSERVE ECAM MEMO
PFPF PNFPNF3.c. FINAL APPROACH
At MDA/H +100 ft :
MONITOR OR ANNOUNCE………..”ONE HUNDREDABOVE”
MONITOR OR ANNOUNCE………………..”MINIMUM“At MDA/H :
ANNOUNCE ....…………………………”LANDING”or …………………“GO AROUND/FLAPS”
MDA/H
AP offFDs offSet Runway Track
”LANDING”
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
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
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 SPEED……………………………CHECKSPEEDBRAKES…………………………….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 •••••• /••
•••• •••°
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 SPEED……………………………CHECKSPEEDBRAKES…………………………….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 :
PFPF PNFPNF2. INTERMEDIATE APPROACH
When cleared for approach :TRK/FPA………………………………………SET
TCAS……………………………………TA 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 BRAKE……………………………CONFIRM
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.
PFPF PNFPNF3.a. FINAL APPROACH
Check that the A/C is actually on the descent path : Slope gradient (θ) 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 :
ANNOUNCE……………”SET GA ALT xx FT”
Bird below the horizon
Consistent V/S
θ(°) = θ(%) 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
PFPF PNFPNF3.b. FINAL APPROACH
SLIDING TABLE………………………………STOW
WING A. ICE (if not required)…………………..OFF
EXTERIOR LIGHTS………………………………SET
SLIDING TABLE……………………………….STOW
LDG MEMO ……..…….....………CHECK NO BLUE
CABIN REPORT………..OBTAIN (CM1)
CABIN CREW……………………ADVISE
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