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