PFPF PNFPNFNAV : RA 1+2 FAULTNAV : RA 1+2 FAULT

NAV RA 2 FAULT

NAV RA 1 FAULT

DUAL RA FAULT

A320 - Version 03

PFPF PNFPNF1. NAV RA 2 FAULT

RADIO ALTIMETER2

RADIO ALTIMETER1

Captain’s side First officer’s side

Below 2500 ft :

DETECTION

ECAM ACTIONS

FLIES THE AIRCRAFT

NAVIGATES

CONSIDER AUTOMATION USE

ECAM PROCEDURE

SYSTEM DISPLAY

STATUS

PFPF PNFPNF2. NAV RA 1 FAULT

DETECTION

ECAM ACTIONS

FLIES THE AIRCRAFT

NAVIGATES

CONSIDER AUTOMATION USE

RADIO ALTIMETERDATA

When FLAPS 1 selected :

ECAM PROCEDURE

SYSTEM DISPLAY

STATUS

DECISION

PFCOMMUNICATES

LDG DISTLDG DIST

WEATHERWEATHER

OPERATIONAL ANDCOMMERCIAL

CONSIDERATIONS

OPERATIONAL ANDCOMME RCIAL

CONSIDERATIONS

NOT IFYNOT IFY

DECISIONDECISION

OPS …OPS …

PURSER / PAXPURSER / PAX

ATCATC

STAT US, or

SUMMARY

PFPF PNFPNF3. APPROACH PREPARATION

FMGS…………………………………PREPARE

APPR BRIEFING ............……………PERFORM

ANNOUNCE…………..”YOU HAVE CONTROL ?” ANNOUNCE………………...”I HAVE CONTROL”

APPR BRIEFING :

STANDARD

+

STATUS

FMGS PREPARATION :

STANDARD

+

MANUAL INSERTION OF VAPPVAPP

ANTICIPATES DIRECT LAW CONSEQUENCES

QRH

2.00

PFPF PNFPNF4. L/G DOWN

FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD

!In final stage of the APP it is recommended to fly raw data

Due to Direct Law, use of Manual Thrust is recommended

Close to the ground the Flight Director will command excessive roll rates

SYNTHESIS

DETECTION

ECAM ACTIONSECAM PROCEDURE

SYSTEM DISPLAY

STATUS

When L/G DOWN

PFPF PNFPNFAPPROACH SPEED COMPUTATION

MCDU PERF APPRpage

Select CONF FULL

Read VREF = VLS CONF FULL

Add 10 kt (VREF) to VREF

Add wind correction

Enter VAPP manually

LDG CONFCONF 3

LDG CONF

FULL

VLSVAPP

VAPP = VREF + VREF (10 kt) + wind correction

VREF is given:

On the ECAM, andOn the QRH

LDG in CONF 3 :

Select CONF 3

Check that NEW DESThas been entered

Ensure that VLS & VAPP are basedon the proper weight at destination

PFPF PNFPNF

DUAL RA FAULT

APPROACH PREPARATION:• Plan for ILS approach• CAT I only (Approach mode inhibited)• Configuration 3• Approach speed: VREF + 10

INTERMEDIATE APPROACH:•Localizer intercept ( LOC armed ) or raw data approach•Use Track- FPA

L/G DOWN:•DIRECT LAW is active & AP disconnects Final Approach:

•If LOC was engaged:•FDs off and continue with FPV

SYNTHESIS

PFPF PNFPNF1.b NAV RA 1 FAULT

DETECTION

ECAM ACTIONS

FLIES THE AIRCRAFT

NAVIGATES

CONSIDER AUTOMATION USE : A/THR, AP

PFCOMMUNICATES

RADIO ALTIMETERDATA

When FLAPS 1 selected :

1. ECAM PROCEDURE

2. SYSTEMS DISPLAYS analysis

Review FCOM 3.02 procedure (If time permits)

RADIO ALTIMETERDATA

GPWS INOP Apply extra caution to terrain clearance

FWC - R/A, DH / MINIMUM, Retard auto callouts lost

LOSS OF APPROACH MODE :FMGC

STATUS ANALYSIS

ILS APP can be flown in

LOC mode

TRK / FPA

APP MODE cannot be armed,

No GlideSlope capture (RA info is needed for GS tracking )

ANTICIPATES DIRECT LAW CONSEQUENCESLDG CONF, APPR SPD, LDG DIST

QRH

2.00

FCOM

3.02