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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