PFPF PNFPNFHYD : G+Y SYS LO PRHYD : G+Y SYS LO PR
CONFIGURATION
FINAL APPRGO AROUND
LANDING GEAR EXTENSION
LANDING & DECELERATION
DUAL HYDRAULIC
LAND ASAP
HYD G RSVR LO LVLHYD Y RSVR LO LVL
ECAM ACTIONS
DECISION
A320 - Version 03a
PFPF PNFPNF
DETECTION
ECAM ACTIONS
FLIES THE AIRCRAFT
NAVIGATES
CONSIDER AUTOMATION USE
PFCOMMUNICATES
1. HYD G RSVR LO LVL
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
MASTER CAUTION : No immediate action required,However, execute the ECAM actions as soon as possible
In this case, PTU can overheat and lead to a Yellow HYD SYS Overheat
DUAL HYD FAILURE
!
PFPF PNFPNF
DETECTION
ECAM ACTIONS
FLIES THE AIRCRAFT LOSS OF AP
NAVIGATES LAND ASAP…Short term decision
CONSIDER AUTOMATION USE
DECISION
2. HYD G + Y SYS LO PR
USE SUMMARY…………..….……..CRUISE part
RETURN TO NORMAL TASK SHARING
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
ECAM PROCEDURE
SYSTEM DISPLAY
STATUS
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
PF
COMMUNICATES : MAYDAY message
THS is FROZEN
PFPF PNFPNF3. APPROACH PREPARATION
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
ANNOUNCE…………..”YOU HAVE CONTROL ?”
ECAM STATUS……………………….REVIEW
SUMMARY…………..………………………USE
FMGS…………………………………PREPARE
APPR BRIEFING ............……………PERFORM
APP BRIEFING :
STANDARD
+
STATUS
+
SUMMARY APP, LDG & G/A sections
QRH
1.00
FMGS PREPARATION :
STANDARD
+
MANUAL INSERTION OF VAPPVAPP
ANNOUNCE………………...”I HAVE CONTROL”
PFPF PNFPNF
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
FLAPS EXTENSION ………………USE SUMMARY
When CONF 3 and VAPP
L/G GRAVITY EXTENSION PROC…READ & DOQRH
2.00
Fly a stabilized approach
4. APPROACH
THS is FROZEN
APPROACH SYNTHESIS
PFPF PNFPNF
FLIGHT IS FROZEN TO PERMIT THE PROCEDURE APPLICATION ON THE M/FTD
Roll control is affected by loss of spoilers
SLATS will be slow
FLAPS are lost
SYSTEM PAGE ANALYSIS
SLATS will be slow
FLAPS are lost
BG Y
PFPF PNFPNF
LDG CONF
FULL
VLS
MCDU PERF APPRpage
• Select CONF FULL
• Read VREF = VLS CONF FULL
• Add 25 kt to VREF
• Enter VAPP manually
LDG CONFCONF 3 LDG in CONF 3 :
Select CONF 3
VAPP
VAPP = VREF + VREF (25 kt) VREF is given:
• On the ECAM, and• On the summary
APPROACH SPEED COMPUTATION
Check that NEW DESThas been entered
Ensure that VLS & VAPP are basedon the proper weight at destination
PFPF PNFPNF
STATUS
E/WDPROC
INCRZ
APPPREP
APP
DECISION
VAPP
BRIEFING
1
2
3
4
5
6
7
8
USE OF SUMMARY
PFPF PNFPNF
STATUS
E/WDPROC
INCRZ
APPPREP
APP
DECISION
VAPP
BRIEFING
1
2
3
4
5
6
7
8
USE OF SUMMARY
PFPF PNFPNF
ALTERNATE LAW :
Autotrim function through the elevator
DIRECT LAW :
No autotrim, but The average elevator positionbefore gear extension is used as zero input position
Aircraft stabilization at Vapp before gear extension, ensures a proper zero input position.
This is especially useful in case of go around
THS IS FROZEN
UPON
LANDING GEAR
EXTENSION
PFPF PNFPNF
ALTERNATE LAW :
Autotrim function through the elevator
DIRECT LAW :
No autotrim, but The average elevator positionbefore gear extension is used as zero input position
Aircraft stabilization at Vapp before gear extension, ensures a proper zero input position.
This is especially useful in case of go around
THS IS FROZEN
UPON
LANDING GEAR
EXTENSION
PFPF PNFPNF
CONFIGURATION
LDG WITH FLAPS JAMMED
UNSUAL SEQUENCE CONFIG 1, 2, 3
GO AROUNDGEAR CANNOT BE RETRACTED
(DOORS WILL REMAIN OPEN)
LANDING GEAR EXTENSION
L/G GRAVITY EXTENSION
LANDING & DECELERATIONBE AWARE OF :
HIGH PITCH
NO ANTISKID, NO REVERSER(BRK PRESSURE MONITORED BY PNF)
PARTIAL LOSS OF GRND SPOILERS
DISREGARD USE MAN PITCH TRIM ON FMA
ALTN LAW
DIRECT LAW
APPROACH SYNTHESIS