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