Dual_HYD Fault

PF HYD : G+B SYS LO PR PRPNF Common LR 

HYD G RSVR LO LVL HYD B ENG 2 PUMP LO PR DUAL HYDRAULIC LAND ASAP ECAM ACTIONS DECISION

CONFIGURATION

LANDING GEAR EXTENSION GO AROUND

FINAL APPR

LANDING & DECELERATION LR - Version 02b

PF

PNF LR  1. HYD GCommon RSVR LO LO LVL

DETECTION  FLIES THE AIRCRAFT NAVIGATES CONSIDER AUTOMATION USE 

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE  SYSTEM DISPLAY  STATUS 

PF COMMUNICATES

PF

PNF LR  2. HYD G Common + B SYS LO PR PR

DETECTION  FLIES THE AIRCRAFT NAVIGATES

LOSS OF AP

LAND ASAP…Short ASAP…Short term decision

CONSIDER AUTOMATION USE 

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE  SYSTEM DISPLAY  STATUS  USE SUMMARY…………..….……..CRUISE part RETURN TO NORMAL TASK SHARING  STATUS,or 

DECISION 

SUMMARY

WEATHER L D G D IST IST L D GD I S T OPERATIONAL O PERATIONAL AND COMMERCIAL CONSIDERATIONS

ATC DECISION NOTIFY NO NOTIFY TIFY

PURSER /PAX /PAX /PAX OPS … OPS …

COMMUNICATES : MAYDAY :  MAYDAY message

PF

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

PF

PNF Common LR  3. APPROACH PREPARATION

ANNOUNCE……………… ANNOUNCE… ……………...”I ...”I HAVE CONTROL CONTROL” ”

ANNOUNCE…………..”YOU HAVE CONTROL ?” ECAM STATUS……………………… STATUS……………………….REVIEW .REVIEW SUMMARY…………..………………………USE FMGS…………………………………PREPARE APPR BRIEFING ............……………PERFORM FMGS PREPARATION : STANDARD +

QRH

MANUAL INSERTION OF VAPP APP BRIEFING :

A 330 : A 340 :

2.00

A340-600 :

STANDARD + STATUS QRH

+ SUMMARY APP, LDG & G/A sections

1.00

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

PF

PNF Common LR  4. APPROACH

FLAPS EXTENSION ……………… ………………USE USE SUMMARY



Fly a stabilized a stabilized approach

APPROACH SYNTHESIS

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

PF

APPROACH SPEED COMPUTATION

PNF

A330

Check that NEW DEST has been entered

Ensure that VLS & VAPP are based on the proper weight weight at destination destination

VAPP = VREF + VREF

VREF is given: •  On the QRH, and •  On the summary

VREF = 30 kt MCDU PERF APPR page

•  Select CONF FULL VAPP

VLS

LDG CONF

FULL

•  Read VREF = VLS CONF FULL •  Add  Add 30 kt ( VREF) to VREF •  Enter VAPP manually

PF

APPROACH SPEED COMPUTATION

PNF

A340-300

Check that NEW DEST has been entered

Ensure that VLS & VAPP are based on the proper weight weight at destination destination

VAPP = VREF + VREF

VREF is given: •  On the QRH, and •  On the summary

VREF = 35 kt MCDU PERF APPR page

•  Select CONF FULL VAPP

VLS

LDG CONF

FULL

•  Read VREF = VLS CONF FULL •  Add  Add 35 kt ( VREF) to VREF •  Enter VAPP manually

PF

APPROACH SPEED COMPUTATION

PNF

A340-600

Check that NEW DEST has been entered

Ensure that VLS & VAPP are based on the proper weight weight at destination destination

VAPP = VREF + VREF

VREF is given: •  On the QRH, and •  On the summary

VREF = 25 kt MCDU PERF APPR page

•  Select CONF FULL VAPP

VLS

LDG CONF

FULL

•  Read VREF = VLS CONF FULL •  Add  Add 35 kt ( VREF) to VREF •  Enter VAPP manually

PF

USE OF SUMMARY

PNF

Common LR 

E/WD PROC

1

3

DECISION

5

VAPP

   Z    R   C    N    I

STATUS

2 4 8

   P    E    R  P    P    P   A

  P  A  P

7

6 BRIEFING

PF

RAT MAN USE

PNF

Common LR 

CONSIDER CONS IDER RAT RAT MAN USE



With the RAT extended, the green SYS is recovered. 



This permits slat extension recovery.

With the RAT extended, extended, the fuel consumption consumption increases increases by approx 0.6 ~ 1 %

PF

SYSTEM PAGE ANALYSIS

PNF

Common LR  1. HYD Y SYS LO LVL DUAL HYDRAULIC

  Roll

control is affected affected by loss of spoilers spoilers

  SLATS

FLIES THE AIRCRAFT NAVIGATES

DETECTION 

are lost

OF AP LOSS  FLAPS will will

be slow

LAND ASAP…Short ASAP…Short term decision

COMMUNICATES

MAYDAY message

CONSIDER AUTOMATION USE : A/THR, AP

SLATS are lost

FLAPS will be slow

G

B

Y

2. SYSTEMS DISPLAYS analysis 3. STATUS  USE SUMMARY…………..….……..CRUISE part RETURN TO NORMAL TASK SHARING 

DECISION 

PF

PNF

SYNTHESIS Common LR 

ALTN LAW CONFIGURATION 

LDG WITH SLATS SLATS JAMMED JAMMED

LANDING GEAR EXTENSION

GO AROUND 



GEAR CANNOT BE RETRACTED (DOORS (DOORS WILL REMAIN OPEN)

LANDING & DECELERATION BE AWARE OF : 

NO ANTISKID

(BRK PRESSURE MONITORED BY PNF) 

PARTIAL LOSS OF GRND SPOILERS

L/G GRAVITY EXTENSION

PF

USE OF SUMMARY

PNF

Common LR 

E/WD PROC

1

3

DECISION

5

VAPP

   Z    R   C    N    I

STATUS

2 4 8

   P    E    R  P    P    P   A

  P  A  P

7

6 BRIEFING