PFPF PNFPNFENGINE FAILURE IN CRUISE (WITH DAMAGE)

Detection

ENGINEFAILURE !

ECAMactions

SDanalysis

STATUS

STANDARD

FIXEDSPEED

OBSTACLE

SITUATIONASSESSMENT

STRATEGYDECISIONS

A320 - Version 03

PFPF PNFPNF

ECAM PROCEDURE

ECAM ACTIONS

1. ENG 1 FAIL

DETECTION

PFCOMMUNICATES

FLIES THE AIRCRAFT

NAVIGATES LAND ASAP…Short term decision

CONSIDER AUTOMATION USE

THRUST LEVERS………………………….MCT

A/THR………………………………………..OFF

STOP ECAM actions when :

Deceleration Not below Green Dot

OrOrAndAnd

PFPF PNFPNF2. OBSTACLE STRATEGY

Check GREEN DOT GROSS CEILING

For descent :

GREEN DOT……………………….SET AND PULL

DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR ceiling ...

MCT

Thrust MCT

EO

During descent to Drift Down Ceiling ...

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

PFPF PNFPNF

ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE

ECAM PROCEDURE

ECAM ACTIONSDAMAGE ?

SYSTEM DISPLAY

STATUS

DECISION

RETURN TO NORMAL TASK SHARING

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

APU normal flight envelope :

Consider APU Start DIST & FUEL computations to Landing

•••• •••• •••••••••••••••••••

3. ECAM ACTIONS… DAMAGE

FCOM

3.01.49

PFPF PNFPNF4. OBSTACLE STRATEGY

When obstacles are cleared :

LR CEILING………………………..SET AND PULLLR SPEED….…………………………………….SET

Reaching LR CeilingA/THR….…………….………………………..…...ON

Descent to landingRESUME MANAGED MODES

T/D

Thrust is IDLE

Drift Down Ceiling

A/THR

LRC ceiling

LR SPEED

LONGRANGECRUISE

QRH

4.00

If obstacle : Continue Drift Down Procedure

PFPF PNFPNF

ECAM PROCEDURE

ECAM ACTIONS

1. ENG 1 FAIL

DETECTION

PFCOMMUNICATES

FLIES THE AIRCRAFT

NAVIGATES LAND ASAP…Short term decision

CONSIDER AUTOMATION USE

THRUST LEVERS………………………….MCT

A/THR………………………………………..OFF

STOP ECAM actions when :

Deceleration Not below Green Dot

OrOrAndAnd

A/THR is set to OFF immediately to avoidthrust reduction to IDLE

A/THR is set to OFF immediately to avoidthrust reduction to IDLE

PFPF PNFPNF2. OBSTACLE STRATEGY

Check GREEN DOT GROSS CEILING

For descent :

GREEN DOT……………………….SET AND PULL

DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR ceiling ...

MCT

Thrust MCT

EO

During descent to Drift Down Ceiling ...

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

STRATEGY

FIXED SPEED

ETOPS constraint

As establishedbefore dispatch,

use:

M.82 / 330 KT

Or

M.82 / 310 KT

STANDARD

No obstacle and time constraint

OBSTACLE

To ensure the margins over obstacles

PFPF PNFPNF2. OBSTACLE STRATEGY

Check GREEN DOT GROSS CEILING

For descent :

GREEN DOT……………………….SET AND PULL

DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR ceiling ...

MCT

Thrust MCT

EO

During descent to Drift Down Ceiling ...

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

PERFORMANCE CHECK

LRC and Green Dot Gross Ceiling quick check

GW at ENG FAIL

LRCCeilingLRC

Ceiling ExternalTemperature

Green DotGrossCeiling

Green DotGrossCeiling

Green Dot Gross Ceiling precise check

CRZ FL at fail

DIST TIMEINITIAL SPEED FUEL

LEVEL OFFLEVEL OFFLEVEL OFF

GW atENG FAIL

PFPF PNFPNF2. OBSTACLE STRATEGY

Check GREEN DOT GROSS CEILING

For descent :

GREEN DOT……………………….SET AND PULL

DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR ceiling ...

MCT

Thrust MCT

EO

During descent to Drift Down Ceiling ...

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

if pressed, predictions revertto dual engine predictions

!

PFPF PNFPNF

ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE

ECAM PROCEDURE

ECAM ACTIONSDAMAGE ?

SYSTEM DISPLAY

STATUS

DECISION

RETURN TO NORMAL TASK SHARING

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

APU normal flight envelope :

Consider APU Start DIST & FUEL computations to Landing

•••• •••• •••••••••••••••••••

3. ECAM ACTIONS… DAMAGE

FCOM

3.01.49

DAMAGE OR NO DAMAGE ?

CONSIDER ENGINE DAMAGE IF YOU NOTICE :

High vibration prior to engine stopped, loud noise

Stall

Any Abnormal Indication on ENG Page (such as N1 or N2 ~ 0)

No attempt of RELIGHT