PFPF PNFPNFENGINE FAILURE IN CRUISE (WITH NO DAMAGE)

A320 - Version 03

Detection

ENGINEFAILURE !

ECAMactions

SDanalysis

STATUS

STANDARD

FIXEDSPEED

OBSTACLE

SITUATIONASSESSMENT

STRATEGYDECISIONS

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. STANDARD STRATEGY

During descent to LR ceiling ...

MCT

Thrust MCT

EO

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

For descent :

M.78/300 KT………………………..SET AND PULL

LRC CEILING ALT……..………….SET AND PULL

Check LRC CEILING

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

•••• •••• •••••••••••••••••••

FCOM

3.01.49

3. ENGINE RELIGHT

, RELIGHTQRH

2.00

QRH

4.00

++FCOM

3.06.30

PFPF PNFPNF4. STANDARD STRATEGY

Reaching LRC ceiling

LR SPEED………………………………………….SETA/THR…………………………….………………….ON

Descent to landing

RESUME MANAGED MODES

T/D

Thrust IDLEA/THR

At LRC ceiling ...

LR SPEED

LONGRANGECRUISE

QRH

4.00

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. STANDARD STRATEGY

During descent to LR ceiling ...

MCT

Thrust MCT

EO

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

For descent :

M.78/300 KT………………………..SET AND PULL

LRC CEILING ALT……..………….SET AND PULL

Check LRC CEILING

STANDARD

No obstacle and time constraint

OBSTACLE

To ensure the margins over obstacles

STRATEGY

FIXED SPEED

ETOPS constraint

As establishedbefore dispatch,

use:

M.82 / 330 KT

Or

M.82 / 310 KT

PFPF PNFPNF2. STANDARD STRATEGY

During descent to LR ceiling ...

MCT

Thrust MCT

EO

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

For descent :

M.78/300 KT………………………..SET AND PULL

LRC CEILING ALT……..………….SET AND PULL

Check LRC CEILING

LRC AND GREEN DOT GROSS CEILING QUICK CHECK

GW at ENG FAIL

LRCCeilingLRC

Ceiling ExternalTemperature

Green DotGrossCeiling

Green DotGrossCeiling

QRH

4.00

PFPF PNFPNF2. STANDARD STRATEGY

During descent to LR ceiling ...

MCT

Thrust MCT

EO

Speed controlled by the elevator

REC MAX = EO LRC Ceiling EO CLR Prompt

QRH

4.00

For descent :

M.78/300 KT………………………..SET AND PULL

LRC CEILING ALT……..………….SET AND PULL

Check LRC CEILING

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

•••• •••• •••••••••••••••••••

FCOM

3.01.49

3. ENGINE RELIGHT

, RELIGHTQRH

2.00

QRH

4.00

++FCOM

3.06.30

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

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

•••• •••• •••••••••••••••••••

FCOM

3.01.49

3. ENGINE RELIGHT

, RELIGHTQRH

2.00

QRH

4.00

++FCOM

3.06.30

Descent to LR CRZceilingcomputations

1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime

Descent from LR CRZceiling to landingcomputations

2

QRH

4.00

Remaining distance to diversion airportFuel used in LRC FL Down to LandingTime in LRC FL Down to Landing

PERFORMANCE CHECK

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

•••• •••• •••••••••••••••••••

FCOM

3.01.49

3. ENGINE RELIGHT

, RELIGHTQRH

2.00

QRH

4.00

++FCOM

3.06.30

Descent to LR CRZceilingcomputations

1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime

Descent from LR CRZceiling to landingcomputations

2

QRH

4.00

Remaining distance to diversion airportFuel used in LRC FL Down to LandingTime in LRC FL Down to Landing

PERFORMANCE CHECK

Descent to LR CRZcomputations

FCOM

3.06.30

LRCCeiling

CRZ FL atFailure ΔDist

ΔFuelΔTime

ΔDistΔFuelΔTime

GW at ENG FAIL

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

•••• •••• •••••••••••••••••••

FCOM

3.01.49

3. ENGINE RELIGHT

, RELIGHTQRH

2.00

QRH

4.00

++FCOM

3.06.30

Descent to LR CRZceilingcomputations

1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime

Descent from LR CRZceiling to landingcomputations

2

QRH

4.00

Remaining distance to diversion airportFuel used in LRC FL Down to LandingTime in LRC FL Down to Landing

PERFORMANCE CHECK

LR Cruise to Landing computationsQRH

4.00

DiversionAirport

LR CRZ Ceiling

Fuel used in LRCFL, down to Landingbased on ref weight

Fuel used in LRCFL, down to Landingbased on ref weight

Correctionaccording toΔcomparedto reference

weight

Correctionaccording toΔcomparedto reference

weight

+ =Time in LRC FLdown to landingTime in LRC FLdown to landing

Fuel used in LRC FLDown to Landing

Fuel used in LRC FLDown to Landing

Remaining distance