Flex and Derate Takeoff and Climb

Operational Liaison Meeting – Fly-By-Wire aircraft

2004

Flex/Derate, Engine Bump and Derated climb Related issues

Customer Services

MAIN

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• FLEX TAKEOFF / DERATED TAKEOFF • BUMP • DERATED CLIMB

Flex/Derate comparison, Engine Bump and Derated climb

Page 2

Flexible Thrust Takeoff

Weight Max TOW

Conditions of application: •TREF < Tflex, •Today’s OAT < Tflex •Tflex < Tflex max

Thrust

Available Thrust

Flat rated Thrust

EGT Limit

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Actual TOW

MAXIMUM THRUST REDUCTION

Needed Thrust

This reduction level depends on A/C model OAT OAT Flex/Derate comparison, Engine Bump and Derated climb

Tref

Flex Temp

T Flex max Page 3

Flexible Thrust Takeoff Flexible Takeoff procedure: at any moment, pilot can recover TOGA

Thrust

VMC certified for TOGA thrust

TOGA Thrust

Flat rated Thrust

EGT Limit

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Flexible Thrust

OAT Flex/Derate comparison, Engine Bump and Derated climb

Tref

Flex Temp

Temperature Page 4

Derated Thrust Takeoff Each derate level is certified and is associated to a new set of performance data Certified

Certified

Certified

Certified

Certified

engine © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

engine

engine engine engine

Let’s have a look to the charts ... Flex/Derate comparison, Engine Bump and Derated climb

Page 5

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

For the A340-500/600, two new derate levels have been added: 32% and 40%

Flex/Derate comparison, Engine Bump and Derated climb

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Derated Thrust Take-off on short and contaminated runways 3900 m +32.9 tons 3500 m

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

+83.2 tons

Flex/Derate comparison, Engine Bump and Derated climb

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Derated Thrust Takeoff Derated Takeoff procedure: pilot cannot recover TOGA.

Thrust Thrust for VMC computation at DERATED TO rating TOGA Rating

Derated Rating

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Derated Thrust

OAT

Flex/Derate comparison, Engine Bump and Derated climb

OAT Page 8

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

TOGA DERATE

: VMCG = 105 kts : VMCG = 100 kts

Flex/Derate comparison, Engine Bump and Derated climb

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© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

TOGA DERATE

: VMCG = 105 kts : VMCG = 100 kts

DO NOT USE THESE FIGURES AS A REFERENCE

Flex/Derate comparison, Engine Bump and Derated climb

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ECAM Message Therefore the use of TOGA together with a set of V1/Vr/V2 for DERATE takeoff must be prevented

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

The aircraft protects the crew against MCDU typing errors during cockpit preparation Let’s see how ...

Flex/Derate comparison, Engine Bump and Derated climb

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ECAM Message • Let’s assume that no FLEX/DERATE level has been entered into the FMS But… • The thrust level is set to FLX/MCT at takeoff… A warning message appears on the ECAM

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

IMPORTANT: IMPORTANT: This This message message depends depends on on whether whether the the DERATED DERATEDTAKEOFF TAKEOFFoption optionisis installed installed and and available available on on the the aircraft aircraft

Flex/Derate comparison, Engine Bump and Derated climb

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ECAM Message • For aircraft without the DERATED TAKOFF option on board:

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

The message request the pilot to set TOGA

Even if FLEX takeoff was envisaged by the pilot, TOGA is proposed when the FLEX information is missing in the FMS

Flex/Derate comparison, Engine Bump and Derated climb

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ECAM Message • For aircraft with the DERATED TAKOFF option on board: The message requests that the pilot sets IDLE

CONCLUSION: CONCLUSION: © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

For For those those fleets fleets where where both both options options coexist, coexist, additional additional pilot pilot briefing briefing may may be be required. required. In this case, the risk of performing a TOGA takeoff with DERATE takeoff speeds exists, the takeoff must be aborted

Flex/Derate comparison, Engine Bump and Derated climb

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Reduced Thrust Level

Weight Max TOW

Conditions of application: •TREF < Tflex, •Today’s OAT < Tflex •Tflex < Tflex max

Thrust

Available Thrust

Flat rated Thrust

EGT Limit

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Actual TOW

MAXIMUM THRUST REDUCTION

Needed Thrust

Let’s have a look at these reduction levels more in detail ... OAT OAT Flex/Derate comparison, Engine Bump and Derated climb

Tref

Flex Temp

T Flex max Page 15

Reduced Thrust Level THRUST

ACTUAL SITUATION: • A318/319/320/321 25% (Flex only) % TOGA

• A330-200/300

25%

• A340-200/300

25%

• A340-500/600

40%

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

PLANNED EVOLUTIONS

Tref

Tflex max

AVAILABILITY DATE

• A319-200/300

25% (24% Derate)

Upon Request from MID 2004

• A320-200/300

25% (24% Derate)

Upon Request from MID 2004

• A321-200/300

25% (24% Derate)

Upon Request from MID 2004

• A330-200/300

40%

Under evaluation

Flex/Derate comparison, Engine Bump and Derated climb

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Transition to CLIMB THRUST • At high levels of DERATE, the TAKEOFF THRUST may fall below the CLB THRUST • An increase of thrust must be avoided when pulling the lever to the CLB detent

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• An automatic transition sequence to MAX CLB has been implemented for the different engine models

LET’S LET’S SEE SEE HOW HOW THIS THIS WORKS…. WORKS…. Flex/Derate comparison, Engine Bump and Derated climb

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Transition to CLIMB THRUST TRENT 500 : EPR

CLIMB ADJUSTEMENT ••No No unexpected unexpected thrust thrust increase increase ••Climb Climb performance performance unchanged unchanged

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

CLIMB

FROZEN

FLEX/DERATE

WASHOUT

Time 20 s

Thrust Lever Position

FLX/MCT

40 s CLB

THRST RED ALT Flex/Derate comparison, Engine Bump and Derated climb

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Transition to CLIMB THRUST A319: Low Mach Max Climb Logic Throttle in FLX detent

Throttle in CL detent

Thrust Max Takeoff

Reduced thrust

LOW DERATE

Basic MCL Reduced thrust

LOW MACH MAX CLIMB LOGIC

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

Max Takeoff - 25%

0.30 0.35 (CFM) 0.40 (IAE)

Mach Number

• On A320 and A321, the current Max Climb rating provides sufficient room for 25 % thrust reduction.

• For future evolutions, similar solutions will be applied (25%→ 40% for A330) Flex/Derate comparison, Engine Bump and Derated climb

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MAIN

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• FLEX TAKEOFF / DERATED TAKEOFF • BUMP • DERATED CLIMB

Flex/Derate comparison, Engine Bump and Derated climb

Page 20

Bump • The bump is an increased takeoff thrust .

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• The bump can be occasionally used when the basic maximum takeoff thrust does not provide the required performance.

• There is no possibility to set an intermediate thrust between the basic maximum takeoff thrust and the bump Flex/Derate comparison, Engine Bump and Derated climb

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Bump • Various bumps were defined for the early A320 models, as a function of the customers requirements.

• For the latest A320 family models, the bump can be made available on the following models: 4A321-211

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

4A321-231

AA321A AA3210

4A320-214 4A320-233

Flex/Derate comparison, Engine Bump and Derated climb

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Bump • These bumps provide between 6 and 10% more thrust than the basic one.

• They are available only with specific FADEC standards: 4IAE

engines: SCN18 4CFM engines: 5BL

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• These bumps are available, but not yet certified as no customer has ordered this option yet.

• A lead time of about 9 months will be necessary once we get a customer order

Flex/Derate comparison, Engine Bump and Derated climb

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Bump • Long range aircraft: A340: Presently, a bump is available only for the A340-313 gross weight. 4A330: A bump will be certified mid-2004 on the A330-202. It will provide the thrust of the CF6-80E1A3. © AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

4

Flex/Derate comparison, Engine Bump and Derated climb

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Bump • Bump activation: The bump is activated by two guarded pushbuttons, placed on the thrust levers on the A320 Family and on the external thrust levers on the A340.

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

It can be used with all engines operating and remains active in case of one engine failure.

GUARDED PUSHBUTTONS GUARDED PUSHBUTTONS GUAREGGU

Flex/Derate comparison, Engine Bump and Derated climb

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MAIN

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

• FLEX TAKEOFF / DERATED TAKEOFF • BUMP • DERATED CLIMB

Flex/Derate comparison, Engine Bump and Derated climb

Page 26

Principle of thrust reduction When the MAX CLB thrust is not necessary during the CLIMB phase, it can be performed with less thrust. TOC

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

THRST RED ALT

• It applies to the climb phase, so its use is completely independent of that of the DERATED TO • Benefits of thrust reduction 4save

the engine life (à engine stress) 4reduce maintenance costs Flex/Derate comparison, Engine Bump and Derated climb

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Derated Climb concept • Two levels of derated climb available through MCDU • Implementation: EPR/N1 decrement applied on MCL EPR/N1 • Decrement is function of pressure altitude, delta ISA and engine bleed configuration. • Result:

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

4less

severe engine operations and resulting lower engine DMC, 4slightly increased climb fuel/time to reach the same flight level.

• The DERATED CLIMB is basic in the LR family since 1997 • This option is not available in the SA family Flex/Derate comparison, Engine Bump and Derated climb

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Engine strain reduction In order to maintain the same climb capabilities, the Derated Climb features a Washout function: A340-600 RR Trent 500 Derated climb / Max climb washout function 5

Max climb

Climb thrust derate

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

0

-5

D1

ISA+10°C and below

-10

D2

ISA+40°C

ISA+30°C

ISA+20°C

-15

-20 0

10000

Flex/Derate comparison, Engine Bump and Derated climb

20000

Altitude (ft)

30000

40000 Page 29

Derated climb operational effect • Example:

MTOW MTOW

/ Trent 556 4Initial weight 372t 4ISA 4climb law 250kt/320kt/.82 to FL330

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

4A340-642

Time Timeto toTOC TOC DCL1: DCL1: +6min +6min DCL2: DCL2: +10min +10min

Distance Distanceto toTOC TOC DCL1: DCL1:+40nm +40nm DCL2: DCL2:+64nm +64nm

Flex/Derate comparison, Engine Bump and Derated climb

Fuel Fuel(const (constdist) dist) DCL1: DCL1: +89kg +89kg DCL2: DCL2: +184kg +184kg Page 30

AIRBUS Derated Climb Recommendations ISOTIME WEIGHT (Kg)

REFERENCE MAX STRUCTURAL WEIGHT 250/320/M0.82 MAX CLB

350000

EXAMPLE: TOC FL330 to determine which level of • AIRBUS proposes a =method MCLB MCLB

climb thrust DCLis 1 required to guarantee the same climb capabilityDCL as 2when at MTOW with MAX CLB THRUST

340000

330000

DCL1 DCL1

320000

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

310000

300000

Identically TOW=336.3 The TOW=320.5 tons at DCL2 tons at DCL1 provides provides the same climb time same to tothe TOC as climb Max time Structural TOCatasMAX Max Structural Weight CLB Weight at MAX CLB

DCL2 DCL2

290000 15000

20000

25000

30000

FL330

35000

40000

INITIAL CRUISE ALTITUDE (ft) Flex/Derate comparison, Engine Bump and Derated climb

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This document and all information contained herein is the sole property of AIRBUS S.A.S. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied.

© AIRBUS S.A.S. All rights reserved. Confidential and proprietary document.

The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof.

AN EADS JOINT COMPANY WITH BAE SYSTEMS

Flex/Derate comparison, Engine Bump and Derated climb

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