MEL A320

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REFERENCE: LAN COLOMBIA A320 FLEET MEL ISSUE DATE: 27 FEB 15

COLOMBIA A320

LAN COLOMBIA AIRLINES

MINIMUM EQUIPMENT LIST

Issue date 27 February 2015

This document is based on MMEL rev date: 02 DEC 14

EASA Project N° 0010002556-001 Approval date: 31 OCT 14

Applicable to the following aircrafts:

CC-BAF CC-BAG CC-BAN CC-BAO CC-BAR CC-BAS CC-BAT CC-BAU CC-BAV

CC-BAX CC-BAZ CC-BFA CC-BFB CC-BFC CC-BFD CC-BFE CC-BFG CC-BFH

AIRBUS S.A.S

CUSTOMER SERVICES DIRECTORATE

31707 BLAGNAC CEDEX

FRANCE

The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its

contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may

information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part

without permission in writing from the owners of the copyright.

© AIRBUS 2005. All Rights Reserved.

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REFERENCE: LAN COLOMBIA FLEET MEL ISSUE DATE: 27 FEB 15

COLOMBIA

LAN COLOMBIA AIRLINES

MINIMUM EQUIPMENT LIST

The content of this document is the property of Airbus. It is supplied in confidence and commercial

security on its contents must be maintained. It must not be used for any purpose other than that for

which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must

not be reproduced in whole or in part without permission in writing from the owners of the copyright.

© AIRBUS 2005. All rights reserved.

AIRBUS S.A.S

CUSTOMER SERVICES DIRECTORATE

31707 BLAGNAC CEDEX

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COLOMBIA LAN COLOMBIA AIRLINES MINIMUM EQUIPMENT LIST

LAN COLOMBIA FLEET TRL P 1/2

MEL 27 FEB 15

Issue date: 27 FEB 15

This is the LAN COLOMBIA AIRLINES MINIMUM EQUIPMENT LIST at issue date 27 FEB 15 for

the COLOMBIA and replacing last issue dated 12 DEC 14

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TRANSMITTAL LETTER

Intentionally left blank

LAN COLOMBIA FLEET TRL P 2/2

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LAN COLOMBIA FLEET FI P 1/8

MEL 27 FEB 15

Please incorporate this revision as follow:

Insert Localization

Subsection Title Remove Rev. Date

PLP-LESS

LIST OF EFFECTIVE SECTIONS/SUBSECTIONS ALL 27 FEB 15

PLP-LEDU

LIST OF EFFECTIVE DOCUMENTARY UNITS ALL 27 FEB 15

HOW-PLP-TOC

TABLE OF CONTENTS ALL 27 FEB 15

HOW-PLP-SOH

SUMMARY OF HIGHLIGHTS ALL 27 FEB 15

HOW

How to Use ALL 27 FEB 15

ME-PLP-TOC

ME-PLP-SOH

ME-21

Air Conditioning ALL 27 FEB 15

ME-23

Communications ALL 27 FEB 15

ME-24

Electrical Power ALL 27 FEB 15

ME-26

Fire Protection ALL 27 FEB 15

ME-27

Flight Controls ALL 27 FEB 15

ME-28

Fuel ALL 27 FEB 15

ME-30

Ice and Rain Protection ALL 27 FEB 15

ME-31

Indicating/Recording Systems ALL 27 FEB 15

ME-32

Landing Gear ALL 27 FEB 15

ME-34

Navigation ALL 27 FEB 15

ME-36

Pneumatic ALL 27 FEB 15

ME-47

Inert Gas System ALL 27 FEB 15

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FILING INSTRUCTIONS

MEL 27 FEB 15

Continued from the previous page Insert Localization

ME-70

Engine ALL 27 FEB 15

MI-PLP-TOC

MI-PLP-SOH

MI-00-01

Approval Reference ALL 27 FEB 15

MI-00-08

ECAM and MAINTENANCE STATUS ALL 27 FEB 15

MI-21-00

MAINTENANCE Messages on the STATUS SD page ALL 27 FEB 15

MI-21-01-03

CARGO VENT Overhead Panel ALL 27 FEB 15

MI-21-28

Cargo Compartment Ventilation ALL 27 FEB 15

MI-21-51

Pack Flow Control ALL 27 FEB 15

MI-21-52

Air Cooling System ALL 27 FEB 15

MI-21-63

Cockpit and Cabin Temperature Control ALL 27 FEB 15

MI-22-70

Flight Management System (FMS) ALL 27 FEB 15

MI-22-81-01

Auto Flight Control Panel (FCU) ALL 27 FEB 15

MI-22-81-03

FCU Channel ALL 27 FEB 15

MI-22-83

Flight Management and Guidance Computer (FMGC) ALL 27 FEB 15

MI-23-10

Speech Communication ALL 27 FEB 15

MI-23-73-01

Cabin Intercommunication Data System (CIDS) ALL 27 FEB 15

MI-23-73-03

DEU B ALL 27 FEB 15

MI-23-73-10

Smoke Detection Function ALL 27 FEB 15

MI-23-74

Cabin Crew Panel ALL 27 FEB 15

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MEL 27 FEB 15

MI-24-01-01

ELEC Overhead Panel ALL 27 FEB 15

MI-24-22

AC Main Generation ALL 27 FEB 15

MI-24-26

Galley and Commercial Supply System ALL 27 FEB 15

MI-24-32

DC Main Generation (TR 1, TR 2) ALL 27 FEB 15

MI-26-00

MAINTENANCE Message on the STATUS SD page ALL 27 FEB 15

MI-26-13

APU Fire and Overheat Detection ALL 27 FEB 15

MI-26-16

Cargo Compartment Smoke Detection ALL 27 FEB 15

MI-26-17

Lavatory Smoke Detection ALL 27 FEB 15

MI-27-07

Indications on SD pages ALL 27 FEB 15

MI-27-64

Spoiler Hydraulic Actuation ALL 27 FEB 15

MI-27-94

SEC System (Spoiler and Elevator Computer) ALL 27 FEB 15

MI-28-07-05

Fuel Flow Indication on the FUEL SD page ALL 27 FEB 15

MI-28-07-06

Fuel Used Indication on the FUEL SD page ALL 27 FEB 15

MI-28-21

Main Fuel Pump System ALL 27 FEB 15

MI-28-25

Refuel/Defuel System ALL 27 FEB 15

MI-29-01-01

HYD Overhead Panel ALL 27 FEB 15

MI-29-10

Main Hydraulic Power ALL 27 FEB 15

MI-30-00

MI-30-21

Engine Air Intake Ice Protection ALL 27 FEB 15

MI-30-81

Ice Detection ALL 27 FEB 15

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FILING INSTRUCTIONS

MEL 27 FEB 15

MI-31-00

MI-31-07

Indications on the System Display (SD) ALL 27 FEB 15

MI-31-62

Display Management Computer (DMC) ALL 27 FEB 15

MI-32-07

Indications on the WHEEL SD page ALL 27 FEB 15

MI-32-09

ECAM Alerts ALL 27 FEB 15

MI-32-44

Alternate Braking ALL 27 FEB 15

MI-33-10

Cockpit General Illumination ALL 27 FEB 15

MI-33-51

Cabin Emergency Lighting ALL 27 FEB 15

MI-34-00

MI-34-01-01

ADIRS Overhead Panel ALL 27 FEB 15

MI-34-05

Indications on the Primary Flight Display (PFD) ALL 27 FEB 15

MI-34-10

Air Data/Inertial Reference System (ADIRS) ALL 27 FEB 15

MI-34-22

Attitude and Heading Standby Data ALL 27 FEB 15

MI-34-23

Integrated Standby Instrument System (ISIS) ALL 27 FEB 15

MI-34-40

GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar ALL 27 FEB 15

MI-35-01-01

OXYGEN Overhead Panel ALL 27 FEB 15

MI-35-30

Portable Oxygen ALL 27 FEB 15

MI-36-00

MAINTENANCE Message on the STATUS SD Page ALL 27 FEB 15

MI-36-11

Engine Bleed Air Supply System ALL 27 FEB 15

MI-36-12

APU Bleed Air Supply and Crossbleed Systems ALL 27 FEB 15

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MEL 27 FEB 15

MI-36-22

Leak Detection Loop ALL 27 FEB 15

MI-47-00

MAINTENANCE Message on the STATUS SD Page ALL 27 FEB 15

MI-47-10

Generation/Storage ALL 27 FEB 15

MI-49-10

Power Plant ALL 27 FEB 15

MI-52-33

Bulk Cargo Compartment Door ALL 27 FEB 15

MI-52-51

Reinforced Cockpit Door (CDLS) ALL 27 FEB 15

MI-56-10

Cockpit ALL 27 FEB 15

MI-70-00

MI-73-07

Indications on the ENGINE SD page ALL 27 FEB 15

MI-73-08

Indications on the EWD ALL 27 FEB 15

MI-73-09

ECAM Alert ALL 27 FEB 15

MI-73-10

Distribution ALL 27 FEB 15

MI-74-07

MI-74-09

ECAM Alert ALL 27 FEB 15

MI-74-31

Ignition Starting and Continuous Relight ALL 27 FEB 15

MI-77-07-02

MI-78-08

Indications on the EWD ALL 27 FEB 15

MI-78-30

Thrust Reversers ALL 27 FEB 15

MI-79-07

MI-79-09

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FILING INSTRUCTIONS

MEL 27 FEB 15

MI-79-20

Distribution ALL 27 FEB 15

MI-79-40

IDG Oil Cooling System ALL 27 FEB 15

MI-80-11

Pneumatic Starter and Valve System ALL 27 FEB 15

MO-PLP-TOC

MO-PLP-SOH

MO-21-23

Lavatory And Galley Ventilation ALL 27 FEB 15

MO-21-28

Cargo Compartment Ventilation ALL 27 FEB 15

MO-21-31

Pressure Control and Monitoring ALL 27 FEB 15

MO-21-51

Flow Control and Indicating ALL 27 FEB 15

MO-21-63

Cockpit and Cabin Temperature Control ALL 27 FEB 15

MO-22-60

Flight Augmentation (FAC) ALL 27 FEB 15

MO-22-70

Flight Management System (FMS) ALL 27 FEB 15

MO-23-74

Cabin Crew Panel ALL 27 FEB 15

MO-24-22

AC Main Generation ALL 27 FEB 15

MO-24-26

Galley and Commercial Supply System ALL 27 FEB 15

MO-26-12

Engine Fire and Overheat Detection ALL 27 FEB 15

MO-26-13

APU Fire and Overheat Detection ALL 27 FEB 15

MO-27-64

Spoiler Hydraulic Actuation ALL 27 FEB 15

MO-29-09

MO-30-31

Probe Ice Protection ALL 27 FEB 15

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MEL 27 FEB 15

MO-30-81

Ice Detection ALL 27 FEB 15

MO-31-07

Indications on the System Display (SD) ALL 27 FEB 15

MO-31-62

Display Management Computer (DMC) ALL 27 FEB 15

MO-32-09

MO-32-32

Proximity Detector System ALL 27 FEB 15

MO-32-42

Normal Braking ALL 27 FEB 15

MO-32-51

Steering ALL 27 FEB 15

MO-34-01-01

ADIRS Overhead Panel ALL 27 FEB 15

MO-34-10

Air Data/Inertial Reference System (ADIRS) ALL 27 FEB 15

MO-34-23

Integrated Standby Instrument System (ISIS) ALL 27 FEB 15

MO-34-40

GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar ALL 27 FEB 15

MO-35-01-01

OXYGEN Overhead Panel ALL 27 FEB 15

MO-35-20

Passenger Oxygen ALL 27 FEB 15

MO-36-11

Engine Bleed Air Supply System ALL 27 FEB 15

MO-36-12

APU Bleed Air Supply and Crossbleed Systems ALL 27 FEB 15

MO-36-22

Leak Detection Loop ALL 27 FEB 15

MO-49-10

Power Plant ALL 27 FEB 15

MO-73-20

Controlling ALL 27 FEB 15

MO-74-07

MO-74-31

Ignition Starting and Continuous Relight ALL 27 FEB 15

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FILING INSTRUCTIONS

MEL 27 FEB 15

MO-78-30

Thrust Reversers ALL 27 FEB 15

MO-79-09

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TABLE OF CONTENTS

LAN COLOMBIA FLEET PLP-TOC P 1/2

MEL 27 FEB 15

HOW How to Use

ME MEL Entries

MI MEL Items

MO MEL Operational Procedures

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PRELIMINARY PAGES

TABLE OF CONTENTS

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LAN COLOMBIA FLEET PLP-TOC P 2/2

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LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS

LAN COLOMBIA FLEET PLP-LETDU P 1/2

MEL 27 FEB 15

M Localization DU Title DU identification DU date

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PRELIMINARY PAGES

LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS

Intentionally left blank

LAN COLOMBIA FLEET PLP-LETDU P 2/2

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AIRCRAFT ALLOCATION TABLE

LAN COLOMBIA FLEET PLP-AAT P 1/2

MEL 27 FEB 15

This table gives, for each delivered aircraft, the cross reference between:

- The Manufacturing Serial Number (MSN).

- The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S.

- The registration number of the aircraft as known by AIRBUS S.A.S.

- The aircraft model.

M(1) _MSN _FSN _{Registration Number} _Model

4516 CC-BAF 320-232 4546 CC-BAG 320-232 4758 CC-BAN 320-214 4767 CC-BAO 320-214 4892 CC-BAR 320-214 4896 CC-BAS 320-214 4921 CC-BAT 320-214 4943 CC-BAU 320-214 4972 CC-BAV 320-214 5178 CC-BAX 320-214 5229 CC-BAZ 320-214 5234 CC-BFA 320-214 5263 CC-BFB 320-214 5316 CC-BFC 320-214 5324 CC-BFD 320-214 5364 CC-BFE 320-214 5443 CC-BFG 320-214 5453 CC-BFH 320-214

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PRELIMINARY PAGES

AIRCRAFT ALLOCATION TABLE

Intentionally left blank

LAN COLOMBIA FLEET PLP-AAT P 2/2

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LIST OF MODIFICATIONS

LAN COLOMBIA FLEET PLP-LOM P 1/12

MEL 27 FEB 15

M(1) MODIFICATION Linked SB Incorp. Date Title

P10383 29 MAR 10 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD H2-F5

Applicable to: ALL

K10494 29 MAR 10 AIRBORNE AUXILIARY POWER - GENERAL - INSTALL APIC APS3200 APU AS STANDARD (REPLACES HONEYWELL GTCP36-300)

J1735 29 MAR 10 LANDING GEAR-POSITION AND INTRODUCE LGCIU STD -4D

P9594 29 MAR 10 PNEUMATIC - LEAK DETECTION - ACTIVATE PYLON LEAK DETECTION MONITORING

J2879 07 JUN 11 INERT GAS SYSTEM - CERTIFY FUEL TANK INERTING SYSTEM AND ACTIVATE MONITORING Applicable to: MSN 5178-5453

K1806 29 MAR 10 ELECTRICAL POWER-AC/DC ESSENTIAL POWER DISTRIBUTION-PROVIDE PROVISIONS FOR ETOPS-Applicable to: ALL

P11146 19 JUL 11 LANDING GEAR - PARKING/ULTIMATE EMERGENCY BRAKING ACTIVATE PARKING BRAKE MONITORING FUNCTION ON SA A/C

P11632 19 JUL 11 INDICATING/RECORDING SYSTEM SDAC ACTIVATETRAN SPONDER MONITORING BY PIN PROGRAMMING

Applicable to: MSN 4516-4758, 4892-5263

P3379 29 MAR 10 INDICATING/RECORDING SYSTEMS - DEFINE CPIP3

J0071 29 MAR 10 WINGS-WING TIP FENCES-INTRODUCE WING TIPS INCLUDING

FENCES-Applicable to: ALL

P9873 11 JAN 11 POWER PLANT - GENERAL - INTRODUCE CFM56-5BX/3 ENGINE (SAC) "TECH INSERTION PROGRAM"

Applicable to: MSN 4758-5453

K0052 29 MAR 10 INDICATING/RECORDING SYSTEMS - INSTALL AN AIRCRAFT INTEGRATED DATA SYSTEM -Applicable to: ALL

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PRELIMINARY PAGES

MEL 27 FEB 15

Continued from the previous page M(1) MODIFICATION Linked SB Incorp. Date Title

J2963 29 MAR 10 WINGS - MAIN STRUCTURE - REDUCE THE QUANTITY OF MAGNETIC LEVEL INDICATORS Applicable to: ALL

P7754 29 MAR 10 NAVIGATION - DDRMI - REPLACE THALES DDRMI P/N 63543-150-3 BY P/N 63543-150-4.

P10098 24-1120 03 29 MAR 10 ELECTRICAL POWER - AC ESSENTIAL GENERATION SWITCHING - INSTALL AUTO SWITCHING SYSTEM FOR AC AND DC ESS BUS

K7755 25-1305 06 29 MAR 10 EQUIPMENT FURNISHINGS-CURTAINS AND PARTITIONS-MODIFIED INTRUSION AND PENETRATION RESISTANT COCKPIT DOOR Applicable to: ALL

K0024 29 MAR 10 DOORS- BULK CARGO COMPARTMENT- INSTALL AN ADDITIONAL DOOR AT FR

60/62-Applicable to: ALL

P10777 29 MAR 10 AUTO FLIGHT - FAC (FLIGHT AUGMENTATION COMPUTER) - INTRODUCE FAC SOFTWARE STANDARD "BAM0620"

P2798 29 MAR 10 NAVIGATION - VOR/MARKER - MODIFY VOR ANTENNA FAIRING

K0036 29 MAR 10 FIRE PROTECTION AFT CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM

-Applicable to: ALL

K0037 29 MAR 10 FIRE PROTECTION - CARGO COMPARTMENT FIRE EXTINGUISHING - INSTALL A SINGLE SHOT SYSTEM

K0035 29 MAR 10 FIRE PROTECTION FWD CARGO COMPARTMENT INSTALL SMOKE DETECTION SYSTEM

P9196 06 MAY 14 NAVIGATION - STANDBY DATA: INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) - INSTALL ISIS STD WB01

P7125 29 MAR 10 INDICATING RECORDING INTRODUCE FWC STANDARD H2 F1 Applicable to: ALL

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MEL 27 FEB 15

P1362 29 MAR 10 EQUIPMENT/FURNISHINGS - COCKPIT - ADD A FIFTH STRAP ON 4TH OCCUPANT SEAT SHOULDER HARNESS

P4287 29 MAR 10 INDICATING/RECORDING SYSTEMS FWC DEFINE OEB REMINDER WITHIN FWC STD -E1 AND SUBSEQUENT

P8671 29 MAR 10 INDICATING/RECORDING SYSTEMS-ELECTRONIC INSTRUMENT SYSTEM(EIS)- INSTALL DISPLAY MANAGEMENT COMPUTER SOFTWARE EIS2 S4-2 Applicable to: ALL

K3680 29 MAR 10 APU - STORAGE AND DISTRIBUTION - MODIFY APU COMMON LUBRICATION SYSTEM

K3737 29 MAR 10 AIR CONDITIONING AIR COOLING SYSTEM INTRODUCE MODIFIED RAM AIR INLET Applicable to: ALL

K3681 29 MAR 10 APU - CONTROL AND MONITORING - MODIFY ECB FORCOMMON LUBRICATION SYSTEM APU/GEN Applicable to: ALL

P5638 29 MAR 10 NAVIGATION-STANDBY DATA : ALTITUDE AND HEADING - INSTALL INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)

K2770 29 MAR 10 AIRBORNE AUXILIARY POWER - CONTROL AND MONITORING - INTRODUCE ECB P/N 304640-3 Applicable to: ALL

P3524 29 MAR 10 ELECTRICAL POWER - AC AUXILIARY GENERATION (APU GENERATOR) - INTRODUCE MODIFIED GENERATOR

K0402 29 MAR 10 ICE AND RAIN PROTECTION - DRAIN MAST ICE PROTECTION - INSTALL TEMPERATURE REGULATED HEATING SYSTEM

P7005 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INTRODUCE STD 9 BSCU (TWIN VERSION)

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PRELIMINARY PAGES

MEL 27 FEB 15

P10801 02 JUL 13 AUTO-FLIGHT-FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC)-INSTALL FMGC HONEYWELL H2C13 ON CFM A/C

K3682 29 MAR 10 AIRBORNE AUXILIARY POWER - MODIFY WIRING FOR COMMON LUBRICATION SYSTEM APU/GEN Applicable to: ALL

P9126 22-1203 01 29 MAR 10 AUTOFLIGHT - FMGC - INSTALL FMGC IAE/PW STD P1I10 (WITH FMS2 HONEYWELL) ON A/C FITTED WITH IAE OR PW POWERPLANTS

P3924 29 MAR 10 LANDING GEAR - MLG - MESSIER - INTRODUCE BRAKES P/N C202253

J0376 29 MAR 10 LANDING GEAR - MLG - MINOR IMPROVEMENTS INTRODUCED FROM A/C 44

P6146 29 MAR 10 INDICATING/RECORDING SYSTEM FWC INTRODUCE "F/CTL FLAP LVR NOT ZERO" RED WARNING

K8400 29 MAR 10 COMMUNICATIONS-CIDS-INTRODUCE ENHANCED CIDS (A318 VERSION) AND RELATED SYSTEMS ON SINGLE AISLE FAMILY

P11807 13 AUG 14 INDICATING/RECORDING SYSTEM - ELECTRONIC INSTRUMENT SYSTEM (EIS) - INSTALL NEW EIS2 SOFTWARE S9

Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

P8799 34-1352 01 29 MAR 10 NAVIGATION- GPWS - USE LATERAL GPS POSITION WITH AUTOMATIC DESELECTION

P5121 19 JUL 12 INDICATING/RECORDING SYSTEMS - DATA LOADING SYSTEMS -INSTALL A MULTIPURPOSE DISC DRIVE UNIT IN A COCKPIT

Applicable to: MSN 4516-4972 P5518 32-1232 01

32-1336 01 29 MAR 10 LANDING GEAR-NORMAL BRAKING- INTRODUCESTD 8 BSCU (TWIN VERSION) Applicable to: ALL

K6461 29 MAR 10 LIGHTS-EMERGENCY LIGHTING-INTRODUCE LED EXIT SIGNS

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MEL 27 FEB 15

J1617 29 MAR 10 FLIGHT CONTROLS-GENERAL- DELETION OF L.A.F. FEATURE FROM A320 A/C (SERIAL SOLUTION) Applicable to: ALL

K4913 29 MAR 10 HYDRAULIC POWER - AUXILIARY HYDRAULIC POWER - INSTALL A319 RAM AIR TURBINE ON A320 Applicable to: ALL

P12367 11 APR 12 ENGINE FUEL AND CONTROL- FADEC INSTALL ECU SOFTWARE STANDARD 5BS ON CFM56-5B ENGINES

P9522 29 MAR 10 AUTO-FLIGHT-MULTIPURPOSE CONTROL AND DISPLAY UNIT(MCDU) - ACTIVATE BACK-UP NAV FUNCTION

P12877 06 MAY 14 ENGINE FUEL AND CONTROL- FADEC INTRODUCE NEW ECU SOFTWARE 5BS2 ON CFM56-5B ENGINES

P4885 29 MAR 10 NAVIGATION - GPWS - ACTIVATE ENHANCED FUNCTIONS OF THE EGPWS

P5253 29 MAR 10 NAVIGATION - ADIRS - REPLACE ADIRS CDU BY MSU (MODE SELECTOR UNIT)

P10443 19 JUL 11 FLIGHT CONTROL - ELAC SYSTEM - INTRODUCE ELAC "L93" SOFTWARE STANDARD

P10402 17 NOV 10 COMMUNICATIONS AUDIO MANAGEMENT MODIFY AMU POWER SUPPLY TO COPE WITH DC ESSENTIAL BUS LOSS

J0739 29 MAR 10 LANDING GEAR-MLG-INTRODUCE TORQUE LINK APEX DAMPER

P11819 02 OCT 12 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD H2-F6

K6443 29 MAR 10 AIR CONDITIONING-AIR COOLING- INSTALL A NEW ECS

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MEL 27 FEB 15

P1631 29 MAR 10 NAVIGATION MODIFY GPWC WARNING -Applicable to: ALL

K1522 11 JAN 11 COMMUNICATIONS - INSTALL PA IN USE INDICATORS LIGHT

P9655 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INSTALL BSCU SOFTWARE STD "L4.9"

K3901 29 MAR 10 COMMUNICATIONS-CIDS-INTRODUCE MODIFIED DIRECTOR POWER SUPPLY PRINCIPLE Applicable to: ALL

P5451 29 MAR 10 ELECTRICAL POWER - GENERAL - AC-DC MAIN DISTRIBUTION - INSTALL AC-DC SHEDDABLE BUSBARS

P6125 34-1249 02 29 MAR 10 NAVIGATION-ADIRU-INSTALL HONEYWELL ADIR U 4 MCU AD11 (NEW HARD)

P7268 34-1252 00 29 MAR 10 NAVIGATION-ADIRU-RESTORE RVSM 3 CIRCUIT CAPABILITIES (SERIAL SOLUTION)

P2650 29 MAR 10 ICE AND RAIN PROTECTION ICE DETECTION INSTALL DUAL ADVISORY ICE DETECTION SYSTEM Applicable to: ALL

P10439 11 JAN 11 AUTO-FLIGHT - FMGC - INSTALL FMGC HNWL STD P1C12 ON CFM A/C

J3240 18 DEC 12 FUEL - QUANTITY INDICATING - ACTIVATE FUEL LEAK DETECTION WARNING SYSTEM Applicable to: MSN 5364-5453

P4801 29 MAR 10 ELECTRICAL POWER-GENERAL-DEFINE NEW ELECTRICAL GENERATION CONCEPT FOR SINGLE AISLE A/C

P3957 11 JAN 11 HYDRAULIC POWER-GENERAL-INTRODUCE AN HYDRAULIC SHUT-OFF VALVE ON THE CFM T/R SYSTEM

P7175 29 MAR 10 ELECTRICAL POWER - GENERAL - INSTALL A COMMERCIAL SHEDDING PUSH-BUTTON SWITCH IN COCKPIT

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MEL 27 FEB 15

P3956 29 MAR 10 HYDRAULIC POWER-GENERAL-INTRODUCE AN HYDRAULIC SHUT-OFF VALVE ON THE IAE T/R SYSTEM

P4808 29 MAR 10 LANDING GEAR-WHEELS AND BRAKES- INTRODUCE BSCU COMMON STD

J2765 19 JUL 12 WING MAIN STRUCTURE TOP SKIN PANEL NO. 2 REMOVE MANUAL REFUEL APERTURE

K4574 17 NOV 10 AIR CONDITIONING-FLOW CONTROL AND INDICATING INTRODUCE MODIFIED AIR CONDITIONING FLOW CONTROL Applicable to: ALL

P6538 29 MAR 10 INDICATING/RECORDING SYSTEMS-FWC TO COMPLY WITH EM2 BSCS WARNING/ECAM INDICATIONS

P13023 18 DEC 12 INDICATING RECORDING INTRODUCE FWC STANDARD H2-F7 Applicable to: MSN 4516-4767, 4972-5178, 5234, 5443-5453

K9473 29 MAR 10 AIR CONDITIONING - PRESSURE CONTROL AND MONITORING - INSTALL RPCU AND WIRING PROVISIONS FOR RPWS

P10300 17 NOV 10 ELECTRICAL POWER AC MAIN GENERATION INSTALL EEPGS GCU SOFTWARE STANDARD "5.2" Applicable to: ALL

P4151 29 MAR 10 INDICATING/RECORDING SYSTEM - INSTALL A PORTABLE DATA LOADER CONNECTOR AND DISK STOWAGE

P1063 29 MAR 10 AUTO FLIGHT - IMPROVE SEGREGATION OF AUTO PILOT DISCONNECT CIRCUIT

K2450 49-1029 27 29 MAR 10 AIRBORNE AUXILIARY POWER UNIT - INTRODUCE APIC APS-3200

P6319 17 NOV 10 COMMUNICATIONS AUDIO MANAGEMENT INSTALL TEAM DIGITAL AMU P/N 4031-SA-01 Applicable to: ALL

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PRELIMINARY PAGES

MEL 27 FEB 15

P10653 07 NOV 13 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD H2-F3P

P4149 29 MAR 10 ENGINE FUEL AND INTRODUCE E.E.C. SOFTWARE SCN 10A ON IAE V2500-A5

P0661 29 MAR 10 EQUIPMENT/FURNISHINGS-COCKPIT-ADD A FIFTH STRAP ON 3RD OCCUPANT SHOULDER HARNESS-Applicable to: ALL

P8341 11 JAN 11 NACELLES / PYLONS - PYLONS - IMPROVE AERODYNAMIC SHAPE OF CFM PYLON Applicable to: MSN 4758-5453

P6801 31-1231 01 29 MAR 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC STANDARD H2E4

J3283 18 DEC 12 WINGS-GENERAL-CERTIFY SHARKLET INSTALLATION FOR A320/A319/A318 Applicable to: MSN 5453

P2316 29 MAR 10 AUTO FLIGHT - ACTIVATE WINDSHEAR FUNCTION Applicable to: ALL

P12126 13 AUG 14 AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL FAC 622 (SHARKLET PROJECT) Applicable to: MSN 5443-5453

J0012 29 MAR 10 LIGHTS - NAVIGATION LIGHTS - INSTALL A SECOND NAVIGATION LIGHT SYSTEM

P0197 29 MAR 10 COMMUNICATIONS - HF SYSTEM - INSTALL A SINGLE SYSTEM

P5429 11 JAN 11 ENGINE FUEL AND CONTROL-FADEC CFM56-5B-SAC-INTRODUCE ECU SOFTWARE 5BI Applicable to: MSN 4758-5453

K8905 29 MAR 10 EQUIPMENT/FURNISHINGS-CURTAINS AND PARTITIONS-INSTALL DEADBOLT ON CENTER LATCH OF REINFORCED COCKPIT DOOR Applicable to: ALL

P7945 17 NOV 10 ELECTRICAL POWER - AC MAIN INSTALL NEW GCU SOFTWARE STD 5.1 ON SA A/C EQUIPPED WITH ENHANCED EPGS

(45)

MEL 27 FEB 15

22-1359 00 07 JUN 12 AUTO-FLIGHT-FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC)-INSTALL FMGC HONEYWELL H2C13 ON CFM A/C

Applicable to: MSN 4758, 4892-4972

P4576 29 MAR 10 LANDING GEAR-ALTERNATE BRAKING- INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM Applicable to: ALL

K9995 29 MAR 10 AIR CONDITIONING - PRESSURE CONTROL AND MONITORING - REMOVE RESIDUAL PRESSURE CONTROL UNTI (RPCU) (ANTI MOD TO 34673) Applicable to: MSN 4516-4546

J0006 29 MAR 10 FUEL- INSTALL A CENTRE TANK SYSTEM-Applicable to: ALL

P4170 29 MAR 10 FLIGHT CONTROLS - FCDC SYSTEM - PROVIDE A VISUAL INDICATION FOR SIMULTANEOUS SIDE STICK ACTION

P6954 29 MAR 10 AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INTRODUCE FAC SOFTWARE "BAM0616" Applicable to: ALL

P8257 27-1149 02 29 MAR 10 FLIGHT CONTROLS - SEC SYSTEM - INSTALL SPOILER AND ELEVATOR COMPUTER SOFTWARE FOR A318 EIS (BAM0511)

P4023 29 MAR 10 GENERAL - SYSTEM PROVISION FOR HIGH ALTITUDE OPERATION UP TO 14100 FT Applicable to: ALL

P9107 31-1267 03

31-1300 02 29 MAR 10 INDICATING/RECORDING SYSTEMS - FLIGHTWARNING COMPUTER (FWC) - INSTALL FWC STANDARD H2F3

P4977 29 MAR 10 INDICATING/RECORDING SYSTEMS FWC PROVIDE NEW SYNTHETIC VOICE "DUAL INPUT" Applicable to: ALL

P8757 07 JUN 12 ENGINE FUEL AND CONTROL - GENERAL INTRODUCE HMU P13 ON CFM56-5A/5B ENGINES Applicable to: MSN 4758-5453

K1498 29 MAR 10 HYDRAULIC POWER-BLUE SYTEM RELOCATE CONNECTOR

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PRELIMINARY PAGES

MEL 27 FEB 15

P9824 31-1276 01 29 MAR 10 INDICATING/RECORDING SYSTEMS-ELECTRONIC INSTRUMENT SYSTEM(EIS)-INSTALL DISPLAY MANAGEMENT COMPUTER SOFTWARE EIS2 S7 Applicable to: ALL

P2493 29 MAR 10 EQUIPMENT/FURNISHINGS COCKPIT SEATS INTRODUCE TYPE A340 SEATS

P11620 24 JAN 12 INDICATING/RECORDING SYSTEMS FWC ACQUISITION/INTERFACE ACTIVATE MONITORING OF ATC/XPDR

P0033 06 MAY 14 COMMUNICATIONS - HF SYSTEM - INSTALL SYSTEM PROVISION FOR A SINGLE SYSTEM

P4502 29 MAR 10 INFORMATION SYSTEM - AIR TRAFFIC AND INFORMATION SYSTEM (ATIMS) - INSTALL ATSU COMPUTER FOR ACARS

P8863 11 APR 12 INDICATING/RECORDING SYSTEM FWC

ACQUISITION INTERFACE CONNECT FWC TO RPWS TO PREVENT DOOR OPENING WITH RESIDUAL CABIN PRESSURE

J2361 18 DEC 12 FUEL-QUANTITY INDICATION-REMOVE FUEL LEAK DETECTION FUNCTION ASSOCIATED WITH FQIC 13-9 (ANTI-MOD FOR MOD 32650)

J2360 29 MAR 10 FUEL - QUANTITY INDICATION - INTRODUCE FUEL LEAK DETECTION

K2962 29 MAR 10 HYDRAULIC POWER-BLUE MAIN HYDRAULIC POWER-IMPROVE MAINTENANCE STATUS OF BLUE HYDRAULIC RESERVOIR

P6578 29 MAR 10 INDICATING RECORDING SYSTEMS- EIS-INSTALL DMC, DU AND DISKETTES FOR EIS2

P10891 32-1350 00 29 MAR 10 LANDING GEAR - NORMAL BRAKING - INSTALL BSCU SOFTWARE STD "L4.9 B" (EM2) Applicable to: ALL

(47)

MEL 27 FEB 15

P7092 19 JUL 11 INDICATING/RECORDING SYSTEM - EIS - ACTIVATE FUEL FLOW/DELTA ISA FUNCTION BY PIN PROGRAMMING ON DMC

P11484 19 JUL 11 FLIGHT CONTROLS - FCDC SYSTEM - INTRODUCE FCDC STANDARD 58

P8340 29 MAR 10 NACELLES / PYLONS - PYLONS - IMPROVE AERODYNAMIC SHAPE OF IAE PYLON Applicable to: MSN 4516-4546

J2832 28-1159 00 29 MAR 10 FUEL - MAIN FUEL PUMP SYSTEM - INSPECT AND ADMINISTER CORRECT TORQUE AND SCREW LOCKING ON FIXING BOLTS

P0159 29 MAR 10 EQUIPMENT/FURNISHINGS - ADD A FIFTH STRAP TO FLIGHT CREW SHOULDER HARNESS

K4160 29 MAR 10 DOORS-CARGO COMPARTMENT INTRODUCE MODIFIED ACTUATOR FITTING AND ATTACHMENT

P8303 29 MAR 10 NAVIGATION - DDRMI - REMOVE DDRMI VOR/ADF/DME INDICATORS

K7790 29 MAR 10 DOORS-PASSENGER COMPARTMENT FIXED INTERIOR DOORS-INSTALL ELECTRICAL COCKPIT DOOR RELEASE SYSTEM

P10762 13 AUG 14 AUTO FLIGHT - FMGC - INSTALL FMGC HWL H2C12 (RELEASE 1A) ON CFM A/C

K5446 29 MAR 10 INDICATING/RECORDING INTRODUCE A COMBINED FDIU/DMU Applicable to: MSN 4516-4758, 4892-5453

P10763 13 AUG 14 AUTO FLIGHT - FMGC - INSTALL FMGC HWL H2I11 (RELEASE 1A) ON IAE AND PW A/C

K0070 21-1047 05 29 MAR 10 AIR CONDITIONING - CARGO COMPARTMENT - VENTILATION - INSTALL SYSTEM IN AFT COMPARTMENT

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PRELIMINARY PAGES

MEL 27 FEB 15

P0053 29 MAR 10 EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT - INSTALL SLIDING TABLES AT PILOT'S STATION

P5794 19 JUL 12 INDICATING RECORDING SYS-DATA LOADING -INTRODUCE A MULTIPURPOSE DISK DRIVE UNIT P/N AC68A200 IN THE COCKPIT

K0064 29 MAR 10 LIGHTS - EXTERIOR LIGHTS - INSTALL SYNCHRONIZED STROBE LIGHTS Applicable to: ALL

P5706 31-1257 01 29 MAR 10 INDICATING RECORDING INTRODUCE FWC STANDARD H2/E3P Applicable to: ALL

J1764 19 JUL 11 FUEL-QUANTITY INDICATING-INTRODUCE MODIFIED PRE-SELECTOR UNITS P/N 0203

J1570 29 MAR 10 CROSS FEED VALVE P/N-2 Applicable to: ALL

P1970 29 MAR 10 COMMUNICATIONS - INSTALL HF1 FOR ETOPS Applicable to: ALL

J0937 29 MAR 10 LANDING GEAR - MAIN LANDING GEAR (TWIN WHEELS) - INTRODUCE A NEW STANDARD TORQUE LINKS DAMPER AND ABEX PIN.

P4539 29 MAR 10 AUTOFLIGHT-FLIGHT CONTROL UNIT- (FCU) INTRODUCE SEXTANT MODULAR FCU Applicable to: ALL

P0040 29 MAR 10 EQUIPMENT/FURNISHINGS - FLIGHT

COMPARTMENT INSTALL A 4TH OCCUPANT SEAT -Applicable to: ALL

P0143 29 MAR 10 COMMUNICATIONS RADIO MANAGEMENT INSTALL A 3RD RMP

P3365 29 MAR 10 ICE AND RAIN PROTECTION-ICE PROVIDE ICE DETECTOR ILLUMINATION Applicable to: ALL

K2335 29 MAR 10 FIRE PROTECTION - LAVATORY SMOKE DETECTION - INTRODUCE AMBIENT SYSTEM Applicable to: ALL

(49)

(50)

(51)

PRELIMINARY PAGES - TABLE OF CONTENTS

LAN COLOMBIA FLEET HOW-PLP-TOC P 1/2

MEL 27 FEB 15

Revision Manager...A Foreword... B Questions and Suggestions... C MEL Contents...D How to get the MMEL updated?...E Documentary Unit (DU)... F MEL Revision Management...G Optional Equipment (If Installed)



... H Removal of Item...I How to Use the MEL Entries Section? ...J How to Use the MMEL Items Section? ... K How to Use the MEL Operational Procedures Section?... L Landing Capabilities ( CAT 2, CAT 3 SINGLE, CAT 3 DUAL) ... M Required Navigation Performance (RNP)...N Reduced Vertical Separation Minimum (RVSM)...O Futur Air Navigation System (FANS)... P Abbreviations... Q

(52)

HOW TO USE

PRELIMINARY PAGES - TABLE OF CONTENTS

Intentionally left blank

LAN COLOMBIA FLEET HOW-PLP-TOC P 2/2

(53)

PRELIMINARY PAGES - SUMMARY OF HIGHLIGHTS

LAN COLOMBIA FLEET HOW-PLP-SOH P 1/2

MEL 27 FEB 15

Localization

Title IndexToc ID Reason

HOW

(54)

HOW TO USE

PRELIMINARY PAGES - SUMMARY OF HIGHLIGHTS

Intentionally left blank

LAN COLOMBIA FLEET HOW-PLP-SOH P 2/2

(55)

LAN COLOMBIA FLEET HOW P 1/26

MEL A → 27 FEB 15

REVISION MANAGER

Ident.: HOW-20800653.9001001 / 27 FEB 15

This DU contains the name of the person in charge of MEL custumization as the name of the person

in charge of performing the final crosscheck in order to deliver the document to the Aeronautical

Authority for approval.

1

_{AIRBUS A320}

DATE CUSTOMIZED CROSSCHECKED

MAY 18/11 A.MARTÍ E.LÓPEZ LIBARDI JUL 29/11 A.MARTÍ E.LÓPEZ LIBARDI SEP 12/11 A.MARTÍ E.LÓPEZ LIBARDI NOV 02/11 A. MARTÍ E.LÓPEZ LIBARDI AGO 01/11 N. PATINO J.C RODRIGUEZ NOV 18/11 N. PATINO J.C RODRIGUEZ ENE 13/12 N.PATINO J.C RODRIGUEZ SEP 01/12 N.PATINO J.C RODRIGUEZ FEB 01/13 N.PATINO J.C RODRIGUEZ MAY 13/13 N.PATINO J.C RODRIGUEZ NOV 05/13 N.PATINO J.C RODRIGUEZ APR 02/14 L. DELGADO J. TORRES JUN 20/14 L. FELIZZOLA L. DELGADO JUL 18/14 L. FELIZZOLA L. DELGADO OCT 10/14 C. SIMBAQUEBA L. FELIZZOLA DIC 12/14 C. SIMBAQUEBA L. FELIZZOLA FEB 27/15 C. SIMBAQUEBA L. FELIZZOLA

AIRBUS A319

MAY 25/11 A.MARTÍ E.LÓPEZ LIBARDI SEP 12/11 A.MARTÍ E.LÓPEZ LIBARDI DEC 12/11 A.MARTÍ E.LÓPEZ LIBARDI FEB 24/12 A.MARTÍ E.LÓPEZ LIBARDI MAY 31/12 A.MARTÍ E.LÓPEZ LIBARDI AUG 17/12 A.MARTÍ E.LÓPEZ LIBARDI NOV 27/12 A.MARTÍ E.LÓPEZ LIBARDI FEB 14/13 A.MARTÍ E.LÓPEZ LIBARDI APR 22/13 A.MARTÍ E.LÓPEZ LIBARDI

(56)

HOW TO USE

MEL ← A to D → 27 FEB 15

AIRBUS A319/A320

AUG 01/13 A.MARTÍ E.LÓPEZ LIBARDI

FOREWORD

Ident.: HOW-00012802.0001001 / 12 SEP 11

This Master Minimum Equipment List ( MMEL ) is a reference manual published in English. It

is approved by the European Aviation Safety Agency ( EASA ). This MMEL must be used as a

reference by the Operator to develop its MEL .

This MMEL takes into account the specific configuration of each aircraft of the Operator's fleet. The

aircraft validity is managed at Documentary Unit (DU) level.

Refer to HOW Documentary Unit (DU)

This MMEL is produced in XML format and can be published in PDF format and in electronic format

for electronic consultation on EFB .

Airbus also proposes a set of tools to create and publish the Operator’s MEL based on this MMEL .

QUESTIONS AND SUGGESTIONS

Ident.: HOW-00012803.0001001 / 18 JUL 14

For any questions or comments related to this manual, the Operator’s Flight Operations Management

may contact the Airbus Flight Operations & Training support department.

MEL CONTENTS

Ident.: HOW-00012804.0001001 / 10 OCT 14

This MEL has four sections:

‐ How to Use (HOW) : This section contains general information and describes the organization

of the manual.

‐ MEL Entries (ME) : This section lists all the ECAM alerts and indicates the associated

MEL item (if any) to apply for dispatching the aircraft. This section is a

user-friendly entry point for the flight crew and the maintenance personnel

when an ECAM alert reports a system failure.

‐ MEL Items (MI)

: This section is approved by the Aeronautical Authorities and lists all the

MEL items with the associated dispatch conditions.

(57)

MEL ← D to F → 27 FEB 15

‐ MEL Operational

Procedures (MO)

: This section gives the operational procedures that are associated with the

MEL items.

‐ NEF(Non-Essential

Equipment &

Furnishings)

: This section list are all items installed on the aircraft as part of the original

type certification, supplemental type certificate, or other form of alteration

that have no effect on the safe operation of flight and would not be

required by the applicable certification rules or operational rules.

Note: The MEL Maintenance Procedures are published in the AMM.

HOW TO GET THE MMEL UPDATED?

Ident.: HOW-00012805.0001001 / 17 SEP 10

Airbus provides the Operator with an MMEL which reflects the aircraft configuration at delivery, and

the necessary revisions to reflect configuration changes due to Airbus approved modifications.

The Operator must inform Airbus without delay of the effective changes to the aircraft delivery

configuration made through Airbus Service Bulletin (SB). This permits Airbus to provide the Operator

with the MMEL revisions/updates.

The Operator must timely report any SB embodiment to the following address:

E.MAIL

: [email protected]

Airbus will not provide revisions, and will not take responsibility for any effect on the MMEL:

‐ Due to modifications installed by third parties without an Airbus SB, and/or

‐ Due to modifications installed through an Airbus SB, if Airbus is not informed of the SB

embodiment.

DOCUMENTARY UNIT (DU)

Ident.: HOW-00012806.0001001 / 12 SEP 11

This MEL is made of Documentary Units (DU). The DUs contain the technical data.

In the MEL, a DU can be:

‐ An ECAM alert,

‐ An MEL item,

‐ An MEL operational procedure.

The List of Effective Documentary Units (LEDU) lists all the DUs that constitute this MEL.

The DUs are arranged into sections and subsections (also called PSL). The List of Effective

Sections/Subsections (LESS) lists all the subsections that constitute this MEL. The subsections

contain the DUs.

(58)

HOW TO USE

MEL ← F 27 FEB 15

DU IDENTIFICATION STRIP

In the PDF format, below the title of the DU, the grey identification strip indicates for each DU:

‐ The DU identification (Ident.). Each DU is identified by its unique identification number. This DU

identification is used to cross-refer to the LEDU.

‐ The DU date. For approved DUs (MEL items DU), this date corresponds to the approval date by

the Aeronautical Authority of the MEL revision. For non-approved DUs, this date corresponds to

the date of release of the DU by Airbus.

‐ The "Applicable to" field that lists the aircraft to which the DU applies.

Note: 0012-0220 means that the DU applies to all MSNs (listed in the AAT) from MSN 0012

up to and including MSN 0220.

In the electronic format, the same information is available by selecting the “DOC REF” option in

the INFO drop down list. The electronic format also displays the “Criteria” field that indicates the

aircraft configuration to which the DU applies.

LIST OF EFFECTIVE DOCUMENTARY UNITS (LEDU)

For each DU, the LEDU indicates the following information:

‐ The “M” field that may indicate the following Evolution Code:

• The “E” letter indicates an aircraft validity change of the DU. The list of aircraft to which the

DU applies has changed compared to the previous MEL revision, by addition or deletion of

one or several aircraft.

• The “N” letter indicates a new DU added by this MEL revision.

• The “R” letter indicates a revised DU. The content of the DU is updated by this MEL revision.

‐ The "Localization" field that is the identification of the subsection that contains the DU. In the

PDF format, this cross-refers to the page footer, which permits the user to localize the DU within

the manual.

‐ The DU title.

‐ The DU identification (Ident.). Each DU is identified by its unique identification number. This DU

identification is used to cross-refer to the LEDU.

‐ The DU date. For approved DUs (MEL items DU), this date corresponds to the approval date by

the Aeronautical Authority of the MEL revision. For non-approved DUs, this date corresponds to

the date of release of the DU by Airbus.

‐ The criteria: This field indicates the aircraft configuration to which the DU applies.

‐ The "Applicable to" field that lists the aircraft to which the DU applies.

Note: 0012-0220 means that the DU applies to all MSNs (listed in the AAT) from MSN 0012

up to and including MSN 0220.

(59)

MEL G → 27 FEB 15

MEL REVISION MANAGEMENT

Ident.: HOW-00012807.0001001 / 12 SEP 11

MEL REVISION CYCLE

The MEL revision adds, updates, or deletes information. The Operator determines the revision

cycle. For urgent update, Airbus issues an immediate revision regardless of the revision cycle.

MEL ISSUE DATE

An issue date identifies each MEL revision.

The issue date appears:

‐ In the Transmittal Letter for the PDF format, and

‐ In the LIBRARY panel of the OPS LIBRARY Browser for the electronic consultation.

Note: The issue date is different from the Aeronautical Authority approval date. The

Aeronautical Authority approval date appears in the MEL Approval Reference of the MEL

Preamble. The applicability date of this MEL is based on the issue date and not on the

Aeronautical Authority approval date (

Refer to MI-00-01 Approval Reference

).

MEL REVISION CONTENTS

Each MEL revision contains the following information that is useful to update the MEL and to

identify the changes that the revision has inserted:

‐ The Transmittal Letter (in PDF format only),

‐ The List of Effective Sections/Subsections ( LESS ) (in PDF format only),

‐ The Filling Instructions (in PDF format only),

‐ The List of Effective Documentary Units ( LEDU ),

‐ The Summary of Highlights ( SOH ).

Each MEL revision also contains:

‐ An Aircraft Allocation Table ( AAT ),

‐ A List of Modifications ( LOM ).

When there is a change within a DU, the MEL revision updates the whole subsection that contains

the DU.

TRANSMITTAL LETTER

The Transmittal Letter is a way of communication between Airbus and the Operators. The

Transmittal Letter also specifies the issue date of the MEL revision.

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HOW TO USE

MEL ← G → 27 FEB 15

PDF PAGE HEADER AND FOOTER

In the PDF format, the header of the page contains the subsection title whereas the footer

contains:

‐ The subsection identification,

‐ The subsection issue date. The subsection issue date corresponds to the issue date of the

latest MEL revision that has revised the subsection.

‐ The page number within this subsection and the total number of pages within this subsection.

‐ The Table of Contents ( TOC ) indexing.

This TOC indexing uses the TOC indexes. Each TOC entry has an alphabetical index that

identifies this TOC entry within its subsection. The manual user can easily find a TOC entry

content within the manual thanks to this alphabetical index and the subsection identification. Both

are indicated in the TOC and both cross-refer to the PDF page footer.

In the PDF page footer, the TOC indexing is of the following type:

‐ B

: The PDF page contains the whole "B" TOC entry content.

‐ B to D

: The PDF page contains the whole "B", "C" and "D" TOC entries contents.

‐ B→

: The "B" TOC entry content starts on this PDF page and continues on the

following PDF page.

‐ ←B

: The "B" TOC entry content starts on a previous PDF page and finishes on this

PDF page.

‐ ←B→

: The "B" TOC entry content starts on a previous PDF page and continues on the

following PDF page.

‐ B to D→ : The PDF page contains the whole "B" and "C" TOC entries contents but the "D"

TOC entry content starts on this PDF page and continues on the following PDF

page.

‐ ←B to D : The PDF page contains the whole "C" and "D" TOC entries contents but the

"B" TOC entry content starts on a previous PDF page and finishes on this PDF

page.

‐ ←B to D→ : The PDF page contains the whole "C" TOC entry content but the "B" TOC entry

content starts on a previous PDF page and finishes on this PDF page and the

"D" TOC entry content starts on this PDF page and continues on the following

PDF page.

Note: 1. The indexes follow the alphabetical order: A, B, C, ..., Z, AA, AB, AC, ..., AZ, BA,

BB,BC, ...

2. For each subsection, the index starts again from A.

LIST OF EFFECTIVE SECTIONS/SUBSECTIONS ( LESS )

The manual is organized by sections and subsections (also called PSL ). The subsections contain

the DUs.

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MEL ← G → 27 FEB 15

The LESS lists all the subsections that constitute this MEL . The LESS only exists in the PDF

format.

When there is a change within a DU, the MEL revision updates the whole subsection that contains

the DU. This subsection gets a new date that corresponds to the issue date of the MEL revision.

Note: Each subsection has its own date that corresponds to the issue date of the latest MEL

revision that has revised the subsection. Therefore subsections of a same manual might

have different dates.

For each subsection, the LESS indicates:

‐ The subsection identification (also referred to as localization),

‐ The subsection title,

‐ The subsection issue date. The subsection issue date corresponds the issue date of the latest

MEL revision that has revised the subsection.

‐ The "M" field that may indicate the following Evolution Code:

• The “E” letter indicates only an aircraft validity change of one or several DUs of this

subsection compared to the previous MEL revision. No DU content of this subsection has

changed compared to the previous MEL revision.

• The “M” letter indicates a subsection that has moved compared to the previous MEL revision.

• The “N” letter indicates a new subsection added by this MEL revision.

• The “R” letter indicates a revised subsection. The content of one or several DUs of this

subsection is updated by this MEL revision.

Each PDF page footer indicates the subsection identification and the subsection issue date for

cross-reference with the LESS . Therefore the manual holder can use the LESS to ensure that the

MEL is up-to-date and that no page is missing.

FILLING INSTRUCTIONS

The Filling Instructions enable the manual holder:

‐ To update the paper MEL when a new MEL revision is available, and

‐ To quickly identify the subsections that the new MEL revision has revised.

The Filling Instructions notify the manual holder to remove a subsection, to add a new subsection

or to update an existing subsection.

For each revised subsection, the Filling Instructions also indicate:

‐ The subsection identification (also referred to as localization),

‐ The subsection title,

‐ The new issue date of the subsection.

After incorporating the new revision with the Filling Instructions, the manual organization must

correspond to the LESS .

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HOW TO USE

MEL ← G → 27 FEB 15

Each PDF page footer indicates the subsection identification and the subsection issue date for

cross-reference with the Filling Instructions. Therefore the manual holder can use the Filling

Instructions to update the paper MEL and to identify the latest revised subsections.

HIGHLIGHTS AND REVISION MARKS

In the PDF format, a vertical bar in the margin of the DU identifies the modified part. Each vertical

bar has a numerical index that refers to the associated reason of the change in the Summary of

Highlights ( SOH ).

The SOH lists all the changes and associated reasons of the change (if necessary) that the

revision has inserted.

In electronic consultation, the vertical bar is available by selecting the “REV MARKS” option in the

INFO drop down list. The user can display the associated reason of the change by clicking on the

bar.

AIRCRAFT ALLOCATION TABLE ( AAT )

The AAT indicates the list of aircraft that are taken into account in this MEL . For each aircraft, the

AAT indicates the following information:

‐ The MSN number,

‐ The Fleet Serial Number ( FSN ) of the aircraft as known by Airbus,

‐ The registration number of the aircraft as known by Airbus,

‐ The aircraft model.

The “M” field may indicate the following Evolution Code:

‐ The “N” letter indicates a new aircraft added by this MEL revision,

‐ The “R” letter indicates a change of the FSN or registration number or aircraft model.

LIST OF MODIFICATIONS ( LOM )

The LOM lists the criteria (Modification Proposals ( MP ) and Service Bulletins ( SB )) which the

installation on the aircraft affects the MEL .

Note: Each MP has one or more associated MOD s. The MP / MOD correlation is available in

AirN@v / Engineering.

The LOM also indicates:

‐ The title of the criteria,

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MEL ← G to J → 27 FEB 15

‐ The list of aircraft that have the criteria,

‐ The “M” field that may indicate the following Evolution Code:

• The “E” letter indicates an aircraft validity change of the criteria. The list of aircraft to which

the criteria applies has changed compared to the previous MEL revision, by addition or

deletion of one or several aircraft.

• The “N” letter indicates new criteria added by this MEL revision,

• The “R” letter indicates a change in the criteria title or associated SB .

OPTIONAL EQUIPMENT (IF INSTALLED) 

Ident.: HOW-00012808.0001001 / 17 SEP 10

The (If Installed) symbol  indicates that a paragraph is applicable only if the aircraft has the

related equipment.

When a DU title has the (If Installed) symbol  , this indicates that the DU might not apply to all the

aircraft listed in the DU validity.

The Operator is responsible for:

‐ Managing the aircraft validity for the DU in the MEL and removing the (If Installed) symbol  , or

‐ Removing the DU from the MEL if the DU does not apply to the Operator’s fleet.

REMOVAL OF ITEM

Ident.: HOW-00012809.0001001 / 17 SEP 10

When operating under MEL , it is not permitted to remove the item from its place in the aircraft,

unless the associated dispatch condition clearly authorizes the Operator to do it.

Note: The (If Installed)  symbol does not mean that the Operator can remove the item. This

symbol indicates that the configuration of some aircraft of the Operator's fleet might not

include this item.

Refer to HOW Optional Equipment (If Installed)

.

HOW TO USE THE MEL ENTRIES SECTION?

Ident.: HOW-00012810.0001001 / 12 SEP 11

This section lists all the ECAM alerts. The ECAM monitors the condition of some systems. In the

case of malfunction of one or more systems, the ECAM provides the flight crew with an associated

ECAM alert.

Refer to MI-00-08 ECAM and MAINTENANCE STATUS

.

For each ECAM alert, this section indicates the associated MEL item (if any) to be applied for the

dispatch.

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HOW TO USE

MEL ← J 27 FEB 15

When an ECAM alert reports a system failure, the flight crew and the maintenance personnel should

refer to this section as a user-friendly entry point in the MEL .

AIRCRAFT STATUS COLUMN

An ECAM alert may cover one or several failure modes of the monitored system.

For each failure mode, the AIRCRAFT STATUS column may indicate the following status:

‐ NIL

: When there is only one failure mode, the AIRCRAFT STATUS column

indicates NIL .

When there are several failure modes, the AIRCRAFT STATUS column

might give a short description of each failure mode and/or a simple way

to identify each failure mode. If the MEL does not give this information,

the column displays NIL .

‐ Actual alert

: This indicates that the monitored system is inoperative. The failure mode

is the failure of the monitored system.

‐ False alert

: This indicates that the monitoring system is inoperative. The failure

mode is the failure of the monitoring system. The monitored system

remains fully operative.

The Operator is responsible for identifying the failure mode.

CONDITION OF DISPATCH COLUMN

For each failure mode, the CONDITION OF DISPATCH column gives the applicable MEL item(s)

for dispatch. But the flight crew is responsible for checking that the condition of the aircraft

systems/components complies with the MEL requirements. If not, the dispatch of the

aircraft is not permitted.

The CONDITION OF DISPATCH column may also give the following alternate possibilities:

‐ NO DISPATCH : It is not permitted to dispatch the aircraft when the ECAM displays this

alert.

‐ Not related to MEL : The ECAM alert does not report a system failure but a reversible

abnormal condition such as the state of a system or an aircraft

configuration or an external condition. This condition is not a system

failure and is not related to MEL . The MEL shall not be used.

This is not a NO-GO situation. The corrective action to revert to normal

condition is immediate, obvious or well known by flight crew and/or

maintenance personnel.

(65)

MEL K → 27 FEB 15

HOW TO USE THE MMEL ITEMS SECTION?

Ident.: HOW-00012811.0001001 / 10 OCT 14