Minimum Equipment List MEL Dornier 328-100.pdf

AEROLNEADEANTIOQUIA

MINIMUMEQUIPMENTLIST

INACCORDANCEWITH:

MASTERMINIMUMEQUIPMENTLISTREV411/25/1998FAA

Dornier328100

AIRCRAFTDO328120S/N3084DO328120S/N3039

02REVISION19/03/2013

Page:II Date:09/03/2012

Revision:OriginalMinimumEquipmentListDo328100

EngineeringDepartment

PRELIMINARY

Page:III Date:19/03/2013

Revision:02MinimumEquipmentListDo328100


RevisionsLogThe Minimum Equipment List of Dornier 328100 fleet, is under the control of theEngineeringDepartmentofAerolneadeAntiquia,aheadoftheFleetEngineer.OnlytheFleetEnginnercanmodifythisMELandlogtherevisioninthenextcontroltable,subsequentAuthorityapproval.

Revision DateofRevision AcceptanceDate InsertedbyOriginal 09/03/2012 01/06/2012 EngineeringDep.

01 08/10/2012 EngineeringDep.02 19/03/2013 EngineeringDep.

REVISIONHIGHLIGHTS

REVISIONNo CHANGESORIGINAL AdditionDornier328fleetofAerolneadeAntioquiaS.A.ADA.

1 Preambleactualizationandweatherradarrequirednumberfordeparture.

2

GeneralRevision(RACreferences,verificationwithDispatchDeviationProceduresGuide,weatherradarrequirednumberfordeparture,

emergencymedicalkitinstalledandrequirednumberfordeparture)andDornier328HK4917S/N3039addition.

NOTE:THISMANUALSHOULDBEDISTRIBUTEDTOTHENEXTPLACES:

Dornier328100HK4849S/N3084. Dornier328100HK4917S/N3039. EngineeringDepartment. MaintenanceDepartment. OperationsDepartment. DispatchDepartment. BarranquillaBase. MonteriaBase. UAEAC.

Page:IV Date:19/03/2013



EffectivePagesPage Revision Date

I 02 19/03/2013II Original 09/03/2012III 02 19/03/2013IV 02 19/03/2013V 02 19/03/2013VI Original 09/03/2012VII Original 09/03/2012VIII Original 09/03/2012IX Original 09/03/2012X Original 09/03/2012XI Original 09/03/2012XII Original 09/03/2012XIII Original 09/03/2012XIV Original 09/03/2012XV 02 19/03/2013XVI Original 09/03/2012XVII 02 19/03/2013XVIII Original 09/03/2012XIX Original 09/03/201211 Original 09/03/201212 02 19/03/201313 02 19/03/201321 Original 09/03/2012211 02 19/03/2013212 02 19/03/2013213 02 19/03/2013214 02 19/03/2013215 02 19/03/2013216 02 19/03/2013217 02 19/03/2013218 02 19/03/2013219 02 19/03/20132110 02 19/03/20132111 02 19/03/20132112 02 19/03/20132113 02 19/03/2013221 02 19/03/2013222 02 19/03/2013223 02 19/03/2013224 02 19/03/2013

Page Revision Date225 02 19/03/2013231 02 19/03/2013232 02 19/03/2013233 02 19/03/2013234 02 19/03/2013241 02 19/03/2013242 02 19/03/2013243 02 19/03/2013244 02 19/03/2013245 02 19/03/2013246 02 19/03/2013247 02 19/03/2013248 02 19/03/2013249 02 19/03/20132410 02 19/03/20132411 02 19/03/20132412 02 19/03/20132413 02 19/03/20132414 02 19/03/20132415 02 19/03/20132416 02 19/03/20132417 02 19/03/20132418 02 19/03/2013251 02 19/03/2013252 02 19/03/2013253 02 19/03/2013254 02 19/03/2013255 02 19/03/2013261 02 19/03/2013262 02 19/03/2013263 02 19/03/2013271 02 19/03/2013272 02 19/03/2013273 02 19/03/2013274 02 19/03/2013275 02 19/03/2013276 02 19/03/2013277 02 19/03/2013281 02 19/03/2013

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Page Revision Date282 02 19/03/2013283 02 19/03/2013284 02 19/03/2013285 02 19/03/2013286 02 19/03/2013287 02 19/03/2013288 02 19/03/2013289 02 19/03/20132810 02 19/03/20132811 02 19/03/20132812 02 19/03/20132813 02 19/03/20132814 02 19/03/2013291 02 19/03/2013301 02 19/03/2013302 02 19/03/2013303 02 19/03/2013304 02 19/03/2013305 02 19/03/2013306 02 19/03/2013307 02 19/03/2013308 02 19/03/2013309 02 19/03/20133010 02 19/03/20133011 02 19/03/20133012 02 19/03/20133013 02 19/03/20133014 02 19/03/20133015 02 19/03/20133016 02 19/03/20133017 02 19/03/20133018 02 19/03/20133019 02 19/03/2013311 02 19/03/2013312 02 19/03/2013321 02 19/03/2013322 02 19/03/2013323 02 19/03/2013331 02 19/03/2013

Page Revision Date332 02 19/03/2013333 02 19/03/2013334 02 19/03/2013341 02 19/03/2013342 02 19/03/2013343 02 19/03/2013344 02 19/03/2013345 02 19/03/2013346 02 19/03/2013347 02 19/03/2013348 02 19/03/2013351 02 19/03/2013352 02 19/03/2013353 02 19/03/2013361 02 19/03/2013362 02 19/03/2013363 02 19/03/2013364 02 19/03/2013365 02 19/03/2013366 02 19/03/2013491 02 19/03/2013611 Original 09/03/2012731 02 19/03/2013732 02 19/03/2013733 02 19/03/2013734 02 19/03/2013735 02 19/03/2013736 02 19/03/2013771 Original 09/03/2012791 Original 09/03/2012

Page:VI Date:09/03/2012



AcronymsA/C Aircraft

AC AlternatingCurrent

AAS AntiIceAdvisorySystem

AC AdvisoryCircular

ACMP AlternatingCurrentMainPump

ACO AircraftCertificationOffice

AD AirworthinessDirective

ADC AirDataComputer

ADF AutomaticDirectionFinding

ADg AccidentalDamage

ADP AutomaticDataProcessing

AECMA AssociationEuropeennedesConstructeursdeMatrielAerospatial

AEG AircraftEvaluationGroup

AEP AgeExplorationProgram

AFT Aft

AHRS AttitudeandHeadingReferenceSystem

ALD AirworthinessLimitationsDocument

ALI AirworthinessLimitationItem

AMM AircraftMaintenanceManual

APU AuxiliaryPowerUnit

ATA AirTransportAssociation

ATC AirTrafficControl

ATPCS AutomaticTakeoffPowerControlSystem

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BITE BuiltInTestEquipment

BO Borescope

CA CriticalityAnalysis

CAA CivilAviationAuthority

CAC CrewAlertingComputer

Cal Calendar

CDH ControlDeliveryHead

CDL ConfigurationDeviationList

CMM ComponentMaintenanceManual

CMP ContinuousMaintenanceProgram

CMR CertificationMaintenanceRequirement

CAT Category

CPCP CorrosionPreventionandControlProgram

CVR CockpitVoiceRecorder

DC DirectCurrent

DCMP DirectCurrentMainPump

DI DetailedInspection

DME DistanceMeasuringEquipment

DON DornierStandard

DPI DyePenetrantInspection

DS Discard

DT DamageTolerance

EC EddyCurrent

ECS EnvironmentalControlSystem

Page:VIII Date:09/03/2012



ECTM EngineConditionTrendMonitoring

ED EnvironmentalDeterioration

EDU EngineDiagnosticUnit

EFCV EjectorFlowControlValve

EFIS ElectronicFlightInstrumentSystem

ELT EmergencyLocatorTransmitter

EMM EngineMaintenanceManual

EMSG EuropeanMaintenanceSystemGuide

E/POV ElectroPneumaticOutflowValve

EPS EmergencyPowerSupply

EPSU EmergencyPowerSupplyUnit

ERL EconomicRepairLife

EWIS ElectricalWiringInterconnectionSystem

FAA FederalAviationAdministration

FADEC FullAuthorityDigitalEngineControl

FAR FederalAviationRegulation

FC FlightCycle

FCk FunctionalCheck

FD FatigueDamage

FDR FlightDataRecorder

FH FlightHour

FI FlightIdle

FL FlightLevel

FLP FleetLeaderProgram

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Flt Flight(s)

FMEA FailureModeandEffectsAnalysis

FMECA FailureMode,EffectsandCriticalityAnalysis

FR Frame

ft Foot/Feet

FWD Forward

GPS GlobalPositioningSystem

GPW GroundProximityWarning

GPWS GroundProximityWarningSystem

GSE GroundSupportEquipment

GVI GeneralVisualInspection

HF HighFrequency

HIRF HighIntensityRadiatedFields

HMU HydroMechanicalUnit

HP HighPressure

HSI HotSectionInspection

IN Inspection

IRS InertialReferenceSystem

ISC IndustrySteeringCommittee

ISMP IntegratedStructuralMaintenanceProgram

ITT InterTurbineTemperature

JAA JointAirworthinessAuthorities

JAR JointAirworthinessRequirement

L Liter

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LBA LuftfahrtBundesamt

LC LineCheck

LCF LowCycleFatigue

LH LeftHand

LOC LocatorLPLiquidPenetrant

LP LowPressure

LRU LineReplaceableUnit

LSA LogisticSupportAnalysis

LU Lubrication

MAP MaintenanceAnalysisPolicy&Procedures

MaPeI MajorPeriodicInspection

MEL MinimumEquipmentList

MII MajorInspectionInterval

MLDIC MaintenanceandLimitationsDocumentforIntensiveCare

MLG MainLandingGear

MLS MicrowaveLandingSystem

MMEL MasterMinimumEquipmentList

MMH/FH MaintenanceManHours/FlightHour

MP MagneticParticle

MPD MaintenancePlanningDocument

MPDH MaintenanceProgramDevelopmentHandbook

MPI MagneticParticleInspection

MPP MaintenanceProgramProposal

MR ManufacturerRecommendation

Page:XI Date:09/03/2012



MRB MaintenanceReviewBoard

MSC MaintenanceSteeringCommittee

MSG3 MaintenanceSteeringGroup3rdtaskforce

MSI MaintenanceSignificantItem

MTA MaintenanceTaskAnalysis

MTBF MeanTimeBetweenFailure

MTD MaintenanceTaskDescription

MTH Month(s)

MWG MaintenanceWorkingGroup

NAA NationalAviationAuthority

NDMT NonDeletableMaintenanceTask

NDT NonDestructiveTest

NH HighCompressorSpeed

NL LowCompressorSpeed

NLG NoseLandingGear

NP PropellerSpeed

NR NationalRequirement

NRV NonReturnValve

NTM NonDestructiveTestingManual

OC OperationalCheck

OH Overhaul

OI OpportunityInspection

Oxy Oxygen

PBE ProtectiveBreathingEquipment

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PCU PropControlUnit

PIN PartIdentificationNumber

PL PowerLever

PMP PrimaryMaintenanceProcess

PN PartNumber

POV PneumaticOutflowValve

PPH PolicyandProcedureHandbook

PR+R PressureRegulatorandReliefValve

PSEU ProximitySwitchElectronicUnit

PSU PassengerServiceUnit

PT PowerTurbine

PWC Pratt&WhitneyCanada

QPA QuantityPerAircraft

Qty Quantity

R Rating

RAC ReglamentosAeronuticosdeColombia

RF MandatoryRetrofit

RH RightHand

RPM RevolutionsPerMinute

RS Restoration

Ref Reference

Rev Revision

SB ServiceBulletin

SDI SpecialDetailedInspection

Page:XIII Date:09/03/2012



SIP StructuresInspectionProgram

SL SafeLife

SMP StandardMaintenanceProgram

SSI StructuralSignificantItem

STA Station

STBY Standby

SV Servicing

TBD ToBeDetermined

TBO TimeBetweenOverhaul

TC TireChange

TCAS TrafficControlAlertingSystem

TCS TouchControlSteering

TI ThresholdInspection

TII ThresholdInspectionInterval

TLD TimeLimitedDispatch

TPS TemporaryProtectionSystem

TT TapTest

UT UltrasonicTest

VC VisualCheck

VDR Vendor

VHF VeryHighFrequency

VI VisualInspection

VIP VeryImportantPerson

VLF VeryLowFrequency

Page:XIV Date:09/03/2012



VOR VHFOmnidirectionalRadioRange

WF FuelFlow

WG WorkingGroup

WO WWeightonWheel

WY Weekly

XR XRay

YRS Years

Page:XV Date:19/03/2013



Definitions

1.SystemDefinitions.SystemnumbersarebasedontheAirTransportAssociation (ATA)SpecificationNumber100anditemsarenumberedsequentially.

a."Item"(Column1)meanstheequipment,system,component,orfunctionlistedinthe"Item"column.b. "Number Installed" (Column 3) is the number (quantity) of items normallyinstalled in the aircraft. This number represents the aircraft configurationconsidered in developing this MMEL. Should the number be a variable (e.g.,passengercabinitems)anumberisnotrequired.c."NumberRequiredforDispatch"(Column4) istheminimumnumber(quantity)of itemsrequiredforoperationprovidedtheconditionsspecified inColumn4aremet.

NOTE: WheretheMMELshowsavariablenumberrequired fordispatch,theMELmustreflect theactualnumber required fordispatchor an alternatemeansof configurationcontrolapprovedtheAdministrator.

d."RemarksorExceptions"(Column5) inthiscolumn includesastatementeitherprohibitingorpermittingoperationwith a specificnumberof items inoperative,provisos(conditionsandlimitations)forsuchoperation,andappropriatenotes.e.Averticalbar(changebar)inthemarginindicatesachange,additionordeletionintheadjacenttextforthecurrentrevisionofthatpageonly. Thechangebar isdroppedatthenextrevisionofthatpage.

2."Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for typecertificationandapprovedby the responsible FAAAircraftCertificationOffice.The FAAapprovedAFM/RFM for the specific aircraft is listed on the applicable Type CertificateDataSheet.3."AsrequiredbyFAR/RAC"meansthatthelisteditemissubjecttoprovisions(restrictiveorpermissive)expressedintheFederalAviationRegulationsoperatingrules.ThenumberofitemsrequiredbytheFAR/RACmustbeoperative.WhenthelisteditemisnotrequiredbyFAR/RACitmaybeinoperativefortimespecifiedbyrepaircategory.4.Eachinoperativeitemmustbeplacardedtoinformandremindthecrewmembersandmaintenancepersonneloftheequipmentcondition.

Page:XVI Date:09/03/2012



NOTE: To the extent practical, placards should be located adjacent to the control orindicatorfortheitemaffected;however,unlessotherwisespecified,placardwordingandlocationwillbedeterminedbytheoperator.5.""symbol inColumn3and/orColumn4 indicatesavariablenumber(quantity)oftheiteminstalled.6. "Deleted" in the remarks columnaftera sequence item indicates that the itemwaspreviouslylistedbutisnowrequiredtobeoperativeifinstalledintheaircraft.7. "ER" refers toextended rangeoperationsofa twoengineairplanewhichhasa typedesignapproval forERoperationsandcomplieswith theprovisionsofAdvisoryCircular12042A.8. "Federal Aviation Regulations" (FAR) means the applicable portions of the FederalAviationActandFederalAviationRegulations.9. "Flight Day" means a 24 hour period (from midnight to midnight) either UniversalCoordinated Time (UCT) or local time, as established by the operator, duringwhich atleastoneflightisinitiatedfortheaffectedaircraft.10."IcingConditions"meansanatmosphericenvironmentthatmaycauseicetoformontheaircraftorintheengine(s).11. Alphabetical symbol in Column 5 indicates a proviso (condition or limitation) thatmustbecompliedwithforoperationwiththelistediteminoperative.12. "Inoperative"means a system and/or componentmalfunction tothe extent that itdoesnotaccomplish its intendedpurposeand/or isnotconsistentlyfunctioningnormallywithinitsapprovedoperatinglimit(s)ortolerance(s).13. "Notes:" in Column 5 provides additional information for crewmember ormaintenance consideration. Notes are used to identify applicable material which isintendedtoassistwithcompliance,butdonotrelievetheoperatoroftheresponsibilityforcompliancewithallapplicablerequirements.Notesarenotapartoftheprovisos.14. Inoperative components of an inoperative system: Inoperative items which arecomponentsofasystemwhichisinoperativeareusuallyconsideredcomponentsdirectlyassociated with and having no other function than to support that system.(Warning/caution systems associated with the inoperative system must be operativeunlessreliefisspecificallyauthorizedpertheMMEL).

Page:XVII Date:19/03/2013



15. "(M)" symbol indicates a requirement for a specificmaintenance procedurewhichmustbeaccomplishedpriortooperationwiththelistediteminoperative.Normallytheseproceduresareaccomplishedbymaintenancepersonnel;however,otherpersonnelmaybequalifiedandauthorizedtoperformcertainfunctions.Proceduresrequiringspecializedknowledgeorskill,orrequiringtheuseoftoolsortestequipmentshouldbeaccomplishedby maintenance personnel. The satisfactory accomplishment of all maintenanceprocedures,regardlessofwhoperformsthem,istheresponsibilityoftheoperator.Appropriateproceduresarerequiredtobepublishedaspartoftheoperator'smanualorMEL.16."(O)"symbolindicatesarequirementforaspecificoperationsprocedurewhichmustbe accomplished in planning for and/or operating with the listed item inoperative.Normallytheseproceduresareaccomplishedbytheflightcrew;however,otherpersonnelmay be qualified and authorized to perform certain functions. The satisfactoryaccomplishmentofallprocedures,regardlessofwhoperformsthem, istheresponsibilityof theoperator.Appropriateprocedures are required tobepublished as apartof theoperator'smanualorMEL.NOTE: The (M) and (O) symbols are required in the operator'sMEL unless otherwiseauthorizedbytheAdministrator.17."Deactivated"and"Secured"meansthatthespecifiedcomponentmustbeputintoanacceptableconditionforsafeflight.Anacceptablemethodofsecuringordeactivatingwillbeestablishedbytheoperator.18."VisualFlightRules"(VFR)isasdefinedinFARPart91andRAC4.2.2.3.ThisprecludesapilotfromfilinganInstrumentFlightRules(IFR)flightplan.19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment issuch thatwouldallowa flight toproceedunder thevisual flight rulesapplicable to theflight.ThisdoesnotprecludeoperatingunderInstrumentFlightRules.20."VisibleMoisture"meansanatmosphericenvironmentcontainingwaterinanyformthatcanbeseen innaturalorartificial light;forexample,clouds,fog,rain,sleet,hail,orsnow.21."PassengerConvenienceItems"meansthoseitemsrelatedtopassengerconvenience,comfortorentertainmentsuchas,butnotlimitedto,galleyequipment,movieequipment,ashtrays,stereoequipment,overheadreadinglamps,etc.

Page:XVIII Date:09/03/2012



22.RepairIntervals:AllusersofanMELapprovedunderFAR121,125,129and135musteffect repairs of inoperative systems or components, deferred in accordancewith theMEL,atorpriortotherepairtimesestablishedbythefollowingletterdesignators:

Category A. Items in this category shall be repaired within the time intervalspecifiedintheremarkscolumnoftheoperator'sapprovedMEL.CategoryB. Items in thiscategoryshallbe repairedwithin three (3)consecutivecalendardays (72hours),excluding theday themalfunctionwas recorded in theaircraftmaintenancerecord/logbook. Forexample, if itwererecordedat10a.m.onJanuary26th,thethreedayintervalwouldbeginatmidnightthe26thandendatmidnightthe29th.CategoryC. Items in this category shallbe repairedwithin ten (10) consecutivecalendardays(240hours),excludingthedaythemalfunctionwasrecordedintheaircraftmaintenancerecord/logbook. Forexample, if itwererecordedat10a.m.onJanuary26th,the10dayintervalwouldbeginatmidnightthe26thandendatmidnightFebruary5th.Category D. Items in this category shall be repaired within one hundred andtwenty (120) consecutive calendar days (2880 hours), excluding the day themalfunctionwasrecordedintheaircraftmaintenancelogand/orrecord.

23.ElectronicfaultalertingsystemGeneralDornier328equippedwithEngine IndicatingandCrewAlertingSystems (EICAS)providedifferentprioritylevelsofsystemmessages(WARNING,CAUTION,ADVISORY,STATUSandMAINTENANCE).AnymessagesthataffectsairplanedispatchstatuswillbedisplayedataSTATUSmessagelevelorhigher.The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY)indicatesthatthesystem/component isoperatingwithin itsapprovedoperating limitsortolerances.Systemconditionsthatresultonlyinamaintenancelevelmessage,i.e.nocorrelationwithahigherlevelEICASmessage,donotaffectdispatchanddonotrequireactionotherthanasaddressedwithinanoperatorsstandardmaintenanceprogram.24. "Administrative control item"means an item listedby theoperator in theMEL fortrackingandinformationalpurposes.Itmaybeaddedtoanoperator'sMELbyapprovalofthePrincipalOperations Inspectorprovidedno relief isgranted,orprovided conditionsand limitations are contained in an approved document (i.e. Structural RepairManual,airworthinessdirective,etc.).

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Ifreliefotherthanthatgrantedbyanapproveddocumentissoughtforanadministrativecontrolitem,arequestmustbesubmittedtotheAdministrator.Iftherequestresultsinreview and approval by the FOEB, the item becomes an MMEL item rather than anadministrativecontrolitem.25."***"symbol inColumn1 indicatesan itemwhich isnotrequiredbyregulationbutwhichmayhavebeen installedonsomemodelsofaircraftcoveredby thisMMEL. Thisitemmaybe includedon theoperator'sMELafter theapprovingofficehasdeterminedthatthe itemhasbeen installedononeormoreoftheoperator'saircraft. Thesymbol,however,shallnotbecarried forward into theoperator'sMEL. Itshouldbenoted thatneither thispolicynor theuseof this symbolprovideauthority to installor removeanitemfromanaircraft.26."ExcessItems"meansthoseitemsthathavebeeninstalledthatareredundanttotherequirementsoftheFARs.27. "Day of Discovery" is the calendar day an equipment/instrument malfunction wasrecorded in theaircraftmaintenance logandor record. Thisday isexcluded from thecalendardaysorflightdaysspecifiedintheMMELfortherepairofaninoperativeitemofequipment.ThisprovisionisapplicabletoallMMELitems,i.e.,categories"A,B,C,andD."

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Revisin:OriginalMinimumEquipmentListDo328100


CHAPTER1INTRODUCTION


Revisin:02MinimumEquipmentListDo328100


1.PreambleThefollowingisapplicableforauthorizedcertificateholdersoperatingunderReglamentosAeronuticosdeColombia(RAC)Part4.5:TheRACrequirethatallequipmentinstalledonanaircraftincompliancewiththeAirworthinessStandardsandtheOperatingRulesmustbeoperative. However,theRulesalsopermitthepublicationofaMinimumEquipmentList(MEL)wherecompliancewithcertainequipmentrequirementsisnotnecessaryintheinterestsofsafetyunderalloperatingconditions.Experiencehasshown thatwith thevarious levelsof redundancydesigned intoaircraft,operation of every system or installed component may not be necessary when theremaining operative equipment can provide an acceptable level of safety. A MasterMinimum Equipment List (MMEL) is developed by the FAA, with participation by theaviation industry, to improve aircraft utilization and thereby providemore convenientandeconomicairtransportationforthepublic.TheFAAapprovedMMELincludesthoseitemsofequipmentrelatedtoairworthinessandoperatingregulationsandotheritemsofequipmentwhichtheAdministratorfindsmaybeinoperativeandyetmaintainanacceptable levelofsafetybyappropriateconditionsandlimitations;itdoesnotcontainobviouslyrequireditemssuchaswings,flaps,andrudders.The MMEL is the basis for development of individual operator MELs which take intoconsideration theoperator'sparticularaircraftequipmentconfigurationandoperationalconditions.OperatorMELs,foradministrativecontrol,mayincludeitemsnotcontainedinthe MMEL; however, relief for administrative control items must be approved by theAdministrator.Anoperator'sMELmaydifferinformatfromtheMMEL,butcannotbelessrestrictivethantheMMEL.The individualoperator'sMEL,whenapprovedandauthorized,permitsoperationoftheaircraftwithinoperativeequipment.Equipmentnot requiredby theoperationbeing conductedandequipment inexcessofFAR/UAEAC requirements are included in the MEL with appropriate conditions andlimitations. The MEL must not deviate from the AircraftFlight Manual Limitations,EmergencyProceduresorwithAirworthinessDirectives.Itisimportanttorememberthatall equipment related tothe airworthiness and the operating regulations of the aircraftnotlistedontheMMELmustbeoperative.Suitableconditionsandlimitationsintheformofplacards,maintenanceprocedures,crewoperating procedures and other restrictions as necessary are specified in the MEL toensurethatanacceptablelevelofsafetyismaintained.




TheMELisintendedtopermitoperationwithinoperativeitemsofequipmentforaperiodoftimeuntilrepairscanbeaccomplished.Itisimportantthatrepairsbeaccomplishedattheearliestopportunity.Inordertomaintainanacceptable levelofsafetyandreliabilitytheMMELestablishes limitationson thedurationof and conditions foroperationwithinoperativeequipment.TheMELprovidesforreleaseoftheaircraftforflightwithinoperativeequipment.Whenanitemofequipmentisdiscoveredtobeinoperative,itisreportedbymakinganentryintheAircraftMaintenanceRecord/LogbookasprescribedbyRAC.TheitemistheneitherrepairedormaybedeferredpertheMELorotherapprovedmeansacceptabletotheAdministratorpriortofurtheroperation.MELconditionsandlimitationsdo not relieve the operator from determining that the aircraft is in condition for safeoperationwithitemsofequipmentinoperative.When these requirements are met, an Airworthiness Release, Aircraft MaintenanceRecord/Logbookentry,orotherapproveddocumentationisissuedasprescribedbyRAC.Such documentation is required prior to operation with any item of equipmentinoperative.Operatorsareresponsibleforexercisingthenecessaryoperationalcontroltoensurethatan acceptable level of safety ismaintained.When operatingwithmultiple inoperativeitems,theinterrelationshipsbetweenthoseitemsandtheeffectonaircraftoperationandcrewworkloadwillbeconsidered.Operators are to establish a controlled and sound repair program including the parts,personnel,facilities,procedures,andschedulestoensuretimelyrepair.WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL ISREQUIRED.

2.CoveredFleet

Aircraft Model S/NDornier DO328100mod.20 3084Dornier DO328100mod.20 3039


Revisin:OriginalMinimumEquipmentListDo328100


CHAPTER2SYSTEMSANDSUBSYSTEMS

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1SystemandSequencenumbers

2RectificationInterval 3NumberInstalled

4NumberRequiredforDispatch 5RemarksorExceptions

21AIRCONDITIONING1CabinAltitudeWarningSystem2CabinTemperatureControlSystem

1AutomaticMode2ManualMode

3 Flight Compartment TemperatureControlSystem

1AutomaticMode2ManualMode

4RecirculationFans5EFISFan

CCCCCCB

1111121

0000O00

May be inoperative providedoperationsareconductedatorbelow10,000feetMSL.Maybe inoperativeprovidedManualModeoperatesnormally.May be inoperative providedAutomaticModeoperatesnormally.Maybe inoperativeprovidedManualModeoperatesnormally.May be inoperative providedAutomaticModeoperatesnormally.M)Maybeinoperativeprovided:

a) Inoperative Fan(s) isdeactivated,b) Both ECS Packs operatenormally,andc)ECSFlowMode isoperatedinHIGH.

(M)This itemmaybeperformedbyaqualified crewmember. Todeactivateinoperativefan,pullandsecureC/Bincockpit for affected fan using alockoutring.(M)Maybeinoperativeprovided:

a) Inoperative Fan isdeactivated,b)AvionicFanoperatesc) Both ECS Packs operatenormally,and

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21AIRCONDITIONING5EFISFan(Cont.)6AvionicFan7HeatExchanger(HX)Fans

BBC

112

001

d)ECSFlowModeisoperatedinHIGH.

(M)This itemmaybeperformedbyaqualified crewmember. Todeactivateinoperativefan,pullandsecureC/Bincockpit for affected fan using alockoutring.(M)Maybeinoperativeprovided:

a) Inoperative Fanisdeactivated,b)EFISFanoperatesnormally,c) Both ECS Packs operatenormally,andd)ECSFlowModeisoperatedinHIGH.

(M)This itemmaybeperformedbyaqualified crewmember. Todeactivateinoperativefan,pullandsecureC/Bincockpit for affected fan using alockoutring.(M) (O) One may be inoperativeprovided:

a) Inoperative Fan isdeactivated,b)SingleECSPackTakeoffandLanding procedures aredevelopedandused,c) Associated Pack is notoperatedontheground,d) Associated Pack is notoperatedinflightatairspeedsbelow120KIAS,ande) During single Packoperations,ECSFlowMode isoperatedinHIGH.

(M)This itemmaybeperformedbyaqualified crewmember. Todeactivateinoperativefan,pullandsecureC/Bincockpit for affected fan using alockoutring.

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21AIRCONDITIONING7HeatExchanger(HX)Fans(Cont.)8ECSECONFlowMode9 Cabin Pressurization ControlSystem(CPCS)

1AutomaticSystem

CCC

211

100

(O) a) Ensure associated ECS Pack isOFFforallgroundoperations.

b) After takeoff selectassociated ECS PackON withairspeed greater than 120KIAS,andabove1.500AGL.c) Prior to landing, selectassociated ECS Pack OFF atBefore Landing Checklistwithairspeedabove120KIAS.

(O)Maybeinoperativeprovided:

a) HIGH Mode operatesnormally,andb)FlightPlanning isbasedonECSHIGHFuelConsumption.

(O) Operate ECS flow mode in HIGHduringallECSOperations.(M)(O)Maybeinoperativeprovided:

a) Manual PressurizationSystemoperatesnormally,b) CPCS Automatic Controllerisdeactivated,c) EICAS CPCS System Pageoperatesnormally,d)Dumpfunctionisverifiedtooperatenormally,ande) Alternate procedures forcontrolling Pressurizationmanually are established andused.

(O) MAN CABIN ALT Selector asrequired to follow pressurizationschedule.

Donotexceed500fpm. Do not exceed CABIN DIFF

PRESSof6.75. Do not exceed CABIN ALT of

8000ft.

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21AIRCONDITIONING9 Cabin Pressurization ControlSystem(CPCS)(Cont.)

2 Automatic and Manualsystems

3CPCSBackupModule

CCC

121

000

(M)This itemmaybeperformedbyaqualified crewmember. Todeactivatepull and secure the CPCS AUX andCPCS PRIMARY C/B using a lockoutring.(M)(O)Maybeinoperativeprovided:

a) Flight restricted to 10,000feetorbelow,b) Either outflow valve issecuredopen,andc) Both ECS packs operatenormally.

(O)a)Flightarerestrictedto10.000ftorbelow.

b)OperatebothECSpacks.(M)TosecureElectropneumaticOFVinopenposition

a) Press CAB DUMPpushbuttonSw.b)Pulland secureCABPRESSDUMP, CAB PRESS 1, CABPRESS2C/B.

To secure Pneumatic OFV in openposition:

a) Open the Vacuum Line atthevalve.b) Placard ControlledINOPERATIVE VACUUM LINEDISCONNECTED

(M)Maybeinoperativeprovided:

a) CPCS Backup Module isdeactivated,andb)EICAS"CPCSMISCOMPARE"CautionMessageisremoved.

(M)This itemmaybeperformedbyaqualifiedcrewmember.Todeactivate,pull and secure the CPCS BackupModuleC/Busingalockoutring.

Pgina:215 Fecha:19/03/2013






21AIRCONDITIONING9 Cabin Pressurization ControlSystem(CPCS)(Cont.)

4CPCSDigitalDisplay10 "MAN" Annunciator Light onPRESSURIZATION Control AUTO/MANPushbutton(OverheadPanel)11 "MAN" Annunciator Light onCOCKPIT Temperature Control ModePushbutton(OverheadPanel)

CCC

111

000


a) System page operatesnormally,andb) Alternate procedures areestablishedandusedtoverifylanding elevation on theCPCS/OXYpage.

(O)UsingtheCPCS/OXYsystempage,verify landing elevation before eachtakeoff.(M) Light may fail to illuminateprovided:

a) Pressurization AUTO/MANselection function is verifiedtooperatenormally,b) EICAS "CPCS CTRL MODEMAN" Status Message isverified to operate normally,andc) EICAS CPCS System Pageoperatesnormally.

(M)This itemmaybeperformedbyaqualifiedcrewmember.

a)SelectthePRESSURIZATIONAUTO/MAN Pushbutton toMANb)VerifytheCPCSCTRLMODEMAN Blue CAS StatusMessageilluminatesonEICASc)SelectthePRESSURIZATIONAUT/MAN Pushbutton toAUTOd)VerifytheCPCSCTRLMODEMAN Blue CAS StatusMessageextinguishes.

(M)(O)Lightmayfailtoilluminateprovided:

a) Cockpit TemperatureControl Mode selectionfunction isverifiedtooperate

Pgina:216 Fecha:19/03/2013






21AIRCONDITIONING11 "MAN" Annunciator Light onCOCKPIT Temperature Control ModePushbutton(OverheadPanel)(Cont.)12 "MAN" Annunciator Light onCABIN Temperature Control ModePushbutton(OverheadPanel)

CC

11

00

normally,b) EICAS CPCS System Pageoperatesnormally,andc) Alternate procedures fordetermining CockpitTemperature Control Modeareestablishedandused.

(O) Select the cockpit Temp ControlMode Selector to MAN position(Pressed In) or AUTO position(PressedOut).(M)This itemmaybeperformedbyaqualifiedcrewmember.WiththeECSSystemPageDisplayed:

a) Select the Cockpit TempControl Mode pushbutton In(Flush)b) Note the digital CockpitTemperature readout isreplacedbydashes()c) Select the cockpit TempControl Mode Pushbutton totheoutposition(notflush)d)Notethedashes() intheCockpit Temperature readoutis replaced by a digitalreadout of Cockpittemperature.

(M) (O) Light may fail to illuminateprovided:

a)CabinTemperatureControlMode selection function isverifiedtooperatenormally,b) EICAS CPCS System Pageoperatesnormally,andc) Alternate procedures fordetermining CabinTemperature Control Modeareestablishedandused.

Pgina:217 Fecha:19/03/2013






21AIRCONDITIONING12 "MAN" Annunciator Light onCABIN Temperature Control ModePushbutton(OverheadPanel)(Cont.)13 Vertical (Pack ValveOpen) FlowBar Lights on ECS PACK Pushbuttons(OverheadPanel)

CC

12

00

(O) Select the cockpit Temp ControlMode Selector to MAN position(Pressed In) or AUTO position(PressedOut).(M)This itemmaybeperformedbyaqualifiedcrewmember.WiththeECSSystemPageDisplayed:

a) Select the Cockpit TempControl Mode pushbutton In(Flush)b) Note the digital CockpitTemperature readout isreplacedbydashes()c) Select the cockpit TempControl Mode Pushbutton totheoutposition(notflush)d)Notethedashes() intheCockpit Temperature readoutis replaced by a digitalreadout of Cockpittemperature.

(M) (O)Light(s)may fail to illuminateprovided:

a) Associated Pack(s) isverifiedtooperatenormally,b) Associated PACKPushbutton "OFF"AnnunciatorLight(s)isverifiedtooperatenormally,c) EICAS ECS System Pageoperatesnormally,andd) Alternate procedures fordetermining associatedPack(s)operational statusareestablishedandused.

(O) a) Confirm PACK PushbuttonselectedON(IN)orOFF(OUT)b)Verify PackValve positionVia thePack Valve Synoptic on ECS systempage.

Pgina:218 Fecha:19/03/2013






21AIRCONDITIONING13 Vertical (Pack ValveOpen) FlowBar Lights on ECSPACK Pushbuttons(OverheadPanel)(Cont.)14 "OFF"AnnunciatorLightsonECSPACKPushbuttons(OverheadPanel)

CC

22

00


a) Run associated BLEEDselected ON, select affectedPACKPushbuttonONb) With associated BLEEDselected ON, select affectedPACKPushbuttonONc) Verify Pack pushbuttonOFF, annunciation lightextinguishesd)VerifyPACKValveSynopticon ECS System page showOPENe) Select PACK PushbuttonOFF(pushbuttonOut)f) Verify the associated PACKPushbutton OFF AnnunciatorLightilluminates,andthatg)ThePACKvalvesynopticonECS System page showsClosed.


a) Associated Pack(s) isverifiedtooperatenormally,b) Associated PACKPushbutton Vertical (PackValveOpen)FlowBarLight(s)isverifiedtooperatenormallyc) EICAS ECS System Pageoperatesnormally,andd) Alternate procedures fordetermining associatedPack(s)operational statusareestablishedandused.

(O) Ensure PACK Pushbutton is ON(IN)orOFF(OUT).

Pgina:219 Fecha:19/03/2013






21AIRCONDITIONING14 "OFF"AnnunciatorLightsonECSPACKPushbuttons(OverheadPanel)(Cont.)15 "HIGH"AnnunciatorLightonECSFLOW MODE Pushbutton (OverheadPanel)

CC

21

00


a)Runassociatedengineb) With associated BLEEDselected ON, select affectedPACKPushbuttonONc) Verify Pack pushbuttonVertical Flow BarAnnunciationLightilluminatesd)VerifyPACKValveSynopticon ECS System page showOPENe) Select PACK PushbuttonOFF(pushbuttonOut)f) Verify the associated Packpushbutton Vertical Flow BarAnnunciation Lightilluminates,andthatg)ThePACKvalvesynopticonECS System page showsClosed.


a)ECSFLOWMODE selectionfunction isverifiedtooperatenormally,b) EICAS ECS System Pageoperatesnormally,andc) Alternate procedures fordetermining ECS Flow Modeareestablishedandused.

(O)a)SelecttheECSFlowmodetoHIGH, ECS flow modepushbuttonout(notflush),orb) Select the ECS flow modeto ECON (dark), ECS flowmodepushbuttonin(flush)c)ConfirmECS flowstatusontheECSsystempage

Pgina:2110 Fecha:19/03/2013






21AIRCONDITIONING15 "HIGH"AnnunciatorLightonECSFLOW MODE Pushbutton (OverheadPanel)(Cont.)16 "OFF" Annunciator Light onRECIRC FAN Pushbutton Light(OverheadPanel)17 "OFF"Annunciator Lighton EFISFAN Pushbutton Light (OverheadPanel)

CCC

111

000

(M)This itemmaybeperformedbyaqualifiedcrewmember.WiththeECSsystempageselected:

a) Select the ECS flow modepushbuttonin(flush)b) Note the HIGH statusmessage on the ECS systempagec) Select the ECS flow modepushbutton to the outposition(notflush)d)Note theECONOMY statusmessage on the ECS systempage.


a) Recirculation Fans aredeactivated,b) Both ECS Packs operatenormally,c) "HIGH" LightonECSFLOWMODEPushbuttonoperatesd) ECS System is operated inHIGHMode.

(O) Operate the ECS system in theHIGHmode(M)This itemmaybeperformedbyaqualified crewmember. Pull andsecure the recirculation Fans C/Busingalockoutring.(M) (O) Light may fail to illuminateprovided:

a) EFIS Fan is verified tooperatenormally,b)EFISFANPushbutton"FAIL"Annunciator Light operatesnormally,c) EICAS "EFIS FAN FAIL"CautionMessageoperates.

Pgina:2111 Fecha:19/03/2013






21AIRCONDITIONING17 "OFF"Annunciator Lighton EFISFAN Pushbutton Light (OverheadPanel)(Cont.)18 "FAIL"Annunciator LightonEFISFANPushbutton(OverheadPanel)

CC

11

00

d) Alternate procedures fordetermining EFIS Fanoperational status areestablishedandused.

(O) Ensure that the EFIS FANpushbuttonisselectedON(IN)orOFF(OUT)ASREQUIRED(M)This itemmaybeperformedbyaqualifiedcrewmember.

a) Select the EFIS, AVIONICand RECIRC FAN pushbuttonOFFb) Select the EFIS FANSpushbuttonIn(Flush)c)Audiblynote theoperationoftheEFISfansd) Select the EFIS FANSpushbutton to the outposition(NotFlush)e) Audibly note that theoperation of the EFIS fansceases.


a) EFIS Fan is verified tooperatenormally,b)EFISFANPushbutton"OFF"Annunciator Light operatesnormally,c) EICAS "EFIS FAN FAIL"Caution Message operatesnormally,andd) Alternate procedures fordetermining EFIS Fanoperational status areestablishedandused.

(O) Ensure that the EFIS FANpushbuttonisselectedON(IN)orOFF(OUT)ASREQUIRED

Pgina:2112 Fecha:19/03/2013






21AIRCONDITIONING18 "FAIL"Annunciator LightonEFISFANPushbutton(OverheadPanel)(Cont.)19 "OFF" Annunciator Light onAVIONIC FAN Pushbutton (OverheadPanel)

CC

11

00


a)SelectEFISFanpushbuttonONb) Note EFIS Fan operationaudiblyc)PullEFISFanC/Bd)NoteEFISFANFAILCautionilluminatesonEICASe)ResetC/Bf) Select EFIS FanpushbuttonOFFg) Note EFIS Fan operationceasesaudibly


a) AVIONIC Fan is verified tooperatenormally,b) AVIONIC FAN Pushbutton"FAIL" Annunciator Lightoperatesnormally,c) EICAS "AVIONIC FAN FAIL"Caution Message operatesnormally,andd) Alternate procedures fordetermining AVIONIC Fanoperational status areestablishedandused.

(O) Ensure that the AVIONIC FANpushbuttonisselectedON(IN)orOFF(OUT)ASREQUIRED(M)This itemmaybeperformedbyaqualifiedcrewmember.

a) Select AVIONIC FanpushbuttonONb) Note AVIONIC Fanoperationaudiblyc)PullAVIONICFanC/Bd)Note AVIONIC FAN FAILCautionilluminatesonEICAS

Pgina:2113 Fecha:19/03/2013






21AIRCONDITIONING19 "OFF" Annunciator Light onAVIONIC FAN Pushbutton (OverheadPanel)(Cont.)20 FAIL Annunciator Light onAVIONIC FAN Pushbutton (OverheadPanel)

CC

11

00

e)ResetC/Bf) Select AVIONIC FanpushbuttonOFFg) Note AVIONIC Fanoperationceasesaudibly


a) AVIONIC Fan is verified tooperatenormally,b) AVIONIC FAN Pushbutton"FAIL" Annunciator Lightoperatesnormally,c) EICAS "AVIONIC FAN FAIL"Caution Message operatesnormally,andd) Alternate procedures fordetermining AVIONIC Fanoperational status areestablishedandused.

(O) Ensure that the AVIONIC FANpushbuttonisselectedON(IN)orOFF(OUT)ASREQUIRED(M)This itemmaybeperformedbyaqualifiedcrewmember.

a) Select AVIONIC FanpushbuttonONb) Note AVIONIC Fanoperationaudiblyc)PullAVIONICFanC/Bd)Note AVIONIC FAN FAILCautionilluminatesonEICASe)ResetC/Bf) Select AVIONIC FanpushbuttonOFFg) Note AVIONIC Fanoperationceasesaudibly

Pgina:221 Fecha:19/03/2013






22AUTOFLIGHT1Autopilot2ControlWheelDisengageSwitches3TouchControlSteering(TCS)Switches4 Go Around (GA) Switches (on PowerLevers)5FlightGuidanceControlUnit

1 Reduced Bank Angle (BANK)Mode

CCCCCCC

1222211

0100000

May be inoperative providedapproachminimumsdonotrequireit'suse.One may be inoperative providedthe autopilot is not utilized at lessthantheinitialapproachaltitude.May be inoperative providedAutopilotisnotused.(O)May be inoperative providedalternateGoAroundProceduresareestablishedandused.(O For go around operations fromside(s) with inoperative go aroundpowerleverswitches:

a)Disconnectautopilotwithcontrol wheel disengageswitchesb) Rotate to go aroundattitude by reference toattitudeindicatorc) Set go around torque byreference to torqueindicators.

May be inoperative providedAutopilotandFlightDirectorarenotused.Maybeinoperativeprovided:

a)BANKModeisnotusedb) Auto Pilot and FlightDirectorarenotengaged inHeading (HDG) Mode ifReduced Bank AngleSynopticis displayed ineitherPrimaryFlightDisplay(PFD).

Pgina:222 Fecha:19/03/2013






22AUTOFLIGHT5FlightGuidanceControlUnit(Cont.)

2Navigation(NAV)Mode

3Approach(APP)Mode

4BackCourse(BC)Mode

5FlightLevelChange(FLCH)Mode

BBCB

1111

0000

Maybeinoperativeprovided:

a) NAV Mode is notengaged.b) Auto Pilot and FlightDirectorarenotengaged if"LNAV," "VOR," "LOC," or"AZ" Mode Annunciationsare displayed on eitherPrimaryFlightDisplay(PFD).


a) Approach Minimums donotrequireitsuse,b) APP Mode is notengaged,andc) Auto Pilot and FlightDirector are not engaged if"LOC," "*VOR," or "AZ"Mode Annunciations aredisplayedoneitherPrimaryFlightDisplay(PFD).


a)BCMode isnotengaged,andb)AutoPilotandFlightDirectorarenotengagedif"BC"ModeAnnunciationisdisplayedoneitherPrimaryFlightDisplay(PFD).


a) FLCH Mode is notengaged,andb) Auto Pilot and FlightDirector are not engaged if"FLCH" Mode Annunciationis displayed on eitherPrimaryFlightDisplay(PFD).

Pgina:223 Fecha:19/03/2013







6VerticalSpeed(VS)Mode

7VerticalNavigation(VNAV)Mode

8 "BANK"PushbuttonAnnunciationLight

9 "NAV" Pushbutton AnnunciationLight

10 "APP"PushbuttonAnnunciationLight

11 "BC" Pushbutton AnnunciationLight

BCCCCC

111111

000000


a)VSMode isnotengaged,andb) Auto Pilot and FlightDirector are not engaged if"VS" Mode Annunciation isdisplayedoneitherPrimaryFlightDisplay(PFD).


a)VNAVisnotengaged,andb) Auto Pilot and FlightDirector are not engaged if"VALT," "VFLCH," or"VPATH" ModeAnnunciationsaredisplayedon either Primary FlightDisplay(PFD).

LightmayfailtoilluminateprovidedReduced Bank Angle SynopticoperatesnormallyonbothPrimaryFlightDisplays(PFD).Lightmayfailtoilluminateprovided"NAV"ModeAnnunciationsoperatenormally on both Primary FlightDisplays(PFD).Lightmayfailtoilluminateprovided"LOC" and "VOR" ModeAnnunciations operate normally onbothPrimaryFlightDisplays(PFD).Lightmay fail to illuminateprovided"BC" Mode Annunciationsoperatenormally on both PrimaryFlightDisplays(PFD).

Pgina:224 Fecha:19/03/2013







12"FLCH"PushbuttonAnnunciationLight

13 "VS" Pushbutton AnnunciationLight

14 VNAV PushbuttonAnnunciationLight"VNAV"PushbuttonAnnunciationLight15 "ALT" PushbuttonAnnunciationLight

16 "CPL" PushbuttonAnnunciationLights

17 "AP" Pushbutton AnnunciationLights

CCCCCBCB

11112222

00001010

Lightmayfailtoilluminateprovided"FLCH" Mode Annunciationsoperate normally on both PrimaryFlightDisplays(PFD).Lightmayfailtoilluminateprovided"VS" Mode Annunciations operatenormally on both Primary FlightDisplays(PFD).Lightmayfailtoilluminateprovided"VNAV" Mode Annunciationsoperate normally on both PrimaryFlightDisplays(PFD).Lightmayfailtoilluminateprovided"ALT"ModeAnnunciationsoperatenormally on both Primary FlightDisplays(PFD).One Light may fail to illuminateprovided Flight Director CoupleAnnunciator Arrows operatenormallyonbothPFD's.Light(s) may fail to illuminateprovided Flight Director CoupleAnnunciator Arrows operatenormallyonbothPFD's.One Light may fail to illuminateprovided Autopilot Status ("AP" &"TCS") Annunciations operatenormallyonbothPFD's.Light(s) may fail to illuminateprovided Autopilot Status ("AP" &"TCS") Annunciations operatenormallyonbothPFD's.

Pgina:225 Fecha:19/03/2013






22AUTOFLIGHT6 Autopilot Disconnect Warning System(AuralandPFDVisualWarnings)7FlightDirector8YawDamper

CCC

111

000

May be inoperative providedAutopilotisnotused.May be inoperative providedTakeoffMinimumsand/orApproachMinimumsdonotrequireitsuse.May be inoperative providedAutopilotisnotused.

INTENCIONALMENTEENBLANCO

Pgina:231 Fecha:19/03/2013






23COMMUNICATIONS1 Communications Systems (VHF,HF,UHF)

1VHFTx/Rx

2HFTx/Rx

2PassengerAddressSystem

DDB

211

100

(O)MaybeinoperativeprovidedbothVHF are operative for IFR andextendedoverwaterflightsand isnotpoweredbythehotbatteryBus.(O)VerifypropercommunicationwithHFTx/Rx.(O)Onemay inoperativeprovidedHFTx/Rx are operative for IFR andextendedoverwaterflightsand isnotpowered by the hot battery Bus oressentialbus.(O)VerifypropercommunicationwithVHFTx/Rx.(O)Maybeinoperativeprovided:

a) Alternate, normal andemergencyproceduresand/oroperatingrestrictionsareb) Flight Deck/CabinInterphone established andused, and System and auralalerting (chime) operatesnormally.

NOTE: Any station that operatesnormallymaybeused.(O)Usepassengeraddress systemasalternateproceduresforallnecessaryinternalcommunications.NORMAL PROCEDURES: Before takeoffcabincrewwillmakeadirectvoicecommunications with all passengers.Allpreflightannouncementsmustbecompleted prior to takeoff. All inflight announcements are by directvoice communication withpassengers.

Pgina:232 Fecha:19/03/2013






23COMMUNICATIONS2PassengerAddressSystem(Cont.)3CrewmemberInterphoneSystem

1FlightDecktoCabin,CabintoFlightDeck,CabintoCabin

2FlightDecktoGround4AlertingSystem(Chime/Light)

1FlightDeckCallLight

BBCB

1111

0000

EMERGENCY PROCEDURES: Flightdeck crew uses interphone tocommunicate with cabin crew. Ifrequired, all emergencyannouncements will be via directvoice communication withpassengers.(O)Maybeinoperativeprovided:

a) PA system operatesnormally,and canbeusedasan alternate communicationslink between the flight deckandthecabin,andb) Alternate communicationsprocedures between theaffected Flight Attendantsstation(s) and the flight deckareestablishedandused.

NOTE: Any station that operatesnormallymaybeused.(O)Usepassengeraddress systemasalternateproceduresforallnecessaryinternal communications; verify thatthepassengeraddress system is fullyoperationalpriortoflight.(O) May be inoperative providedalternate procedures are establishedandused.(O)Handmadesignalswillbeusedforcommunication from Flight deck toground.May be inoperative provided theflightdeckchimeisoperative.NOTE: The flight deck chime mustalwaysbeoperative.

Pgina:233 Fecha:19/03/2013






23COMMUNICATIONS4AlertingSystem(Chime/Light)(Cont.)

2FlightAttendantCallLight

3FlightAttendantChime5 Prerecorded PassengerAnnouncementSystem6 Cockpit Voice Recorder System(CVR)7Microphones

1 Headset/BoomMicrophones

2HandMicrophones8SELCALSystem

BBCAADCD

11112200

00000000


a)PAsystemisoperative,andb) Affected light is not usedfor Lavatory Smoke DetectorAlerting.


a)PAsystemisoperative,andb)AffectedChime isnotusedfor Lavatory Smoke DetectorAlerting.

(O) May be inoperative providedalternate procedures are establishedandused.(O) All announcements must to bemadebytheflightattendantMaybeinoperativeprovided:

a) FlightDataRecorder (FDR)operatesnormally,andb) Repairs are made withinthreeflightdays.


a) Hand microphones andHeadsets are installed andoperatenormally,b) FlightDataRecorder (FDR)operatesnormally,andc) Repairs are made withinthreeflightdays.

May be inoperative providedalternate procedures are establishedandused.May be inoperative providedproceduresdonotrequireditsuse.

Pgina:234 Fecha:19/03/2013






23COMMUNICATIONS9ClearanceDeliveryHead(CDH)10RadioManagementUnits(RMU's)

1 Nav/Comm TuningFunction

11 PassengerToFlight AttendantCallButtons(LightsandAuralTones)

CCB

1222

0111

May be inoperative provided RadioManagement Units (RMU's) operatenormally.(O)May be inoperative on oneRMUprovided:

a) Backup Engine andNavigation Displays of bothRMU'soperatenormally,b) Clearance Delivery Head(CDH)operatesnormally,andc) Alternate proceduresfortuning Nav/Comm's areestablishedandused.

(M) Individual Call Buttons may beinoperativeprovided:

a) Associated Seat(s) isBlocked and Placarded "DONOTOCCUPY",b) Inoperative Call ButtonLight(s), and associated AuralTones, failed ON aredeactivated,andc) IfLavatoryCallButtonsareinoperative, Lavatory is notused for any purpose, andaffected Lavatory Door islocked closed and Placarded"INOPERATIVE" DO NOTENTER.

(M)a)Ifacallbuttonfails,removeaffectedbulbandplacardseatDO NOT OCCUPY BlockingCard.b) If a call light fails, placardseatwith DONOTOCCUPYBlockingCard.c) If lavatory call button isinoperative,closeandlockthedoor. Placard the doorINOPERATIVE DO NOTENTER.

Pgina:241 Fecha:19/03/2013






24ELECTRICALPOWER1TransformerRectifierUnit(TRU)2 "FAIL" Annunciator Lights onInverter (INV 1/INV 2) Pushbuttons(OverheadPanel)

BC

12

00


a) DC Voltmeters and all DCGenerator and Main BatteryEICAS Failure Indicationsoperatenormally,b) Both Main DC Batteriesoperatenormally,c)Main DC Batteries are notusedforEngineStarts,andd)AfterEngine Start,Voltageof each Main DC Battery isverified to be a minimum of23Volts.


a) Associated Inverter(s) isverifiedtooperatenormally,b)Associated INVPushbutton"OFF" Annunciator Lightoperatesnormally,c)EICASElectricSystemPage,operatesnormally,d)Associated"INV1,orINV2FAIL" EICAS Caution(s) isverified to operate normally,ande) Alternate procedures fordetermining Inverteroperational status areestablishedandused.

(O) Confirm position of inverterpushbutton IN (On) or OUT (Off),Reference EICAS for abnormalindications.(M)This itemmayaccomplishedbyaqualifiedcrewmember.

a) With aircraft power ON,and the Electric System Pageselected;turnbothinverters

Pgina:242 Fecha:19/03/2013






24ELECTRICALPOWER2 "FAIL" Annunciator Lights onInverter (INV 1/INV 2) Pushbuttons(OverheadPanel)(Cont.)3 "OFF" Annunciator Lights onInverter(INV 1/INV2)Pushbuttons(OverheadPanel)

CC

22

00

OFF and insure affectedinverter OFF and insureaffected inverter OFFAnnunciatorlightilluminates.b)Turnaffected invertersONand verify the inverter busesarepowered.c) Select the other inverterON, and pull the C/B to theaffectedinverter.d) Verify failmessage on theelectric system pageilluminates.e)ResettheC/B.


a) Associated Inverter(s) isverifiedtooperatenormally,b)Associated INVPushbutton"FAIL" Annunciator Lightoperatesnormally,c)EICASElectricSystemPage,operatesnormally,d)Associated"INV1,orINV2FAIL" EICAS Caution(s) isverified to operate normally,ande) Alternate procedures fordetermining Inverteroperational status areestablishedandused.

(O) To determine the associated INVpushbutton is selected toOFF,Verifythe pushbutton is selectedOUT (NotFlush).(M)This itemmayaccomplishedbyaqualifiedcrewmember.

a) With aircraft power ON,andtheElectricSystemPage

Pgina:243 Fecha:19/03/2013






24ELECTRICALPOWER3 "OFF" Annunciator Lights onInverter (INV 1/INV 2) Pushbuttons(OverheadPanel)(Cont.)4 "FAIL" Annunciator Lights onAlternator (ALTLH/ALTRH)Pushbuttons(OverheadPanel)

CC

22

00

selected; turn both invertersOFF and insure affectedinverter OFF and insureaffected inverter OFFAnnunciatorlightilluminates.b)Turnaffected invertersONand verify the inverter busesarepowered.c)PulltheC/Btotheaffectedinverter. (location is #1 A22and#2M9)d) Verify INV 1 or INV 2 failmessage on the electricsystempageilluminates.e)ResettheC/B.


a) Associated Alternator(s) isverifiedtooperatenormally,b)AssociatedALTPushbutton"OFF" Annunciator Lightoperatesnormally,c)EICASElectricSystemPage,operatesnormally,d) Associated "L, or RALTFAIL" EICAS Caution(s) isverified to operate normally,ande) Alternate procedures fordetermining Alternatoroperational status areestablishedandused.

(O) Confirm position of inverterpushbutton IN (On) or OUT (Off).Reference EICAS for abnormalindications.(M)This itemmaybeperformedbyaqualified crewmember. With thedisplay inhibit selected, selectassociate ALT pushbutton ON, verifyassociated ALT FAIL amber cautionmessageilluminatesonEICAS.

Pgina:244 Fecha:19/03/2013






24ELECTRICALPOWER5 "OFF" Annunciator Lights onAlternator (ALTLH/ALT RH)Pushbuttons(OverheadPanel)6Inverters

CA

22

01


a) Associated Alternator(s) isverifiedtooperatenormally,b)AssociatedALTPushbutton"FAIL" Annunciator Lightoperatesnormally,c)EICASElectricSystemPage,operatesnormally,d) Associated "L, or R ALTFAIL" EICAS Caution(s) isverified to operate normally,ande) Alternate procedures fordetermining Alternatoroperational status areestablishedandused.

(O) To determine the associatedALTpushbutton is selected toOFF,Verifythe pushbutton is selectedOUT (NotFlush).(M)Thisitemmaybeaccomplishedbya qualified crewmember. Withenginesrunningandpropellersoutoffeather:

a)SelectbothALTpushbuttonON(Flush)b)SelectACTIEClosedc) Select associated ALTpushbuttonOFF(out)d) Observe AC TIE close bymonitoringACTIEpushbuttonflowbarannunciationlightse) Select ALT pushbuttonON(Flush)f)ObservetheACTIEopen.

Onemaybeinoperativeprovided:a) Inverter FailureIndication(s) (EICAS andOverheadPanel)foroperativeInverteroperatenormally,

Pgina:245 Fecha:19/03/2013






24ELECTRICALPOWER6Inverters(Cont.)7DCVoltmeter8 Vertical (BusTied)FlowBarLightson NonEssential Bus (NONESS 1/2)Pushbuttons(OverheadPanel)

ACC

222

110

b) Takeoff, Approach, andLanding Minimums do notrequireitsuse,andc) Operations are limited totwo flightdaysbefore repairsaremade.

One may be inoperative providedEICAS Failure Cautions for DCGenerators and Main DC Batteriesoperatenormally.(M) (O)Light(s)may fail to illuminateprovided:

a) Associated NONESSPushbutton(s) is verified tooperatenormally,b) Associated NONESSPushbutton "OFF" Light(s) isverifiedtooperatenormally,c) EICAS Electrical SystemPageoperatesnormally,andd) Alternate procedures fordetermining NonEssentialBusstatusareestablishedandused.

(O) Confirm position of NON ESS pushbutton IN (On) or OUT (Off) asrequired. Reference EICAS forabnormalindications.(M) With DC power applied to theaircraft:

a) Select the associatedNONESSpushbuttonOUT(Off)andensure the pushbutton OFFannunciator light illuminatesand that the affected bus isunpowered on the ELECTRsystempage.

Pgina:246 Fecha:19/03/2013






24ELECTRICALPOWER8 Vertical (Bus Tied)FlowBar LightsonNonEssential Bus(NONESS1/2)Pushbuttons(OverheadPanel)(Cont.)9 "OFF"AnnunciatorLightsonNonEssential Bus (NONESS 1/2)Pushbuttons(OverheadPanel)

CC

22

00

b) Select the associatedNONESS pushbutton IN (On), andensure the pushbutton OFFannunciator lightextinguishesand that the affected bus ispowered on the ELECTRsystempage.


a) Associated NONESSPushbutton(s) is verified tooperatenormally,b) Associated NONESSPushbutton Vertical Flow BarLight(s) is verified to operatenormally,c) EICAS Electrical SystemPageoperatesnormally,andd) Alternate procedures fordetermining NonEssentialBusstatusareestablishedandused.

(O) Confirm position of NON ESS pushbutton IN (on) or OUT (off) asrequired. Reference EICAS forabnormalindications.(M) With DC power applied to theaircraft:

a) Select the associatedNONESSpushbuttonOUT(off)andensure the pushbuttonsvertical bar (white)annunciator light isextinguished and that theaffectedbusinunpoweredontheELECTRsystempage.b) Select the associatedNONESS pushbutton IN (on) andensurethepushbutton

Pgina:247 Fecha:19/03/2013






24ELECTRICALPOWER9 "OFF"AnnunciatorLightsonNonEssential Bus (NONESS 1/2)Pushbuttons(OverheadPanel)(Cont.)10 Vertical (Bus UnTied) Flow BarLightonDCBus Tie (TIE)Pushbutton(OverheadPanel)

CB

21

00

vertical flow bar (white)annunciator light isilluminated and that theaffected bus is powered ontheELECTRsystempage.


a) DC Bus TIE Pushbutton isverifiedtooperatenormally,b) DC Bus TIE PushbuttonHorizontal(BusTied)FlowBarLight is verified to operatenormally,c) COLD/CROSS Pushbutton"ON" Light is verified tooperatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining statusofBusTieFunction are established andused.

(0)ConfirmpositionofOCBUSTIEPushbuttonsselectedIN,FlowBarLight(BUSTIEO)mustilluminate(M) With DC Power applied to onlyone side (LH or RH), and EXT powernoton:

a) Select the DC Bus TiePushbuttons 0UT (Open) andensure the PushbuttonsHorizontal Flow Bar (White)Annunciator Light isextinguished and that BusVoltage is only indicated ononesideoftheDCBusTieontheELECTRSystemPage.

Pgina:248 Fecha:19/03/2013






24ELECTRICALPOWER10 Vertical (Bus UnTied) Flow BarLightonDCBus Tie (TIE)Pushbutton(OverheadPanel)(Cont.)11 Horizontal (Bus Tied) Flow BarLightonDCBus Tie (TIE)Pushbutton(OverheadPanel)

BB

11

00

b)SelecttheDCBusTiePushbutton IN (CLOSED), andensure the PushbuttonHorizontalFlowBar(WHITE).

Annunciator Light is illuminated andthe BusVoltage is indicated on bothsidesoftheOCBustieontheELECTRSystemPage.(M) (O) Light may fail to illuminateprovided:

a) DC Bus TIE Pushbutton isverifiedtooperatenormally,b) DC Bus TIE PushbuttonVertical (Bus UnTied) FlowBarLightisverifiedtooperatenormally,c) COLD/CROSS Pushbutton"ON" Light is verified tooperatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining statusofBusTieFunction are established andused.

(O) Confirm position of DC BUS TIEPushbuttonIN(Tied)orOUT(UnTied)With pushbutton selected IN, FlowBarLight(BUSTIED)mustilluminate(M) With DC Power applied to onlyone side (LH or RH), and EXT powernoton:

a) Select the OC Bus TiePushbutton OUT (open) andensure the PushbuttonHorizontal Flow Bar (White)Annunciator Light isextinguished and that BusVoltageisonlyindicatedon

Pgina:249 Fecha:19/03/2013






24ELECTRICALPOWER11 Horizontal (Bus Tied) Flow BarLightonDCBus Tie (TIE)Pushbutton(OverheadPanel)(Cont.)

B

1

0

onesideoftheDCBusTieontheELECTRSystemPage.b) Select the DC Bus TiePushbutton IN (CLOSED), andensure the PushbuttonHorizontal Flow Bar (WHITE)annunciator Light isilluminated and that BusVoltage is indicated on bothsidesoftheDCBusTieontheELECTRSystemPage.

(O) Confirm position of DC BUS TIEPushbutton IN (On) or OUT (Off) asrequired. With pushbutton selectedOUT Flow Bar Light (BUS TIE) mustilluminated.(M) With DC Power applied to onlyone side (LHor LH) , andEXTpowernoton:

a) Select the DC Bus TiePushbutton OUT (open) andensure the PushbuttonVertical Flow Bar (White)Annunciator Light isilluminated and that BusVoltage is only indicated ononesideoftheDCBusTieontheELECTRSystemPageb) Select the DC Bus TiePushbutton IN(CLOSED) ,andensure the PushbuttonVertical Flow Bar (WHITE)Annunciator Light isextinguished and that BusVoltage is indicated on bothsidesoftheDCbusTieontheELECTRSystemPagec) Select COL/CROSSPushbuttons ON (IN) andensurelightilluminates.

Pgina:2410 Fecha:19/03/2013






24ELECTRICALPOWER12 EssentialBusLED (BusPowered)Lights(OverheadPanel)13"FAIL"AnnunciatorLight(s)onDCGenerator (GENLH/RH) Pushbutton(s)(OverheadPanel)

CC

22

10


a) Associated Generator(s) isverifiedtooperatenormally,b)AssociatedGENPushbutton"OFF" Annunciator Light(s)operatesnormally,c)Associated "LorRDCGENFAIL" EICAS CautionMessage(s) is verified tooperatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining operationalstatus of associated DCGenerator(s) are establishedandused.

(0) Confirm position of DG GENPushbutton IN (ON) or OUT (Off) asrequired. Reference EICAS forabnormalindications(M)This itemmaybecompletedbyaqualifiedcrewmember

a) Start the Engine with theaffectedGeneratorb) Check the affectedGenerator OFFAnnunciatorlight is OUT (OFF) andilluminatedc)TurnGeneratorONd)Display theElectricSystemPage and verify no failureMessage illuminates for theaffectedGenerator.

Pgina:2411 Fecha:19/03/2013






24ELECTRICALPOWER14"OFF"AnnunciatorLight(s)onDCGenerator (GENLH/RH) Pushbutton(s)(OverheadPanel)15 "FAIL" Annunciator Light(s) onMainBattery(BAT1/2)Pushbutton(s)(OverheadPanel)

CC

22

00


a) Associated Generator(s) isverifiedtooperatenormally,b)AssociatedGENPushbutton"FAIL" Annunciator Light(s)operatesnormally,c)Associated "LorRDCGENFAIL" EICAS CautionMessage(s) is verified tooperatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining operationalstatus of associated DCGenerator(s) are establishedandused.

(O) Confirm position of DCGEPushbutton IN (On) or OUT (Off) asrequired. Reference EICAS forabnormalindications(M)Thisitemmaybecompletedbyaqualifiedcrewmember

a) Start the Engine with theaffectedGeneratorb) Check the affectedGenerator"FAIL"Annunciatorlightisilluminatedc)TurnGeneratorONd)Display theElectricSystemPage and verify no failureMessage illuminates for theaffectedGenerator.


a) Associated Battery(s) isverifiedtooperatenormally,

Pgina:2412 Fecha:19/03/2013






24ELECTRICALPOWER15 "FAIL" Annunciator Light(s) onMainBattery(BAT1/2)Pushbutton(s)(OverheadPanel)(Cont.)

C

2

0

b)AssociatedBATPushbutton"OFF" Annunciator Light(s)operatesnormally,c) Associated "BATT 1, orBATT2 FAIL" EICAS CautionMessage(s) is verified tooperatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining operationalstatus of associated MainBattery(s)areestablishedandused.

(O) Confirm position of BAT 1/2Pushbutton IN(On) or OUT (Off) asrequired. Reference EICAS forabnormalindications(M) With external power applied totheaircraft:

a) Select associated BatterySwitch OFF and verifyassociated BAT Pushbutton1"OFF"annunciatorlightsb) Disconnect associatedBatteryc)VerifyAssociatedBAT1or2FAIL Caution illuminates onEICAS and on ELECTR SystemPaged)ReconnectBattery

Pgina:2413 Fecha:19/03/2013






24ELECTRICALPOWER16 "OFF" Annunciator Light(s) onMainBattery(BAT1/2)Pushbutton(s)(OverheadPanel)

C

2

0


a) Associated Battery(s) isverifiedtooperatenormally,b)AssociatedBATPushbutton"FAIL" Annunciator Light(s)operatesnormally,c) Associated "BATT 1, orBATT2 FAIL" EICAS CautionMessage(s)isverifiedto

operatenormally,d)EICASELECTRSystemPageoperatesnormally,ande) Alternate procedures fordetermining operationalstatus of associated MainBattery(s)areestablishedandused.

(O) To select associated Battery OFFSelect BAT Pushbutton to the OUTposition (Not Flush). To select theassociatedBatteryON,selecttheBATPushbuttontotheINposition(Flush)(M) With external power applied totheaircraft:

a) Disconnect associatedBatteryb)VerifyassociatedBAT1or2FAIL1Caution illuminatesonEICAS and on ELECTR SystemPagec)ReconnectBattery

17 "AVAIL" and "ON" AnnunciatorLights on DC External(EXT)Pushbutton(OverheadPanel)

C 2 1 (O)Either"AVAIL,"or"ON"Lightmayfailtoilluminateprovided:

a) "ON," and "NOT USED"External Power AnnunciatorLights on Exterior Paneloperatenormally,b) Alternate Procedures fordeterminingExternalPower.

Pgina:2414 Fecha:19/03/2013






24ELECTRICALPOWER17 "AVAIL" and "ON" AnnunciatorLights on DC External (EXT)Pushbutton(OverheadPanel)(Cont.)

C

2

1

availability and operationstatus are established andused,andc) Alternate FlightCrew/Ground Crewcommunication proceduresfor connecting anddisconnecting External Powerareestablishedandused.

(O) For the "AVAIL lightcommunicate with ground personnelviaestablishedhandsignalsForthe"ONLight:WithTheExternalPowerselected"ONby1)Withenginesoperating:

a) Verify the EXT PushbuttonisselectedIN(ON),andb) Verify the ON (EXT) bluesynopticmessage isdisplayedontheELECTRSystemPage

2) With the engines not operating,verify the Non Essential Busses areONasindicatedontheELECTRSystemPageortheNONESS1/2PushbuttonONannunciatorlights.

18 "NOT USED" and "ON"Annunciator Lights on DC ExternalPushbutton(ExteriorPanel)

C 2 1 (O)Either"NOTUSED,"or"ON"Lightmayfailtoilluminateprovided:

a)"ON,"and"AVAIL"ExternalPower Annunciator Lights onOverhead Panel operatenormally,b) Alternate Procedures fordetermining External Poweravailability and operationstatus are establishedandused,andc) Alternate FlightCrew/Ground Crewcommunication proceduresforconnectingand

Pgina:2415 Fecha:19/03/2013






24ELECTRICALPOWER18 "NOT USED" and "ON"Annunciator Lights on DC ExternalPushbutton(ExteriorPanel)(Cont.)

C

2

1

Disconnecting ExternalPowerareestablishedandused.

(O) For the "AVAIL" Lightcommunicate with ground personnelviaestablishedhandsignalsForthe"ON"light:

a) Brief the Ramp Supervisoron EXT power status andmeans to determine EXTPushbutton "ON" or "AVAIL"lightsontheoverheadpanelb)Priorto leavingtheaircraftunattended,ensurebootBAT1/2areselectedOFF.

19 Vertical (Bus UnTied) Flow BarLightonACBus Tie (TIE) Pushbutton(OverheadPanel)

C 1 0 (M) (O) Light may fail to illuminateprovided:

a) AC Bus Tie function isverifiedtooperatenormally,b)ACBusTIEHorizontal (BusTied) Flow Bar annunciatorLightoperatesnormally,c) AC Alternator (ALT LH/RH)Pushbutton"FAIL,"and"OFF"Annunciator Lights operatenormally,d) EICAS ELECTR Pageoperatesnormally,ande) Alternate procedures fordeterminingACBusTiestatusareestablishedandused.

(O) Pushbutton IN (On) orOUT (Off)as required. Reference EICAS forabnormalindications.(M) This item may be completed byaqualified Crewmember. With theDISPLAY INHIBIT Selected. SelectassociatedALTPushbuttonON.Verifyassociated ALT FAIL Amber CautionMessageilluminatesonEICAS.

Pgina:2416 Fecha:19/03/2013






24ELECTRICALPOWER19 Vertical (Bus UnTied) Flow BarLight on AC Bus Tie(TIE) Pushbutton(OverheadPanel)(Cont.)

C

1

0

With engines running and thepropelleroutoffeather:

a) With the AC TIE SelectedOPEN (Out) Select onealternatorOFF.b)Note that no AC power isindicated on the AC BUSassociated with inoperativealternator on ELECTR SystemPage.c) Select the AC TIEPushbuttonCLOSED(flush)d) Note that AC Power isindicated on the AC BUSassociated with theinoperative alternator on theELECTRSystemPagee) AC BUS TIE PushbuttonHorizontal Flow Bar (White)Lightisilluminated

20 Horizontal (Bus Tied) Flow BarLightonACBus Tie (TIE) Pushbutton(OverheadPanel)

C 1 0 (M) (O) Light may fail to illuminateprovided:

a) AC Bus Tie function isverifiedtooperatenormally,b)ACBusTIEVertical(BusUnTied) Flow Bar annunciatorLightoperatesnormally,c) AC Alternator (ALT LH/RH)Pushbutton"FAIL,"and"OFF"Annunciator Lights operatenormally,d) EICAS ELECTR Pageoperatesnormally,ande) Alternate procedures fordeterminingACBusTiestatusareestablishedandused.

(0) Confirm position of AC BUS TIEPushbuttonIN(On)orOUT(Off)asrequired. Reference EICAS forabnormalindications.

Pgina:2417 Fecha:19/03/2013






24ELECTRICALPOWER20 Horizontal (Bus Tied) Flow BarLightonACBus Tie (TIE) Pushbutton(OverheadPanel)(Cont.)

C

1

0

(M)This itemmaybecompletedbyaqualified Crewmember. With theDISPLAY INHIBIT Selected, selectassociatedALTPushbuttonON.Verifyassociated ALT FAIL. Amber CautionMessageilluminateonEICAS.With engines running and thepropelleroutfeather:

a) With the AC TIE SelectedOPEN (Out) Select onealternatorOFF.b)Note that no AC power isindicated on AC BUSassociated with inoperativealternator on ELECTR SystemPage.c) AC BUS TIE PushbuttonVerticalFlowbar(White)Lightisilluminated.d) Select the AC TIEPushbuttonCLOSED(flush)e) Note that AC Power isindicated on the AC BUSassociated with theinoperative alternator on theELECTRSystemPage

21 "AVAIL" and "ON" AnnunciatorLight(s) on AC External PowerPushbutton(OverheadPanel)

CC

22

00

May be inoperative providedproceduresdonotrequiretheiruse.(O) May be inoperative providedalternateprocedures fordeterminingavailability and operational status ofAC External Power are establishedandused.(O) For the "AVAIL" Lightcommunicate with ground personnelvia established hand signals For the"ON"Light:

Pgina:2418 Fecha:19/03/2013






24ELECTRICALPOWER21 "AVAIL" and "ON" AnnunciatorLight(s) on AC External PowerPushbutton(OverheadPanel)(Cont.)22APUGenerator24DCExternalPowerSystem25ACExternalPowerSystem

CCCC

2111

0000

a) VerifytheEXTPushbutton

isselectedIN(On)and

b) Verify the ON (EXT) BlueSynopticmessage isdisplayedontheELECTRSystemPage

(M) (O)Maybe inoperativeprovidedAPUGeneratorisselectedoff.(O)VerifyAPUGENswisselectedOff(M)This itemmaybecompletedbyaqualifiedCrewmember

a) Pull and secure APU GENcircuitbreakerb) Placard APU GEN sw"INOPERATIVE"

INTENCIONALMENTEENBLANCO

Pgina:251 Fecha:19/03/2013






25EQUIPMENT/FURNISHINGS1FlightAttendantSeatAssembly

A

1

0

(M)(O)FlightAttendantseatmaybeinoperativeprovided:

a) Affected Seat or seatassemblyisnotoccupied,b)FlightAttendantdisplacedby inoperative seat positionoccupies thepassenger Seatmost accessible to theinoperativeseat,c) Alternate procedures areestablished and used aspublished in thecrewmembersmanuals,d) Folding type Seat isstowed or secured in theretractedposition,e) Passenger Seat assignedto the Flight Attendant isplacarded "FOR FLIGHTATTENDANTUSEONLY",andf) Repairs are made withintwo(2)flightdays.

(O) Cabin attendant assigned toaffected jump seat will occupy apassengerseatascloseto,orcloserthan the nearest seated passengerto the associated exit. On VIPDornier aircraft this seatwill be ID.From this seat the cabin attendantcan reach the assigned emergencyexit in essentially the same time asfrom the jump seat. Passenger seatoccupied by the Cabin attendant isto be placarded (blocked) for suchpurpose.(M)Thisitemmaybecompletedbyaqualified Crewmember. Ensure theSeat is retracted and placard theSeatwithaSeatblockingcard.

Pgina:252 Fecha:19/03/2013






25EQUIPMENT/FURNISHINGS2EmergencyLocatorTransmitter(ELT)

C

1

1

The Emergency Locator Transmittermust be operative in accordancewithR.A.C.4.2.2.4.NOTE: If the ELT failure occurs in aremote base where the repairscannot be accomplished, the crewcould perform a Ferry flight to amaintenance facility where therepairs could be made. (RAC4.2.2.4.d.4.).

3"FastenSeatBeltWhileSeated"Signs

C 22 1 One or more Signs or Placardsmaybeillegibleormissingprovidedalegible Sign or Placard is readablefromeachoccupiedPassengerSeat.

4PassengerSeat(s)

1ReclineMechanism

DD

3230

00

Maybeinoperativeprovided:a) Seat does not block anEmergencyExit,b)Seatdoesnotrestrictanypassengerfromaccesstothemainaisle,andc) The affected seat(s) areblocked and placarded "DONOTOCCUPY".

NOTE 1:A seatwith an inoperativeseatbeltisconsideredinoperative.NOTE 2: Inoperative seats do notaffecttherequirednumberofFlightAttendants.NOTE3:Affectedseat(s)mayincludethe seat(s) behind and/or adjacentoutboardseats.May be inoperative and seatoccupiedprovidedseat issecured intheuprightposition.

Pgina:253 Fecha:19/03/2013






25EQUIPMENT/FURNISHINGS4PassengerSeat(s)(Cont.)

2Underseat Baggage RestrainingBars

5PassengerConvenienceItems

1Traytables2Toilet3Overheadbin4Armrestseat

DDDDD

20321710

00000


a) Baggage is not stowedunderseat with inoperativebar,b) Associated seat isplacarded "DO NOT STOWBAGGAGE UNDER THISSEAT",andc) Procedures areestablished to alert CabinCrew of inoperativerestrainingbar.

(0) Upon report of inoperativeRestrainingbaronAircraftLog.CrewwilladviseFlt.Attendant.Placard affected seat "DO NOTSTOWBAGGAGEUNDERTHISSEAT"(O) Secure the tray in the closedpositionandplacardINOPERATIVE0) Placard the toilet INOPERATIVEand block the seat in the downpositionwithtape(O)Ifthedoorwillclose,placardthedoorlatchINOPERATIVE(M)Ifthedoorwillnotclose,removethe door from the overhead bin,place a piece of tape across theopeningandplacardNOSTORAGEINTHISBIN(O)Securetheinoperativearmrestintheuprightpositiontotheseatback.(M)Ifthearmrestcannotbesecuredin the upright position, remove thearmrestformtheseat.

Pgina:254 Fecha:19/03/2013






25EQUIPMENT/FURNISHINGS6ObserverSeat

1PrimaryObserverSeat(IncludingAssociatedEquipment)

A

1

0


a)Theprimaryobserverseatisavailablewiththerequiredminimum safety equipment(safetybeltandoxygen)andacceptable to the UAEACinspector for theperformance of officialduties,andb) Repairs are made withintwoflightdays.

NOTE 1: These provisions areintendedtoprovideforoccupancyofthe above seats by an UAEACInspector when minimum safetyequipment (OxygenandSafetyBelt)is functional and the inspectordetermines the conditions to beacceptable.NOTE2: ThePilotInCommandwilldetermine if the minimum SafetyEquipment is functional for otherpersons authorized to occupyObserverSeat.

7 Flight Attendant Flashlight/HolderAssembly(s)

C 1 0 May be inoperative or missingprovided Cabin Crewmember(s)assignedtoassociatedSeat(s)hasanequivalent, operating Flashlightreadilyavailable.

8FirstAidKits D 1 1 Any in excess of those required byRAC may be opened or missing,provided required distribution ofoperativeKit(s)ismaintained.

9OverWaterEquipment1LifeVest2Liferaft

CC

361

361

Required on over water operationonly(N/AduetoADAoperation)Required on over water operationonly(N/AduetoADAoperation.

Pgina:255 Fecha:19/03/2013






25EQUIPMENT/FURNISHINGS10CargorestraintSystem

DD

22

00

May be inoperative or missingprovided acceptable cargo loadinglimits from an approved source ie;Cargo Loading manual, CargoHandling manual, or Weight andBalancedocumentareobserved.May be inoperative or missingprovided cargo compartmentremainsempty.

11EmergencyMedicalKit

D 0 0 Any in excess of those required byRAC may be opened or missingprovided required distribution ofremainingKit(s)ismaintained.

12CockpitSunvisor C 2 0 Maybeinoperativeprovided:a) No visual restrictions totheflightcrew,b)Acceptable to flightcrew,andc) Affected sunvisor isremovedorstowed.

13 Galley Waste Receptacles AccessDoors/Covers

C 1 0 (M)Maybeinoperativeprovidedthecontainer isemptyandtheaccess issecured to prevent wasteintroductionintothecompartment.(M) Remove waste from container,secureaccessdoorandplacard"DONOTTHROWWASTEINSIDE"

14LavatoryDoorAshtrays

1Airplaneswithonlyonelavatorydoorashtrayinstalled

A

1

0

May be missing provided it isreplacedwithin3calendardays.

Pgina:261 Fecha:19/03/2013






26FIREPROTECTION1PortableFireExtinguisher

D

3

2

Any in excess of those required byRAC may be inoperative or missingprovided:

a) The inoperative FireExtinguisher is tagged"INOPERATIVE," removedfrom the installed position,and placed out of sight so itcan not be mistaken for atfunctionalunit,andb) Required distribution ismaintained

2 Fire Extinguisher ThermalDischargeDiscs

C 5 0 (M)(O)Maybeinoperativeormissingprovided:

a) Adequate charge ofassociated Extinguisher isverifiedeachflightday,andb) Associated Engine FireProtection Discharge BottleLights are tested each flightday.

(O)Priortoeachtakeoff:

1) Select the FIREPROTECTION TEST switch tothe FAIL AGN position andcheck the AGN lights areilluminatedand2)EnsuretheDIS lights inthefire bottle (BTL) buttons arechecked to the notIlluminated

(M)Remove affected FireBottle andperformweightcheck IADornierMMchapter 26. Document task inMaintenanceLogonboardAircraft

Pgina:262 Fecha:19/03/2013






26FIREPROTECTION3LavatorySmokeDetectionSystem

CC

11

00

May be inoperative provided thelavatory fire extinguisher systemoperatesnormally.(M)(O)Maybeinoperativeprovided:

a) Lavatory waste receptacleremainsempty,b) Lavatory door is lockedclosed and placarded"INOPERATIVE DO NOTENTER",andc)Lavatoryisnotusedforanypurpose.

NOTE 1: These provisos are notintended to prohibit lavatoryinspectionsbycrewmembers.Note 2: Lavatory smoke detectionsystem is not required for allcargooperations.(M) (O) This itemmaybeperformedby qualified flight Crewmember.Ensure Lavatory Smoke DetectionSystemoperatesnormallyor removeallwaste from Receptacle and close,lockandplacarddoor"INOPERATIVEDONOTENTER""FUERADESERVICIONOENTRE"

4LavatoryFireExtinguishingSystems

CC

11

00

Maybe inoperative foreach lavatoryprovided associated lavatory smokedetectionsystemoperatesnormally.(M) (O)May be inoperative for eachlavatoryprovidedassociated:

a) LavatoryWasteReceptacleremainsempty,b) Lavatory Door is lockedclosed and placarded"INOPERATIVE DONOTENTER",andc)Lavatoryisnotusedforanypurpose.

Pgina:263 Fecha:19/03/2013


Documents

Minimum Equipment List MEL Dornier 328-100.pdf