LIST
EQUIPMENT
767MINIMUM
MA-004
R E V I S I ON
No . : 1 7
ISSUEDATE:MAY.30./2007.
EFFECTIVEDATE:The Sthday after NTA CAA approval
Preparedby:
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MALEVcAMo Supervisor
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Accepted by:
Date. ,l t:; t i Af t .i.'A 1
Accepted by:
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pagefor Revision
No.17.
MAY.30/2007
BOEING767
LIST
EQUIPMENT
MINIMUM
Directorate
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Continuing Ainrvorth
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FLEET
MALEV B767.200/300
LIST of EFFECTM AIRCRAFT for
MINIMUM EQUIPMENT LIST
Reqist.
Model ll stl
L/N
v/N
HA-LHA
8767-27GF,R
27048
475
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HA.LHB
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CF680c2B6F
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LEAC PAGE1
REV17 MAR10/2007
787
A?E'/YG
ABBREVIATIONS:
R - Revised
A - Added
Section
TitleRev.Pages
Section
EICASMessages
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Page R/A
1
MAY30/07
Listof EffectiveA,/c
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Listof EffectivePages
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LEP PAGE1/3
REV 17 MAY30/2007
787'
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Section
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21-11 R
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LEP PAGE2/3
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Scction
Date
Page R/A
MAR10/07
31-6
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POWER
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LEP PAGE3/3
ReV tZ lrlnY sOtZOOzI
ttMlEV
Hungarian Airlines,fi
BOEIIUE
7Ez
LIST
MINIMUM
EQUIPMENT
RECORDOF REVISIONS
Rev.
No.
L
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Rev.
No.
Mav14193
Jul 15/93
Oct 30/93
Sep 15/94
Nov15/95
Jun 15/96
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1 7 . Mar10/07
5.
ROR
PAGE1/1
REV17 MAR10/2007
tlU,EV
Hungarian Airlines
fi
EAETTUE
787
LIST
EQUIPMENT
MINIMUM
RECORDOF TEMPORARY
REVISIONS
, R e v . N o . . 1.,lsgue Date Diie lndertcd
1s-1.
Mav.05./04. Mav.10./04.
Aua.31./04.
15-2.
Auo.31./04
16-1.
Jan.06./05 Jan.06./05
ROTR
PAGE1/1
REV17 MAR10/2007
7CF.SarEtjYGt
LIST
EQUIPMENT
MINIMUM
ATA CHAPTERSLIST
SYSTEMNO.
21
22
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Air Conditioning
AutoFlight
Communications
ElectricalPower
EquipmenVFurnishings
FireProtection
FlightControls
Fuel
Hydraulic
Power
lce andRainProtection
Indicating/Recording
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LandingGear
Lights
Navigation
Oxygen
Pneumatic
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25-1THRU25-8
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27-1THRU27-5
28-1THRU28-12
29-1THRU29-8
3G.1THRU30-6
31-1THRU31-6
32-1 THRU32-12
33-1THRU33-7
34-1THRU34-26
35-1THRU35-4
36-1THRU36-14
38-1THRU38-1
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ATACHAPTERS
REV17
PAGE 1
MAR10/2007
EAEfiryE
787
LIST
EQUIPMENT
MINIMUM
HIGHLIGHTS
FORREVISION17.
(lncorporated
8767-300MEL ltems)MinimumEquipment
RevisionNo. 17 to MALEV8767-200/-300
Relevant
of
the
FAAMMELRev.31.,and the applicable
Listis a reissueof the document.
changes
partsof BoeingDDG Rev.26., and JAR-OPSI TGL LEAFLET26, issuedafterthe effectivedate of
16-1.
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No.16,andMELTemporary
theMALEV8767MELRevision
a change.
A verticalbar (changebar)in the marginindicates
PREABMLE:
ITEM
DESCRIPTION
Approvalpage
Revision
No.:17.
Listof Effective
Newaddedpages
Paqes
No.:17. Mar.10.2007.
Recordof Revisions NewaddedRevision
Recordof Temporary New
addedTR-2of Rev.16.
Revisions
and GENERAL
New added pages - added JAR-OPS1 requirements
on boardthe
of the MEL.;Installation
PRINCIPLES
for the DEVELOPMENT
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andReporting
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Annex1
EICASMessages New
added.A cross referencelist of EngineIndicationand Crew Alerting
lntraduction
Mal6vMinimumEquipment
System(EICAS)messagesand cirresponding
Annex1
provided
in thissection.
List(MEL)itemsis
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Revisedtext in NOTE and new added EICAS STATUSMESSAGESand
21-25-1
PLACARD
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21-31-1
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21-31-2
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21-45-1
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21-51-1
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21-51-2
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(O)data
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(O)data;AddedEICASSTATUSMESSAGE
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Deletedin linewithFAAMMELRev30.
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Revisedreferto JAA policy(TGL26);
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Revisedin linewithFAAMMELRev31;ChangeNOTEdata.
"B " and
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HOR Page2/7
REV 17MAY 30/2007
25-11-1
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25-28-1
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and PLACARD
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Added(M)for REMARKS,
andPLACARD
27-41-2
27-48-1
27-51-1
27-62-1
27-81-1
28-21-2
28-22-1
HOR Page3/7
REV t7 MAY 30/2007
26-za-3
Revisedtext in REMARKS(addedg) point)and addedsub itemsand added
(O)
PLACARD
andOPERATIONS
Revisedtext in REMARKSfromER to ETOPS
(added(M))
Revised
textin REMARKS
NewaddedPLACARD
and PLACARD
NewaddedEICASSTATUSMESSAGES
zo-c t-c
New added PLACARD
2840-1
Revisedtextin REMARKSfromER to ETOPS
Revisedtext in REMARKS(addedh) point)and addedsub item (AD, SB
referring),
and changedNoTE 1, and addedNOTE3,4, and addedEICAS
STATUSMESSAGESand PLACARD,and correctedfuel imbalancedata of
(O)4./Cpoint
theOPERATIONS
Newaddedsub-item(1), and addedd), e) pointto sub item 2, and added
andPLACARD
NOTE.EICASSTATUSMESSAGES
NewaddedPLACARD
Revisedtext in REMARKS((addedd) and e) point)),and addedNOTEand
PLACARD
28-22-2
28-22-3
28-25-1
28-25-?
28-41-'1
2841-2
2841-6
2841-7
2843-1
New addedPLACARD
2 9 - 11 - 3
(o)
AddedNOTEand PLACARD,
andaddeditem4., 4/A./8.OPERATIONS
(O)
NewaddedNOTESandOPERATIONS
Revisedtext in item,and sub item 1, 2, 3, and new addedNOTESand
OPERATIONS
NOTE
tv-J
IJ-JZ-
t-t
|
30-11-1
30-11-2
3Q-21-1
30-21-2
30-31-5
30-32-1
Revised
andaddedPLACARD
textin REMARKS,
(O)
NewaddedPLACARD,and revisedtext in OPERATIONS
Revisedtext in REMARKS,and addedNOTES,EICASSTATUSMESSAGES
and PLACARD.
andaddedD, E, F. G subpointsfor2.
(O)
Newaddedsubitemc), andchangedtextOPERATIONS
NewaddedPLACARD
NewaddedPLACARD
30-33-1
New added PLACARD
30-41-1
3042-1
30-43-1
Changed
in subitemnumber
Revisedtext in REMARKS(changedfrom5 nauticalmilesto 5 statutemilet
Newaddeditem
Revisedreferto JAA policy(TGL26); Deleted1) and 2) in linewith NOTE2;
data.
datalAddedPLACCARD
AddedEICASSTATUSMESSAGES
Newentryin linewith FAAl\tlMEL
Newentry in linewith FAA MMEL
data;
Revisedin linewithFAAMMEL|AddedEICASSTATUSMESSAGES
AddedPLACCARD
data
31-31-1
31-35-1
31.35-3
3141-1
31-5'1-1
31-61-1
31.61-4
32-30-1
32-31-1
Jl-Jl-
|
3241-1
Added PLACCARDdata
Deleted
accto MMELRev31,
data;
Revisedin linewithFAAMMELAddedEICASSTATUSMESSAGES
AddedPLACCARD
data
(O),
NewaddedPLACARD,
and revisedtext in 3.pointof the OPERATIONS
(O)
andadded4.oointto OPERATIONS
(O)
NewaddedPLACARD,
andrevisedtextin 3.pointof the OPERATIONS
(270 KIAS)
Revised
textin REMARKS
(O),and changedfrom2.C , D to
Revisedtextin 2.8./3of the OPERATIONS
2.C.and added-300/-80C2itemfor table
HOR Page4/7
REV 17MAR 10/2007
32-41-2
3241-3
3242-1
32-42-2
3?42-3
32424
3244-5
3245-3
3246-1
32-51-1
32-61-1
32-61-2
32-71-1
52- | t-t
33-11,1
33-14-1
33-16-1
33-21-1
33-31-1
JJ-J
I -Z
oo-J t-o
33-3'1-4
33-37-1
33-41-1
3342-1
3342-2
33-42-3
33-43-1
33-44-1
33-45-'1
33-51-1
33-51-2
33-51-3
34-00-1
34-10-1
34-10-2
34-13-1
u-13-2
34-13-6
34-16-1
34-21-1
(O)
(Ca),-b)),andaddedOPERATIONS
Revised
textin REMARKS
pointofthe
(O)
NewaddedPLACARD,
OPERATIONS
andchanged1
Revisedtext in NOTE 1., and added EICASSTATUSMESSAGESand
1.,andrevisedtext2./bpoint
PLACARD,
andaddedd) pointto OPERATIONS
of theOPERATIONS
NewaddedNOTEand EICASSTATUSMESSAGES
(O)
Revised
textin 1./bpointof theOPERATIONS
NewaddedPLACARD
New added PLACARD
Newaddeditem(TPIS)
Newaddeditem(BTMS)
Changedrepair intervalfrom C to B, and added PLACARD,and added
(O)
CAUTION
to OPERATIONS
Revisedtext in REMARKS
NewaddedEICASSTATUSMESSAGES
Newaddeditemfiail Skid)
Newaddeditem(TailSkidIndicationSystem)
Revisedreferto FM MMELRev31; Newentry,referto FAAMMELRev31;
AddedremarkPLACCARD:
Newitem,referto FAAMMELRev3l
Newitemaddedreferto FAAMMELRev31
Revisedreferto FM MMELRev31;
Revised,referto JAA policv(TGL26)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Revisedreferto FAAMMELRev31:
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark{PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Addedremark(PLACARD)
Revised
referto FAAMMELRev31;and
Revised,referto JAA policy(TGL26)
AddedremarkOPERATION
NOTE
(O)procedure
step1.A,8;revisedtext;
Addedinformation
in OPERATIONS
Newentry,referto JAA policy(TGL26)
Newentry,referto JAA policy(TGL26)
(O)procedure.
in OPERATIONS
Revised
text;Addedmissinginformation
Addedrelief,Dartiallv
in linewithFAAMMEL
RevisedRemarksin linewithJAA policy(TGL)Addedremark(PLACARD)
Addedremark(PLACARD)
Revisedreferto JM policy(TGL26)
Edited
in NOTE'1i
theMELreference
Addedan'(M)"requirement;
Updated
data
ERto ETOPS:AddedOPERATIONS(O)
HOR Page5/7
REV 17MAY 30/2007
34-22-5
34-22-6
34-22-7
34-24-1
34-24-2
34-25-1
u-31-1
u-32-1
34-33-1
3443-1
3446-1
3446-2
34-51-1
34-53-1
34-55-1
34-60-1
34-61-2
AddedEICASSTATUSMESSAGE
data;
Editedtitleof themainitemandsubitems1 and2. AddednewMELrelieffor
howto obtain
subitems
datadescribing
3 and4. AddedOPERATIONS
navioational
information.
AddedNOTEfor claritv.
Revisedreferto JAA policy(TGL26)
ModifiedMELin accordance
with FAAMMEL;EditedER to ETOPS;Added
OPERATIONS(O)
data
Addedin linewithFAAMMEL
Revisedrepairintervalreferto JAA policy(TGL26);AddedOPERATIONS
NOTEdata:
Revised
repairrnterval
in linewithJAApolicy(TGL26)iAddedOPERATIONS
NOTEdata:
(O)in linewithFAAMMELentry;Added
Revised
OPERATIONS
MAINTENANCE
NOTE:
Revisedin linewith FAAMMELentry;Revisedrepairinterval,referto JAA
policy(TGL);AddedOPERATIONS(O)
data;AddedEICASSTATUS
MESSAGEdata;AddedPLACCARD|
AddedNOTEwith ETOPS
requirements.
Revised,referto JAA policy(TGL26);AddedEICASSTATUSMESSAGES
datal
deleted
data;
Revisedreferto JM policy(TGL26);AddedPLACCARD
data
Revisedreferto JAA policy(TGL26);AddedPLACCARD
data
Revisedreferto JAA policy(TGL26);AddedPLACCARD
Revisedreferto JAA policy(TGL26);AddedPLACCARD
data
Revisedreferto JAA policy(TGL26);AddedPLACCARD
data;Added
MAINTENANCE
steo
35-11-2
35-20-1
35-21-1
35-31-1
Revised
in linewithFAAMMELRev31;
Revisedreferto JAA policy(TGL26);
Revisedin linewithFM MMELRev31
Revisedreferto JAA oolicv
36-11-1
36-11-2
Revisedtextin REMARKS,
and addedNOTE1, 2, and PLACARD
andchangedOPERATIONS(O)
NewaddedNOTE1,2, andPLACARD,
andchangedOPERATIoNS(o)
NewaddedNOTEandPLACARD,
NewaddedPLACARD
3 6 - 11 - 3
36-114
36-11-6
36-11-7
36-11-8
36-12-1
JO- | Z-Z
50-zz- |
36-22-3
36-22-5
36-22-6
38-10-1
New addedPLACARD
NewaddedNOTE
(i. k. points),and addedNOTE1, 2, and changed
Revisedtextin REMARKS
(O)
OPERATIONS
Revisedtext in REMARKS(i. points),and addedNOTE1,2, and changed
(O)
OPERATIONS
limited
New added PLACARD'and added table of the reduceperf'ormance
weiqhts
(O),
NewaddedNOTE,and addedsub pointsA, B to l.pointOPERATIONS
and chanoedtrcm75VoN2 to 80o/o
N2
New addedNOTE,and addedsub points1),2) to 1 A.pointOPERATIONS
(O).and chanoedtrom75o/o
N2 to 80oloN2 in 4.C Doint
Newitemaddedreferto FAAMMELRev31
Newitemaddedreferto FAAMMELRev31
NewaddedPLACARD
HOR Page6i7
REV 17MAY 30/2007
38-30-1
49-11-1
49-15-1
49-70-2
49-54-1
52-11-1
52-114
52-50-1
52-51-3
52-71-1
73-21-1
73-21-7
for
Newaddedsubitem(767-300),
andchangedfrom4 to 5 NumberRequired
Disoatchfor 767-200
New added sub-item, Remarks,Notes and Placard parts Changed and
ReDlacement
Newaddedsub-item,Remarks,Notes,EICASSTATUSMESSAGES,Placard
andOPERATIONS
oartsChanoedandReolacement
part
Revised
textin OPERATIONS
Replacement
EICASSTATUSMESSAGES
Revisedtext in REMARKS
Newaddedsubitem(2)for767-300
Newaddeditem(FlishtCrewRestDoor)
Changedsub item from 1-5 to 1-11 accordingto JAR-OPS1.730TGL
Leaflet26
NewaddedEICASSTATUSMESSAGES
and PLACARD
Revisedtexi in REMARKSand Reolacement
EICASSTATUSMESSAGES
and PLACARD
Replacement
and PLACARD
NOTE.EICASSTATUSMESSAGES
73-21-8
Added (O) for REt\ilARKS(Minimumground idle) and added EICAS STATUS
MESSAGESand PLACARD
73-31-'l
Revised
textin REMARKS
b),c) andNOTE4, 5, 6
74-00-1
and PLACARD
ReDlacement
EICASSTATUSMESSAGES
7s-21-1
75-23-1
75-24-1
75-24-2
77-1?-2
Added (O) for REMARKSand added EICAS STATUS MESSAGES and
PLACARDand OPERATIONS(O)
Added(O)for REI\,IARKS
and PLACARDand OPERATIONS(O)
Revisedtext in NOTEand table
NewaddedNOTE(+table)
andEICASSTATUSMESSAGESANdPLACARD
(O) Exceptfiom REMARKS
Revised
textin REMARKS
78-31-1
78-34-2
78-34-3
/o-Jo- |
I6-50-t
78-36-3
79-31-1
New added NoTE and EICAS STATUS MESSAGES and OPERATIONS (O)
and PLACARD
New added EICAS STATUS MESSAGES and PLACARD and revised
OPERATIONS(O)
NewaddedPLACARDand OPERATIONS(O)
NewaddedPLACARDand OPERATIONS(O) and Added(o) for REMARKS
Newadded PLACARD
New added EICAS STATUS MESSAGES and OPERATIONS (O) and
PLACARD
NewaddedPLACARD
79-33-1
79-34-2
79-35-'1
New added NOTE
80-00-2
80-11-2
(O)
NewaddedPLACARD
textin OPERATIONS
and Revised
(O)
NewaddedPLACARDand Revisedtext in OPERATIONS
Newaddeditem
NewaddedNOTE,EICAS STATUS MESSAGESand PLACARD
HOR Page7/7
17
REV MAY 3Ol2007
EAEhUE
787
PREAMBLE
A. INTRODUCTION
1. JAR-OPS1.030requirethatMALEVshallestablish,for eachaircraft,a MinimumEquipment
than,the
List(MEL)approvedby NTACAA.Thisshallbe basedupon,but not lessrestrictive
by NTACAA.
relevant
MasterMinimumEquipment
List(MMEL),if thisexists,accepted
prescribe
2. JAR-OPS1.630(aX2)
thata flightshallnotcommence
andJAR-OPS1.845(aX3)
K andL arein operable
unlesstheinstruments
required
undersubparts
andequipment
exceptas providedin the MEL.
conditionfor the kindof operationsbeingconducted,
3. JAAAdministrative
& GuidanceMaterialSectionFour:PartThree:TemporaryGuidanceLeaflet
for
No 26 is usedto giveMal6vthe guidancenecessaryto developthe MELprovisions
1
and
JARin
order
that
JAR-OPS
equipment,
andconditions
for itsunserviceability,
MMEL/MEL
are properlycompliedwith.However,TGL26 is guidancematerialonly,and
agreedwiththe operator's
shouldnot be usedto oveMritethe MMELunlessspecifically
Authority- referto Appendixfor e flowdiagramfor the useof TGL26 in a MEL.
1. EFFECTIVITY
MALEVCAMOdevelopedthe MALEV8767 MELfor Boeing767 aircaftot theMALEVHungarian
and
Airlines.This MELtakesintoconsideration
MALEVparticularaircraftequipmentconfiguration
operationalconditions,routes being flown and establishedrequirementfor current regulation,
of thosecountries
by LocalAuthorities
including
JAROPS1 andanyotherrequirement
demanded
overwhichthe aircraftwillfly.
2, GENERAL
LIST(MEL)for the MALEV'S
By approvalof this MALEVBoEING767 MINIMUMEQUIPMENT
8767 airplanes,NTACM permitsdispatchof the airplanefor revenueand trainingflightswith
certainitems or componentsinoperativeprovidedan acceptablelevelof safetyis maintainedby
appropriate
operation,by a transferof the functionto anothercomponent,or by referenceto other
providingthe requiredinformation.
instruments
or components
NOTES
1. The dispatchprovisionsof this MELare applicableuntilthe airplanecommencesthe flight.
The commencement
of flight is definedas beingthe pointat whichthe aircraffbeqinsto
moveunderits own oower.
The flightcrewtakinginto accountthis MEL shallcarefullyassessfailuresafterthat point
and all otherrelevantfiactorsrelatedto the intendedflight.
2.
For dispatch with secondary airframe or engine parts missing, refer to the
CONFIGURATION
DEVIATION
LIST (CDL)which is a sectionof the AirplaneFlight
Manual.
Suitableconditionsand limitationsin the form of placards,maintenanceprocedures,crew
operatingproceduresand otherrestrictionsas necessaryare specifiedin the MEL to ensurethat
an acceptablelevelof safetyis maintained.
of theMEL.
3. GENERAL
PRINCIPLES
forthe DEVELOPMENT
3.1 MELBasicformat
The MELshouldincludethe following:a Listof EffectivePages,a Tableof Contents,the
Preamble,Notesand Definitions,
a sectionfor eachaircraftsystem,andamendment
recordpage.The Preambleand Definitions
shallbe basedupon,but no lessrestrictive
PREAMBLE
PAGE1
REV17 MAR10/2007
aOEfiUE
787
PREAMBLE
Mal6vmustspecifytherevision
than,therelevant
MMELas perJARMMEUMEL.060(a).
suchas a
andanyotherdocuments
statusof theMMELandJAAMMELSupplement,
Deviations
this
MEL.
Dispatch
used
in
the
development
of
Guide,
3.2 MELPageformat
MELformatis at the discretionof the operator,providedthatit is clearand unambiguous.
Mal€vMELpageformatfollowthe JM MMELpageformatof fivecolumns(seeAppendix
MELitems,however,
1 to ACJJAR-MMEL/ME1.025).
Thepagenumbering,
andindividual
shouldbe in accordance
withtheATA2200codesystem.
3.3 Listof EffectivePages
lt mustlist
A Listof EffectivePages(LEP)is usedto ensurethateachMELis up-to-date,
for eachpageof the MEL.The dateand revisionstatusof
the dateof the lastamendment
to that shownon the Listof EffectivePages.
eachpageof the MELmustcorrespond
3.4 Tableof Contents
TheTableof Contentspageshouldlistthe sectionfor eachaircraftsystemusingthe ATA
2200listingas foundin the MMEL.Pagesshouldbe numberedwiththe ATAsystem
numberfollowedbythe itemnumberfor thatsystem(e.9.,the pagefollowing27-2-1would
be27-2-2).
3.5 MELPreamble
The purposeofthe MELPreambleis to providedirectionto companypersonnelon the
philosophy
and useof the MEL.An exampleMELpreamblewhichis acceptablefor useby
An operatormay
an operatoris publishedin Appendix1 to ACJ JAR-MMEL/MEL.065.
chooseto developtheirown preamblebut it shouldcontainat leastthe information
contained
in JAR-MMEL/MEL.
3.6 NotesandDefinitions
Notesand Definitions
are requiredto allowthe userto interpretthe MELpropedy.
andMaintenance
Procedures
3.7Ooerational
a) Dispatchwith inoperative
itemsis oftenacceptableonlywiththe creationof special
operational
or maintenance
Drocedures.
b) Wherethe MELindicatesthatthis is the case,Mal6vmustestablishappropriate
procedures.
bythe TypeCertificateHolderin mostcases
Proceduresrecommended
for providingacceptable
can be adoptedfor this purpose,but the ultimateresponsibility
willensurethatan
orocedures
withthe MELrestswiththe operator.Theseprocedures
The TypeCertiflcateHolderis requiredto
acceptablelevelof safeg will be maintained.
procedures
produceoperational
suchas DispatchDeviationGuides,
and maintenance
Theseproceduresmaybe inserted
for useby operators(seeJAR-MMEL/ME1.035(a)).
intothe appropriate
MELpages,and submittedby the operator,to formpartof the
MEL.DispatchDeviationGuidesis notapprovedby theAuthority,norcantheyreplace
or maintenance
the MEL.lf the TypeCertificateHolderhas not publishedoperational
procedures,
procedures
and,if requested,
the Malevshoulddevelopappropriate
submitthemto theirAuthority.
c) Mal€v,whencomparing
theMELagainsttheMMEL,shouldensurethatwherethe (O)
procedurehasbeendeveloped
or maintenance
or (M)symbolsappear,an operational
personnelof the
that providescleardirectionto the crewmembersand maintenance
actionto be taken.This procedureshouldbe includedin the MELor associated
Operator's
Manual(seeACJJAR-MMEUMEL.075).
in anotherdocumentthat is
d) The onlyexceptionis whenthe procedureis contiained
(for"(O)"
1.1045)
Manual(JAR-OPS
available,
e,g.otherpartof theOperations
"(M)'
procedures)
procedures).
In the lattercases,the
Manual(for
or the Maintenance
MELmayreferto a sectionof the appropriate
documentie.g.
- to thecabincrewmembers,
Manualor CabincrewManual;
suchas a Operations
- to the maintenance
ManualDeactivation
an
Aircrafr
as
Maintenance
crew,such
ControlManual,
etc.
Proeedures
Manual),
Maintenance
PAGE2
PREAMBLE
REV17 MAR10/2007
EAEIIUE
7Az
PREAMBLE
as these
e) lt is notacceptableto onlyreferencethe JARSor similardocuments,
documentsmaynot be carriedon boardthe aircraftand couldbe subjectto
misinterpretation.
The objectiveis to providepersonnelwithclear,concisedirectionon
howtheyare to proceed.Wherethe MMELcolumn5 states''asrequiredby Operating
of the
Requirements",
thiswordingshallnotappearin theMEL;rather,a synopsis
Regulation
shallappear.
ManuelProcedures
3,8Ooeration
MALEVmustestablishprocedures
in the OperationsManualfor the useand guidance
mustalignwiththosein the
of crewmemberswhenusingthe MEL.The procedures
Maintenance
to JAR-OPS.1045,
the MELis pertof the
ControlManual.
According
Operations
Manual,
3.9 MALEVMELDevelopment
Policy:
The MELfor MALEVaircraftoperatedin accordance
withJAR-OPS1 shouldbe
developedusingthe followingprinciples:
or
in accordance
withJAR-MMEL/MEL
a) Theprovisions
of theMMEL,as approved
with precedingnationalreguiation,
shouldbe used.
the operatofsparticular
b) The contentof the MELshouldtake intoconsideration
and operational
conditions,routesbeingflown
aeroplaneequipment,configuration
Authority.
and requirements
set by the appropriate
AiMorthinessDirectiveor any
c) Thatthe MELdoesnot deviatefromanyapplicable
thanthe MMEL.
otherMandatoryRequirement
and is not lessrestrictive
for MELPolicymaybe
Document
d) lf no MMELexists,thecontentof theGuidance
of the
usedas a guideline
theMEL,subjectto agreement
forestablishing
HungerianNTACM.
e) Theflowdiagramin Appendix
below,explains
howto useTGL26 whenpreparing
the MEL.
PAGE3
PREAMBLE
REV17 MAR10/2007
B?E
TUG 787
PREAMBLE
APPENDIX
FLOWDIAGRAMFORTHE USEOF TGL 26 IN A MEL
hlhisTGL26
€N€vi€lionp.@ided in lhis
TG! 26
IGL 26or MMEL
Note 1: All itemsrelatedto lhe airworthiness
of the aeroplaneandnot includedin the list,are
automatically
requiredto be operative.
is providedin the
Note2: All itemsrequiredby JAR-OPS1 mustbe operativeunlessalleviation
M[ilELor thisTGL26.
Note3: Equipment
obviouslynot requiredfor safeoperationofthe aeroplanemaynot be listed.
for failuresthatare not listedto
An effectivedecisionmakingprocessshouldbe established
determineifthey are relatedto aiMorthinessand requiredfor safeoperation.
Note4: Fornon-JAAMMELS,
TGL26 shouldbe usedto oveMritethe IVMELentrywhereit is basedon
non-JM policy(FAA)andnot designconsiderations,
Note5: In non-JM MMELS,similarstalemenlssuchas 'As requiredby FARS"or ?s requiredby Regulations"
"Asrequiredby OperatingRegulations'
etc.shouldbe interpreted
as meaningthe sameas
PREAMBLE
PAGE4
REV17 MAR10/2007
EZE
TYG 787
PREAMBLE
b
OF MEL
CONTENTS
that may be inoperativepriorto
The MEL containsonly those itemsof aiMorthinesssignificance
provided
procedures
limitations
are
dispatch,
observed.
and appropriate
such as wings,rudders,flaps,engines,
Equipmentobviouslybasicto airplaneairworthiness
landinggear,etc.is not listedand mustbe operativefor all flights.lt is importantto notethat:
AND NOT
OF THEAIRPLANE
ALL ITEMSWHICHARE RELATED
TO THEAIRWORTHINESS
REQUIRED
INCLUDED
ON THELISTAREAUTOMATICALLY
TO BE OPERATIVE:
Equipmentobviouslynot requiredfor safe operationof the airplanesuch as galleyequipment,
passengerconvenience
items,etc. is not listed.
item.
NOTE:Lavatorydoorashtrayis not considered
a convenience
FORDISPATCH
CRITERIA
The pilot in commandonly is authorizedto determinethat the flightin questioncan be continued
safelywith inoperative
equipmentand may requireequipmentto be operativeoverand abovethat
underwhichthe flightis to be
listed,when,in hisjudgement,
suchis requiredfor the conditions
below.
continued,however,he shallneveracceptreouirements
it mustbe checkedthatany
Beforedispatching
an airplenewith multipleMEL itemsinoperative,
in
in the levelof safetyandior
not
result
degradation
interrelationship
betweeninoperative
itemswill
an undue increase in crew workload, lt is particulerlyimportantin this area of multiple
discrepancies
and especiallydiscrepancies
in relatedsystems,that goodjudgement,basedon the
circumstances
of the caseincludingclimaticand enrouteconditionsmustbe used.
Wheneverthe pilot in command and/or the respectivemaintenancestaff have any doubt
mustbe
Control(OCC)(SITA:BUDWWMA)
concerning
theapplication
of thisMEL,the Operation
contacted.
to the pilot in
Takinginto accountall relevantfactors,OCC will then releasea recommendation
command.
D. MAINTENANCE
ACTION
Every etfort shall be made by Maintenanceto correct all technicalirregularitiesas early as
condition.
practicable
basein fullyoperational
and that the airplanebe releasedfrom maintenance
and to
MEL requirement
The decisionof the pilotin commandto complywith the appropriate
postpone
The pilotin commandmustbe
maintenance
activitywillsupersede
any otherintention.
shouldit be impossibleto repairthe inoperative
informedby meintenance
as soonas practicable,
itemprlorto departure.
the following
for dispatchwith item inoperative,
Wheneveran airplaneis releasedby maintenance
is required:
The Deferredltem Record(DlR) aboardthe airplanemust containa detaileddescriptionof the
item(s),specialadviceto the flightcrew,if necessary,
and informationaboutcorrective
inoperative
actionteken.
PAGE5
PREAMBLE
REV17 MAR10/2007
azE
tue
787
PREAMBLE
When they are accessibleto the crew in flight, the control(s)relatedto inoperativeunit(s)or
paragraph
(4).
component(s)
mustbe clearlvolacarded.
SeeH- DEFINITIONS,
produce
must
be
renderedinoperative
ff inadvertentoperationcould
a hazardsuch equipment
(physically)
given
in the appropriate
Maintenance
Procedure.
as
in all caseswherea
The symbol"(M)"is printedin the column"REMARKS
OR EXCEPTIONS'
specificmaintenanceprocedurebecomesnecessaryduringapplicationof certainMEL items.The
'8767MELDisDatch
in MELcanbe foundon board.
Deviation
Guide"referenced
The 8767 MEL DDG (M) procedureis a referencewith AMM. All cases where a maintenance
procedurebecomesnecessaryAMMtasksshellbe used.
E. deletedFERRYFLIGHT
F. PERMITTO FLIGHT (European
Commission regulation (EC)
No.
37512007)
A Permitto Fly is generallyissuedwhen a certificateof aiMorthinessis temporarilyinvalid,for
cannotbe issuedfor
exampleas the resultof a damage,or when a certificateof airworthiness
or
for airworthiness
instancewhen the aircraftdoes not complywith the essentialrequirements
whencompliancewith thoserequirements
has not yet beenshown,but the aircraftis nevertheless
capable of performinga safe flight. EASA is responsible for the approval of the flight
conditions on the basisof whicha permitto fly can be issuedby the NTACM.
The EASA approvea the Flight Conditions in cases related to the safety of the design,
definedas follows:
1. the aircraftdoesnotconformto an approveddesign;or
or an AiMorthiness
Maintenance
Requirement
2, an Airworthiness
Limitation,
a Certification
Directivehas not beencompliedwith;or
3. the intendedflight(s)areoutsidethe approvedenvelope;
Caseswherethe EASAis not involved:
Whenthe approvalof flightconditionsis not relatedto the safetyof the design,the EASAis not
involved,but onlythe NTACAA.Examplesof suchconditionsare:
previously
acceptedbythe EASAfor the
1. demonstrating
withthe stiandard
continuingconformity
-) certificateof aiMorthiness.
for a (restricted
aircraftor typeof aircraftto qualifyor re-qualiry
2. development;
crewtraining;
3. designorganization
or production
organizations
production
4.
flighttestingfor the purposeof conformityestablishment;
5. delivery/export
flightof a newaircraftthe designof whichis approved;
6. flyingthe aircraftfor Authorityacceptance;
7. flyingthe aircraftfor customeracceptance;
or aiMorthinessrevieware to be performed,
8. flyingthe aircraftto a locationwheremaintenance
or to a placeof storage;
takeoffweightfor flight
9. flyingan aircraftat a weightin excessof its maximumcertificated
where
adequate
landingfacilitiesor
land
areas
beyondthe normalrangeoverwater,or over
appropriate
fuelis notavailable;
requirements
beforeconformityto the
10. flyingaircraftmeetingthe applicableairworthiness
environmental
reouirements
hasbeenfound.
aircraftor typesfor whicha
11. for non-commercial
flyingactivityon individualnon-complex
is notappropriate.
or restrictedcertificateof airworthiness
certificateof airworthiness
PAGE6
PREAMBLE
REV17 MAY30/2007
EAE,IUE
787
PREAMBLE
Applicableproceduresfor obtaininga permitto flight
to obtaina permitto fly, MALEVas an applicant,the MALEVCAMOhasto followthe
Consequently,
followingprocess:
1. Sendan electronicapplication
formto EASAin orderto get an EASAapprovalof the flight
conditionsproposedto supportthe issueof a permitto fly bythe MemberStateof Registry,or
marks: EASAform 37.
by theMemberStateprescribing
the identification
permittoflv.html)
(http://www.easa.eu.inuhome/c
for a permitto fly to the
2. Simultaneously
or followingEASAapproval,sendan application
the
Competent
Authorityof the MemberStateof Registry,or of the MemberSteteprescribing
marks,togetherwiththe EASAForm188 approvedby the Agency,usingEASA
identification
Authority.
Form 21 or anyacceptable
form prescribedby thatCompetent
WITHTHESTATEDINTENTOF THEPREAMBLE,
WHENUSINGTHISMEL,COMPLIANCE
IN THISMELIS
ANDTHECONDITIONS
ANDLIMITATIONS
SPECIFIED
DEFINITIONS,
REOUIRED.
F. REGULATIONS
FORCATEGORY
OPEMTIONS
IYIIIALL-WEATHER
(Thispartetfectivependingon CATlylll operational
approval.)
(1)General
MALEV8767 aircrafthavebeencertifiedto operateto CAT lllB LandingMinimaand will be to
thisstandardunlessreclassified
dueto a systemdefect.
lf an airplanehas beenreclassified
to non-CATlllB, the aircraftmayoperatein this conditionin
accordancewith MEL requirementsprovidedthe aircraftis not requiredto land in CAT lllB
weatherconditions.
The instrumentand automaticflight control systems meet the associatedperformance
if the listedminimumequipment
is operative
at the time the CAT lllB approachis
standards
initiated.
(2)Procedureof the re-classification.
(a)Failure
occurson ground
accordingto MALEV
Dueto a systemdefectthe associatedairplanemustbe reclassified
CPM,
(b)Failureoccursin flight
- followthe FlightManualandOperation
ManualInstructions,
- advirethe MALEVOperationConholaboutthe CATchanges.
procedures
(3)Categoryll/lllB operationsupplementary
(a)General
PREAMBLE
PAGE7
REV17 MAY30/2007
7A7
EZEftUE
PREAMBLE
For maintaining
safeall-weather
op€rationsaccordingto FAAAdvisoryCircularsNo. 120-29
and 120-28Cspecial maintenanceproceduresare demandedfor certain components.
arecalledCATlulllComoonents
andaredefinedas follows.
ThesecomDonents
and
thatareespecially
for CATll/llloperation,
Components
required
- thatdirectlyetfectthe performance
or accuracyof a CATll/lll approach,and
- for whichdeterioration
or accuracycan not be excluded,and
of the performance
- forwhichan adjustment
veluespossible.
to thenominal
(b) ldentification
andStorageLimits(COSL)
Operating
CATlVlllcomponents
areidentified
in theComponent
undercolumnCATby "C",
Cat ll/lll components
are markedwitha yellowplacardwithblueleftering:
.ATTENTION
CATIVIIICOMPONENT
(c)Rulesof suspension
of Category
ll/llloperations
lf e CAT ll/lll componentis substituted
by a componentwhich has not a CAT ll/lll
placardor/andAuthorizedReleaseCertificateor AiMorthinessApprovalTag
identification
(ARC/AAT,JM FormOne),the CAT lvlll OperationPermissionfor the affectedaircraftwill
willbe installed.
suspended,
untila properCATll/lllcomponent
NOTES:
1. lf a CAT lll componentsubstitutedby a non-CATlll componentthe affectedAutoflight
Channelis not allowedto be used for CAT lll approaches.In this case no CAT lll
approachescan be performed.The no affectedchannel of the AutoflightSystem,
however,canstillbe used,for CATll Approaches.
Department
approval.
2, Allotherprocedures
aresubjectthe MALEVEngineering
procedureshouldmeet MALEVCPM and this MEL TemporaryFlight
3. Reclassification
OperationLimitationand Reportingprocedure..
PAGE8
PREAMBLE
REV17 MAY30/2007
tUiE 7Ez
AOE
PREAMBLE
AIRBORNE
EQUIPMENT
LISTOF REQUIRED
at the
Followingtablesprovidethe listof the minimumequipmentthathasto be serviceable
to checkMEL
as e guidance
of theCategory
ll or lll approach.
lt is provided
commencement
provisions
thatreferto "approach
minimums"
specifications,
of flight,referto
Aftercommencement
This listis not intendedto be a "NormalChecklistOperation".
procedures
perform
AFM
to
a Categoryll or lll approach.
FOR
REQUIRED
NUMBER
CATIIIA CATIIIB
CAT II
2
(INAPPMODE)
1
AUTOPILOT
ANDFLIGHT AP CHANNEL
2(a)
2(a)
2(al
DIRECTOR
SYSTEM
FLIGHTDIRECTOR
1
1
1
LIGHTS
AP DISENGAGE
1
1
AURALWARNING
AP DISENGAGE
2
AP DISENGAGE
SWITCHES
2
1(b)
AUTOLANDSTATUS
(ASA)
ANNUNCIATOR
-(c)
1
A.iTINCLUDINGBOTH
{c)
COMPONENTS
DISENGAGELIGHTS
MODE
FLIGHT
ANNUNCIATOR
ALPHAVANESENSOR
ILS
RIGHT(INCL.HEATER)
LEFT (INCL.HEATER)
RECEIVERS
(COURSE
BARAND
INDICATIONS
GSPOINTER)
ALERT
DEVIATION
1
1
1
1
2
1
1
1
1
1
2(e)
1
2(e\
2
2(e)
2(e)
2(e)
1
2(e)
2(d\
IRS
EADI
INDICATIONS
ATTITUDE
ATTITUDE
COMPARATOR
COMMBARS
FLIGHT
DIRECTOR
TRANSCEIVER
INDICATION
DHWARNING
LRRA
DADC
WIPERS
WINDSHIELD
ELECTRICAL
POWER
SOURCE
HYDRAULIC
SYSTEM
(a)
(b)
(c)
(d)
(e)
(f)
(g)
2
2(el
1
2(e\
2(e)
2(e)
2
2(t)
2(s)
2(e)
2(e)
2
2(f)
3(f)
3
maybe selected.
combinations
Onlythe Leftand Rightor theCenterandRightFlightDirector
Mustbe operativefor the captainaccordingto MALEVSOPpolicy.
lf pilotcan keepapproachspeedwithint 5 knotslimitthe targetspeed
withengagedautopilotin NAVmode.
Associated
Mustbe suppliedby separatesymbolgenerators.
One maybe the APUgenerator.
Associated
withengagedautopilotchannels.
PAGE9
PREAMBLE
REV17 MAY30/2007
EAEUIUE
787
PREAMBLE
FORRVSMOPERATION
REGULATING
(1)General
unlessthey are
MALEV8767 aircrafthavebeencertifiedto operateunderRVSMregulations,
change
reclassified
dueto a fuselagedamageor configuration
lf an aircrafthas been reclassified
to Non-RVSMoperation,it is not allowedto operateunder
RVSMregulations.
(2)Procedureof the reclassification
In case of fuselagedamageor configurationchange,associatedto RVSM regulation,the
aircraftmustbe reclassified
to Non-RVSM
acc.to MALEVCPM.
procedures
(3)RVSMOperationsupplementary
(l) To ensureaircraftabilityto operatesafelyunderRVSMrules,somesystemsand components
(seetable)shouldbe installed
(i,a.w.JAROPS1.872,leaflet26.)
andoperable.
EQUIPMENT
LISTOF REQUIRED
AIRBORNE
COMPONENTS
AIR DATACOMPUTER
ALERTING
SYSTEM
ALTITUDE
AUTOPILOT
SYSTEM
ATCTRANSPONDER
PITOTHEATER
STATICPORTHEATER
NUMBER
REQUIRED
1
1
1
NOTE: Fuselagedamageto the afeadefinedby the relevantSructuralRepairManualmust
for operationin RVSM
withthe requirements
be assessedto ensurecompliance
arrspace
exceptADC,
(a) All Components
certifiedfor 8767AlrcraftsatisfywithRVSMrequirement,
(b) ADCshouldbe P/N4040800-906
one.
or upgraded
(ll) ldentification
Componentsrelatedto RVSMoperationare identifiedin 8767 MaintenanceProgramunder
CATcolumnby Letter"R".
PAGE1O
PREAMBLE
REV17 MAY30/2007
EOEIIUE
7A7
PREAMBLE
H, REGULATIONSFOR BRNAV/RNPOPERATION
(1) General
MALEV8767 aircraffhavebeencerti{ledfor operationsin areaswith specifiednavigationperformance
changeof
(RNAV)(JAROPS 1.243) unlessthey are reclassified
due to a configuration
requirements,
RNAVequipment.
(RNP-5)
Performance
BasicRNAV(BRNAV)and RequiredNavigation
JAA TGL2,
BRNAVis definedas RNAV,includingthe functionsdescribedin ICAODoc 9613-AN1937,
thatmeetsa trackkeepingaccuracyequalto or betterthan+/- 5 NMfor 95%of the flighttime..
(RNP)is a statementof the navigationperformancenecessaryfor
RequiredNavigationPerformance
operationwithin a defined airspace.(FAA AC No.: 90-96) RNP Types are establishedacc. to
positionfxing.
performance
navigalional
accuracyin the horizontalplane,that is, lateraland longitudinal
The type is identified as an accuracy value expressed in nautical miles (e.9., RNP-s).
(MNPS)
Performance
MinimumNavigation
Specification
MALEVoperatesaeroplanein MNPSairspaceequippedwith navigationequipmentthat complywith
minimumnavigationperformance
specificationprescribedin ICAO Doc 7030 in the form of Regional
Procedures.
Supplemenlary
(2) Limitations
are requiredfor theiruse
ThefollowingnavigationsyslemshaveRNAVand MNPScapability,limitations
whenconducting
operationsin designated
BRNAViRNP/
airspace.
In the MNPSairspace
referto: (MELATA)
ln the BRNAV/RNP
airspace
referto: (MELATA)
Inedial ReferenceSystem
VOR
DME
GPS
FMCS
HF radio
I.
34-21-1
34-51-1
34-55-1
34-60-t
34-61-1
X
u-21X
34-60-1
34-61-1
23-11-1
DEFINITIONS
Number100and items
1. Systemnumbersare basedon the Air TransportAssociation(ATA)Specification
are numberedsequentially.
(a) "ITEM"meansthe equipment,
systemcomponentor functionlistedin the ,ITEM'column.
(b) ,,NUMBER
INSTALLED"
is lhe number(quantity)of itemsnormallyinstalledin the aircraft.
of ilemsrequiredfor
(c) "NUMBERREQUIRED
is the minimumnumber(quantity)
FOR DISPATCH"
columnare met
OR EXCEPTIONS'
operationprovidedthe conditions
specifiedin ,,REMARKS
or permittingoperationwith a
(d) ,,REMARKS
OR EXCEPTIONS'
includesa statementeitherprohibiting
specificnumberof items inoperative,provisos(conditionsand limitations)for such operation,and
appropriate
notes.
(e) A verticalbar (changebar) in the marginindicatesa change,additionor deletionin the adjacenttext
for the currentrevisionof thatpageonly.Thechangebar is droppedat the nextrevisionof thatpage.
PREAMBLE
PAGE,11
REV17 MAY30/2007
EZE
TUE 787
PREAMBLE
Flight Manual"(AFM/RFM)is the documentrequiredfor type certillcationand
,Airplane/Rotorcraft
approvedby ihe responsible
Office.The FAAapprovedAFM/RFMfor Cenificate
FAAAircraftCertification
DataSheet.
NOTE; Condition"As requiredby FAR" in the FAA Master MEL has been replacedby detailed
requirements
of the HungarianCAA(HgCAA)in thisdocument.
4 . Each inoperativeitem must be placardedto inform and remindthe crewmembersand maintenance
personnelot equipmentconditionNOTE1: To the extentpractical,placardsshouldbe locatedadjacentto the controlor indicatorfor lhe
item affected.
wherenecessary.
NOTE2: Placardwordingand locationwill be determinedby PLACARDinstruction,
Whenplacardwordingnotdelermined,
useof INOPplacardis sufficient.
"NUMBER
columnsindicates
REQUIRED
5. '-'symbolin "NUMBER
FORDISPATCH"
INSTALLED"
and/oT
a variablenumber(quantity)
of the iteminstalled.
o.
"DELETED'in the "REMARKS EXCEPTIONS'
oolumnaftera sequenceilem indicatesthat the iiem
OR
waspreviously
listedbut is nowrequiredto be operativeif installedin the aircraft.
'ETOPS"(+ "ER"referslo extendedrangeoperationsof a two-engineairplanewhichhas a typedesign
of HungarianCAA. Boeing
approvalfor ETOPSoperalionsand complieswith applicablerequirements
767-200/300ER
aircraflof |\4ALEV
havetypedesignapprovalfor ETOPS.
Mal6vLtd.philosophyis thataircraftshallbe preparefor all flightsaccordingto ETOPSrules(if aircrafiis
tit for ETOPSflighq.
ETOPSmaintenance
are regulatedin ETOPSMANUAL.
andoperatingprocedures
Mal6vETOPSMANIJALcontaintwo part: Part l. ETOPSMainlenanceProceduresand Part ll. Flight
Operatingprocedures.Each parl has an individualapprovalprocess,becausethey have a different
is performedstrictlyin one block.
requirement
and responsibility
system,butthe distribution
shall be maintain,and all
To ensurecontinuosETOPSc€pabilityof the aircraflETOPSconflguration
requirementsspecifiedin ETOPSMANUALregard,ngmainlenanceprogram,maintenanceplanning,
maintenance
accomplishment,
and materialsupplymustbe fulfilled.
Rulesdescribedin ETOPSMANUALappliesthe employeeof Mal6vLtdor Nlal6vcontractedpartner,who
groundhandling,planning,etc.) relatedwith ETOPS
are involvedin technicalactivities(maintenance,
ofthe aircraft.Conientsof ETOPSMANUALshallbe trainedfor personnelinvolved.
oDeraiion
ETOPSMANUAL is valid for thefollowineairuaft:
Reg.mark: HA.LHA
Type: 8767-200ER
Reg.mark: HA.LHB
Type: 8767-200ER
Reg.mark: HA.LHC
Type: 8767-300ER
S/N:
27048
S/N:
27049
s/N:
UN:
475
UN:
482
U N : 738
Eng.type: cF6-80C2-B4F
Eng.type: cF6-80C2-84F
28884
Eng.type: cF6-80C2-B6F
in 31.August1998,and15.April2007.
MalevLtd.hasreceived
the 170minETOPSapproval
PAGE12
PREAMBLE
REV17 MAY30/2007l .
E?E
TUE
787
PREAMBLE
Verification
Flightshallbe initiatedin thefollowingcases.
An ETOPS
lrON EIOPS Veification
Flight
in case of engine change
Verfiication Flight
a// cases
in caseof failurein ETOPSsignificant
when the
systemif detectcan not be
pte
reproducedon grcund,or afrerdefect disru d/mai ntai ned system
rectificationsystemwotkingordercan has not direct, unambiguous
indication in flight deck
not be proved by systemcheck
when the
disrupbd/maintained
syatem has direct"
unambiguousindicationin
flight deck
dis ru pted/ mai ntained system
has not direct, unambiguous
indication in ttight deck
when the
disrupted/mainEined
system has direct"
unamhiguous indi cation in
flight deck
if duing maintenance check or defect
rcctitication both duplicaled ETOPS
significant systems were disrupted
alonganydesired
flight
(RNAV).Thisis a method
navigation
whichpermiis
aircraft
8. AreaNavigetion
pathwithinthecoverage
of selfnavigation
aidsorwithinthelimitsofthecapability
oftheassocialed
contained
aids,ora combination
of thesemethods.
awayfromland,wichis suitable
overwaterat distance
9. 'ExtendedOveMaterFlight"meansoperation
for makingemergency
landing,greaterthan 120 minutesat cruisingspeedor 400 nauticalmiles,
whichever
is lesserby respective
(FAR)in the FAAMasterMELhasbeenreplaced
AviationRegulalions"
10.NOTE;"Federal
requirements
document.
Time
Coordinated
Universal
11."Flight
Day"meansa 24 now period(frommidnightto midnight)
(UTC)duringwhichat leastone flightis initiatedfor the atfectedaircraft.
meansan atmospheric
environment
11."lcing
conditions"
thatmaycauseiceto formon theaircraft
in
the
engine(s).
or
that must be
or limitation)
l2.Alphabetical
symbolin Column4 indicatesa proviso(condition
compliedwithfor operationwiththe listediteminoperative.
to the extentthat it does not
l3."lnoperative'meansa systemand/orcomponentmalfunctions
accomplishits intendedpurposeand/or is not consistentlyfunctioningnormallywithin its
approvedoperatinglimits(s)or tolerance(s).
column Drovidesadditionalinformationfor
14."Notes:"in "REMARKSOR EXCEPTIONS"
crewmemberor maintenanceconsideration.Notes are used to identifyapplicablematerial
whichis intendedto assistwithcompliance,
butdo not relievethe personnelof the responsibility
Notesare nota partof the provisos.
for compliance
withall applicablerequirements.
'l5.lnoperative
of a
itemswhichare components
components
system:Inoperative
of an inoperative
systemwhich is inoperativ€are usuallyconsideredcomponentsdirectlyassociatedwith and
PREAMBLE
PAGE13
REV17 MAY30/2007
EOE
'YE
787
PREAMBLE
systemsassociatedwith i
havingno otherfunctionthanto supportthatsystem.(Warning/caution
authorizedperthis MEL).
the inoperative
systemmustbe operativeunlessreliefis specifically
procedure
whichmust be
for a specificmaintenance
16,"(M)"symbolindicatesa requirement
accomplishedprior to operationwith the listed item inoperative.Normallymaintenance
personnelaccomplishthese procedures;however,other personnelmay be qualifiedand
authorizedto performcertainfunctions.Proceduresrequiringspecializedknowledgeor skill,or
personnel.
by maintenance
requiring
the useof toolsor testequipment
shouldbe accomplished
proceduresreferredaboveare generallyprovidedin the 8767 Dispach I
NqtE: Maintenance
DeviationGuidedocument.The 8767 DDG (M) procedureis referencewithAMM.All cases I
procedurebecomesnecessaryAMMtasksshellbe used.
wherea mainlenance
I
'17."(o)"symbol indic€tesa requirementfor a specificoperationsprocedurewhich must be
Normallythe flight
accomplished
in planningfor and/oroperatingwiththe listediteminoperative.
crew accomplishesthese procedures;however, other personnelmay be qualified and
authorized
to performcertainfunctions.
mustbe putintoan acceptable
18."Deactivated"
component
and"Secured"
meanthatthesoecified
conditionfor safeflight.
is such that
1g."Visual
Meteorological
(VMC)meansthe atmospheric
environment
Conditions"
wouldallowa flightto proceedunderthevisualflightrulesapplicable
to theflight.Thisdoesnot
preclude
operating
underInstrument
FlightRules.
containing
waterin anyformthatcanbe
20."Visible
Moisture"
environment
meansan atmospheric
seenin naturalor artificiallight,for example,clouds,fog, rain,sleet,hail,or snow.
comfort
21."Passenger
convenienceltems"meanthose itemsrelatedto passengerconvenience,
ash trays,
movieequipment,
or entertainment
suchas, but not limitedto, galleyequipment,
slereoequipment,overheadreadinglamps,etc.
Note:Lavatorydoorashtrayis notconsidereda convenience
22,"REPA|RINTERVAL":
All MALEVoersonneland, in the extentof their scopeof activity,
personnel(2. g. subcontractors,
handlingagents)must effectrepairs
associatedorganization
with this MEL,at or priorto the
of inoperative
deferredin accordance
systemsor components,
repairtimesestablished
by the followingletterdesignators:
CategoryA. ltems in this categoryshall be repairedwithinthe time intervalspecifiedin the
"REMARKS
OR EXCEPTIONS"
column.
calendardays
CategoryB. ltems in this categoryshallbe repairedwithinthree(3) consecutive
(72 hours), excludingthe day the malfunctionwas recordedin the aircraft
For example,if it were recordedat 10 a.m. on
maintenancerecord/logbook.
January26'n,the three-deyintervalwouldbeginat midnightthe 26th and end at
midnight
the29'".
calendardays
CategoryC. ltems in this categoryshallbe repairedwithinten (10) consecutive
(240 hours), excludingthe day the malfunctionwas recordedin the aircraft
For example,if it were recordedat. 10. a.m. on
maintenance
record/logbook.
January26rh,the 10 d-ayintervalwould begin at midnightthe 26tnand end at
February
midnight
5'".
PAGE14
PREAMBLE
REV17 MAY30/2007
BAEfiUE
787
PREAMBLE
CategoryD. ltems in this categoryshall be repairedwithin one hundredand twenty(120)
consecutivecalendardays (2880hours),excludingthe day the malfunctionwas
recordedin the aircraftmaintenance
record/logbook.
Theletterdesignators
INTERVAL"
column.
arein the"REPAIR
In a case, if the deviationcan not be fixed withinthe specifiedtime, TechnicalDirectorof
MALEVPlc. can duplrcatethe intervalaccordingto the appropriatecategory(exceptfor
levelof safetyis maintained.
category"A")@, providedan acceptiable
23.Enginelndicatingand CrewAlertingSystem(EICAS)provideditferentprioritylevelsof system
Any message
(WARNING,
messages
STATUSand MAINTENANCE).
CAUTION,
ADVISORY,
that affectsairplanedispatchabiliV
will be displayedat a STATUSmessagelevelor higher.The
indicates
ADVISORY)
CAUTION,
absenceof an EICASSTATUSor higherlevel(WARNING,
thatthe system/component
is operatingwithinits approvedoperatinglimitsor tolerances.
a
Systemconditionsthat resultsonly in maintenancelevel message,i.e. no correlationwith
"A
at
next
repair
level
but
it
is
suggested_to
higher
EICASmessage,do not affectdispatch,
check,if the necessarymaterialand equipmentis available,exceptMALEV(operator)refuses
repairdueto anyreason.
was recordedin the aircraft
24. Day of Discoveryis the calendarday an equipmenVinstrument
This day is excludedfrom the calendardays or flight days
maintenancerecord/logbook.
specifiedin the MEL for the repairof an inoperativeitem of equipment.This provisionis
"A, B, C, andD"
applicable
to all MELitems,i.e.categories
25. Combustible
Materialin remarkscolumnrefersto materialwhichis capableof catchingfire and
(or flammableor
burning.In particularif a MEL item prohibitsloadingof combustible
inflammable)
material,no materialmaybe loadedexceptthe following:
( unloaded,
emptyor withballast)
1. Cargohandling
equipment
2. Flyawaykits( excludinge.g.cansof hydraulicfluid,cleaningsolvents,batteries
tyresare included,theyshouldonly
capacitorschemicalgeneratorsand if serviceable
be inflatedto a minimumpressurethatpreservestheirserviceability
no
3. Inflightservicematerial(returncatering- onlyclosedcateringtrolleys/boxet,
newspapers,
no alcoholor dutyfreegoods
PAGE15
PREAMBLE
REV 17 MAY30/2007|
lVadlEl/
EAE|IUE
Hungarian Airlinesfi
7A7
EQUIPMENT
LIST
MINIMUM
PROCEDURE
TEMPORARY
FLIGHTOPERATION
LIMITATION
and REPORTING
AT HOMEBASE
1.
GENERAL
of
This proceduredeterminestasks concerningthe temporarylimitation(reclassification)
definitespecialflightauthorizations
accordingto AOCof MalevLtd,suchas:
E , l- C A T l l ; E 2 - C A T l l l A ;E 3 - C A T l l l B ;E 6 - M N P S ;E 7 - E T O P SE; 8 - B - R N A V ;
E 9 - RVSM;E {0 - RNP,andotherMELbasedlimitation.
PRESERVATION
NOTE: THE OTHERTASKSRELATEDTO THE GONTINUING
IN ETOPSMANUAL
OF ETOPSAUTHORIZATION
ARE PRESGRIBED
PARTI. MAINTENANCE
PROCEDURE.
2.
RECLASSIFICATIONPROCESS
2.1
Necessityof temporaryreclassification
Defermentof defect rectificationsmay require the limitationof any type of operation
and the rate
(reclassification)
detailedin paragraph.1. The defectsaffectingthe authorizations
of reclassification
are determinedby the approvedMinimumEquipmentList (MEL) of the
relatedaircraft.
2.2
Accomplishmentoftemporary
reclassification
processshallbe carriedout by the employeedeferringthe rectification
The reclassific€tion
to the completionof Deferredltem
of defectinfluencingthe authorization,
simultaneously
Record(DlR)in thefollowing
order:
causedby the defectto be
1. Referringto MELdefinesthe compliancedegradation
defened.
and i or AdditionalCrewand /
2. Recordthe rate of reclassification
in block"LIMITATION
or Maintenance
Procedure"
of the DIRform,
ACTIONTAKEN" of the AFL
3. Recordthe rateof reclassification
in field " CORRECTIVE
form.
ETOPSsigns(Non-ETOPS;
4. Informthe flightcrewand stickstemporaryreclassification
pilot
as well
in command's,
Y, OnlyCAT-Y;Non-RNAV;
Non-RVSM;
INOP;etc.)on the
as on the flrstofficer'sinstrumentDanels.
into the cockpit
5. Placethe red copy of the DIR containingthe causeof reclassification
information
file.
document
6. Informthe Shift Leaderof AeroDlexLtd. who shell foMard the relevantDIR to the
Malev/Aeroplex
Maintenance
Controlvja Fax (+36-1-296{928).
7. The Mal5v/Aeroplex
Maintenance
ControlshallforuardSlTAtelexto the belowlisted
addressees
AdMiNistlAtioN/
AUTHORITYGiViIAViAtiON
BUDXTYF- NATIONALTRANSPORT
lgazgat6seg
NEMZETIKoZLEKEDESIHAT6SAGPolgariL6gikaizleked6si
(ONLY the fo owing cases ,tust be repofted to the Authority:
: 7- ETOPS;
E 1 - C A T l l :E 2 - C A T l l l AE: 3 - C A T l l l BE: 6 - M N P S E
E8-B-RNAV;E I - RVSM;E 10-RNPJ/
BUDNBMA- ShorthaulFlght
BUDWWMA- OperationsControl Center
DispatchSection
BUDKFMA- Uzemeltet6sl16nyitisi
BUDFOMA- GockpitCrew Dispatch
Osztily / EDPFlight Preparatory
- CockpitCrewPlanning
BUDTDMA- UzemanyagOsztely/
BUDFPMA
Diszp6cser
PAGE:1/4
PROCEDURE
TR. FL.OP.LlM.REPORTING
REV 17 MAY30/2007
./V'aAi'E/ Hungarian Airlinesfi
7Ez
EZEI/VE
- FlightPlanningSection
BUDNSMA
LIST
MINIMUM
EQUIPMENT
BUDNFMA- LonghaulFllght
DispatchSection
ACE
BUDMMMA.
R<ividtivriKarbantart5stervezds
BUDKBMA- ForgalmiOsztely,Forgalmi
BUDFEMA- Arukezel6siOsztSly,
Expod
lroda T2A
BUDFHMA- Arukezel6slOszt6ry,
BUDPBMA UtasforgalmiOsziily /
Jiratkiszolgil{si Csoport
Jegyk€zel6sT2A
BUDPCMA- UtasforgalmiOsdely ,
BUDWBMA- Forgalmilgazgat6sag/Terminal
Control
Szolg6latvezet6kT2A
the
information
reclassification
as
follows:
containing
on the
BUDDSMA- Repiil6sbiztonsagiOsztely
Number:
Registratron
Defect:
MEL:
DIRNo:
Limitation:
2.3
Terminationofreclassification
should be done as followsby the employee
Terminationof the temporaryreclassification
or by the employee
recordingthe rectification
of the defeneddefectcausingreclassification,
causeddefects
recordingthe rectification
of the lastdefectin caseof severalreclassification
exrst:
documentfile.
1. Repealand removesthe relevantDIRfromthe cockpitinformation
2. Removethe warningstickersfromthe pilots instrumentpanels.
3. Inform the Malev/AeroplexMaintenanceControl who forward a SITA-telexabout
termination
of the reclassiflcation
to addresseslistedin the pointTof paragtaph2.2.
2.4
Validity of temporary.eclassificationreport
Controlis valid
The temporaryreclassification
reportissuedby Mal6v/AeroplexMaintenance
preliminary
reclatsification
date
of
untilrevocationadditionallythe reportcontainsthe
expiry
purpose
butonlyfor information
only.
3.
ADDITIONAL
REPORTING
OBLIGATIONS
3.{
ETOPScompliance
Malev/ AeroplexMaintenance
Controlshallnotifyvia SITAtelexthe responsiblebelowlisted
MALEVservicesand NTA CA'/AaboutETOPSstatusof aircraftas far as possible2 hours
priorto the scheduled
ETOPSflightfromBudapest.
BUDXTYF- NATIONALTRANSPORT
AUTHORITYCivil Aviation Administration/
lgazgat6sSg
NEMZETIKOZLEKEDEsIHAToSAGPolgariL6gikaizleked6si
BUDWWMA- Uzemeltet6s116nyitasi
Osztily , OperationsControl Center
- CockpitCrewPlanning
BUDFPMA
- LonghaulFlightDispatchSection
BUDNFMA
BUDNBMA- ShorthaulFlightDispatchSection
- FlightPlanningSection
BUDNSMA
BUDMMMA- TechnicalDirectorate/ Karbantartistervez6siOszt6ly
PAGE.,214
PROCEDURE
TR . FL.OP.LIM.REPORTING
REV17 MAR10/2007
/VadEV
Hungarian Airlinesfi
AZEZIIYE
787
LIST
MINIMUM
EQUIPMENT
TEMPORARY
FLIGHTOPERATION
PROCEDURE
LIMITATION
and REPORTING
AT OUTSTATION
1.
GENERAL
a). This proceduredeterminestasks of employeeof contractedoutstationmaintenance
partnerconcerningthe temporarylimitation(reclassiflcation)
of definitespecial flight
authorizations
accordingto AOCof MalevLtd,suchas:
E 1 - C A T l l ;E 2 - C A T l l l AEi 3 - C A T l l l BE; 6 - M N P S E
; 7- ETOPS;
E8-B-RNAV;E9-RVSM; E 10- RNP,andotherMELbasedlimitation.
Control
b). The chaptercontainsthe responsibility
of Malev/ AeroplexMaintenance
concerningto reportof operationallimitation.
OF
NOTE:THEOTHERTASKSRELATED
PRESERVATION
TO THECONTINUING
ETOPS
PART
I.
ETOPSAUTHORIZATION
IN
MANUAL
ARE PRESCRIBED
MAINTENANCE
PROCEDURE.
RECLASSIFICATION
2.
PROCESS
2.' | Necessityof temporaryleclassification
Defermentof defect rectiflcationsmay requirethe limitationof any type of operation
(reclassification)
and the rate of
in paragraph1. The defectsaffectingthe authorizations
reclassification
are determined
by the approvedMinimumEquipmentList (MEL)of the
relatedaircraft.
2.2
Accomplishmentof temporaryreclassification
processshallbe carriedout by the employeedefeningthe rectification
The reclassification
of defectinfluencingthe authorization,
to the completionof "CORRECTIVE
simultaneously
ACTIONTAKEN'fieldAFLin thefollowing
order:
1. Referringto MEL definesthe compliancedegradationcaused by the defect to be
deferred.
2. Recordthe rateof reclassification
ACTIONTAKEN' of the AFL
in field" CORRECTIVE
form.
3. Informthe flightcrew.
NOTE:ETOPSNON-COMPLIANGE
OF 8767, AIRCRAFTSHALL ALSO BE
"NONDOCUMENTED
IN THE AFL BLOCK 21lb CIRCLINGBLOCK
ETOPS".
in wriften
4. Informthe Malev/AeroDlex
MaintenanceControlabout the reclassification
formatvia one of the blowlistedmethod.
Fax:+ 36 1 296 8928
Telex:BUDMCMA
E-mail:maintenancecontrol@malev.hu
Usingthe aircraft'sAGARSsystem (if available)
5. The Malev/Aeroplex
Controlshallfollowthe same procedureas describe
Maintenance
in the point 7 of paragraph2.2 ol procedure"Temporaryflight operationlimitation
reportingprocedureat homebase".
2.3
Temination of reclassification
shouldbe done as followsby the employee
Terminationof the temporaryreclassiflcation
or by the employee
causingreclassification,
recordingthe rectification
the
deferred
defect
of
caused
recordingthe rectificationof the last defect in case of severalreclassification
defectsexist:
ACTIONTAKEN''of the AFL
1. Recordthe correctiveactiondonein field .CORRECTIVE
form.
PAGE:3/4
PRoCEDURE
TR. FL.OP.LlM.REPORTING
REV17 MAY30/2007
/ltUaEV
Hungarian Airlinesfi
EOEtttYE
787
L]ST
MINIMUM
EQUIPMENT
2. Removethewarningstickersfromthe pilot'sinstrumentpanels.
3. Informthe flightcrew.
Controlin writtenformatvia one of the below
4. lnformthe Malev/Aeroolex
Maintenance
listedmethod.
Fax:+ 36 1 296 8928
Telex:BUDMCMA
E-mail:maintenancecontrol@malev.hu
Usingthe aircraft'sACARSsystem (if available)
5. The Malev/Aeroplex
Maintenance
Controlshallforwarda SITA-telexaboutterminationof
to addresseslistedin the point5 of paragraph2.2.
the reclassification
PAGE'.414
PROCEDURE
TR . FL.OP.LIM.REPORTING
REV17 MAR10/2007
tlallEW
Hungarian Airlines,fi
.74.-
,azTEtivzF
LIST
MINIMUM
EQUIPMENT
Annex1
EICASMessages
lntraduction
Cross ReferenceList
and
A crossreference
litt of EngineIndication
andCrewAlertingSystem(EICAS)messages
TheMELlists
in thissection.
MalevMinimumEquipment
corresponding
List(MEL)itemsis provided
equipment
underwhichdispatchis
the itemsof airplane
thatmaybe inoperative,
andtheconditions
the properMEallowed.Thecrossreferencelist is intendedto assistoperatorin quicklyidentifying
possible
itemto consultfor
dispatchrelief.All EICASmessagesal statuslevelor higherare listedby
providedin eachcolumnof the
messagetext in elphabeticorder.A description
of the information
crossreferencelistfollows.
listseachmessageexactlyas it wouldappearon
MessageText Thiscolumnalphabetically
EICASLevel
The appropriateEICASmessagelevelis listed:warning,caution,advisory,comm
E. commF. or status.
or
of the message:
basic,optional,
Thiscolumnindicates
theapplicability
orovisional.
Provisional
messagesarethosefor whichprovisionshavebeenmadein EICAS,
butthe messageis notyet available.'Optional'meanstheteitherthe messageor
whilenotoptional,
theassociated
Somebasicmessages,
equipment
is optional.
sincetheymayhavebeenadded,deletedor
stillmaynotappearin allairplanes,
revisedin laterEICAScomputers.
In somecases,messagesare specificto particularMal6v8767fleet'sairframe
versions
or enginetypes:
GE
B0C2
engines
GeneralElectric
including
engines,
GeneralElectric
CF6-80C2
FADEC80N2 GeneralElectricCF6-80Aand 8042engines
Condition
MEL
-200
767-200
-300
767-300
Thiscolumnprovidesa description
of the conditionor faultindicatedby the
message.
dispatch
MELitem(s)to consultfor possible
ItemThiscolumnliststheappropriate
reliefwiththe associatedmessagedisplayed.EICASmestagesthatdo not have
a specificMMELitemto allowdispatchare listedwithone of the followingcross
references:
N/A Notapplicable.Thereis no MELitemlistedbecausethe messagedoesnot
indicatea systemfailure.
indicated
bythismessage.
NoneThereis no MELitemfor thefailurecondition
EICASlntraduction1/3
REV17 MAR1Ol2007
.t*MIEW Hungarian Airlines
4
.787
.?zEztyzF
LIST
EQUIPMENT
MINIMUM
Annex I
EICASMessages
lntraduction
EICASMessaqes
EICASconsolidates
engineand subsystemindications
and providesa centrallylocatedcrewalerting
function.
communication
alerts,andstatus
EICASdisplays
systemale(s (warning,
caution,andadvisory),
on the
arenormally
displayed
messages
as described
below.All of thefollowing
EICASmessages
upperEICASdisplay,exceptstatusmessageswhichare displayedon the statuspageof the lower
EICASdisDlav.
Waming
A non-normaloperationalor systemconditiondisplayedin redtext
accompanied
of the masterwaminglightsandan
by annunciation
(bell,
auralwaming
siren,clacker,waileror voice).Immediatecrew
awareness
andcorrectiveactionis required.
Caution
A non-normaloperationalor systemcondition displayedin ambertext
accompanied
ofthe mastercautionlightsandan auralcaution
by annunciation
(voiceor beeper).
Immediatecrew awarenessis requiredandcorrectiveactionmay be required.
Advisory
A non-normaloperationalor systemconditiondisplayedin ambertext and
indentedone spaceto the right. Routinecrew awarenessis requiredand
correctiveactionmay be required.
CommE
anda
Medium-prioritycommunication
requiringimmediatecrewawareness
promptresponse.
Displayedin whitetext with a bulletat the bottomofthe
by an auralchime.
message
areaccompanied
field, thesemessages
Comm F
Also
andresponse.
Low-prioritycommunication
requiringtimely awareness
E
below
the
comm
with
a
bullet,
these
messages
are
displayedin whitetext
which
messages
andindentedonespaceto the right. StatusA systemcondition
affectsairplanedispatch,displayedin white text on the statuspage.Status
messages
arecheckedpriorto enginestartandtheconditionshouldbe corrected
perthe operator'sminimumequipmentlist (MEL). Thereareno
or dispatched
inflight crewprocedures
associated
with statusmessages.
Status
A systemconditionwhich affectsairplanedispatch,displayedin white text on
the statuspage.Statusmessages
arecheckedprior to enginestartandthe
perthe operator'sminimum
conditionshouldbe correctedor dispatched
with
associated
equipmentlist (MEL). Thereareno inflight crewprocedures
Statusmessases.
levelmessagesare not includedin the crossreferencelist,sincetheydo not
Maintenance
affectthe aiMorthinessreleaseof the airplane.Systemfaultswhichresultonlyana
message
or maintenance
actionpriorto
maintenance
do notrequireMELconsideration
program.
dispatch.Theyare addressedwithinan operator'sstandardmaintenance
EICASIntraduction2/3
REV17 MAR10/2007
;+UJEV
Hungarian Airlines'fi
.?zrEttvzF
.787
LIST
MINIMUMEQUIPMENT
Annex1
EICASMessages
lntraduction
Considerations
for DispatchwithDisolavedEICASMessaoes
Any monitoredfaultsthat affectairplanedispatchabilitywill be displayedon EICASas a statusor alert
level(warning,caution,advisory)message.Systemfaultsdisplayedat statuslevelor alertlevelshould
be resolvedby MELcomplianceor maintenance
actionpriorto enginestart.Afterenginestart,EICAS
alert messagesare the primarymeans of alertingthe crew to non-normalconditionsor improper
configuration.
of the appropriatenon-normal
Displayof any alert messagerequiresaccomplishment
procedureby the crew. Upon completionof the procedureand priorto takeotf,the operator'sMEL
should be consultedto determinetf relief is availablefor continuedoperationwith systemfeults
displayedat the alertlevel(warning,caution,advisory).
Dispatchcapabilitywith an invalidEICASmessagedependson the messagelevel. Dispatchwith
invalidstatuslevelmessages
is allowedby MMELitem31S1-4,providedthateitherthe associated
equipmentis verifiedto operatenormallyor the dispatchdeviationsfor the associatedequipmentare
observed.However,thereis no specificitemIn the MMELfor dispatchwith invalidalertlevel(warning,
caution,or advisory)messages,since they are requiredfor inflightcrew awarenessor action as
dispatchis allowed
described
at the beginning
of Section1. Thus,if an alertmessageis displayed,
only if thereis MMELrelieffor the associatedequipmentfaultor failure,and the applicabiedispatch
deviationsare applied.lf system deactivationproceduresresult in an associatedalert message
remalningoff, dispatehmay be acceptableif no inflightalertis neededfor the deactivatedequipment.
placardsor flightlogentriesprovidesufficientcrewawareness.
In mostcases,appropriate
EICASIntraduction 3/3
REV17 MAR10/2007
:IMIEW
Hungarian Airlines
h
,azrEtjve
-78.-
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessageCross ReferenceList
EICASMessaoes
ACARS
ACARS
ACCESSDOORS
AFTCABINTEMP
AFTCARGODET1
AFT CARGODET2
AFT CARGODOOR
Notes
Condition
MELltem
NIA
or ATCmedium
Option Company
priorityuplinkhasbeenreceived.
NIA
CommF Basic Lowpriorityuplinkhas been
recetved.
52-71-1
Advisory Basic Fwdand E/Eaccessdoors
unlatched.
Advisory Basic Aft cabinsupplyducttemperature 21-61-l
greaterthan88' C, or zone
21 -614
21-61-6
eft cabinchannel
temperature
failureor switched
OFF.
-204
26-16-1
Aft cargodetectorloopI
Status
-300
unsatisfectory
testor smoke
detected,
Inhibited
byAFT
CARGOFIREor OVHT
message.
-200/
26-16-1
Aft cargodetectorloop2
Status
-300
unsatisfactory
test or smoke
detected.Inhibitedby AFT
CARGOFIREor OVHT
message.
52-71-1
Aft cargodoornotclosedand
Basic
Caution
locked.Two or moreindividual
Advisory
willcause
dooropenmessages
CARGODOORmessage.
CommE
Basic
Aft cargofire detected.
zo- to- |
AFT CARGOOVHT
Warning
Advisory
Basic
Aft cargooverheatdetected.
?140-1
AFT EQ EXH FAN 1
Status
Basic
21-58-5
AFT EQ EXH FAN2
Status
Basic
AFT EQPTCLG FAN
Status
Basic
AFT FUELX-FEED
Advisory
Basic
Aft equipmentcoolingexhaust
fan I failure.
coolingexhaust
Aftequipment
fan 2 failure.
Aft equipment
coolingexhaust
fansland2failure.
Aft switch/valve
disagreeinhibitsFUELCROSSFEED
advisorymessagewhendual
crossfeedsystemis installed.
AFTCARGOFIRE
Annex1-02-1
21-58-5
21-58-5
28-22-3
REV17
MAR 10/2007
rtMlEV
Hungarian Airlines,fi
.787
.S2rEttrYE
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessageCross ReferenceList
EICASMessaqes
Level
AFT GND EXHVAL
Status
AFT IFE COOLING
Status
AILERONLOCKOUT
Advisory
Status
AIR/GNDDISAGREE
Condition
Notes
MELltem
Aft primaryor backupground
coolingexhaustvalvedisagree
position.
withcommanded
N/A
Aft coolingsystemfan failure,
actualsmokedetected,IFEcard
failure,or inboardshutoffvalve
failedclosed.
21-58-13
Basic
Aileronlockoutfailure.
tt- | t-z
Basic
SystemI and system2 air/ground
None
Prov'n
disagree.
AIR/GNDSYS
ALTCALLOUT
ALTCALLOUTS
ALT DISAGREE
ALTITUDE
ALERT
ALTNANTISKID
Annex 1-02-2
SystemI or system2 airlground
logicfailsto "aif' whileon
ground(below80 KCAS),or the
mainbatterybus is not powered
causingthe lossof systeml. lf an
RTOis required,
or uponlanding,
the followingstoppingsystems
Thrust
willbe inoperative:
AutoSDeedbrake
Reversers:
Autobrakes;
and
deployment;
groundspoilerposition
for
soeedbrakes.
Advisory Option Groundproximitywarning
comouterdetectsthe lossof the
automaticaltitudecallout
function.
Lossof EnhancedGPWSaltitude
Advisory Basic
calloutsfunction.
Altitudedifferenceof 200 feet
betweencaptain'sand first
officer'sair datasources.
Inhibitedbelow400 feet radio
altitudeor if samesourceis
selected.
Deviationfromselectedaltitude
Caution
by 300feet.
Antiskidsystemdetectsfaultin
alternatesystem.
Advisory Basic
None
3446-1
3446-1
None
34-16-1
3242-1
3242-?
REV17
MAR'10/2007
IVUaEV
Hungarian eir1nes,fi
.zarEt/vaF
.747
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessageCross ReferenceList
EICASMessaqes
Level
ANTISKID
Antiskidsystemdetectsfaultin
normalsystem(oralternate,if
selected).
Parkingbrakevalveclosedwith
Advisory Basic
parkingbrakereleased,or lossof
oowerto all fourantiskid
channels.
or ootionalantiskid
switchoositioned
OFF- inhibits
message,
ANTISKID
advisory
Option APU batterychargerfailurewith
Status
90-minutestandbysystemby rightAC busoff.
inhibited
at 4
Advisory Option APU batterydischarging
go-minute
ampsor morewith
standbysystem.
Status
Option APU batteryis not paralleledwith
mainbatteryfor standbypower
with90-minute
whencommanded
standbysystem.
ANTISKID
OFF
APUBATCHGR
APUBATDISCH
APU BAT NO STBY
Notes
Condition
Advisory Basic
APUbleedvalvenotin
position.
commanded
APU bottlelow pressure.
APU BLEEDVAL
Advisory Basic
APU BTL
Advisory Basic
APUBTLI
Advisory Option APU bottleI low pressure.
MELltem
32-42-1
3242-1
3244-2
24-31-2
24-3'l-1
24-31-1
36-1'14
26-20-1
26-22-1
to-Lv-
|
26-22-1
26-20-1
26-22-1
49-15-1
APUBTL2
Advisory Option APU bottle2 low pressure.
APUDOOR
Status
APU FAULT
Advisory Basic
faultshutdown.
APUautomatic
49-11-1
APUFIRE
Warning Basic
APUfire detectedin bothloops.
26-15-1
APUFIRELPI
Status
APUflre loop 1 fire or fault
by APUFIRE
output- inhibited
26-15-1
APU FIRE LP 2
Annex1-02-3
Status
Basic
Basic
APU doordisagreewith selected
position.
message.
APUfire loop2 fire or fault
byAPUFIRE
output- inhibited
message.
26-15-1
REV17
MAR10/2007
.*MIEW
Hungarian Airlines
fi
.GUZr,EttvaF
.7aF?
LIST
MINIMUM
EQUIPMENT
Annex{
EICASMessageCross ReferenceList
EIGASMessages
EICASMessaoes
Level
Notes
APUFUELVAL
Advisory Basic
APUGENOFF
Advisory Basic
APUISLNVAL
Status
Basic
APUOILQTY
Status
Basic
CommE
ATCFAULT
ATT DISAGREE
ATT FAIL
AUTOSPEEDBRAKE
AUTOBRAKES
AUTOPILOT
Condition
APUfuelvalvedisagreeswiththe
commanded
Dosition.
generator
auxiliarypower
APU
breaker(APB)openwithAPU
runningand externalpower
(EPC)openor APU
contactor
generatorcontrolswitchoff.
APU fuelisolationvalve
withcommanded
disagrees
position.
APUoil quantitylow levelswitch
detects30 hoursruntime
withAPUrunning,
or
remaining
APUoilquantity
optional
readsADD.
indication
Ootion ATCuplinkhas beenreceived.
Air trafficcontroltransponder
fault.
comparatorunit
Caution Option Instrument
sensesleftand rightattitude
disagreement-CAA-required
message.
Advisory Prov'n Instrumentcomparatorunit
Ootion sensesinvalidattitudedata.
Advisory Basic Autospeedbrakesystemdetects
fault.
Advisory Basic Autobrakesdisarmedor
inooerative.
Caution Basic Lossof ADC,FMC,stabilizer
trim,ILSor RA inputsto active
autopilot.
Advisory
Basic
MELltem
28-25-2
24-OO'2
28-25-3
49-94-1
N/A
34-53-1
34-21-1
34-22-3
34-22-5
34-?5-1
27-62-1
324?4
22-10'1
34-31-1
34-33-1
34-61-1
DISC
AUTOPILOT
Warning
Basic
Lossof all engagedautopilots.
?2-10-1
AUTOTHROT
DISC
Caution
Basic
Manualor automatic
or
of autothrottle,
disengagement
power
from
remove
failureto
servo.
autothrottle
22-30-1
Advisory
Basic
BATTERYOFF
Annex1-024
Batteryswitchoff.
N/A
REV17
MAR10/2007
Hungarian Airlines
ttMlEV
fi
.7Ez
.AaTEtt'Ye
LIST
EQUIPMENT
MINIMUM
Annex I
EICASMessages
EICASMessaqes
EICASMessageGross ReferenceList
Level
BODYDUCTLEAK
Caution
BODYDUCTLP I
Status
BODYDUCTLP2
Status
BRAKESOURCE
BULKCARGODOOR
BULKCARGOFAN
Advisory
Advisory
Status
Notes
Condition
DuctleakbetweenAPUand
centerisolation
valve.
Option Centerductleak loop1 overheat
or faultcondition.
Option Centerductleak looo2 overheat
Basic
Basic
or faultcondition.
Hydraulicbrakepressuresupplied
by accumulator
only.
Basic Bulkcargodoorunlatched- two
or morecargodoormessageswill
causeCARGODOORSadvisory
message,
Option Bulkcargofan failure- fan
messagesinhibitedwhen
respectivebus unpowered.
Option Bulkcargounderfloor
greaterthan32"C
temperature
(90'F)andbulkcargoflow
controlvalvefaalsto close.
Prov'n CenterADIRUPitotHeatpower
or continuitylossor incorrect
powerlevel
PW4,
fault.
CF6F, CenterAir Dataself-detected
RR
Centerbleedisolationvalvenot in
Basic
position.
commanded
BULKCARGOOVHT
Advisory
C ADIRUPITOT
Advisory
C AIR DATA
Advisory
C BLDISLNVAL
Advisory
C DEM HYD OVHT
Advisory Basic Centerair-drivenpumpoverheat.
Advisory Prov'n CenterGLShasfailed.
CGLS
C HYDI OVHT
Advisory
Basic
CHYDzOVHT
Advisory
Basic
Annex1-02-5
CenterelectricoumoI
exceeds225"F.
temperature
Centerelectricpump2
temoerature
exceeds225"F.
MELltem
26-18'1
26-18-1
26-18-1
3241-2
52-71-1
2140-1
2140-1
None
34-26-1
36.11-7
29-32-1
34$0-3
None
29-1 1-2
zJ-J1-
|
REV17
MAR'10/2007
Hungarian Airlines
rtMlEV
fi
.7Az
,?arEtllYG
EQUIPMENT
LIST
MINIMUM
Annex I
EIGASMessages
EICASMessageCross RefelenceList
Condition
MELltem
EICASMessaoes
Level
Notes
C HYDDEMPUMP
Advisory
Centerair-drivenpumpoutput
pressurelow- inhibitedby C
HYDSYSPRESScaution
message.
Prov'n CenterADIRUPitotHeatpower
or continuitylossor incorrect
powerlevel.
generator
option Centerhydraulic
powered- memorylatchedin air
only.
Option Centerhydraulicgeneratorsupply
valvenotfullyclosed.
Basic
CenterelectricalpumpI output
pressure
low- inhibited
by C
HYDSYSPRESScaution
message.
Basic Centerelectricalpump2 output
pressure
low- inhibited
by C
HYDSYSPRESScaution
message,
Basic Centerhydraulicreservoirlow
quantity.
Basic Centerhydraulicpressurebelow
2800psi with bothengines
runnmg.
Basic Centersystempressurelow.
29-11-3
29-31-2
C H Y D D E MS P D S N S R
Status
CHYDGENON
Status
C HYDGENVAL
Status
C HYDPRIMI
Advisory
C H Y D P R I M2
Advisory
C HYDQTY
Advisory
Basic
None
N/A
24-25-1
24-25-2
None
29-11-2
29-31-2
29-33-1
29-33-2
29-11-3
C HYD SYS MAINT
Status
C HYDSYSPRESS
Caution
CILS
Basic
CenterILShasfailed.
34-31-1
C IRSDCFAIL
Advisory
Advisory
Basic
34-21-1
C IRSFAULT
Advisory
Baric
Centerinertialreferencesystem
DCfailure.
Centerinertialreferencesystem
C IRSON DC
Advisory
CMLS
C TAILHYDVAL
Advisory
Advisory
Annex1-02-6
fault.
Basic Centerine ial referencesystem
on DC power.
Prov'n CenterMLShasfailed.
flightcontroltail
Basic Centerhydraulic
by FLT
valveclosed inhibited
message.
CONTVALSadvisory
:
29-11-2
29-11-3
34'21:l
34-?1-1
None
27-03-1
REV1i
,
MAR10/200
:tMlEW
Hungarian Anfines
4
,?zrEt'yaF
.7e?
LIST
MINIMUM
EQUIPMENT
.i:'
Annex 1
EICASMessages
EICASMessageCross ReferenceLiil
EICASMessaqes
Level
C WING HYDVAL
Advisory
Basic
CABINALERT
UOMME
Basic
CABINALTAUTOI
Notes
Basic
Condition
MELltem
Centerhydraulicflightcontrol
wingvalveclosed-inhibitedby
FLTCONTVALSadvisory
message.
Alertcall hasbeenreceivedover
cabininterohone.
27-O3-1
Automaticpressurization
failure.
controllerI self-detected
Automaticoressurization
failure.
controller2 self-detected
21-31-1
None
N/A
21-31-1
CABINALT AUTO2
Status
Basic
CABINALTITUDE
Warning
Basic
above10,000feet.
Cabinaltitude
CABINAUTOJNOP
Caution
Basic
CABINCALL
CommE
Basic
21-31-1
Lossof #1 and#2 automatic
pressurization
or
controllers,
manualselected,
cellhasbeenreceived NIA
Interphone
frompassengercabin.
Status
Basic
CAPT PJTOT
Advisory
Basic
CAPTPVD
Advisory
Option
Status
Option
CARGOA/C CONT
Advisory
option
CARGOA/C CONT
Status
Option
CARGOA/C TEMP
Status
Option
CAPT INSTRXFER
CAPTSTBYINV
Annex1-02-7
instrument
bus
Captain's
withleft mainbusstill
transferred
powered.
mainpitotheaterpower
Captain's
loss,or incorect
or continuity
powerlevel.
paravisual
display
Captain's
(PVD)systemfault.
Ceptain'sstandbyinverterselfdetectedfault.
Packflowcargoair conditioning
(PFCAC)controllerself-detected
fault- provisionsfor firvdcargo
conditioning
system.
Lossof datafromcargoA/C
controller- orovisionsfor fwd
system.
cargoconditioning
Forwardcargosupplyduct
>88'C - provisions
temperature
for fwd cargoconditioning
system.
None
30-31-1
30-31-5
NIA
None
21-28-1
21-28-1
21'28-1
REV17
7
MAR10/200
.ttU,EV
Hungarian Airlines
d
.GrzrEttYZF
.7Ez
LIST
EQUIPMENT
MINIMUM
":'
Annex{
EICAS Message Cross Referencc List
EICASMessages
EICASMessaoes
CARGOBTLI
Level
Notes
Advisory Basic
Condition
CargobottleI low pressure.
MELltem
26-20-1
z0-ao- |
CARGOBTL2
Advisory Basic
Cargobottle2 low pressure.
CARGODETAIR
Status Basic
CARGODOORS
Advisory Basic
CARGOEXH FAN
Status Option
CARGOEXHVALVE
Status Option
CARGOTRIM AIR
Status Option
CGOFLOOROVHT
Advisory Option
of
Lowpressuredownstream
forwardor aft cargosmoke
detectorblower.
Two or moredoorsnotclosedand
locked.
Forwardcargoexhaustfan failure
- provisions
for fwd cargo
system.
conditioning
Forwardcargoexhaustvalve
withcommanded
disagree
position- provisions
for fwd
system.
cargoconditioning
FoMardcargotrim/heatshutoff
valvedisagreewithcommanded
position- provisionsfor fwd
system.
cargoconditioning
>32'C
Underfloortemperature
andfoMardcargoheatflow
controlvalvefailsto closeprovisionsfor fwd cargo
conditioning
system.
26-20-1
26-23-1
26-14-1
26-16-1
52-71-1
21-28-1
21-28'1
21-28-1
21-28-1
E/EACCESSDOOR
Advisory Basic
E/E baydoorunlatched- bothgE
and forwardaccessdoorsopen
willcauseACCESSDOORS
advisorymessage.
EECCONFIG
Status
EICASCONTPNL
Advisory -200/
-300
Leffand rightEECconfiguration 73-21-1
codesdisagree.
3141-1
EICASdisplayselectcontrol
panelfault.
Annex1-02-8
80c2
52-71-1
REV17
MAR10/2007
Hungarian Airlinesh
ttElEV
.7A.7
.EarEtwAF
LIST
MINIMUM
EQUIPMENT
Annex I
EICASMessages
EICASMessaaes
EICASMessageCross ReferenceList
Level
Notes
-200/
-300
EICASDISAGREE
Status
EICASDISPLAY
/
Advisory -200
-300
EICASSCC
Status
EICASSCC//F
EICASSOFTWARE
Status
ELECFILTER
Status
ELEVFEEL
Status
ELTON
Advisory
EMERDOORS
Advisory
EMERLIGHTS
Advisory
-200
/
-300
Condition
faultcausingan engine
Computer
parameterdisagreementcode
(betweenleftand rightEICAS
or a computerfault
computers)
effectingthe cautionalerting
-message
willexistuntil
function
faultcodeis clearedfrom EICAS
testpage.
EICASupperor lowerpilots
displayunitfailed,off,or blank
due to computerfault.
card
EICASsignalconsolidation
fault.
self-detected
Lossof datafromsignal
card,or cardnot
consolidation
oowered.
OPC/OPS
lncompatible
MELltem
3141-1
73-31-1
:31-41-1
31-61-4
31-61-5
31-614
31-61-5
None
configuration.
24-51-2
Option Oneor morein-flight
systemvoltage
entertainment
harmonicfiltershavefailed.
Elevatorfeelsystemdetectsfault None
- inhibited
untilall hydraulic
- latchedin
systemspressurized
aironly.
locatortransmifterhas None
Option Emergency
beenactivated,
52-71-1
Two or moreemergencydoors
Basic
unlatched.
lightswitchin OFFor
Emergency
None
ON Dosition.
ENGBTL1
Advisory
Basic
EnginebottleI low pressure
26-20-1
ENGBTL2
Advirory
Basic
Enginebottle2 low pressure
26-20-1
ENGINECONTROLS
Advisory
RR,
CF6F
Bothleftand rightengineshaveCl
faultmessage.
7Z-21-1
Annex1-02-9
REV17
MAR10/2007
;tfrlEV
Hungarian Airlinesfi
.78^.Ea7EtltYG
LIST
MINIMUMEQUIPMENT
Annex I
EICASMessages
EICASMessaqes
EICASMessageCross ReferenceList
Level
Notes
F'OINSTRXFER
Status
Basic
F/O PITOT
Advisory
Basic
F/O PYD
Advisory
Option
FASI/SLO14/
FAIL
Advisory
Prov'n
Option
FD COMMANDFAIL
Advisory
Prov'n
Fl RE/OYHT
SYS
Advisory
Basic
FLAPLD RELIEF
Advisory
Basic
FLAP/SLATELEC
Status
FLAPS
Warning Basic
FLT CaNT VALS
Advisory
FLT DATA ACO
Status
FLT DATAREC
Status
Annex1-02-10
Basic
Basic
Basic
Condition
Firstofficeis instrumentbus
to alternatepower
transferred
sourcewith rightmainbus stiu
powered.
Firstofficer'smainpi tot heat
poweror continuityloss,or
incorrectpowerlevel.
Firstotficer'sparavisualdisplay
systemfault.
Instrument
comparatorunit
sensesinvalidfasvslowcommand
data.
unit
Instrument
comparator
sensesinvalidflightdirector
com manddatia.
systemfailure.
Fireloverheat
MELltem
None
30-31-1
30-31-5
None
22-30-1
34-22-4
s4-13-10
J4-121
26-11-1
26-11-2
26-15-1
26 16-1
27-51-'l
Flapsfail to relieveat proper
airspeedor fail to recover.
None
Flapslatelectronicunitselfdetectedfailure- inhibitedby
standbybusoff.
None
LE andTE flapsnot in takeoff
positionfor a takeoffand takeoff
on eitherenginethrustselected
whentakeoffthrustis deselected,
but
warninglightis extinguished
remains
for
message
10 seconds.
approximately
Twoor moreflightcontrolvalves 27-03-1
ctoseo.
dataacquisition 31-31-1
Flightrecorder
unitfaultwithbothengines
running- latchedin air only.
31-31-'1
offwithboth
Flightrecorder
enginesrunning- latchin aironly.
REV17
MAR10/2007
Hungarian Airlinesfi
llaillEV
.747
EtlvE
.at
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessaoes
EICASMessageCross ReferenceList
Level
Notes
MELltem
Condition
FLTDECKDOOR
Advisory Option Flightdeckdoorunlocked.
52-71-1
FLTDECKHUMID
Advisory
Prov'n Flightdeckhumidifierswitchon
on belowFL210
Option andhumidifier
or off aboveFL210.
Flightdecksupplyduct
Advisory Basic
greaterthan88'C
temperature
(190'F),or zonetemperature
flightdeckchannelfailureor
switchedoff.
Advisory -2001 LandR FlightDeckWindowsare
-300
open.
Status
Option Flightdeckcrewrestsmoke
evacuationvalvenot in
position.
commanded
N/A
FLT DECKTEMP
FLTDKWINDOWS
FLT RESTSMKVAL
CommE
FWDACCESSDOOR
Advisory
FWD CABINTEMP
Advisory
FWDCARGOA/C
Advisory
FWD CARGODET 1
Status
Annex 1-02-1'1
N/A
None
Option Flightdeckcrewrestshutoff
position.
valvenotin commanded
FLTREST
SOV
FMC
21$1-2
21-614
21-61€
Basic
Basic
AOCuplinkhasbeenreceived.
N/A
FoMardaccessdoorunlatchedbothE/Ebayand foMarddoors
openwillcauseACCESS
message.
DOORSadvisory
Forwardcabinsupplyduct
greaterthan88'C
temperature
(190'F);or zonetemperature
fwd
cabinchannelfailureor switched
off.
52-71:l
Option Self{etectedfaultin auxiliary
or
zonetemDselector/controller
foMardcargoconditioning
shutoffvalvedoesnot openafter
for fwd
20 seconds- provisions
cargoconditioning
system.
-2001 FoMardcargodetectorloop1
-300
unsatisfactory
testor smoke
detected- inhibitedby FWD
CARGOFIREor OVHT
message.
21-61-1
21-614
21-61-6
21-28-1
26-16-1
REV17
MAR10/2007
tta4lEV Hungarian Airlinesfi
.7Ez
.aZ7EtlUE
EQUIPMENT
LIST
MINIMUM
Annex I
EICASMessages
EICASMessaqes
FWD CARGODET2
FWDCARGODOOR
EICASMessageCross ReferenceList
Level
Notes
Status
-2001
-300
Advisory
FWDCARGODOOR
Caution
FWDCARGOFAN
Status
FWDCARGOFIRE
Warning
FWDCARGOOYHT
Advisory
FWD CGO BACKUP
Advisory
FWD EQ EXH FAN
Status
FWDEQSUPFANI
Status
FWD EQ SUP FAN2
Status
Annex1-02-12
Basic
Condition
FoMardcargodetectorloop2
testor smoke
unsatisfactory
detected- inhibitedby FWD
CARGOFIREor OVHT
message.
FoMardcargodoornotcloted
and locked.
Option Largeforwardcargodoornot
closedand locked.
Option FoMardcargoventfan feilureprovisionsfor forwardcargo
system.
conditioning
flre
Forwardcargocompartment
Basic
detected.
Basic Forwardcargounderfloor
>32"C(90'F)and
temperature
iwd cargoheatflowcontrolvalve
failsto close.
Option Forwardcargofire bottlesnot
armedw/FWDcargoselectorin
AUTOand FWDcargoAJCnot
(after30 minon gnd)
inhibited
moreof thefollowing:
one
or
and
cargoducttemp>88'C,
temp
compartmenVunderfloor
>32"C,or FWDcargotrimmod
valvefailsto closeafter60 sec,
FWDtrim/heatshutotfvalve
disagreesafter20 sec,or FWD
sensor
cargocompartmenuduct
fault.
fan I in zoneB hasfailed,
Basic Forwardequipmentexhaustfan
inhibited
failure- fan messages
whenrespectivebusunpowered
cooling
Basic FoMardequipment
supplyfen I failure.
cooling
FoMardequipment
Basic
supplyfan2 failure.
MELltem
26-16-1
52-71-1
21-28-1
26-16-1
2140-1
2140-2
21-28-1
21-584
21-58-3
21-58-3
REV17
MAR10/20C7
ztMlEW
Hungarian Airlines
fi
,aa}EtlYe
.7Ez
LIST
EQUIPMENT
MINIMUM
".'
Annex I
EICASMessages
EICASMessaoes
EICAS Message Cross Reference List
Level
Notes
Condition
MELltem
FWDEOPTCOOLING
Caution
Basic
No coolingair flowdetected.
21-58-1
21-58-2
21-58-3
21-58-4
FWDEOPTOVHT
Advlsory
Basic
21-58-1
21-58-2
21-58-3
21-584
FWD EQPTSMOKE
Advisory
Basic
Lowflowsensedin flightdeckor
coolingduct,or
EiEcompartment
temperature
at fan outlet
supply
greaterthan55"C(systeminhibits
for 5
LOWFLOWOVERHEAT
minuteswhenmodeswitched
fromAUTOto STBY).
Smokein forwardequipment
coolingexhaustducts.
FoMardequipment
supplyor
exhaustvalvesdisagreewiththe
commandedposition.
FWD EQPT VAL
Advisory
Basic
FWD FUELX-FEED
Advisory
FWD GND EXHVAL
Status
FWDIFECOOLING
Status
G/SDISAGREE
Advisory
G/SFAIL
Advisory
disagreeFoMardswitch/valve
inhibitsFUELCROSSFEED
message
whendual
advisory
crossfeedsystemis installed.
Option FoMardprimaryor backup
groundcoolingexhaustvalve
disagreewithcommanded
Position.
Option Forwardcoolingsystemfan
failure,actualsmokedetected,
IFEcardfailure,or inboard
shutoffvalvefailedclosed.
unit
Prov'n Instrument
comDarator
Option sensesleftandrightglideslope
disagreement.
comparator
unit
Option Instrument
sensesinvalidglideslopedata.
GEARDISAGREE
Annex1-02-13
Caution
Basic
Basic
SystemsI and 2 bothindicateany
geardisagreeup or nosegearnot
downor bothsideand dragon
eithermaingearnotdown.
21-58-16
21-58-6
21-58-7
21-58-8
21-58-10
21-64-2
28-22-3
21-58-14
21-58-13
34-31-1
None
None
REV17
MAR10/2007
tlanilEW Hungarian Airlines,fi
.787
,eZEtt'YAF
EQUIPMENT
LIST
MINIMUM
Annex1
EICASMessagecross ReferenceList
EICASMec8ages
EICASMessaoes
GEARDOORS
GEARNOT DOWN
GND EXHVALS
GNDPROXBITE
GNDPROXSYS
GPS
GPSFAIL
GROUNDCALL
HOGDISAGREE
HOGt<ntL
HF DATALINK
Annex1-02-14
Level
Notes
Condition
Any landinggeardoornotclosed
and locked(systemI and 2)
exceptfor nosegeardoorswhen
gearis down.
Warning Basic
Eitherthrottleat dle and below
800feet radioaltitudeand any
gearnotdownand lockedor
landingflapsandanygearnot
downand locked.
Advisory Option Bothprimaryand backupfoMard
IFEcoolingsystemand/orboth
primaryand backupaft IFE
coolingsystemand/orforward
air
cargocompartment
systemground
conditioning
exhaustvalvesarefailedopen
(failedto closewhen
commanded).
-2001
Groundproximitysystemfault.
Status
-300
MELltem
None
Advisory Basic
None
21-58-1
21-58-14
3446-1
34-33-1
3446-1
Advisory Basic
Status
BasicGPWSor enhanced
featuresarefailed.
J{
Advisory Option
Advisory -2001
-300
BothleftandrightGPSfailed.
34€0-3
LeftandRightGPSfailure.
34-60-3
call receivedfrom
Interphone
APU remotecontrolpanelon
nosegear.
unit
comparator
Advisory Prov'n Instrument
sensesleftand rjghtheading
disagreement.
unit
comparator
Advisory Prov'n Instrument
sensesinvalidheadingdata.
Advisory Option Failureof datafunctionof leftand
by
rightHF dataradios.Inhibited
DATALINK
advisorymessage
SYS.
CommE
Basic
JJ-
|
N/A
34-21-l
34-22-:i
34-22-5
34-25-'l
23-11-1
REV17
MAR10/2007
tt'AIEV
Hungarian Airlinesfi
.7Ez
.?aTEtttUZF
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessaoes
EICASMessageCross ReferenceList
Level
Notes
Condition
HF DATALINKOFF
CommF
HI FLOWINHIBIT
Status
Option ACARSdetectsHF dataradionot
selectedto datamode.Inhibited
by advisorymessagesHF
andDATALINK
DATALINK
SYS.
-2001 Packhighflowmodeinhibited.
Status
-300
Option Eitherpackon highflowwith
HI FLOWON
bothenginesrunning.
HUDALERT
HUDEXCESSDEY
HUDGUIDANCE
HUD NO AII
HUDNOAIII
H U DN O G N D R O L L
Annex1-02-15
HUDhasa systemfailureor
guidance
during
modeloss/failure
takeotfor a HUDsystemfeilure,
or excessiveperformance
deviation
duringmodeAlllor
takeoffmodeandthe altitudeis <
500ft,and the groundspeedis >
20 kts.
Caution Prov'n Airplane
flightpath,airspeed,
verticalspeedor performance
exceedspredefinedlimitswhile
HUDis engagedin All or Alll
modeapproach.
loss/
Advisory Prov'n Alllor TO modeguidance
in allflight
failure.Displayed
phasesexceptwhenHUDWARN
is present.
Advisory Prov'n Lossof HUDAll guidance
capability.This messageprovides
awarenessthatthe futureuseof
modeis
the HUDAll approach
unavailable.
Advisory Prov'n Lossof HUDAlll guidance
capability.Thismessageprovides
awarenessthatthe futureuseof
modeis
theHUDAlllapproach
unavailable.
Advisory Prov'n HUDdetectsa lossof the ground
capability.
rollguidance
MELltem
N/A
21-25-1
21-51-2
21-25-1
21-51-1
21-51-2
None
None
None
None
None
None
REV17
MAR10/2007
I*MIEV
Hungarian AirlinesA
.787
.a?Et/vaF
LIST
MINIMUM
EQUIPMENT
Annex 1
EICASMessages
EICASMessaoes
EICASMessageCross ReferenceList
LEVEI
Condition
Notes
HUDSYS
Advisory Prov'n
HUDSYS
Status
Prov'n
HUDSystemfailurethatrenders
theHUDunuseable.
Partialor totalHUDSystem
MELltem
None
None
failure.
Option Eitherautomaticice detectorunit
detectsengineicingconditions
witheitherleftor rightengine
anti-iceswitchmanuallyselected
otf (in air only)- for primaryice
detectionsystem.
Option Eitherautomaticice detectorunit
with
detectswingicingconditions
switch
manually
thewinganti-ice
selectedotf (in ak only)- for
primaryice detectionsystem.
Leftandrightengineminimum
!JE
idledisagree.
idle/approach
PW4
RR
Option Any instrumentswitchedto
ALTNsourceon bothcaptain's
andfirstofficer'sinstrument
sourceselectswitches.
30-80-1
ICINGENGINE
Caution
ICINGWING
Advisory
IDLEDISAGREE
Advisory
INSTRSWITCH
Caution
LACBUSOFF
Caution
Basic
LeftAC mainbusunpowered.
None
L AFT EMERDOOR
Advisory
Option
-200i
Basic
-300
Leftaft emergencydoor
unlatched- two or moredoors
openwillcauseEMERDOORS
advisorymessage.
52-71-1
L AFT ENTDOOR
Advisory
Basic
L AFT FUELPUMP
Advisory
LALTNT/R
Advisory
L ANALOGN2
Status
Annex'1-02-16
Leftaft entrydoorunlatched.
Basic Lowfuel pumpoutputpressureinhibited
by L FUELSYSPRESS
cautionmessage.
Option Leftthrustreverseralternate
hydraulicsourcevalvedisagrees
withcommanded
Dosition.
Basic DigitalleftN2 aboveidleand
analogleft N2 lessthan40ol0.
JT9D
30-80-1
73-21-8
34-00-1
34-22-5
52-71-1
28-22-1
78-31-1
REV17
MAR10/2007
rtMlEV
Hungarian Airlinesfi
.aGrE-'UG
.7e,-
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessaqes
L AOAPROBE
EICASMessag€cross ReferenceList
Level
Notes
Advisory
Basic
Condition
30-32-1
Leftangleof attackprobeheat
poweror continuityloss- two or
individual
morewillreDlace
messageswithadvisorymessage
PROBEHEAT.
30-3'1-1
Leftauxiliarypi tot heatpoweror
continuityloss,or inconectpower
level- two or moreprobeheat
failures
willcausePROBEHEAT
message.
advrsory
Ductleakbetweenleftengineand 26-18-1
valve.
isolation
36-11-6
Leftbleedisolationvalvenot in
position,
commanded
L AUX PITOT
Advisory
-2001
-300
L BLD DUCTLEAK
Caution
Basic
L BLDISLNYAL
Advisory
Basic
L BUSISOLATED
Advisory
Basic
L COWLDUCTLEAK
Status
PW4
Leftisolationbustie
locked
or manually
automatically
open,
Leftcowltempswitchon with
CF6F
engineerunning.
L CTRENTDOOR
Advisory
L DATALINK
SYS
Status
L OEM HYD OVHT
Advisory
LDRAGBRACE
Caution
L DUCTLEAKLP 1
Status
L DUCT LEAKLP 2
Status
Annex1-02-'17
Leftcenterentrydoorunlatchedtwo or moreopenleftentrydoors
willcauseL ENTRYDOORS
advisorymessage.
Option Failureof leftACARSmonitor
unitor its EICASinterface.
Basic Leftelectricalpumptemperature
exceeds2250F.
Basic SystemsI and 2 bothindicate
geardisagreeand leftdragbrace
is not locked.
Option Leftduct leakloop 1 overheator
- inhibited
by L
faultcondition
BLDDUCTLEAKOTL STRUT
OCTLEAKcautionmessage.
Option Leftductleakloop2 overheetor
- inhibited
by L
faultcondition
BLDDUCTLEAKoTL STRUT
OCTLEAKcautionmessage.
Basic
MELltem
None
30-21-1
52-71-1
23-22-1
29-32. 1
None
26-14-1
26-18-1
REV17
MAR10/2007
.tvAlEW Hungarian Airlines
d
.7A?
.ezrEttruZF
LIST
MINIMUM
EQUIPMENT
Annex I
EICASMessages
EICASMessageCross ReferenceList
EICASMessages
L EECOFF
L EICASCMPTR
L EMER DOOR
Caution
Status
Advisory
JTgD,
GE
except
CF6F
-2001
-300
Basic
Status
Basic
L ENGANTI-ICE
Advisory
Basic
L ENG BLD OVHT
Advisory
L ENG BLEEDOFF
Advisory
PW4
RR
80C2
Basic
L ENGCONTROL
Advisory
L ENGANALOGN2
Condition
Notes
PW4
CF6F
RR
LeftEECswitchedoff andfull
foMardthrustleverposition
selected.
LeftEICAScomputerfailedor
off.
Leftemergencydoorunlatchedwill
twoor moredoorsunlatched
causeEMERDOORSadvisory
message,
LeftengineanalogN2 is lessthan
40%for morethan3 seconds
whiledigitalN2 is aboveidle.
Leftenginecowlanti-icevalve/
switchdisagreewithengine
runmn9.
Enginebleedair overheat;
pressure
valve(PRV)
regulating
closes.
Leftenginepressure-regulating
shutoffvalveclosedwithengine
runnmg.
LeftEECis in a nodispatch
withcomputed
configuretion
airspeedlessthan80 knotsor
invalid.
MELltem
N/A
3141-'l
52-71-1
77-12-2
30-21-1
30-21-2
None
36-1 1-1
None
IJl(
Status
L ENG EEC
L ENG EEC CI
L ENG EEC MODE
Annex1-02-18
RR
CFOF
Advisory JTgD
GE
except
CF6F
Status
CF6F
PW4
RR
Advisory RR
PW4
CFGF
Left EECis in a no-dispatch
None
configuration.
LeftEECfailureor switchedoff
withenginerunning.
73-21-1
73-21-2
LeftEECfaultwithtime-limited
dispatchconfiguration.
73-21-1
LeftEECchannelcontrolin an
alternatemodewithengine
runnmg.
tJ-zt-l
REV17
MAR10/2007
t|'lAlJiW Hungarian Airlines
fi
.7Ez
.?aFEtlVE
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessages
EICASMessageCross ReferenceList
Level
Notes
Condition
MELltem
Leftengineeleventhstagecooling
valvefailedclosedwithengine
runmng.
Failureof the leftenginein flight.
75-24-2
L ENGESCV
Status
CF6F
L ENG FAIL
Caution
L E N GF I R EL P I
Status
Basic,
Option
Basic
LeftenginefireloopI flreor fault
by L ENGINE
output- inhibited
L ENG FIRELP 2
Status
Basic
L ENG FUELFILT
L ENG FUELVAL
Status, GE
Advisory PW4
RR
Advisory Basic
L ENGFWSOV
L ENGPRV
Caution -200/
-300
80c2
PW4
L ENGREVPOS
Status
L ENGRPIULIM
L ENGSHUTDOWN
L ENG SPEEDCARD
PW4
CF6F
Advisory CF6F
PW4
RR
Caution Basic
FIREwarningmessage.
Leftenginefire loop2 fire or fault
by L ENGINE
output- inhibited
FIREwarningmessage.
pressureacrossleft
Ditferential
enginefuelfilterapproaches
bypass.
None
26-11-1
26-11-1
Leftenginefuelvalvedisagrees
withcommanded
Dosition.
Leftenginefirewallshutotfvalve
closed.
openwhencommanded
73-21-3
valvefailure
regulating
Pressure
in a bleedsystem
resulting
condition,or failure
overpressure
of the PRVto closewhen
commanded.
Leftreverserttatus failurewith
enginerunnrng.
LeftengineNl or N2 is at red line
limit.
36-11-8
Leftenginefire switchpulledor
leftenginefuelcontrolswitchin
CUTOFF.
LeftengineN2/N3speedsensing
None
36-11-9
78-36-3
N/A
None
relayfault.
Annex1-02-19
REV17
MAR10/2007
tlanilEV Hungarian Airlines
fi
.-E.?aTEtjvaF
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessages
EICASMessageCross ReforenceList
Level
Notes
L ENGSTARTER
Advisory Basic
L ENGTAIVALVE
Status
L ENGINE
FIRE
L ENTRYDOORS
Warning Basic
Advisory Basic
L FLTDKWINDOW
Advisory Basic
PW
GE
L FMCFAIL
Advisory Basic
L FUELHEATVAL
Advisory Option
JT9D
L FUELJET PUMP
Advisory Option
L FUELSPARVAL
Advisory Basic
L FUELSYSPRESS
Caution
L FWD EMER DOOR
Advisory Option
-200;
Basic
-300
L FWD ENT DOOR
Advisory Basic
L FWD FUELPUMP
Advisory Basic
Basic
Condition
disagree
Leftstartervalve/switch
- inhibited
by L STARTER
CUTOUTcautionmessage.
of left
Highpressuredownstream
thermalanti-icevalve.
Leftenginefire detected.
Twoor moreleftentrydoors
unlatched.
L FlightDeckWindowis open.
computer
Leftflightmanagement
fault.
Leftenginefuel heatervalve
withcommanded
disagrees
position.
Leftfueljettisonpumplow
pressurewithfueljettisonswitch
in theON position.
Leftsparvalvedisagreeswith
position.
commanded
Bothleftmainpumpsandcenter
tankleftpumplow
auxiliary
pressureand fuelcrossfeedvalve
closed,or allsix pumpslow
pressureor turnedoff.
Leftforwardemergencydoor
unlatched- two or moredoors
openwillcauseEMERDOORS
advisorymessage.
Leftforwardentrydoorunlatched
- two or moredoorsopenwill
causeL ENTRYDOORS
advrsorymessage.
Lowfuel pumpoutputpressure-
MELltem
80-00-1
80-00-2
80-'11'2
30-21-1
None
52-71-1
N/A
34-61-1
73-14-1
28-31..3
52-71-1
52-71-1
28-22-1
inhibited
by L FUELSYSPRESS
cautionmessage.
Annex1-02-20
REV17
MAR10/2007
:tAdlEV Hungarian AirlinesA
'7Ez
,?ZTE,,VE
LIST
EQUIPMENT
MINlMUM
Annex {
EICASMessageg
EICASMessagecross ReferenceList
EICASMessaqes
Level
L FWDWINDOW
Advisory Basic
L GEN DRIVE
Advisory Basic
L G E NO F F
Advisory Basic
(Caution
for
cAA)
L GLS
L GPS
L GPSFAIL
L HF DATALINK
L HYD DEM PUMP
L HYDFUELPR
L HYDGENON
L HYDGENVAL
Notes
MELltem
LeftfoMardwindowheatover
or powerloss- two or
temperature
messages
will
moreindividual
causeWNDOW HEATadvisory
message.
Leftgeneratordrivelow oil
pressureor highoil temperature
withenginerunning.
Leftgeneratorcontrolbreaker
(GCB)openwithenginerunning.
30-41-1
Advisory Prov'n
LeftGLShasfailed.
34-60-3
Advisory Option
LeftGPSor GPSSUlailureor
GPSRF inputfailure.
34-60-3
2440-1
24-00-1
LeftGPSor GPSSUfailureor
GPSRF inputfailure.
Status Option Failureof datafunctionof left HF
by advisory
dataradio.Inhibited
SYS.
messageDATALINK
Leftelectricpumpoutput
Advisory Basic
pressurelow - inhibitedby L
HYDSYSPRESScaution
message.
Advisory Option Lefthydraulicfuelsystemlow
pressure
withenginerunning.
JT9D
Option LefthydraulicAeneratorpowered
Status
- memorylatchedin air only.
34$0-3
generator
supply
Lefthydraulic
valvenotfullyclosed.
pumpoutput
Leftengine-driven
pressure
lowwithenginerunning
- inhibited
by L HYDSYS
PRESScautionmessage.
Lefthydraulicreservoirlow
quantity.
24-25-1
24-25-2
None
Advisory Option
Option
L HYD PRIM PUMP
Advisory Basic
L HYDQTY
Advisory Basic
Annex1-02-21
Condition
23-11-1
None
N/A
29-33-1
zv-5c-a
REV17
MAR10/2007
t'l:MIEW
Hungarian AirlinesA
^azrEt/vaF
.78-
LIST
MINIMUM
ESUIPMENT
Annex I
EICASMessageg
EICASMessaqes
EICASMessageCross ReferenceList
Level
Notes
Basic
L HYDSYSMAINT
Status
L HYDSYSPRESS
Caution Basic
L ICEDETECTOR
Status
Condition
Lefthydraulicpressurebelow
2800psiwithbothengines
runmng.
Leftsystempressurelow.
L IOGFILTER
Option Leftautomaticice detectionunit
self-detected
fault- latchedin air
- for primaryice detectionsystem.
bypass,
Option LeftIOGfilterimpending
L IOGOILTEMP
Status
JT9D
JT9D
L IOGTEMPSENS
Status
JT9D
L IOGVALVE
Status
Basic
LILS
MELltem
None
None
30-80-1
24-00-1
LeftIOGoutlettempabove
by L
ISSaC(311 OF)- inhibited
IOGTEMPSENSstatus
message.
24-00-1
sensor
LeftIDGtemperature
failure(temprisereads>175"C).
LeftIOGcoolingvalvefailure.
75-21-1
Advisory Basic
LeftILShasfailed.
34-31-1
L IRSDC FAIL
Advisory Basic
LeftIRSDC failure.
34-21-1
L IRSFAULT
Advisory Basic
LeftIRSfault.
34-21-1
L IRSON DC
Advisory
Basic
LeftIRSon DC power.
34-21-1
L JETXFRVALVE
Advisory
Option Leftfueljettisontransfervalve
withcommanded
disagrees
positionand fueljettisonswitchis
in theON position.
28-31-3
L MLS
Advisory
Advisory
Prov'n LeftMLShasfailed.
Option LeftenginerunningwithleftNl
JT9D >16%andleftN1/N2mismatch
L N1/N2MISIVIATCH
L O I LF I L T E R
L PACK OFF
Annex1-02-22
Advisory
Status
Advisory
Basic
Basic
detected.
Leftengineoil filterdifferential
pressureapproaches
bypass.
LeftpackswitchedOFFor
compressoroutlettemPerature
exceeds254'C.
None
None
79-35-1
79-35-2
21-51-1
21-51-2
21-51-3
REV17
MAR10/2007
ttU,EV
Hungarian Airlines
#
.aa7Et/ve
-787
LIST
MINIMUM
EQUIPMENT
Annex 1
EICASMessages
EICASMessaqes
EICASMessagecross RefetEnceList
Level
Notes
LPACKTEMP
Advisory Basic
L PRIM HYD OVHT
Advisory Basic
Condition
Leftpackoutlettemperature
exceedsSS'C,orcompressor
exceed8
outlettemperature
254'C,or criticalsystemfailure
detectedby left packcontroller.
Leftprimaryhydraulicpumpcase
MELltem
21-51-1
21-51-2
21-51-3
29-32-1
drainoverheat.
L RECIRFAN
Advisory Basic
tan tailed.
Leftrecifculation
2'l-25-1
L REV INTERLOCK
RR
PW4
CF6F
Advisory Basic
Status
Leftthrustreverserinterlockfails
to blockthrustlevermotion.
78-u-2
L REV ISLNVAL
Status
Leftthrustreverserisolationvalve 78-31-1
by LACBUS
fault- inhibited
OFFcautionmessage.
Option ACARS/leftSATCOMinterface 23-22-1
23-25-1
faifure.
23-25-1
Option Lossof left SATCOMvoice
left
capabilitydue to failurein
SATCOMhighgainsystem.
L SATCOM DATA
Status
L SATCOMHI GAIN
Status
L SATCOMSYSTEM
Status
VOICE
L SATCOM
Advisory Option
L SIDEBRACE
Caution
L SIDEWINDOW
Advisory Easic
L STARTER
CUTOUT
Caution
Annex1-02-23
Option
Basic
Basic
LeftSATCOMsystemfailure.
23-25-1
23-25-1
Lossof leftSATCOMvoice
failure
to
in
left
capability
due
SATCOMhighgainsystem.
Inhibitedby advisorymesseges
SATCOMandSATCOMVOICE.
None
Syst€ms1 and 2 bothindicate
geardisagreeand leftside braceis
notlocked.
3041-1
Leftsidewrndowheatoverpower
30-41-2
or
loss
two
or
temperature
messages
will
moreindividual
causeWINDOWHEATadvisory
message.
80-00-2
Leftenginestartervalveopen
80-11-2
aboveengineRPMatwhich
cutoutshouldoccur.
REV17
MAR10/2007
IIMIEV
Hungarian Airlinesfi
.787
EaTEIJVZF
LIST
MINIMUM
ESUIPMENT
Annex I
EICASMessages
EICASMessaoes
L STRUTOCTLEAK
L STRUTOCT LP 1
L STRUTOCT LP 2
L TAIL HYO YAL
L TAT PROBE
L UTILBUSOFF
L WINGANTI-ICE
EIGASMessageCross ReferenceList
Level
Caution
Notes
Condition
RR
PW4
80c2
Option
closureofthe PRYdue
Automatic
to strutovertemperature.
36-11-8
26-18-1
26-18-1
Leftstrutduct loopI overheator
by L
faultconditioninhibited
STRUTDCTLEAKCEUtiON
message.
26-18-1
Status
Option Leftstrutduct looo2 overheator
- inhibited
by L
faultcondition
STRUTDCTLEAKcaution
message.
27-03-1
Lefthydraulicflightcontroltail
Advisory Basic
valveclosed inhibitedby FLT
CONTYALSmessage.
probe
30-31-2
Advisory Option Lefttotalair temperature
-2001
30-33-1
heaterpoweror continuityloss
-300;
messages
more
individual
twoor
Basic willcausePROBEHEAT
-400
advrsorymessage.
24-51-1
Basic
Leftutilitybusunpoweredwith
Advisory
leftAC mainbuspowered.
Status
Advisory
Leftwinganti-icevalve/switch
disagree.
flightcontrolwing
Lefthydraulic
Basic
valveclosed inhibitedby FLT
CONTVALSmessage.
Basic
Leftwingslidedoorunlatchedtwo or moreopenemergency
doorswillcauseEMERDOORS
advisorymessage.
Leftyawdamperfailure,power
Basic
lossor switchedoff.
Option Smokein lavatory.
Basic
L WING HYDVAL
Advisory
L WING SLIDE
Advisory
L YAW DAMPER
Advisory
LAVATORYSMOKE
Caution
Advisory
LAV/COMPT
SMOKE
Advisory
Option
LDGGEARMONITOR
Status
Basic
LESLATASYM
Caution
Basic
Annex1-02-24
MELltem
30-11-1
30-1 1-2
27-03-1
52-71-1
20-zo-5
Smokein levatory/compartment, 26-26-3
32-61'2
Systemland system2landing
gearpositionindications
disagree.
None
Leadingedgeslat asymmetryor
REV,17
MAR10/2007
:+MIEW Hungarian Airlines
d
.7Ez
.garEtttYZF
LIST
MINIMUM
EQUIPMENT
Annex 1
EICASMessages
EICASMessages
LE SLATDISAGREE
EICASMessageCross ReferenceList
Level
Caution
Condition
Notes
Basic
MELltem
slat loss.
Leadingedgeslatdisagreement None
withselectedposition.
LE SLATSHUTDOWN
Status
LaCDISAGREE
Advisory
LaCFAIL
Advisory
LOWCREWOXYGEN
Advisory
Leading
edgeslatfailure
protectionshutdown- inhibited
by LE SLATASYMcaution
message.
unit
comparator
Prov'n Instrument
right
localizer
Option sensesleft and
disagreement.
comparator
unit
Option lnstrument
data.
sensesinvalidlocalizer
Option Crewoxygenpressureis below
None
34-31-1
34-31-1
35-11-2
5UU OSI.
LOWFUEL
TRIM
MACH/SPD
Advisory
Basic
MAINBATCHGR
Status
Basic
MAINBAT DISCH
Advisory
MID CABINTEMP
Advisory
NORMANTISKID
Status
Annex1-02-25
Advisory
None
Machspeedtrim systemfailure.
Mainbatterychargerfiailure-
None
inhibited
by R AC BUSOFF
cautionor anyHYDGENON
statusmessage.
at 4
Mainbatterydischarging
Basic
ampsor more.
Option Midcabinsupplyduct
-2001 temperature
>88'C,zone
-300;
midcabinchannel
temoerature
Basic failure,or switchedoff_400
Basic Antiskidsystemdetecttfaultin
NOSEA/GDISAGRE
NOSEA/G
SYS
Lowfuelquantityin maintanks
(approximately
4,400lbs).
Basic
normatsyslem.
SystemI and system2 noseair/
groundlogicdisagree.
NoseairlgroundsystemI
ON GROUND,
and
indicates
noseairlgroundsystem2
lN AlR.Inhibited
above
indicates
80 KCAS,and by leftor rightAC
busotf.
None
None
2l -61-1
21-61-4
2151-6
3242-1
None
None
REV17
MAR10/2007
ztadEV
Hungarian Airlines
#
.827Et/ve
.7e7
LIST
EQUIPMENT
MINIMUM
'':
Annex 1
EICASMessages
EICASMessaoes
EICAS Message Cross Reference List
LEVEI
Notes
OVERSPEED
Warning Basic
PARKING
BRAKE
Warning Basic
PARKING
BRAKE
Advisory
Basic
PASSOXYGENLOW
Advisory Option
PASSOXYGENON
Advisory
PILOTRESPONSE
Warning
Caution
Advisory
PRINTER
CommE
PROBEHEAT
CommF
Advisory
Except
767F
Prov'n
Option
Option
Condition
Aircraftspeed(L or R ADC)
VMO/MMO.
exceeds
Parkingbrakeset and takeotf
on eitherengine.
thrustselected
Parkingbrakeset (valveclosed)
(inhibited
on groundfor 767400).
Passengeroxygenpressureis less
than500psi.
serviceunit
OxygenpasEenger
(PSU)latchenergized.
radio
No MCDU,EFIS/EICAS,
panel,
or MCPactivity
control
andno HFA/HFflightdeck
detectedby airline's
transmission
timedelay;or, in
requested
coupledLNAV /NAV cruise
operation,excessivedeviation
fromlateralflightplan,cruise
altitude,predictedthrustor target
airspeedis detected;or reaching
TODand no crewactivityfor
timedelay.
airline-requested
Datalinkprintermessageis
pnnrng.
Twoor moreprobeheatfailuresprobeheatfailure
individual
messagesare suppressed.
MELltem
None
N/A
3244-3
35-21-1
35'21-1
None
N/A
30-31-2
30-31-5
30-32-1
30-33-1
30-34-1
R AC BUSOFF
Caution
Basic
RightACmainbusunpowered.
None
RAFT EMERDOOR
Advisory
Option
-200:
Basic
-300
52-71-1
RAFTENT DOOR
Advisory
Basic
Rightaft emergencydoor
unlatched- two or moredoors
openwillcauseEMERDOORS
message.
Rightaftentrydoorunlatched
two or moreentrydoorsopenwi
causeR ENTRYDOORS
advrsorymessage.
Annex1-02-26
5?-71-1
REV17
MAR10/2007
t+UaEV
Hungarian Airlines
fi
.eaTEttuG
.7e7
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessages
EICASMessageCrose ReferenceList
Level
Notes
Condition
R AFT FUELPUMP
Advisory
RANALOG
N2
Status
RALTNTIR
Advisory
RAOAPROBE
Advisory
RAUXPITOT
Advisory
R BLD DUCTLEAK
Caution
R BLDISLNVAL
Advisory
Lowfuel pumpoutputpressureinhibited
by R FUELSYSPRESS
cautron
messa9e.
Basic DigitalrightN2 aboveidleand
JT9D
analogrightN2 lessthan40%
alternate
Option Rightthrustreverser
hydraulic
sourcevalvedisagrees
withcommanded
Dosition.
Rightangleof attackprobeheat
Basic
poweror continuityloss- two or
moreprobeheatfailureswill
causePROBEHEATadvisory
message.
-200/
Rightauxiliarypitotheatpower
-300
or continuitylossor incorrect
powerlevel- two or moreprobe
heatfailureswillcausePROBE
HEATadvisorymessage.
Basic Ductleakbetweenrightengine
valve.
andisolation
valvenotin
Basic Rightbleedisolation
Basic
commanded
oosition.
isolation
bustie
Right
locked
or manually
automatically
ooen.
switch
Rightcowltemperature
MELltem
28-22-1
77-12-2
78-31-'l
30-32-1
30-3'1-1
26-18-1
36-11-6
None
R BUSISOLATED
Advisory
Basic
R COWLDUCTIEAK
Status
CF6F
RCOWLOVHT
Caution
PW4
RR
ONwithenginerunning.
230'C
Rightcowltemperature>
(446'F).
R CTRENTDOOR
Advisory
Basic
R DATALINKSYS
Status
Option
R OEM HYD OVHT
Advisory
Basic
Rightcenterentrydoorunlatched 52-71-1
- twoor moreopenrightdoors
willcauseR ENTRYDOORS
message.
advisory
23-22-1
Failureof rightACARSmonitor
interface.
unitor its EICAS
29-32-1
Rightelectricpumptemperature
30-21-1
30-2'1-3
exceeds225'F.
Annex1-02-27
REV17
MAR10/2007
/VAIEV
Hungarian Airlinesfi
.azrEttUe
.78,7
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessag€Cross ReferenceList
LCVEI
R DRAGBRACE
None
Systemsland 2 bothindicate
geardisagree
andrightdragbrace
is notlocked,
Status
Option Rightduct leakloopI overheator 26-18-1
- inhibited
by R
faultcondition
BLDDUCTLEAKoTR STRUT
DCTLEAKcautionmessage.
or 26-18-1
Status
Option Rightductleakloop2 overheat
- inhibited
faultcondition
by R
BLDDUCTLEAKOTR STRUT
DCTLEAKcautionmessage.
N/A
JT9D, RightEECswitchedoff and full
position
f,orward
thrustlever
\Jtr
excepr selected.
CF6F
-200t
failedor
31-41-1
RightEICAScomputer
Status
-300
oTT.
- 52-71-1
doorunlatched
Advisory Basic Rightemergency
will
twoor moredoorsunlatched
DOORS
advisory
causeEMER
message.
77-12-2
Status
RightengineanalogN2 is less
than40%for morethan3 seconds
whale
digitalN2 is aboveidle.
R DUCTLEAKLP I
R DUCTLEAKLP 2
R EEC OFF
R EICASCMPTR
R EMERDOOR
R ENGANALOGN2
Caution
R ENG ANTI-ICE
Advisory
R ENG BLD OYHT
Advisory
R ENG BLEEDOFF
Advisory
R ENG BLEEDYAL
Caution
Annex1-02-28
Notes
Condition
MELltem
EICASMessaqes
Basic
80C2
RR
PW4
Basic
8oN2
JT9D
30-21-1
Rightenginecowlanti-icevalve/
30-21-2
switchdisagreewithengine
runnmg.
Enginebleedairoverheat;
pressure
valve(PRY)
regulating
closes.
36-11-1
Rightenginepressure-regulating
shutoffvalveclosedwithengine
running.
bleed 36-11-2
Rightenginehighpressure
valveopenwhencommanded
closed.
REV17
MAR10/2007
aVUIEV Hungarian Airlinesd
.78.?Z}Et/VZF
LIST
MINIMUM
EQUIPMENT
Annex 1
EICASMessages
EIGASMessageCross ReferenceLi6t
Condition
MELltem
EICASMessages
Level
R ENGCONTROL
None
RightEECis rna no-dispatch
withcomputed
configuration
airsoeedlessthan80 knotsor
RR
invalid.
OR
RightEEC is in a no-dispatch
None
Status
CF6F
configuration.
73-21-1
Advisory JT9D, RightEECfailureor switchedoff
I J-t t-z
withenginerunning.
GE
except
CF6F
Status
CF6F RightEECfaultwithtime-limited 73-21-1
PW4
dispatchconfiguration.
RR
73-21-1
RightEECchennelcontrolin an
Advisory RR
PW4
alternatemode.
CF6F
75-24-2
Status CF6F Rightengineeleventhstage
coolingvalvefailure.
None
Caution Option Failureof the rightenginein
Advisory
Notes
PW4
UTOT
R ENG EEC
R ENG EECC1
R ENG EEC MODE
RENGESCV
R ENGFAIL
R ENGFIRELP I
Basic
R ENG FIRE LP 2
Basic
R ENGFUELFILT
R ENG FUELVAL
RENGHPSOV
flight.
26-11-1
Rightenginefire loopI fire or
by R
faultoutput inhibited
ENGINEFIREwarningmessage.
26-11-1
Rightenginefireloop2 fireor
by R
faultoutput inhibited
ENGINEFIREwarningmessage.
pressureacrossright
Dilferential
enginefuelfilterapproaches
bvpass.
Advisory GERR
Advisory Basic Rightenginefuelvalvedisagrees 73-21-3
withcommanded
Dosition.
-200
bleed 36-11'2
/
Rightenginehighpressure
Caution
-300
valveopenwhencommanded
PW4
closed.
RR
D(JUZ
Annex1-02-29
REV17
MAR10/2007
/VAIEV Hungarian Airlinesfi
747
.AaEt'YZF
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessages
R ENGIGNITOR
1
EICASMessageCross ReferenceList
LCVEI
Status
R ENGIGNITOR2
Noter
CF6F
RR
CF6F
RR
Condition
Rightenginefailsto lightusing
by R ENG
ignitorf - inhibited
FUELVALadvisory
message.
Rightenginefailsto lightusing
ignitor2 - inhibited
by R ENG
MELltem
74-00-1
74-00-1
FUELVALadvisory
message.
R ENGLIM PROT
Caution
RENGO/SGOV
Status
RENGOHLPI
RR
PW4
CF6F
CF6F
PW
GE
RENGOHLP2
Status
GE
PW
R ENGOILPRESS
Advisory
(Caution
for
cAA)
Basic
RENGOVHT
Caution
PW
RENGPRV
Caution
R ENGREVPOS
pas
RENGREV
RENGRPMLIM
Status
GE
-2OOl
-300
80C2
PW4
hasfailedits initialization
test.
Rightenginenacelleoverheat
detectorloop1 overheator fault
by R ENG
output- inhibited
OVHTcautionmessage.
Rightenginenacelleoverheat
detectorloop2 overheator fault
output- inhibited
by R ENG
OVHTceutionmessage.
below
Rightengineoil pressure
limitwithenginerunning.
Rightenginestrutor nacelle
overtemperature.
Pressureregulatingvalvefailure
resultingin a bleedsystem
condition,or failure
overpressure
of the PRYto closewhen
commanded.
Rightreverserstatusfailurewith
PW4
CF6F englnerunnlng.
Rightreverserstatusfailurewith
RR
deleted englnerunmng.
Advisory CF6F
RR
PW4
Annex1-02-30
Thrustsettingexceedsmaximum
ratingwithenginecontrolset to
ALTNmode.
governor
Rightengineoverspeed
RightengineNl or N2 is at red
linelimit.
None
73-21-7
26-11-2
26-11-2
79-33-1
None
36-11-8
78-36-3
78-36-3
N/A
REV17
MAR10/2007
ttMlEW Hungarian Airlinesfi
.7Ez
.SZE''VZF
EQUIPMENT
LIST
MINIMUM
Annex 1
EICASMessages
EICASMessageCross ReferenceList
EICASMessaoes
R ENGSHUTDOWN
Notes
Caution
Basic
R ENGSPEEDCARD
R ENGSTARTER
Advisory Basic
R ENGTAIVALVE
Status
(JE
Condition
MELltem
Rightenginetireswitchpulledor
rightenginefuelcontrolswitchin
CUTOFF,
RightengineN2/N3speed
sensingrelayfault.
Rightstartervalve/switch
- inhibited
disagree
by R
STARTERCUTOUTcaution
message.
Highpressure
downstream
of
valve.
rightthermalanti-ice
None
.'
None
80-00-1
80-00-2
80-11-2
30-21-1
R ENGINE
FIRE
Warning Basic
Rightenginefiredetected.
None
R ENTRYDOORS
Advisory Basic
Twoor morerightentrydoors
unlatched.
52-71-1
R FLT OK WINDOW
Advisory Basic
R FlightDeckWindowis open.
None
R FMCFAIL
Advisory Basic
R FUELHEATVAL
R FUELJET PUMP
R FUELSPARVAL
R FUELSYSPRESS
R FWD EMERDOOR
Annex1-02-31
Rightflightmanagement
computerfault.
Advisory Option Rightenginefuelheatervalve
JT9D
disagrees
withcommanded
position,
Advisory Option Rightfueliettisonpumplow
pressurewithfueljettisonswitch
in theON oosition.
Advisory Basic
Rightsparvalvedisagreeswith
commandedposition.
Bothrightmainpumpsandcenter
auxiliary
tankrightpumplow
oressurewithcrossfeedclosed.or
or
allsix pumpslowpressure
turnedoff.
Advisory Option
-200;
Basic
-300
RightfoMardemergencydoor
unlatched- two or more
emergencydoorsopenwillcause
EMERDOORSadvisory
messaoe.
34-61-1
73-14-1
28-31-3
None
None
52-71-1
REV17
MAR10/20C7
.IIMIEW
Hungarian Airlines
B
.78.AA}Et/YZF
LIST
EQUIPMENT
MINIMUM
Annex I
EICASMessages
EICASMessaoes
EICASMessageCross ReferenceList
Level
Notes
R FWDENTDOOR
Advisory Basic
R FWD FUELPUMP
Advisory Basic
R FWDWINDOW
Advisory Basic
R GENDRIvE
Advisory Basic
R G E NO F F
Advisory Basic
(Caution
for
RGLS
RGPS
R GPSFAIL
R HF DATALINK
R HYDOEM PUMP
R HYD FUELPR
RHYDGENON
RHYDGENVAL
Condition
Rightforwardentrydoor
unlatched- two or moredoors
openwillcauseR ENTRY
DOORSadvisorymessage.
Lowfuelpumpoutletpressureinhibited
by R FUELSYSPRESS
cautionmessage.
Rightforwardwindowheatover
or powerloss- two or
temperature
messages
will
moreindividual
causeWINDOWHEATmessage.
Rightgeneratordrivelow oil
pressure
or highoiltemperature
withenginerunning.
Rightgeneratorcontrolbreaker
(GCB)openwithenginerunning.
cM)
Advisory Prov'n RightGLShasfailed.
Advisory Option RightGPSor GPSSUfailureor
GPSRF inoutfailure.
Advisory Option RightGPSor GPSSUfailureor
GPSRF inputfailure.
Status
Option Failureof datafunctionof right
by
HF dataradio.Inhibited
advisory
messageDATALINK
SYS.
Advisory Basic Rightelectricpumpoutput
pressure
bYR
low- inhibited
HYDSYSPRESScaution
message.
fuelsystemlow
Advisory Option Righthydraulic
pressure
withenginerunning.
JT9D
generator
Status
Option Righthydraulic
powered- memorylatchedin air
only'
Status
Option Righthydraulicgeneratorsupply
valvenotfullvclosed.
Annex1-02-32
MELltem
52-71-1
28-22-1
30-41-1
24-00-1
24-00-l
34€0-3
34€0-3
3460-3
23'11-1
None
None
None
24-25-1
24-25-2
REV17
MAR10/2007
z?MIEV
Hungarian Airlines
fi
,az7EtivzF
.?a?
LIST
EQUIPMENT
MINIMUM
Annex I
EICASMessages
EICASMessaqes
EICASMessageCross ReferenceLiat
Level
Notes
R HYD PRIMPUMP
Advisory
Basic
RHYDQTY
Advisory
Basrc
R HYDSYS MAINT
Condition
Rightengineprimarypump
outputpressurelowwithengine
by R HYD
running- inhibited
SYSPRESScautionmessage.
Righthydraulicreservoirlow
quantity.
pressure
below
Righthydraulic
2800psiwithbothengines
runnig.
Rightsystempressurelow.
MELltem
None
29-33-1
ZJ-JJ.Z
None
None
R HYDSYSPRESS
Caution
Basic
R ICEDETECTOR
Status
Option
Rightautomaticice detectionunit
fault- latchedin air
self-detected
- for primaryice detectionsystern
30-80-'1
R IOG FILTER
Status
Option
JT9D
RightIOGfllterimpending
Dypass.
24-00-1
R IOGVALVE
Status
Basic
RightIOGcoolingvalvefailure.
75-21-1
R ILS
Advisory
Basic
RighttILShasfailed.
34-31-1
R IRS DC FAIL
Advisory
Basic
RightIRSDCfailure.
34-21-1
R IRS FAULT
Advisory
Basic
RightIRSfault.
34-21-1
R I R SO N D C
Advisory
Basic
34-21-1
R JET XFR VALVE
Advisory
Option
RightIRSon DC power.
Rightfueljettisontransfervalve
disagreeswithcommanded
positionand fueljettisonswitchis
in the ON position.
RMLS
Advisory
Prov'n
RightMLShasfailed.
None
RNI/N2MISMATCH
Advisory
Option
JT9D
None
R OIL FILTER
Advisory
Basic
Rightenginerunningwithright
N1 >'16%and rightN1/N2
mismatchdetected.
Rightengineoilfilterditferential
79-35-l
pressureapproachesbypass.
79-35-2
Status
R PACKOFF
Annex1-02-33
Advisory Basic
28-31-3
21-51-1
Rightpackswitchedoff or
compressoroutlettemperature 21-51-2
21-51-3
exceeds254'C (489"F).
REV17
MAR10/2007
Hungarian Airlines
tuAlEV
fi
.-87
,?27Et/v2F
LIST
EQUIPMENT
MINIMUM
Annex {
EICASMessages
EICASMessaoes
EICASMessageGross Refer€nceList
Level
Notes
R PACKTEMP
Advisory Basic
R PRIMHYD OY HT
Advisory Basic
Condition
Rightpackoutlettemperature
or
exceeds88'C (190"F),
compressoroutlettemperature
exceeds254"C(489"F),or critical
systemfailuredetectedby pack
controller.
Rightprimaryhydraulrcpump
MELltem
21-51-1
21-51-2
21-51-3
29-32-1
casedrainoverheat.
RRECIRFAN
R REV INTERLOCK
Advisory Basic
Status
RR
PW4
Rightrecirculation
fan failed.
11-25-1
Rightthrustreverserinterlock
failsto blockthrustlevermotion.
78-34-2
Rightthrustreverserisolation
valvefault- inhibited
by R AC
78-31-1
UTOT
R REV ISLNVAL
Advisory
Status
Basic
BUSOFFcautionmessage.
Option ACARs/rightSATCOMinterface
failure.
Option Lossof rightSATCOMvoice
capability
dueto failurein right
SATCOMhighgainsystem.
23-22-1
23-25-'l
23-25-1
R SATCOMDATA
Status
R SATCOMHI GAIN
Status
R SATCOMSYSTEM
Option
RightSATCOMsystemfailure.
23-25-1
R SATCOMVOICE
Status
Advisory
Option
23-25-1
R SIDE BRACE
Caution
Basic
R SIDEWINDOW
Advisory
Basic
R STARTER
CUTOUT
Caution
Basic
Lossof rightSATCOMvoice
capabilitydue to failurein right
SATCOMhighgainsystem.
messages
Inhibited
by advisory
SATCOMand SATCOMVOICE.
Systems1 and 2 bothindicate
geardisagree
andrightsidebrace
is notlocked.
Rightsidewindowheatoveror powerloss- twoor
temperature
messages
will
individual
more
causeWINDOWHEATadvisory
message.
Rightenginestartervalveopen
aboveengineRPMatwhich
cutoutshouldoccur.
Annex1-02-34
30-41-1
30-41-2
80-00-2
80-11-2
REV17
MAR10/2007
;'VlAlEV Hungarian Airlinesfi
.-8.7
,A27EttlYG
MINIMUMEQUIPMENTLIST
Annex 1
EICASMessages
EICASMessaoes
EICASMessageCroas ReferenceList
Level
R STRUTOCTLPI
Status
R STRUTOCT LP 2
Status
R TAIL HYOVAL
Advisory
R TAT PROBE
Advisory
R UTILBUSOFF
Advisory
R WINGANTI-ICE
Advisory
R WING HYOVAL
Notes
Option Rightstrutductlooploverheator
- inhibited
by R
faultcondition
STRUTOCTLEAKCAutiON
message.
Option Rightstrutduct loop2 overheator
- inhibited
by R
faultcondition
STRUTOCTLEAKcaution
message.
flightcontroltail
Basic Righthydraulic
inhibited
by FLT
valveclosed
CONTVALSmessage
Option Righttotalair temperatureprobe
-2001 heaterpoweror continuityloss-300;
two or moreindividualmessages
Basic will causePROBEHEAT
-400
advisorymessege.
Basic Rightutilitybus unpoweredwith
rightAC mainbuspowered.
valveiswitch
Basic Rightwinganti-ice
Advisory Basic
R WING SLIDE
Advisory
Basic
R YAW DAMPER
Advisory
Basic
RA DISAGREE
Advisory
RADIOTRANSMIT
Advisory
RAT UNLOCKED
Advisory
Annex1-02-35
Condition
disagree.
Righthydraulicflightcontrol
wingvalveclosed- inhibitedby
FLTCONTVALSmessage.
Rightwingslidedoorunlatched
wo or moreopenemergency
doorswillcauseEMERDOORS
aovrsorymessage.
Rightyawdamperfailure,power
loss,or switchedoff.
unit
Prov'n lnstrument
comoarator
radio
altitude
left
right
and
Option senses
drsagreement.
ODtion VHFor HFtransmitteris selected
and a push-to-talkswitehis keyed
for 30 secondsor longer,
Basic
Ramairturbineunlocked.
MELltem
26-18-1
26-18-1
27"03-1
30-31-2
30-33-1
24-51-1
30-11-1
30-11-2
27-03-1
52-71-1
22-21-1
34-33-1
23-514
None
REV17
MAR10/2007
tufilEW
Hungarian Airlines
fi
.78=
^StTEttYAt
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMe6sages
EICASMessaoes
EICASMossageCross ReferenceList
Level
Notes
Condition
MELltem
Eitherofthe two reservebrakes
and nosewheelsteeringvalves
disagreewithselectedPosition.
Rudderratiosystemfailure.
None
Lossof bothSATCOMvoiceand
dueto
capability
datalink
gain
(high
failure
equipment
no
lowgainantenna,
antenna,
SATCOMto ACARSbus
activity).
23-25-1
Ootion ACARS/SATCOMinterface
failure.
Option Lossof SATCOMdatalinkdueto
interface
ACARS/SATCOM
failure.lnhibitedby SATCOMor
DATALINKSYSadvisory
message.
Option Lossof SATCOMvoice
capabilitydue to failurein
SATCOMhighgainsystemAccompanied
by SATCOM
message.
VOICEadvisory
Option Failureof SATCOMlowgain
23-22-1
23-25-1
23-25-1
RSVBRAKEVAL
Advisory
Basic
RUDDERRATIO
Advisory
Basic
SATCOM
Advisory
Option
SATCOMDATA
Stetus
SATCOMDATALINK
Advisory
SATCOMHIGHGAIN
Status
SATCOM LOW GAIN
Status
None
23-25-1
23-25-1
antennasystem.
SATCOMMESSAGE
CommE
SATCOMVOICE
Advisory
SATVOICEAVAIL
CommF
Advisory
Annex1-02-36
Option SATCOMairto-groundcall
failure.
Option Lossof SATCOMvoice
capability
dueto failurein
SATCOMhighgainsystem.
Inhibitedby SATCOMadvisory
message.
Option Returnof voicecapabilityafrer
logoffor aftertemporary
reversionto low-gainantenna.
MA
23-25-1
MA
REV17
MAR10/2007
tlMlEW Hungarian Airlines
A
.787
.GraEtluE
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessaqes
SATVOICELOST
EICASMessageCross ReferenceList
Level
Advisory
SELCAL
CommE
SPEEDBRAKESEXT
Caution
Notes
Condition
Option Temporarylossof voice
capabilitydue to logoff,or after
temporaryreversionto low-gain
callsfrom
antenna.Ground-to-air
will not
air tratficcontrollers
flight
deck.
reachthe
viaVHF,HFor
Option Callis received
SATCOM.
deployedbetween
Speedbrakes
or
15 and800feetradioaltitude,
withlandingflapsabove15 feet
radioaltitude.
Spoilersnotdownfor takeoffand
takeoffthrustselectedon either
engine- whentakeoffthrustis
warninglightis
deselected,
butmessage
extinguished
10seconds.
for approximately
Spoilersystemhasdetected
failureof oneor morespoiler
pairs(electronic
and electrical
faultsonly).
One-half
drivespeedin flightor
on ground.
MELltem ,..
23-25-1
MA
27-62-2
None
SPOILERS
Warning
SPOILERS
Advisory
STABTRIM
Advisory
STABILIZER
Warning
Basic
Stabilizernot in correctrangefor
takeoffandtakeoffthrustselected
on eitherengine- whentakeoff
warninglight
thrustis deselected,
butmessage
is extinguished
10
remainsfor approximately
seconds.
None
STANDBY
BUSOFF
Basic
Siandbybusunpowered.
None
STBYINVERTER
Advisory
Status
Basic
None
T.R UNIT
Status
Standbyinvertervoltageoutput
outsidenormallimitswithmain
bafteryswitchon.
Leftor righttransformerrectifier
failure(DCbustieclosed).
Annex1-02-37
None
27-41-2
29-24-1
29-31-1
29-33-1
None
REV17
MAR10/2007
Hungarian Airlines
tlElEV
fi
.7Ez
.?a7Et/lYE
LIST
EQUIPMENT
MINIMUM
Annex I
EICASMessages
EICASMessageCross ReferenceList
Level
Notes
TAILSKID
Advisory
-300/
-400
TAILSTRIKE
Caution
Basic
TAILSTRIKEAHEAD
Caution
Prov'n
EICASMessages
Condition
MELltem
32-71-1
Tail skidnot in commanded
position.
LandingGear#1 and#2 body
contactsensorsdetectaft body
contactfromtailstrike.
HUDsystempredictsa tailstrike
N/A
on approacn.
comparatorunit
Instrument
Option sensesinvalidtrackdata.
Basic Trimair valveselectedclosed
packmode
(75'F temperature
selected).
Option Requirednavigationperformance
accuracynot met.Caution
messageset if duringRNP-based
approach.
Basic Uncommandedstabilizermotion
trim
in autopilot
or Mach/speed
mooes.
Option VHF radiois selectedto voice
andACARScannotcommunicate
viaVHF.
Basic Warningelectronicssystemsingle
powersupplyfailureor stall
warningunitfailure.
Advisory
T R I MA I R
Advisory
UNABLERNP
Caution
Advisory
STABTRIM
UNSCHD
Caution
VHF DATAOFF
CommF
WARNELEX
Status
WHEELWELL FIRE
Basic
Wheelwellfire detected.
26-17-1
WINDOWHEAT
Warning
Advisory
Basic
3041-1
PRED
WINDSHEAR
Status
Basic
WINDSHEAR
REAC
Status
Basic
Two or morewindowheater
or powerloss.
overtemperature
Predictivewindshearfunctionof
theWeatherRadarunitis failed.
Reactivewindshearfunctionhas
WINDSHEARSYS
Annex1-02-38
Advisory
Prov'n
34-25-1
TRACK FAIL
Basic
21-61-3
21-614
N/A
None
NiA
27-3?-2
34-61-1
3443-1
3446-1
failed.
U46-1
Eitherthe predictiveor the
reactivewindshearfunctionshave 3443-1
failed,and theirassociated
alertingis no longeravailable.
REV17
MAR10/2007
.ttElEW
Hungarian eirlines4
.zarEttue
.787
LIST
EQUIPMENT
MINIMUM
Annex 1
EICASMessages
EICASMessageCross ReferenceList
EICASMessaoes
Level
Notes
WNSHRALERTSYS
Advisory
WXRSYS
Status
YSM
Status
Option Goundproximitysystemdetects
-200t
lossof windshearmonitor
-300
function.
Basic WXRdisplayis not pretentwhen
WXRselectedon EFIScontrol
panel.
Failureof oneYSM.
Annex1-02-39
34-46-1
34-43-1
2749-1
REV17
MAR10/2007
.tt'AIEV
Hungarian Airlines4
EOE
TUE 787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-24-1GasoerFan
Fans C
2l-25-1 Recirculation
2
1
C
2
0
Both may be inoperativeprovidedboth packs operate
normally.
NOTE1: With a recirculation
fan failed,or turnedoff, the oppositea/c packgoesto the highflowmode.
1.0%.
NOTE2: For-200 Withbothrecirculation
fansoff the fuelflowwill increaseapproximately
0.6%,
NOTE3: For-300 Withbothrecirculation
fansoff the fuelflowwill increaseapproximately
EICASSTATUSMESSAGES:Hl FLOWlNHlBlT
HI FLOWON
- L(R)RECIRCFANINOP
PLACARDT
As appropriate
21-25-2 RecirculationFan
INOPLights
PLACARD:Affectedlight- LIGHTINOP
21-31-1AutoCabin
PressureControl
Systems
C
2
providedthe manualmodeand
One maybe inoperative
oneautopilotoperatenormallY.
provided:
(M) (O) Bothmaybe inoperative
a) Flight is conducted in an unpressurized
and
configuretion
b) Cargo compartmentsremainempty, or ontynonmaterialsare carried.
combustible
(M) (O) Bothautoand manualpressurecontrolsystems
provided:
maybe inoperative
a) Flight is conducted in an unpressurized
configuration,
and
b) ExtendedOverwaterFlightis prohibited,
c) Cargo compartmentsremainempty, or only nonmaterialsc€rried.
combustible
PAGE21-1
MAR10/2007.
REV.17.
.tt'lAlEV
Hungarian Airlines4
787
B?EUIUE
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIR INTERVAL
FORDISPATCH
NUMBERRESUIRED
REMARKOR/ANDEXCEPTIONS
EICASSTATUS MESSAGES:
CABINALTAUTO1
CABINALTAUTO2
PLACARD
- ALTITUDE
panelas appropriate
On the instrument
LIMITED
TO 10,000FEETMSL
OPERATIONS
{OI
Unpressurized
Flight
'1. Ensurethatforward,aft and bulkcargocompartments
areempty,or containonlynon-combustible
materials.
2. E/E cooling system is configuredfor smoke removal.The Non-Normalprocedure"Forward
"FWD
and EICASmessage,
Equipment
Annunciator
Smoke"is not used.E/E cooling'VALVE"
EQPTVAL"Shouldbe ignored.
3, Limitenroutealtitude
to lessthan10.000feetif Dossible.
NOTES:
A. At or above10,000feet,be prepared
andauralwarning
for CABINALT (red)lightto illuminate
to sound.Auralwarningcanbe silenced.
are satisfiedfor flight
B. Flightabove10,000feet is allowedonly if specialoxygenrequirements
crew,cabincrewand passengers.
packs.
pack.Do not usetwo air conditioning
4. Usezeroor one air conditioning
5. To avoidpessengerdiscomfort,aftertakeotfobstacleclearancehasbeenassured,limitclimband
descentto 500fpm. In orderto avoidE/Ecoolingductdamagelimitclimbto 2000fpm.
NOTE:With bothpacksoff, thereis adequateventilationin the flightdeckand passengercabinto
shouldbe given
ensurethat COzconcentrations
levels.Consideration
do not reachunacceptable
with high
control,particularly
to passengercomfortdue to lack of air circulationand temperature
lf both recirculation
fans are
densityloadsand with extremelyhot or cold ambienttemperatures.
operative,
bothshouldbe used.
6. Flightanendantsshouldbe notifiedthatfoMardgalleychilleris inoperative.
7. Ditching
Requirements.
A. Flightcrewmustnot changeoutflowvalvepositionexceptfor ditching.
PAGE21.2
MAR10/2007.
REV.17.
tlElEW
Hungarian Airlinesfi
EOE
IUE
787
MINIMUMEQUIPMENTLIST
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
B. In caseof ditching,
equipment
coolingOUTBDVALVEcircuitbreakermustbe pushedin.
extendedoveMaterflight is
C. lf outflowvalvetool is installedor outflowvalve is inoperative,
prohibited.
D. lf outflowvalveMAN modeoperatesnormally,extendedoverwaterflightcan be conducted.
Flight crew should not changeoutflowvalve positionwith the manualcontrolexcept as
requiredfor non-normal
orocedures.
21-31-2 ManualCabin
PressureControl
System
C
1
0
provided:
(M) (O) Maybe inoperative
a) Flight is conducted in an unpressurized
configuration,
and
b) ExtendedOveMaterFlightis prohibited,
c) Cargo compartmentsremain empty,or only nonmaterialscarried.
combustible
PLACARD
CabinAltitudeControlModeSelect- MANMODEINOP
OPERATIONS
{Ol (lf flightis to be unpressurized)
(O) - Unpressurized
Flight
See 21-31-1Auto Cabin PressureControlSystem,OPERATIONS
procedure.
(M)21-31-1
MAINTENANCE
21-31-3 OutflowValve
(OI
OPERATIONS
C
1
0
provided:
(M) (O) Maybe inoperative
a) Flight is conducted in an unpressurized
configuration,
and
b) ExtendedOverwaterFlightis prohibited,
c) Cargo compartmentsremainempty, or only nonmaterialscarried.
combustible
See 21-31-1Auto Cabin PressureControl System,OPERATIONS(O) - UnpressurizedFlight
procedure.
PLACARD
CabinAltitudeControlpanel(P5)- OUTFLOWVALVEINOP
PAGE2,1-3
REV.17.MAR 10/2007.
zt'lAlEW Hungarian Airlines4
A?E
TUE 787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
(M)21.31.1
MAINTENANCE
21-32-1 PositivePressure
ReliefValves
C
2
closed.
1 (M) One maybe inoperative
1-
2
provided:
0 (M) (O) Maybe inoperative
a) Flight is conducted in an unpressurized
configuration.
b) ExtendedoveMaterflightis prohibited,
c) Cargo compartmentsremain empty, or only nonmaterials
carried,
combustible
d) Manualcabin pressurecontrol systemsoperates
normaIy.
PLACARD
INOP
CabinAltitude
Controlpanel(P5)- POSPRESSRELIEFVALVE(S)
(OI
OPERATIONS
Flight
(O) - Unpressurized
See 21-31-1Auto Cabin PressureControlSystem,OPERATIONS
Drocedu
re.
21-33-1 CabinRateof
ClimbIndicator
C
May be inoperativeprovidedboth automaticpressure
controlsystemoperatenormally.
|-
provided:
(MXO)Maybe inoperative
a) Flight is conducted in an unpressurized
and
configuration,
remainempty,or only nonb) Cargocompartments
combustible
materialscarrieo.
PLACARD
- CABINRATEINOP
CabinRateof Climblndicator
(O)
OPERATIONS
Flight
(O) - Unpressurized
See 21-31-1Auto Cabin PressureControlSystem,OPERATIONS
orocedure.
PAGE214
REV.17.
MAR10/2007.
tlfrlEV
Hungarian Aitlinesfi
EAEfiUG
787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(M)21-31-1
MATNTENANCE
C
21-33-2CABINDIFF
Pressurelndicator
0
provided:
(O) Maybe inoperative
normally,
and
operates
a) CABINALTindrcator
b) A chartis providedto convertcabinaltitudeto cabin
differentialpressure.
0
provided:
(M) (o) Maybe inoperative
a) Flight is conducted in an unpressurized
configuration.
b) Cargo compartmentsremain empty, or only noncarried.
materials
combustible
PLACARD
(P5)panel- CABINDIFFINOP
CabinDitferential
Pressure
Indicator
-31
-1
(M)
MAINTENANCE 21
OPERATIONS
IOI
Flight
(O) - Unpressurized
See 21-31-1Auto Cebin PressureControlSystem,OPERATIONS
procedure.
pressure:
Usefollowingchartto convertcabinaltitudeto cabindifferential
u-
IJJ
o
f
E
F
z
ot
10
15
CABIN ALTITUDE 1000FT
PAGE21-5
REV.17.
MAR10/2007
tt#lEW
Hungarian Airlinesfi
EOE
TUE 787
MINIMUMEQUIPMENTLIST
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21.33.3 CABINALT
Indicator
0
provided:
(O) Maybe inoperative
e) CABINDIFF pressureindicatoroperatesnormally,
and
b) A chart is providedto convert cabin differential
oressureto cabinaltitude
0
provided:
(M) (O) Maybe inoperative
a) Flight is conducted in an unpressunzeo
configuration,
and
b) Cargo compartmentsremainempty, or onrynonmaterialscarried,
combustible
PLACARD
(PS)panel- CABINALT INOP
CabinAltitudeIndicator
(OI
OPERATIONS
PRESSURIZED
FLIGHT
Indicator".
withMELitem"21-33-2
CabinDIFFPressure
Usethechartorovided
UNPRESSURIZED
FLIGHT
See 21-31-1Auto Cabin PressureControl System,OPERATIONS(O) - UnpressurizedFlight
procedure.
(M)21-31-1
MAINTENANCE
2{-33.4 OutflowVALVE
Position
lndicator
C
1
PLACARD
CabinOutflowValve PositionIndicator(P5) panel- VALVEPOS IND INOP
PAGE21-6
REV.17.
MAR'10/2007
t*AlEW
Hungarian Airlines
fi
EAE
TUE 787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR'ANDEXCEPTIONS
21-33-5AUTOINOPLight
(CabinAltitude
Control)
C
1
0
provided:
(O) Maybe inoperative
pressure
controlsystemsoperate
a) Both automatic
normally,and
b) CABINALT or CABINRATE of Climb indicator
operatesnormally.
PLACARD
Affected
light- LIGHTINOP
(OI
OPERATIONS
Ear discomfortor unscheduled
changein cabinaltitudeare indicationsof both automaticpressure
controlsystemsfailure.In the eventof a dualfailure,selectMANUALon CabinAltitudeControlMode
SelectPanel.Manually
controlcabinaltitude
andrateof change.
21-33-6cabinAltitude
WarningSystem
c
1
0
May be inoperativeprovidedflight remainsat or below
10000feetMSL.
PLACARD
- ALTITUDE
panelas appropriate
TO 10,000FEETMSL
LIMITED
On theinstrument
21.f0-1 CargoHeating
Systems
1) FwdandAft
c
2) Bulk
c
a) BulkCargoVent c
Fan
2
0
(M) Maybe inoperative
deactivated.
l
l
0
(M) Maybe inoperative
deactivated.
(O) May be inoperativeprovided Bulk Cargo Heat
remainsin NORMposition.
Selector
U
temperaturemay drop below
NOTE'1:With cargoheat inoperative,
associatedcargocompartment
freezing.
disengage
the valveselectrically,
NOTE2: To inhibitEICASmessagesgeneratedfromdisconnecting
the assocrated
CARGOHEATswitch.
mayexceed32C,causingthe
NOTE3: Duringhotweathergroundoperationsthe cargotemperature
OVHTlightto illuminateand EICASmessageassociatedCARGOOVHTto display.
EICASSTATUS MESSAGES:
BULKCARGOFAN
l-t\\re
z t-I
MAR10/2007.
REV.17.
)+'AIEV
Hungarian Airlinesfi
AAEfiUE
787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIR INTERVAL
NUII'BERREQUIREDFORDISPATCH
REMARKOR/ANDEXCEPTIONS
PLACARD
- FWD(AFTor BULK)CARGOHEATINOP
AssociatedCargoHeatswitchlight
as appropriate
(O}
OPERATIONS
with the BulkCargoHeatingSystem
Animalsshouldnot be caniedin the BulkCargoCompartment
is givento heat, humidity,and CO2
and/orBulk CargoVent Fan inoperativeunlessconsideration
for
flight.
conditions
2140-2 CargoHeat
IndicatingSystem
(OVHTand/orON
light)
(M) May be inoperativeprovidedoverheatprotective
system(s)is verifiedto operatenormally.
1) FwdandAft
May be inoperativeprovidedassociatedcargo heat
systemis selectedOFF,
(M) May be inoperativeprovidedoverheatprotective
system(s)is verifiedto operatenormally.
2) Bulk
May be inoperativeprovidedbulk cargoheatsystemis
selectedOFF.
PLACARD
Affectedlight- LIGHTINOP
2145-l FlightCrew
Auxiliary
Heat
System(Footand
Shoulder)
c
4
0 Maybe inoperativeprovidedsystemis selectedOFF.
c
4
0 (M) May be inoperativeprovidedassociatedsystem
otf.
deactivated
NOTE:Any portionwhich operaiesnormallymay
used.
PLACARD
- FOOTHEATER(HyLOW)INOPand/orSHOULDER
HEATER(HyLOW)INOP
As appropriate
PAGE21.8
MAR10/2007.
REV.17.
ttAlEV
Hungarian Airlines
A
EOEIIUE
7Az
MINIMIJMEQUIPMENTLIST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O) Except for ETOPS operations,one may be
providedthe airplaneremainsat or belowFL
inoperative
2l-51-1 AirConditioning
Packs
c
2
provided:
(M) (O) Maybe inoperative
in an unpressurized
is
conducted
a) Flight
configuration,
funsoperatenormally,and
b) Bothrecirculation
remainempty,or only nonc) Cargocompartments
materialscanied.
combustible
EICASSTATUSMESSAGES:
HI FLOWINHIBIT
HI FLOWON
PLACARD
- ALTITUDE
panelas appropriate
LIMITED
TO FL 350
On theinstrument
-1
(M)21-31
MAINTENANCE
(OI
OPERATIONS
- lf the secondpackfailsduringthe flight,ventilation
will be very
A. ONE PACKINOPERATIVE
limited,and cabintemperatures
may becomeexcessiveand relativehumiditylevelscouldexceed
information
theflight:
80%.Thefollowing
shouldbe usedin planning
messagemaydisplay
1. Associated
EngineBleedOFFlightand L(R)ENGBLEEDOFFadvisory
duringperiodsof low bleed air demand,for example,with L(R) Pack Flow ControlShutoff
when bleedair demandincreaseto
Valve(s)closed.The lightand messagewill extinguish
openthe PRSOV.
2. lf thesecondpackfailsduringflight,do thefollowing:
a, Closecabinwindowshades.
cabinelectricalpowerincludinggalleychillers,lights,tv monitors,
b, Shutotf all nonessential
andvideoolavers.
Keeprecirculation
fanson.
Manual
d , Slowairplaneto Mach0.4,or slowestsafeoperatingspeed.SeeOperations
table.
section23.10HoldingPlanning
andsection23.20Holding
Selectcabinpressureselectorto manual(MAN).
t, Selectoutflowvalve(OFV)to fullyopenposition.
3. Somelimitedventilation
willbe available
in thecabinandflightdeckdueto air beingdrawninto
the airplanethruthe negativepressurereliefvalveand exhaustedout thruthe outflowvalve
PAGE21-9
REV.17.
MAR10/2007.
fu'lAlEV
Hungarian Airlines
4
EZE
TUE 787
MINIMUMEQUIPMENTLIST
2I, AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
for flightfollowing
4. UseTable1 belowto estimateexpectedCabinand Flightdecktemperatures
proceduresin
pack.
1
in
Table
assume
The temperatures
enroutefailureof the remaining
number1 and2 abovearefollowed.
B. BOTHPACKSINOPERATIVE
1. See 21-31-1Auto Cabin PressureControlSystem,OPERATIONS(O) procedurefor
unpressurized
flight,
2. Someventilation
will be availablein the cabindue to air beingdrawnintothe outflowvalveand
exhausted
outthroughtheE/Ecoolingexhaustvalve.
do the following:
3. To furtherlowercabinand flightdecktemperatures,
a, Closecabinwindowshades
galleychillers,
power,including
lights,tv monitors,
b, Shutoff all nonessential
cabinelectrical
andvideoplayers.
c, Keeprecirculation
fanson.
d, Slow airplaneto Mach 0.4, or slowestsafe operatingspeed. See OperationsManual
table.
section23.10HoldingPlanning
andsection23.20Holding
4. Use Table '1 below to estimateexpectedCabin and Flight deck temperaturesfor flight
followingenroute failure of the remainingpack. The temperaturesin Table 1 assume
in number2 and 3 abovearefollowed.
orocedures
TABLE,1
AFTER30 MINUTES
FLIGHTDECKANDPASSENGER
CABINTEMPERATURES
ESTIMATED
INOPERATIVE
BOTH
PACK
OF FLIGHTAT 95OO
FT MSLWITH
Enroute
AmbientTemperature
(Celsius)
ISADev
tsA-10c
ISA
ISA+10C
6
tsA+20c
16
ISA+25C
21
Cabin
% PassengerFlightDeckTemp Passenger
(Celsius)
Temo(Celsius)
Load
zc
18
26
18
100
21
zc
28
100
zo
ZJ
27
29
100
29
31
25
31
100
31
lc
100
JJ
32
33
32
flighttime.
NOTE1:Add5C to abovevaluesfor unlimited
NOTE2: Flightdecktemperatures
basedon maximumsolarradiation.For nighttimeflight,expected
will be 4C lower.
temperatures
PAGE21-10
REV.17.
MAR10/2007.
ztMlEV
Hungarian Airlines
A
EOE
IUE
787
MINIMUMEQUIPMENTLIST
21,AIRCONDITIONING
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-51-2 PackFlow
ControUShutoff
Valves
0
closed
(M) (O) Exceptfor ETOPS,may be inoperative
pack(s).
for associatedinoperative
1 One may be inoperative provided the remaining
(opposite)packoperatesnormally,
1) Hi FlowMode
EIGASSTATUSMESSAGES:
HI FLOWON
HI FLOWINHIBIT
PLACARD
- L (R ) PACKINOPor HIGHFLOWMODEINOP
PackControlSelector
as appropriate
OPERATIONS
{O)
procedure
for pack(s)
1. See item,21-51-1(Air Conditioning
Packs),for requiredOPERATIONS
Valvesinoperative.
inoperative
whendispatching
withone or bothPackFlowControl/Shutoff
2. Associate
EngineBleedOFF lightand L(R)ENG BLEEDOFF advisorymessagemaydisplay
during periodsof low bleed air demand,for example,with L(R) Pack Flow ControlShutoff
Valve(s)closed.The lightand messagewill extinguish
whenbleedair demandincreasesto open
thePRSOV.
21-51-3 PackTemperatureC
ControlSystems
1) AutoMode
2) StandbyMode
C
2
2
0
May be inoperativeOFF for an associatedinoperative
pack(s).
May be inoperativeprovidedassociatedStandbyMode
operatesnormally.
May be inoperativeprovidedassociatedAuto Mode
operatesnormally.
PLACARD
Pack control selectoras appropriate- AUTO (STBY) PACK CONTROL INOP
PAGE21-11
REV.17.
MAR10/2007.
;+UaEV
Hungarian Airlines
fi
EOE
TUE 787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-514 PackTemDerature C
ControlValves
(M) (O) One may be inoperative
deactivatedin the mid
positionprovided:
a) Associatedpackis operatedin STBY,and
b) Remaining(opposite)pack operates normally in
AUTO,
2
(M) One may be inoperativeclosedin STBY provided
the remaining(opposite)pack operatesnormallyin
AUTO.
C
2
0
Both may be inoperativefor an associatedinoperative
pack(s).
PLACARD
Packcontrolselectoras appropriate- L (R) PACKTEMP CTR VLV INOP MID (CLOSED)POS
OPERATIONS{O}
For Pack TemoeratureControlvalve deactivatedin the Mid-Position:Place associatedPACK Control
Selectorto STBY.
21-51-5PackAltitude
Switch
21-51-7AirCycleMachine
(M) (O) Except ETOPS operations one may be
inoperative
Drovided:
a) Associatedpackis operatedin STBYWARM,
b) Flowcontrolvalvein the associatedpack is verified
to operatenormally,
c) Remaining(opposite)packoperatesnormally,and
d) Associatedpack is turnedOFF at TAT abovezero
degreesC (0C).
NOTE: In case of fiailureof the remaining(opposite)
pack, the associated pack (pack with
inoperativeACM) may be turned OFF below
10000feet MSL lf necessaryto controlcabin
temoerature.
PAGE21-12
MAR10/2007.
REV.17.
:fr4lEV
Hungarian Airlines
fi
EZEITUE
787
MINIMUMEQUIPMENTLIST
21,AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACARD
- L ( R) ACMINOP- OPERATElN STBYW
Associatedpackcontrolselectoras appropriate
(O)
OPERATIONS
ACM may be turnedoff below
1- lf failureof the other packoccurs,the packwith the inoperative
10,000feei if necessaryto controlcabintemperature.
2. Temperaturesin the 767-300flightdeck, c€bin and cargo compartmentsmay become
at the listedflightlevels:
uncomfortably
warmabovethe followingoutsideair temperatures
-29C
FL 350
FL 370
-51C
FL 390
-57C
FL 430
lf comfortabletemperatures
insidethe airplanecannotbe maintainedat altitude,descendto a
lowerflightlevelto improvecooling.
3. Associated
EngineBleedOFFlightand L(R)ENGBLEEDOFFadvisorymessagemaydisplay
during periodsof low bleed air demand,for example,with L(R) Pack Flow ControlShutoff
to open
whenbleedair demandincreases
Valve(s)
closed,The lightandmessage
willextinguish
the PRSOV.
2I.52.1 PACKRESET
Switches
21-52-2 PA'CKINOP Lights
C
2
1 One may be inoperativeprovidedboth packs operate
normally.
c
2
0
Both may be inoperativefor associatedinoperative
pack(s).
1
PLACARD
Atfectedlight- LIGHTINOP
21-52-3AirConditioning
PackOFFLights
(M) One may be inoperativeOFF providedassociated
EICASmessageand all other pack indicationsoperate
normallv.
PLACARD
Affected
light- LIGHTINOP
PAGE21-13
MAR10/2007.
REV,17.
.:tElEV
Hungarian Airlines,fi
EAENYE
787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-53-1 RamAir InleuExit C
DoorSystems
l
2
^
.
0
(M) May be inoperativeprovideddoors are secured
openwithpack(s)operating.
0
pack(s).
for associatedinoperative
Maybe inoperative
PLACARD
- L (R) PACKAUTOMODEINOPor L(R)PACK
Associatedpackcontrolselectoras appropriate
INOP
NOTE
OPERATIONS
A. DoorsSecuredOpen(affectedpackoperational)
then
connector
1. lf Maintenance
hasnot installed
a shortingplugin ramair inletdoorelectrical
pack
inoperative).
cabin
temperature
(AUTo
will
be
in sTBY-w mode
MODE
operateaffected
performance
and/orduringhotday
maybe degraded
duringhotday (32C)groundoperations
highaltitude
operation.
connector
then
2. lf Maintenance
has installeda shortingplug in rem air inletdoor electrical
operateaffectedpackin STBYmode(AUTOmodewill be inoperative).
B. DoorsIn Any Position(affectedpackdeactivated)
withonepackinoperative.
1.See21-51-1foroperations
information
whendispatching
21-58-1 Forward
C
Equipment
Cooling
AUTOSystem
1
0
May be inoperativeprovidedSTBY controlsystem isl
used
I
I
OneSupplyFanInstallation:
cooLlNG DURINGGRoUNDOPERATIONS'
cAUTloN:TOENSUREADEQUATE
EQUIPMENT
ABOVE29"C(85"F).
TEMPERATURES
OPERATE
BOTH(2)PACKSAT AMBIENT
PLACARD
II
Equipment
CoolingControlpanel- AUTOMODINOP
NOTE
OPERATIONS
avoidextended
To minimizeriskof equipmentcoolingoverheatat highambienttemperatures,
groundoperationsin this configuration.
PAGE21-14
REV.17.
MAR10/2007.
ttMlEW
Hungarian Airlines
rt
EOEU^UE
787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-58-3 Forward
EquipmentCooling
SupplyFan
C
1
0
provided:
Maybe inoperative
a) FoMard equipmentcoolingexhaustfan operates
normally,
b) STBYcontrolsystemis used,and
c) For groundoperationabove29C (85F)OAT, main
air.
withconditioned
cabinis suDDlied
at high
riskof equipment
coolingoverheat
To minimize
NOTE:G200/-300)
OneSupplyFanInstallation:
ambienttemperatures,
avoidextendedgroundoperationsin thisconfiguration.
EICASSTATUSMESSAGES:
FWDEOSUPFAN1
MAINTENANCENOTE
Optional procedurefor all 767-200/300installations.ReferenceSSM 2l-58-04. Pull and collar
the forwardequipment
This will deactivate
circuit breakersC331,C332,C654,C655asappropriate.
coolingsupplyfan andextinguishthe associated
FWD EQ SUPFAN I statusmessage.
C
21-58-4 FoMard
Equipment
Cooling
ExhaustFan
1
0
provided
Maybe inoperative
a) FoMard equipmentcoolingsupplyfan operates
normallv.
and
b) For groirndoperationabove29C (85 F) OAT,main
air.
withconditioned
cabinis supplied
EICASSTATUSMESSAGES:
FWD EQ EXHFAN
PLACARD
Equipment
CoolingControlpanel- FWDEQEXHFANINOP
MAINTENANCENOTE
ReferenceSSM21-58-05.Pull andcollarcircuit
Optionalprocedurefor all767-2001300
installations.
breakersC335 on the P6 panel and C687 on the Pll-6 panel.This will deactivatethe forward
equiprnent
coolingexhaustfan andextinguishthe FWD EXH FAN statusmessage.
21-58-5 Aft Equipmenulav/ C
GallevVentFans
2
PAGE21-15
REV.17.
MAR10/2007.
:h'AIEW
Hungarian Airlines
4
EOE
IUE
787
LIST
MINIMUMEQUIPII'IENT
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
EICASSTATUSMESSAGES:
AFTEQPTCLGFAN
AFT EQ EXHFAN1
PLACARD
Equipment
CoolingControlpanel- AFT EQPTCLGFANINOP
C
21-58-7 FoMard
Equipment
Cooling
OverboardExhaust
Valve
1
0
(M) Maybe inoperative
securedclosedprovided:
a) STBYcontrolsystemis used,and
b) For groundoperationabove29C (85 F) OAT,main
air.
withconditioned
cabinis supplied
OneSupplyFanInstallation
CAUTION:TO
ENSUREADEQUATE
EQUIPMENT
COOLINGDURINGGROUNDOPERATIONS,
ABOVE29"C(85"F),
TEMPERATURES
OPERATE
BOTH(2)PACKSAT AMBIENT
PLACARD
Equipment
CoolingControlpanel- FWDEQPTOVBDEXVALINOP
OPERATIONS
NOTE
When maintenanceutilizes procedure2 (Shorting receptacleconnector NOT installed)the
shouldnot be
The AUTOposition
Equipment
CoolingSelectorshouldbe set to STBYfor dispatch.
ManualNon-Normal
position
in theOperations
as identified
used.TheOVRD
canbe used,if needed,
Checklist.
21-58-8 FwdEquipment
CoolingInboard
SupplyValve
C
I
0
(M) Maybe inoperative
securedclosedprovided:
a) STBYcontrolsystemis used,and
b) For groundoperationabove29C (85 F) OAT,main
air.
cabinis suppliedwithconditioned
PLACARD
Equipment
CoolingControlpanel- FWDEQTCLGINBDSUPVLVINOP
NOTE
OPERATIONS
avoidextendedground
To minimizeriskof equipmentcoolingoverheatat highambienttemperatures,
operationsin thisconfiguration
PAGE21.16
MAR10/2007.
REV.17.
IIMIEV
Hungarian Airlines,fi
787
EOETE
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
21-58-9AvionicsCooling
Refrigeration
Unit
(ACRU)
PLACARD
Equipment
CoolingControlpanel- ACRUINOP
21-58-10 ACRUSupply
Valve
0
(M) Maybe inoperative
securedclosed.
CAUTION:TO
ENSUREADEQUATE
EQUIPMENT
COOLINGDURINGGROUNDOPERATIONS,
OVER32C(gOF)
TEMPERATURES
OPERATE
AT LEASTONE(1) PACKAT AMBIENT
(115F).
ABOVE46C
ANDBOTH(2)PACKAT AMBIENT
TEMPERATURES
PLACARD
Equipmentcoolingcontrolpanel- ACRU SUPPLYVLV INOP
21-58-11ACRUlsolation
Valve
0
(M) Maybe inoperative
securedopen.
PLACARD
Equipment
CoolingControlpanel- ACRUISLNVLVINOP
(M) Mey be inoperative
for ETOPSoperationsprovided
availabilityof adequateair flow is verifiedbeforeeach
departure.
21-58-12 Instrument
CoolingMonitor
System
Exceptfor ETOPS,maybe inoperative.
TEMP
21.61.1 COMPT
ControlSystems
(FWD/MID/AFT)
U
J
0
(M) May be inoperativeprovidedassociatedzone trim
valve(s),or trim air regulating/shutoff
air modulating
remains
closed.
valve
PLACARD
Associated
zonetemDerature
controlselector- DO NOTOPERATE- LEAVEOFF
is eithertoo hotor too cold,selecttrim air
OPERATION
NOTE:lf cabincompartment
temperature
switchto OFF.
P A G E2 1 - 1 7
REV.17 MAR 10/2007.
rtAAlEV
Hungarian Airlines
#
EAEfiUE
787
MINIMUMEQUIPMENTLIST
21.AIRCONDITIONING
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
1
0
(M) Both auto and manualmodesmay be inoperative
providedassociatedzone trim air modulatingvalve or
valveremainsclosed.
trimair regulating/shutoff
1) AUTOMode
C
1
0
May be inoperativeprovidedthe MAN mode operates
normally.
2) ManualMode
C
1
0
May be inoperativeprovidedthe AUTO modeoperates
normally.
21-61-2 FlightDeck
Temperature
ControlSystem
PLACARD
- FLTDKTEMPAUTO(MAN)MODEINOPor FLT
Flightdecktempcontrolselectoras appropriate
DKTEMPCONTROL
SYSINOP
(M)21.61.1
MAINTENANCE
closed,flightdeck trim air is not
OPERATIONNOTE: lf the flightdecktrim air valveis deactivated
directly
fromthemixmanifold
is
available.
Cabintrimair remains
available.
Flightdeckair supplied
21{13
TrimAir Regulating C
/ShutoffValve
System(s)
0
providedassociatedtrim air
(M) May be inoperative
regulating/shutoff
valveis securedclosed.
-
0
(M)Maybe inoperative
closed
-
o
provided
thetrimairf
inanvposition
$?:no:"'*:or"Jative
I
1
PLACARD
Trim air switchlieht- TRIM AIR INOP
C
2l-61-4 ZoneTrimAir
Modulating
Valves
c
I
I
valves
NOTE:767-200has3 trimair modulating
valves,767-300has4 or6 trimair modulating
I
PLACARD
I
- FLT DK (FWDCAB,MIDCAB or AFT CAB) |
Associatedzonetemperatureselectoras appropriate
TRIMAIRINOP
2l-61-5 TrimAir oFF Light L
PLACARD
Affectedlight- LIGHTINOP
PAGE21.18
MAR10/2007.
REV.17.
)+UIEV
Hungarian Airlinesfi
AOEUIUE
7Ez
MINIMUMEQUIPMENTLIST
21.AIRCONDIT]ONING
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXGEPTIONS
(M) May be inoperativeprovidedassocietedtrim air
modulating
valveremainsclosed.
21.61.6 COMPTTEMP
INOPLights
c
(M) May be inoperativeprovidedtrim air regulating
/shutoffvalveremainsclosed,
3
PLACARD
Affectedlight- LIGHTINOP
For -200/-300,associated
zonetemperature
controlselector- DO NOT OPERATE- LEAVE OFF
(M)21-61-1
MAINTENANCE
21-61-7TrimAirCheck
Valves
C
2
0
provided
(M) Maybe inoperative
onefailedcheckvalve
is securedclosed.
PLACARD
- L (or R) TRIM AIR INOP
Trim air switchasappropriate
21{4-1 TrimAirValve
Position
Indicator
C
1
0
PLACARD
Trim air valvepositionindicator- POSIND INOP
21.65.1COMPTTEMP
Indications
PAGE21-19
REV.17.MAR10/2007.
.;?MIEV Hungarian Anrfines
B
.7Ez
^8278//YAF
LIST
EQUIPMENT
MINIMUM
22. AUTOFLIGHT
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
22-10-1AutopilotSystems
c
provided:
(M) One maybe inoperative
a) AssociatedFCC SERVOcircuit breakeris pulled
andcollared,
b) AutopilotSystemis verifiednot in a singlesource
priorto eachdeparture,and
configuration
to CategorylllA Landing
c) The aircraftis re-classified
Minima.
provided:
(M) Two maybe inoperative,
a) At leasttwo FCCpowercircuitbreakersremainlN,
b) AssociatedFCC SERVOcircuit breakeris pulled
andcollared,
c) AutopilotSystemis verifiednot in a singlesource
priorto eachdeparture,and
configuration
d) The aircraftis re-classifiedto Categoryll Landing
Minima,
NOTE:One FCCis requiredfor RVSMoperation.
Exceptfor ETOPSand RVSMoperations,all mey be
provided:
inoperative
a) At leastone FCCpowercircuitbreakerremainlN,
b) All three FCC SERVOcircuitbreakeris pulledand
collared,
minimums
do notrequiretheiruse,and
c) Approach
and segmentdurationis
d) Numberof flightsegments
acceptable
to flightcrew.
PLACARD
INOP'
Autopilot
ModeControlPanelas appropriate - ,L(C,R)AUTOPILOT
- ,,cATr(il)oNLY"
panel
P1-3Captein's
maininstrument
- "DONOTSETDHBELOW100(200)
FEET"
Pg foMardelectroniccontrolpanel
22-11-1 ConholWheel
Disengage
Switches
,-
One may be inoperativeprovidedautopilotis not used
altitude.
belowinitialaooroach
PLACARD
Associatedswitch - INOP
Pege22-1
Rev17 MAR10/2007
Hungarian Airlinesfi
tuElEV
.7Az
^g2rEtlUAF
LIST
EQUIPMENT
MINIMUM
22.AUTOFLIGHT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
22-11-2 NP DISCLight
C
1
0
provided:
Maybe inoperative
a) Autopilotis not usedbelow1,500feetAGL,and
b) All other A'lP ditengagement alerts operate
normaV.
22-11-3 ModeControl
PanelSelector
1)VERTSPD
C
Selector(DN& UP)
1
0
providedFL CH modeoperates
(O) May be inoperative
normallv,
C
1
0
(O) Maybe inoperative.
B
1
1
I
0
0
0
(O) Maybe inoperative.
(O) Maybe inoperative.
providedprocedures
or en-route
(O) May be inoperative
operationsdo not requireits use.
PLACARD
Ar appropriate
2) BANKLMIT
Selector
3) Selector
Push
Functions
a) IAS/MACH
b) ALT
c) HDGSEL
NOTE:The rotationalfunctionof these selectorsmust
operatenormally.
PLACARD
AffectedMCPselecto(s)- INOP
(O)
oPERATTONS
lf VERTSPDSelectoris inoperative,
targetedverticalspeedin VerticalSpeedmodecannot
be adjusted.
VerticalSpeedmodemaystillbe usedto holdairplaneverticalspeedat timeof engagement
lf BANKLIMITSelector
is inoperative,
Heading
Selectbankanglelimitcannotbe changed.
Thereis no flightcrewimpactif stuckat AUTO(NORMin someMCPconfigurations).
Selectmodemay
changesin Heading
lf stuckat a lowbankanglevalue,largeheading
greatertimeto complete
thannormal.lf stuckat a highbankanglevalue,
requiresignificantly
at cruise
aggressive
largeheadingchangesin HeadingSelectmodemaybe undesirably
conditions.
Page22-2
Rev17 MAR10/2007
.t'lrAlEV Hungarian Airlinesfi
.78EzTEtttvZF
EOUIPMENT
MINIMUM
LIST
22,AUTOFLIGHT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
c€nnotbe invoked.lf
lf IAS/MACHPushFunctionis inoperative,
V NAVSpeedIntervention
continuedV NAVoperationis desired,speedentriescan be madevia the CDU.
cannotbe invoked.lf
lf ALT PushFunctionis inoperative,V
NAVAltitudeIntervention
can
be
deletedvia the CDU.
continuedV NAVoperationis desired,altitudeconstraints
Heading
(engage
Selectmodecannotbe
lf HDGSELPushFunction
switch)is inoperative,
in L NAVor in manualflight,or usingAPP,LOC,or
engaged.
Turnsmustbe accomplished
B/CRSif appropriate.
22-114 ModeControl
PanelSwitches
May be inoperative provided associated autopilot
systemis consideredinoperative.
1)A/PEngage
C
Switches/Paddles
(L CMD,C CMD,R
CMD)
3
0
2) A/P CWS
EngageSwitches
C
3
O
3) A/T ARMSwitch C
1
0
systemis
OFF providedautothrottle
May be inoperative
consideredinoperative.
4) A,/TSPDMode
EngegeSwitch
C
1
0
(O) May be inoperativeprovided proceduresand
minimums
do notrequireitsuse.
approach
5) F/DSwitches
C
2
0
May be inoperativeOFF provided Flight Director
inoperative.
displaysare considered
6) |AS/MACHSEL
Switch
C
'1
0
May be inoperativeprovided IAS is displayed in
window.
associated
7) APPSwitch
C
1
0
providedapproachminimumsdo not
Maybe inoperative
requirethe useof autopilotor flightdirector.
8) LOCSwitch
C
1
0
(O) Maybe inoperative.
9) B/CRSSwitch
C
1
0
(O) Maybe inoperative.
10)v NAV,FL,
CH,V/S,ALT
HOLDSwitches
C
4
3
(O) One may be inoperativeprovidedproceduresor
enrouteoperationsdo not requireits use.
Page22-3
Rev17 MAR10/2007
tlUaEV
.&ZE.'YZF
Hungarian Airlines
A
.78-
LIST
MINIMUM
EQUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
11)L NAV,HDG
HOLDSwitches
provided:
1 (O) one maybe inoperative
normally,
and
a) HDGSELoperates
b) Proceduresor enrouteoperationsdo not requireits
use.
12)EPR/N1/THR
Switch
0
May be inoperativeprovidedboth thrust levers are
operatedmanuallyfor takeoff.
NOTE:
complywith ltem22-10-1.
lf one or moreA,/PEngageSwitchesis inoperative,
lf A/T ARMswitchis inoperative
OFF,complywithltem22-30-1.
OFF,complywithltem 34-224.
lf one or moreF/DSwitchesis inoperative
PLACARD
- INOP
AffectedMCPswitch(es)
(O)
oPERATTONS
Speedmodecannotbe manually
Autothrottle
lf A/T SPDmodeengageswitchis inoperative,
modeuponexitof FL CH or V NAVor
selected.A"/TSpeedmodeis the defaultautothrottle
SPDswitch.V NAVnormallycommandsthe
G/A,whichis notaffectedby an inoperative
FMC,
whichis alsonotaffectedby an inoperative
autothrottle
to speedsdeterminedby the
SPDswitch.
lf LOCswitchis inoperative,
the Localizermodeis notavailablefor useduringa localizerLDA,or SDF)or
(examples:
localizer
backcourse,
dependent
approach
localizer-only,
departureprocedure.L NAV,HDGSEL,or manualflightmaybe used.
modefor backcourselocalizer
Backcourse
lf eitherthe LOCor B/CRSswitchis inoperative,
is notavailable.
L NAV,HDGSEL,or manualflightmaybe used.
approach
flightcrewsmustconsiderusageof
lf a pitchand/orroll modeengageswitchis inoperative,
otherautopilotmodesappropriate
for the plannedroute,The defaultautopilotmodeis
VerticalSpeedand HeadingHold.Thesemodesmaybe usedto holdverticalspeed(or
V/S = 000)and headingevenif the associatedmodeengageswitches
altitudewithtiargeted
transitionto
FlightLevelChangeandVerticalSpeedmodesautomatically
are inoperative.
AltitudeHoldevenif the ALT HOLDswitchis inoperative.
eitherV NAV,ALTHOLD,or VERT
holdcapability,
Forenroute
operations
requiring
altitude
SPDmaybeused.
Page224
Rev17 MAR10/2007
;+UIEV Hungarian Airlinesfi
.78'7
.AZrEt'YaF
LIST
MINIMUM
EQUIPMENT
22. AUTOFLIGHT
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
22-11-5ModeControl
PanelWindows
1)Airspeed
(IAS/MACH)
c
1
0
(O) May be inoperativeprovidedcommandairspeed
bug on airspeedindicator(and ADI speed tape, if
installed)operatesnormallyon bothsides.
(HDG)
2) Heading
C
1
0
(O) May be inoperativeprovided selected heading
indications
on bothHSI'soperatenormally.
3) VerticalSpeed
(VERTSPD)
C
1
0
providedVerticalSpeedmodeis
(O) Maybe inoperative
notselected.
PLACARD
MaskaffectedMCPwindow(s)- INOP
(O)
oPERATTONS
lf IAS/MACHend/orHDGwindowsare inoperative,
associatedtargetvaluesmaystillbe set
on ADIand/orHSI(PFDfor indications
andappropriate
autopilot
modesusedby observing
400ER).
lf VERTSPDwindowis inoperative,
do not manuallyselectVerticalSpeedmode.Vertical
Speedmodemayengageas the defaultautopilotmode,butanotherpitchmodeshouldthen
be selected.
22-11-6 ModeControl
PanelSwitchLights
1)Autopilot
C
EngageSwitch
Lights(CMD)
2) ModeSelector
SwitchLights
22-14-1 AutolandStatus
Annunciators
C
3
2
-
The lightsfor anytwo switchesmaybe inoperative.
NOTE:A switchwithone lampoperationalis considered
to be operatingnormally.
C
2
0
provided
do not
minimums
approach
Maybe inoperative
requiretheiruse.
PLACARD
As appropriate
Page22-5
Rev17 MAR'10/2007
.ttMlEV Hungarian Airlines
fi
.78'7
.?arEttUZF
EQUIPMENT
LIST
MINIMUM
22.AUTOFLIGHT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
22-14-2 AutomaticLanding
System
(AUTOLAND)
1)Triple
Channel
(LAND3)
Autoland
0
providedThe aircraftis re-classified
May be inoperative
ll LandingMinima.
to Category
0
providedThe aircrafris re-classifled
May be inoperative
Minima.
ll
Landing
to Category
is notedpriorto
NOTE:lf a NO LAND3 annunciation
departureand if no otherindicationsor messagesare
present, the aircraft may be dispatched with no
actionprovidingat leastone autopilotwill
maintenance
engageand approaehminimumsdo not requiretriple
channelautoland.The groundautopilotengagement
is parked.
shouldbe donewhiletheairplane
PLACARD
As appropriate:
AUTOLANDINOP,TRIPLECHANNELAUTOLAND- INOP
22-21-1 Ya\NDamoers
C
2
1
(M) One may be inoperativeprovidedremainingYaw
Damperis verifiedto operatenormally.
equivalent
or production
NqIE: ff ServiceBslletin767-22-7hasnot beenincorporated
Yaw
Damper
lf
remaining
(FCC
limit
exists:
installed
5241T100-102
is installed),
an AFM
failsdo notoperateautopilotat speedsgreaterthan230 knotsor 0.6M.
PLACARD
As appropriate
22-30-1 Thrust
Management
System(lncluding
Autothroftle
System)
1) Autothrottle
Servo
2) Autothrottle
Disconnect
Switches
c
2
0
providedapproachminimumsdo not
Maybe inoperative
its
use.
require
0
provided:
(M) Maybe inoperative
and
aredeactivated,
a) Autothrottles
b) Approach minimums do not require use of
autothrottles.
1
0
provided:
(M) Maybe inoperative
Page22{,
Rev17 MAR'10/2007
Hungarian airfinesfi
ttallEV
.78,.aaTEtjYZF
LIST
MINIMUM
EQUIPMENT
22. AUTOFLIGHT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
and
are deactivated,
a) Autothrottles
b) Approach minimums do not require use of
autothrottle.
3) ThrustMode
SelectPanel
a) DerateSwitches
b)TEMPSEL
Selector
c) TO/GASwitch
C
C
d) CLBSwitch
1
1
0
0
e) CONSwitch
C
1
0
f)
C
1
0
CRZSwitch
0
U
(O) May be inoperativeprovided Automatic Climb
ThrustSelectoptionin installedandoperatesnormally.
providedMaxContinuous
Thrust
(O) Maybe inoperative
if required,
is setmanually
Systemwill be inoperative
Computer,the Autothroftle
NOTE:With an inoperative
ThrustManagement
following
EICAS
will
be
affected:
andthe
displayson
inhibited
during
whicharenormally
1. EGT(andN1,N2,N3for RRengines)
amberindications
takeoffor go-around
willnotbe inhibited,
2. Reference
EPRwillnotbe available,
(if used)will not be available,
3. Assumedtemperature
4. Thrustreferencemode(TO,CLB,etc.)willnot be available.
5. Airplanesthatdo not havespeedtape:the SPDflag mayremainin viewon the EADI
PLACARD
As appropriate:
AffectedTMSPswitch(es)- INOP
(OI
OPERATIONS
lf CLBswitchis inoperative,
AutomaticClimbThrustSelectoptionmustbe installedand
uponselectionof
operatenormally.Takeoffthrustreductionwill be performedautomatically
by
is required,
ClimbThrustmustbe set manually
anypitchautopilot
mode.lf a go-around
Manual/QRH
data.
usingOperations
UseOperations
Thrustmustbe setmanuallylf CONswitchis inoperative,
MayContinuous
Thrustis required.
ManuayORH
dataif MaxContinuous
Page22-7
Rev17 MAR10/2007
Hungarian Airlinesfi
ttElEV
.78?
.gzrEtttyzF
LIST
MINIMUM
EQUIPMENT
22. AUTOFLIGHT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
22-30-2 Go-Aroundand
Takeoff/Go-Around
Switches
1) Go-Around
C
Switches
provided:
(M) Onemaybe inoperative
do notrequireitsuse,and
minimums
a) Approach
Switchis verifiedto operate
Remaining
Go-Around
b)
normally.
provided:
Maybe inoperative
a) Both thrust levers are operatedmanuallyfor goaround,and
b) Autopilotand FlightDirectorare not usedbelow500
feet AGL or applicableapproach minimums,
whichever
is higher.
22-34-1 Autothrottle
Disconnect
(A/TDISC)LiSht
0
NOTE: Flight DirectorGo-aroundand Windshear
guidance are not available with boih Go-Around
switchesinoDerative.
provided:
Maybe inoperative
operatesnormally,
a) AssociatedEICASannunciation
and
b) Associatedauralalertoperatesnormally.
PLACARD
(A/T DISC)Light- INOP
Autothrottle
Disconnect
22.41-1 Maintenance
ControlDisplay
Panel
Page22-8
Rev17 MAR10/2007
nYUIEV
Hungarian Airlines4
EOEIaUG
7ez
MINIMUMEQUIPMENTLIST
23, COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Movedto 23-51-5.
23-00-1 BoomMicrophones
23-10-1 RadioTuning
Panels
(DigitalRTP's)
c
3
2
One may be inoperativeprovidedleft Radio Tuning
Paneloperatesnormally.
PLACKARD
PANELINOP
Associated
Communic€tion
ControlPanel(P8)CONTROL
i.a.w.JAROPS1.865,leaflet26.
23-11-1Communications
Systems
1)VHFComm
D
3
2
a) Frequency
TransferLight
C
3
0
b) Frequency
C
TransferSwitch
3
0
c) Frequency
SelectorKnob
C
3
2
d) Frequency
Indication
C
3
2
Right or Center may be inoperativeprovided Left
operatesnormally.
May be inoperative provided associatedVHF active
frequencycanbe selected.
NOTE:Havingan AFMlimitation
stating"DonotusecenterVHFforATCcommunications
controlsystems,suchas
withACARSoperational",
deactivation
of nonessential
do
possible
Someairplanes
ACARS,maybe
to meetminimumradiorequirements.
not havethisAFMlimitationdue to a VoiceModeProtectioninstallation.
NOTE
MAINTENANCE
1.
2.
lf the VHF radiosrequiredfor the routebeingflownincludethe radioassociatedwith
ACARS,thentheACARSsystemmustbe deactivated
by openingandcollaringboth
ACARSAC and DCcircuitbreakers.
Forairplanes
notequipped
witha C-RCP
(ACARSIntegratedDisplayUnit/lDu/controlled
C-VHFradio)the C-VHFcan not be
usedto meetthe minimumradiocriteriadueto ACARSdeactivation
(continued)
PAGE23-1
REV17 MAR1Ol2007
tiMlEW
Hungarian Airlines,fi
EOEIIUE
787
MINIMUMEOUIPMENTLIST
23.COMMUNICATIONS
NUMBERINSTALLED
REPAIRINTERVAL
NUMBERREQUIRED
FORDISPATCH
REMARKOR/ANDEXCEPTIONS
i.a.w.JAROPS1.865,leaflet26.
2) HighFrequency
(HF)
Communication
System
D
2
Any in excessof thoserequiredfor the routeto be
flown,and not poweredby an emergencybus,maybe
inoDerative.
for not
(o) Any in excessof one maybe inoperative
morethan3 calendardaysfor flighton a routethat
System,(in
requirestwo LongRangeCommunication
MNPSairspace)provided:
a) ACASis operative;and
b) appropriate
alternatecommunication
and used.
orocedures
areestablished
Note: Whentherouteentersa FIRin whichan In
Procedure
exists,select
FlightBlind Broadcast
l.F.B.Frequency
andapplythe
theappropriate
re
oroceou
OPERATIONS
{O)
Requirements
for communication
systemsmustbe determinedby eachoperatorand
procedures
items,if required.
to be usedwithinoperative
appropriate
established
121.351
andJAROPS1.865.
Reference
FAR121.345
through
Mal€v must have determinedcommunicetions
requirementsdependingon their type of
(VFR/IFR)
operation
route
system.
See
FAR121.345through121.351and JAR
and their
OPS 1 regulations.Deactivationof nonessentialcontrolsystems,such as ACARS is
permissible
to meetminimumradiorequirements.
PAGE23-2
REV17 MAY30/2007
.tt'lAlEW Hungarian Airlines4
EZE,IUE
787
MINIMUMEQUIPMENTLIST
23. COMMUNICATIONS
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
i.a.w,JAROPS1.820,leaflet26.
23-12-2EmergencyLocator
(ELT)
Transmitter
-
May be inoperativeprovidedrepairsare madewithin6
furtherflightsor 25 flyinghours,whicheveroccursfirst.
2
(M) For extendedoverwaterflights,any survivalELT in
excess of the two required may be missing or
inoperativeprovided the inoperativeequipment is
placarded inoperative,removed from the installed
locationand placedout of sightso it cannotbe mistaken
unit.(i.a.w.JAROPS1.830,leaflet26)
fora functional
(O) May be inoperativeprovidedalternateprocedures
are established
and used.
23-21-1 SelectiveCall
System(SELCAL)
May be inoperativeprovidedproceduresdo not require
its use.
(O)
OPERATIONS
or when
whenthe SELCALis inoperative
MALEVmustusedevelopedalternateprocedures
individual
channels
of SELCALareinoDerative.
23-22-1 ACARSSystem
C
1
0
May be inoperativeprovidedalterneteproceduresare
estiablished
and used.
D
1
0
May be inoperativeprovidedproceduresdo not require
its use.
NOTE:Any mode which operatesnormallymay be
used.
'1) ACARSPrinter
C
1
0
May be inoperativeprovidedalternateproceduresare
andused.
established
D
1
0
May be inoperativeprovidedproceduresdo not require
Itsuse.
(continued)
PAGE23-3
REV17 MAR1Ol2007
:fr4lEW
Hungarian Airlines
h
EOE
IUG
787
MINIMUMEQUIPMENTLIST
23.COMMUNICATIONS
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATGH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
EICASSTATUSMESSAGES
SATCOMDATA
L SATCOMDATA
R SATCOMDATA
L DATALINK
SYS
R DATALINK
SYS
PLACCARD
As appropriate
(O)
OPERATIONS
Developedalternateproceduresshouldbe usedwhenthe ACARSSystemor ACARSPrinter
are inoperative.
23-25-1 SATCoMSystems
Deleted
23-31-1 Passenger
AddressSystem
i.a.w.JAROPS1.695,leaflet26.
0
provided:
(O) Maybe inoperative
a) Alternate,normalandemergencyprocedures
areestablished
and
and/oroperatingrestrictions
useo,ano
system
/ cabininterphone
b) Flightcrewcompartment
(including
chimesystem)areoperative.
NOTE: Any station function(s)that operate normally
maybe used.
NOTE:
Any stationfunction(s)that operatesnormallymay be
used-
a) Lavatory
Speakers
-
(O) May be inoperativeprovidedalternateprocedures
areestablished
and used.
b) CabinSpeakers
-
May be inoperativeprovidedinoperativespeakersare
not adjacentto eachother.
PLACARD
Associatedcontrolpanelsas appropriate
PAGE23-4
REV17 MAR10/2007
IIMIEV
Hungarian Airlines,rt
EOE,TUE
787
LIST
MINIMUM EGIUTPMENT
23. COMMUNICATIONS
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS
{OI
1.
Passenger
AddressSystem:
whenthe passenger
a) MALEVmusthavedevelopedalternateprocedures
announcement
systemis inoperative.
b) Priorto flight,the pilotin commandmustbraefcabincrewmemberson the emergency
whichwill be used.
orocedures
2.
LavatorySpeakers:
Developed
alternateprocedures
shouldbe usedwhenlavatoryspeakersare inoperative.
23-31-2 Prerecorded
Passenger
Announcement
System
C
1
0
(O) May be inop€rativeprovidedalternateprocedures
andused.
areestablished
D
1
0
May be inoperativeprovidedalternateproceduresdo
not requireits use.
PLACCARD
As appropriate
(O)
OPERATIONS
passengerannouncement
system
Developedalternateprocedures
shouldbe usedwhenpre-recorded
is inoperativePriorto flight,the pilotin commandmust briefcabincrew memberson the emergency
orocedures
whichwill be used.
and
23-31-3 Headsets
Microohones
Movedto 23-51-5.
PAGE23-5
REV17 MAR10/2007
s!'AIEW
Hungarian Airlinesfi
AOE1IUE
7Az
MINIIUUMEQUIPMENTLIST
23. COMMUNICATIONS
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
i.a.w.JAROPS1.690,leaflet26.
23.40-1 Crewmember
Interphone
System
(FlightDeck
Intercommunicalion)
a) FlightDeckto
Cabin,Cabinto
FlightDeck
Functions
B
4
provided:
(O) Maybe inoperative
a) Flightdeckdoor keypad(whereinstalled)is verified
to operatenormally,
b) Flightdeck door automaticlockingsystem(where
installed)is verifiedto operatenormally,
c) Alternatecommunicationproceduresbetweenthe
and
affectedflightattendantstationsareestablished
useo.
d) The PA systemis operative.
NOTE: Any stationfunction(s)that operatesnormelly
maybe used.
b) Cabinto Cabin
Function
C
2
provided:
(O) Maybe inoperative
a) Alternate normal and emergency procedures
betweenthe affectedflight attendantstationsare
and used,and
established
b) The PA systemis operative.
NOTE: Any station function(s)that operate normally
mavbe used.
c) FlightCrewto
Ground/ Groundto
FlightCrew
Function
to
(O) Flightinterphone
flightdeck to ground/ground
providedi
flightdeckfunctionmaybe inoperative
a) Alternatenormal and emergencyproceduresare
andused.
established
b) Nose gear service interphone jack operates
normallv
to
(O) Serviceinterphoneflight deck to ground/ground
providedl
flightdeckfunctionmaybe inoperative
c) Alternatenormal and emergencyproceduresare
andused.
established
d) Nose gear service interphone iack operates
normally
(continued)
PAGE23-6
REV17 MAR10/2007
I*MIEW
Hungarian Airlines
4
EZE
IUG
787
MINIMUMEQUIPMENTLIST
23. COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
d). LargeTurbojet
PoweredAirplanes
Operatingunder
FARPart121
deletedacc.to Ma MELREV17
2. All Other
Aircrafuoperations
deletedaccto Ma MELREV17
OPERATIONS
IO)
1. FlightDeckto Cabin,Cabinto FlightDeckandCabinto Cabin
to be followedduring
Briefthe Crewbeforeflightregardingthe normaland emergencyprocedures
flightusingthePA Systemor othermeansof communication.
2. FlightDeckto Ground
Establishalternateprocedures(e.9. HandSignals)to communicateto GroundPersonnelbefore
anysignific€nt
action(doorclosing,
enginestart,etc.
3. FliohtAftendant
Chime:
tvtAUEV
snoutOdevelooalternateoroceduresbasedon the use of the alternativecommunication
procedure
Priorto flight,thepilotin command
whenthePassenger
AddressSystemis notfunction.
to be used.
shouldbriefcabincrewmemberson the alternateemergencyprocedures
D
23.40-2 CrewRest
Interphone
System
and PA
Announcement
(if installed)
1
0
provided:
(M) Maybe inoperative
and
Associatedcrewrestis not usedby personnel,
Associated crew rest door is locked closed and
DO NOTUSE- COMMINOP.
olacarded,
PLACKARD
Door- DO NOTUSE- COMMINOP
(M)
MAINTENANCE
Securedoorto associatedcrewrestareaand DlackardDO NOTUSE- COMMINOP
PAGE23-7
REV17 MAR10/2007
tVUIEV
Hungarian Airlines
fi
EAE
IUE
787
MINIMUMEAUIPMENTLIST
23. COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
23.41-1 AlertingSystem
(AudioA/isual)
(if installed)
a) FlightDeckCall
VisualAlerting
System
May be inoperativeprovidedthe flight deck audio
alertingsystemoperatesnormally.
b) FlightAttendant
VisualAlerting
System
provided:
Maybe inoperative
a) PA systemoperatesnormally,
b) lf affectedvisualalertingsystemis usedfor
lavatorysmokedetectoralerting,an alternate
lavatorysmokedetectoralert(audioandvisual)
normally,
and
is installed
andoperates
for contactingflight
c) Alternateprocedures
attendantsareeskblishedand used.
to AftendantCallSystemis
NOTE1: Passenger
item.
a passengerconvenience
considered
that
systemfunction(s)
NOTE2: Anyvisualalerting
operetesnormallymaybe used.
c) FlightAttendant
AudioAlerting
System
NOTE:The flghtdeckaudioalertingsystemmust
alwaysbe operative.
0
provided:
(O) Maybe inoperative
a) PA systemoperatesnormally,
b) lf atfectedvisualalertingsystemis uted for
lavatorysmokedetectoralerting,an alternate
lavatorysmokedetectoralert(audioand visual)
is installedandoperatesnormally,and
for contactingflight
c) Alternateprocedures
and used.
are established
aftendants
Call
Systemis
1:
Passenger
to
Attendant
IlqtE
item.
considered
a passengerconvenience
that
NOTE2: Anyvisualalertingsystemfunction(s)
operatesnormallymaybe used.
(O)
OPERATIONS
Developed
alternateprocedures
shouldbe usedfor flightattendantalertingthat maybe
basedon the useof remainingoperativefunctionsof the alertingsystemor on useof the
Passenger
AddressSystem.Priorto flight,the pilotin commandshouldbriefcabincrew
memberson the alternateorocedures
to be used.
PAGE23.8
REV17 MAR10/2007
rlMlEW
Hungarian Airlines
fi
EAE
lUE
787
MINIMUMEQUIPMENTLIST
23. COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2342-1 FlightDecldcabin
Handsets
a) FlightDeck
Handset
provided:
(O) Maybe inoperative
operates
a) Flightdeckto cabincommunication
normally,
and
and used.
are established
b) Alternateprocedures
May be inoperativeprovidedproceduresdo not require
its use.
b) CabinAttendant
Handset(s)
(continued)
provided:
(O) Maybe inoperative
e) Fiftypercentof cabinhandsetsoperatenormally,
b) One handsetmustoperatenormallyat each pairof
exit doors,and
proceduresbetweenthe
c) Altematecommunications
affectedFlightAttendantsstation(s)are established
andused.
NOTE 1: An operativehandsetat an inoperativeflight
attendantseat shall not be countedto satisfythe fifty
percentrequirement.
NOTE2: Any handsetfunction(s)that operatenormally
maybe used.
PLAGGARD
As appropriate
(O)
OPERATIONS
MALEVshoulddevelopalternateproceduresbasedon the use of the PassengerAddressSystem
shouldbriefcabincrewmembers
and/orGabinInterphone
System.Priorto flight,thepilotin command
on the alternateemergencyprocedures
to be used.
normallyconductedusing the flight deck handsetcan be conductedusing the
Communication
andheadset
or flightdeckspeakers
headseUboom
microphone
or usingthehandmicrophone
r'il,tr
zJ-Y
REV17 MAR,10/2007
zt'AIEV
Hungarian Airlines
4
EZE
TUE 787
MINIMUMEQUIPMENTLIST
23.COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMEERREQUIRED
REMARKOR/ANDEXCEPTIONS
23.43-1 GroundCrewCall
System
1) GroundCrew
CallHorn
C
1
0
(O) May be inoperativeprovidedalternateprocedures
are established
and used.
C
1
0
(O) May be inoperativeprovidedalternateprocedures
are established
and used.
(O)
OPERATIONS
1. Providefor continuouscommunicationbetweenFlight Deck and appropriateGround Crew
systemduringgroundoperation
membersthroughinterphone
2. Providefor continuousmonitoringof the FlightDeck(whenflightcrewis not at dutystationduring
groundoperations)to ensureappropriate
actionin the eventa faultdevelopsduringoperationof
E/ECoolingSystem.
3. Ensurethe InertialReferenceUnitis notoperatingon DC power.
23-51-1 FlightDeck
Interphone
System
DeletedRev.30.
23-51-2AudioSelector
Panel
DeletedRev18
NOTE1: Thereis no MMELrelieffor the capatain'sand firstofficer'saudioselectorpanel.
NOTE2: The audioselectorDanelassociatedwiththe firstobserversseatcan be
perMMELitem25-11-2.
inoperative
level
panelin theEE bayis considered
maintenance
NOTE3: Theaudioselector
equipment anddoesnotrequireMMELrelief.
NOTE4: Referto FAAMMELPolicyLetter56 and the revisionhighlightsof 767 MMEL
"ltem
'18.Therevision
wereas follows:
for item23-51-1
revision
18 highlights
deleted.Observer'saudiopanelmovedto ATA25.Thereis no relieffor flight
is a maintenance
crewaudiopanels.Relieffor audiopanelin E&Ecompartment
controlitem."
23-51-3 FlightDeck
Speakers
C
2
0
provided:
Maybe inoperative
not
requiretheiruse,and
do
a) Procedures
normally.
andoperating
areinstalled
b) Headsets
PAGE23-10
REV17 MAR10/2007
ttElEW
Hungarian Airlinesfi
EOE
TUE 787
MINIMUMEQUIPMENTLIST
23,COMMUNICATIONS
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
23-51.4 Push-To-Talk
(PTT)Switches
(M) Onemaybe inoperative:
a) AssociatedAudio Control Panel PTT switch or
and
handheldmikeis operative,
associated
b) Affectedcontrolwheelswatchis deactivated.
1)ControlWheel
PTTSwitches
2) FlightCrew
AudioSelector
PanelPTT
Switches
C
provided:
(M) One maybe inoperative
a) Associated control wheel PTT switches or
associatedhandheldmikeis operative,
b) Affectedaudioselectorpanelswitchis verifiedfailed
oDen.
2
PLACCARD
As appropriate
i.a.w.JAROPS1.650& 1.652,leaflet26
23-51-5FlightCrew
Communication
Equipment
must be
One headset(includingboom microphone)
Any in
deck
duty.
on
flight
requiredcrew member
required
may
be
inoperative.
of
those
excess
Maybe inoperative
or missingprovided:
a) Associated hand microphone is installed and
operatesnormally,
b) FlightDataRecorder(FDR)operatesnormally,and
c) Repairsare madewithinthreeflightdays.
1) Boom
Microphones
2) Hand
Microphones
0
D
3) Headset
Earphones
0
May be inoperativeor missing providedassociated
boommicrophone
operatesnormally.
May be inoperativeor missingprovidedproceduresdo
notreouireitsuse.
Deletedacc.to JAA policy
PAGE23.11
REV17 MAR10/2007
:+UaEV
Hungarian Airlinesfi
EAEttE
7A7
MINIMUMEQUIPMENTLIST
23. COMMUNICATIONS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKORJANDEXCEPTIONS
23-71-1 CockpitVoice
RecorderSvstem
A
1
0
provided:
Maybe inoperetive
a) The airDlanedoes not exceed8 furtherconsecutive
flightswiththe cockpitvoicerecorderunserviceable,
b) Not more then 72 hours have elapsedsince the
cockpit voice recorder was found to be
and
unserviceable,
c) FlightDataRecorder(FDR)requiredto be carriedis
ooerative
to combined
is not applicable
Note: This alleviation
For those combinedsystems,see
CVRyFDRS.
the entries for combination recorders in
(if installad)
item3'1-31
PAGE23-12
REV17 MAR10/2007
,*MIEW
Hungarian Airlinesfi
7ez
.eZEt'YE
EQUIPMENT
LIST
MINIMUM
POWER
24. ELECTRICAL
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
24-00-1 EngineDriven
Generator
Channels
B
2
1 (M) (O) Except for ETOPS operationsbeyond 120
provided:
minutesone maybe inoperative
a) To make sure the APU operatesnormally,do the
followingtasks:MMTASK49-11-00-802402,TASK
and
1, TASK 24-21-00-715-001,
49-16-00-206-01
TASK24-21-00-735-008.
b) APU-drivengeneratoroperates normally and is
used to supplybussesof the inoperativechannel
theflight.
throughout
c) All generatorcontrol units, includingthe APU,
operatenormally,
at leastone HydraulicMotor
d) For ETOPSoperations,
Generators(HMG)is verifiedto operatenormally.
e) lf the APU is to be used as an alternatepower
source and has been operatingfor an extended
period of time in heavy falling or blowingsnow,
beforedepartureinspectthe inlet plenumto verifi/
of snowor ice are not present.
thataccumulations
EICASSTATUSMESSAGE
L IDGFILTER
R IDGFILTER
L IDGOILTEMP
R IDGOILTEMP
L IDGTEMPSENS
R IDGTEMPSENS
PLACCARD
- L (R) GENCONTROLINOP
Electricalsystemcontrolpanelas appropriate
(O)
oPERATTONS
1.
J.
Leaveinoperative
GENCONTswitchin the OFFposition.
StartAPU.
After APU Start,observethat amberBUS OFF, APU GEN OFF and UTILITYBUS
OFFLightsarenotilluminated.
NOTE:Average fuel consumptionfor APU operation is 90 kg (200 lbs) per hour.
AFMperformance
decrementsneedto be appliedwhenoperatingthe APU inflight
(continued)
Page24-1
REV17 MAR1Ol2007
:*MV\V
Hungarian Airlines'fi
^ea?al'yat
.78.7
LIST
MINIMUM
EQUIPMENT
POWER
24. ELECTRICAL
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
24.00-2 APUOriven
Generator
C
0
Exceptfor ETOPS,maybe inoperative.
B
0
(M) Exceptfor ETOPSoperationsbeyond120 minutes,
provided:
maybe inoperative
a) Bothenginedrivengeneratorsoperatenormally,
b) At least one HydraulicMotor Generator(HMG) is
verifiedto oDeratenormallv.
PLACCARD
- APUGENINOP(REMOVED)
Electricalsystemcontrolpanelas appropriate
OPERATIONS
NOTE:
1, lf APU generatoris removed,accountfor effecton airplaneweightand balance.
2, Leaveinoperative
APUFENswitchin theOFFposition.
3. lf externalpoweris not available,accomplishbatterystartprocedure:
ElectricalPowerUp
A. Accomplishthe normalExteriorInspectionandSupplementary
procedure
to:
Establish
B. ElectricalPower.................
NOTE:Groundair sourcemustbe used.
ON
C. RightHydraulicElectricPumpSwitch.................................................
.........I or2
D. EngineIgnitionSelector
. OFF
..............
E. PackControlSelectors
NOTE: Packvalves,ifnot closedduringpreviousairplaneshutdown,mustbe closedby
groundcrewprior to enginestart.
ON
...............
F. lsolationValveSwitch
DOWN
.........................
G. Speedbrake
Lever..................
........................
CLOSE
H. ForwardThrustLever..............
DOWN
...................
I. Reverse
ThrustLever...................
SET
...............................
J. FlapLever
Positionflap leverto agreewith flap position.
"""" """""""""""' sET
K ParkBrake
CUTOFF
L. FuelControlSwitches..............
SET
..........
M. Left AudioSelector
Panel
N. Startoneengineusingusingstandbyengineindicator.ObserveEGT startlimit.
O. ContinuenormalPREFLIGHTorocedures.
Page24-2
REV17 MAR10/2007
..yUlEV Hungarian Airlinesfi
.787
^sZEjvaF
EQUIPMENT
LIST
MINIMUM
POWER
24. ELECTRICAL
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
DRIVE
24-{1-1 Generator
Lights
o
z
(M) Maybe inoperative
OFFprovidedassociatedEICAS
messageis verifiedto operatenormally.
(M) Maybe inoperative
OFFprovidedassociatedIDGis
disconnected.
PLACARD
- L (R)GENDRIVELIGHTINOP
systemcontrolpanelas appropriate
Electrical
or L (R)IDGDISC
24-25-1 HydraulicMotor
(HMG)
Generator
1)AirData
C
(ADC)
Computer
Equipped
Airplanes
maybe inoperative.
(O) Exceptfor ETOPSoperations,
and
normally,
IRS
operates
a) Center
b) Firstotficer'sIRSinstrumentsourceselect
EwitchoperatesnormallY.
for
maybe inoperative
Exceptfor ETOPSoperations,
dayVMCflight.
(O) For ETOPSoperations,up to 120 minutes,may be
provided:
inoperative
a) Both engine driven generators and the APU
generatoroperatenormallY,
b) CenterIRSoperatesnormally,and
c) Firstofficer'sIRSinstrumentsourceselectswitch
operatesnormally.
beyond120minutes,
(M)(O)ForETOPSoperations
provided:
maybe inoperative
andthe
a) Bothenginedrivengenerators
APUgeneratoroperatenormallY,
b) APU is startedbeforereachingthe ETOPS
untilwithin60
segment,thenoperatedcontinuously
minutesof an adequateairport,
c) CenterIRSoperatesnormally,
d) Firstofficels IRS instrumentsource
selectswitchoperatesnormally,and
are limitedto not morethan
e) Operations
threeflightdaysbeforerepairis made.
(continued)
Page24-3
REV17 MAR10/2007
:tMlEW
Hungarian Airlines,f
.ea7Et/ut=
.78.-
EQUIPMENT
LIST
MINIMUM
24. ELECTRICAL
POWER
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
2) Air DataInertial C
ReferenceSystem
(ADIRS)Equipped
Airplanes
(Continued)
0
a
maybe inoperative.
Exceptfor ETOPSoperations,
(M) For ETOPSoperationsup to 120minutes,may be
and
inoperativeprovidedboth enginedrivengenerators
the APU generatoroperatenormally.
may
(M) ForETOPSoperations
up to'120mrnutes,
provided:
be inoperative
a) Both engine driven generators and the APU
generatoroperatenormallY,
b) APU is staredbeforereechingthe ETOPSsegment,
untilwithin60 minutes
then operatedcontinuously
of an adequateairport,and
c) Operationsere limitedto not morethan threeflight
daysbeforerepairis made.
PLACARD
- L @GENDRIVELIGHTINOP
Electricalsystemcontrolpanelas appropriate
orL@IDGDISC
(O)
OPERATIONS
for ooerationof APU.
For ETOPS.observeMELreouirements
software(APM,INFLT)or the Flight
To determineAPUfuelflowutilizeBoeingperformance
Manual.Alternatively,
a conservative
averagefuelflowfor normal
PlanningPerformance
altitudes
is
cruise
75 kg perhour.
G2001300)
RDMIinformation
maybe lost.Captain's
lf allAC poweris lost,Captain's
RDMIinformation
SourceSelector
maybe recoveredby selectingALTNon the FirstOfficedsIRS Instrument
Panel.
EICASSTATUSMESSAGES
HYDGENVAL
C HYDGENVAL
L HYDGENVAL
R HYDGENVAL
Page24-4
REV17 MAR10/2007
;+'LA|'EV Hungarian Airlines4
.ezEt'yzF
'78'7
EQUIPMENT
LIST
MINIMUM
24. ELECTRICAL
POWER
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
24-25-2 HydraulicMotor
GeneratorValves
1)Air Data
C
Computer(ADC)
Airplanes
Equipped
L
0
maybe inoperative.
Exceptfor ETOPSoperations,
for
maybe inoperative
Exceptfor ETOPSoperations,
dayVMCflight.
(O) For ETOPSoperations,
up to 120minutes,maybe
provided:
inoperative
a) Both engine driven generators and the APU
generatoroperatenormallY,
b) CenterIRSoperatesnormally,end
sourceselectswitch
c) Firstofficer'sIRS instrument
operatesnormally.
(M) (o) For ETOPS operations,may be inoperative
orovided:
a) Both engine driven generators and the APU
generatoroperatenormallY,
b) APU is started before reaching the ETOPS
untilwithin60
segment,then operatedcontinuously
adequate
airport,
minutesof and
normally,
c) CenterIRSoperates
d) First officefs IRS instrumentsourceselect switch
operatesnormally,and
e) Operationsare limitedto not morethan threeflight
daysbeforerepairis made.
(continued)
Page24-5
REV17 MAR1Ol2007
Hungarian Airlines
.ttfrlEV
fi
.7Ez
.?A7Et/|YG
LIST
MINIMUM
EOUIPMENT
POWER
24. ELECTRICAL
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
2) Air DataInertial C
ReferenceSystem
(ADIRS)Equipped
Airplanes
c
1
1
0
maybe inoperative.
Exceptfor ETOPSoperations,
maybe
(M)ForETOPSoperations
up to 120minutes,
providedbothenginedrivengenerators
inoperative
operatenormally.
andtheAPUgenerator
(M) (O) For ETOPSoperations
beyond120 minutes,
provided:
maybe inoperative
a) Both engine driven generatorsand the APU
generatoroperatenormally,
b) APU is staredbeforereachingthe ETOPSsegment,
untilwithin60 minutes
then operatedcontinuously
of an adequateairport,end
c) Operationsare limitedto not morethan threeflight
daysbeforerepairis made.
EICASSTATUSMESSAGES
HYDGENVAL
C HYDGENVAL
L HYDGENVAL
R HYDGENVAL
(O)
OPERATIONS
ObserveMELrequirements
for operationof APU (ETOPSonly).
24-27-1 BUSOFFLights
C
2
1 (O) One may be inoperativeprovidedassociatedBUS
TIE ISLN Lightsand GEN CONT OFF light operate
normaly.
PLACARD
Affectedlight- LIGHTINOP
(O)
OPERATIONS
1. Afterstarting
enginesverifythatBUSTIEISLNlightsarenotilluminated.
2. VerifythatGENCONTOFFlightsarenotilluminated.
the bus is
3. lllumination
of boththe ISLNand GENCONTOFFlightsfor a bus indicates
for "Ac BusOff',
FollowOperations
unpowered.
Manualprocedures
Page24-6
REV17 MAR10/2007
tuMlEW
Hungarian Airlinesfi
,azEtjve.TE'7
LIST
MINIMUM
EQUIPMENT
24. ELECTRICAL
POWER
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
24-27.2 GENCONTOFF
Lights
B
2
'1 Onemaybe inoperative
generator.
for an inoperative
PLACARD
Affectedlight- LIGHTINOP
24.27-3 APUGENOFF
Light
C
1
(M) May be inoperativeprovided EICAS message
APU GENOFFverifiedto operateno.mally.
c
1
May be inoperativeprovidedAPU generetoris not
required
forflight.
PLACARD
Affectedlight- LIGHTINOP
24-27.4 BUSTIE ISLN
Lights
c
2
May be inoperativeprovidedthe associatedBUS OFF
lightoperatesnormally.
PLACARD
Affectedlight- LIGHTINOP
24.27-5 UTILITYBUSOFF
Lights
C
2
PLACARD
Affectedlight- LIGHTINOP
24-27-6 GenetatorFIELD
OFFLights
D
3
PLACARD
Affectedlight- LIGHTINOP
24-30-1 StandbyPower
BusOFFLights
C
1
PLACARD
Affectedlight- LIGHTINOP
provided:
(M) (O) Maybe inoperative
a) BothEICASsystemsoperatenormally,and
b) All other StandbyBus indicationsare verified
to operatenormally.
(continued)
Page24-7
REV17 MAR10/2007
tuGlEW
Hungarian Airlines
fi
.78'7
,?aTEtttVZF
EQUIPMENT
LIST
MINIMUM
24. ELECTRICALPOWER
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
(O)
OPERATIONS
standbypowerbus
Substitutethe STANDBYBUSOFFadvisorymessagefor the inoperative
the STANDBY
BUS
OFFlight.WhenSTANDBY
BUSOFFmessagecomeson,accomplish
OFFnon-normal
orocedure.
24-31-1APUBattery
C
1
0
provided:
(M) Maybe inoperative
and
a) APU is consideredinoperative,
b) APU batteryis not required.
NOTE:APU batteryis requiredif theAPU generatoris required.
TheAPU,andAPUgeneratorare requiredfor ETOPSdispatch
EICASSTATUSMESSAGES
APU BATNO STBY
24-31-2APUBattery
Charger
C
1
0
(M) May be inoperative
or deactivatedprovidedAPU is
not required.
NOTE1: Procedures
tor an operational
APUgeneratorrequirean operativeAPU,thereis no
MEL reliefbeyond120 minutesETOPSwithoutthe APU available.For more
informationon reliefwithoutAPU generatoravailable,regardingto ETOPS,see
MELitem24-00-2NOTE2: Understandard
dayconditions,
up to 3 APUstartsmay be madewitha fully
chargedAPU battery.
PLACCARD
As appropriate
Page24-8
REV17 MAR10/2007
.ryAAlEV Hungarian Airlinesfi
'787
,SZEt'yaF
LIST
EQUIPMENT
MINIMUM
24. ELECTRICAL
POWER
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
24-32-1 APUTransformer
Rectifier
D
1
0
thenstartingand usingthe APU
NOTE1: lf theAPUTransformer
Rectifieris inoperatwe,
requires theopeningandcollaring
of a circuitbreakerin theEE bay.TheAPU,
APU pneumatics, andAPUgeneratorare requiredfor ETOPSoperations.
NOTE:
MAINTENANCE
the followingstepis requiredto start
WhentheAPUTransformerRectifierUnitis inoperetive,
theAPU.
1. Openthe TRUAPUSTARTcircuitbreaker(C303)on the P32rightgeneratorpower
identifier.
oanelandattachDO-NOT-CLOSE
PLACCARD
As appropriate
Page24-9
REV17 MAR10/2007
Hungarian Airlines
;IMIEV
B
.7Ez
.?2TEI/VZF
LIST
MINIMUM
EOUIPMENT
POWER
24. ELECTRICAL
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
2441-1 ExternalPower
System
0
(O) May be inoperativeprovidedaltemate
procedures
areestablished
andused.
I) EXT PWR
AVAIL
Light
(Flight Deck)
0
(O) May be inoperativeprovidedaltemateprocedures
areestablished
andused.
2) EXT PWRON
Light
(FlightDeck)
0 (o) May be inoperativeprovidedaltemateprocedures
3) EXTERNAL
POWER
CONNECTED
Light
(Externalpower
panel)
0 (o) May be inoperativeprovidedalternateprocedures
4) EXTERNAL
POWERNOT
IN USELight
(Extemal power
panel)
0
andused.
areestablished
andused.
areestablished
providedalternateprocedures
(O) May be inoperative
and
used.
areestablished
PLACARD
As appropriate
(O)
oPERATTONS
procedures
flightdeckto ground
usinghandsignals,
1. Operators
mustestablish
alternate
lightsor system.
for inoperative
communication
systemsor othermeansto compensate
whenone (or more)external
2. Electricalloadsmaybe shedduringgroundoperations
power systemis inoperative.
Forexample,if a singleexternalpowersourceis usedfor
groundoperations, electricalpowermaynot be availablefor galleys,injlight
entertainment,
etc.
Page24-10
REV 17 MAR 1Ol2007
:*'l/lIEV
Hungarian Airlinesfi
787
EZEIIYE
LIST
EQUIPMENT
MINIMUM
25.EQUIPMENT/FURNISHINGS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
D
25-00-1 Crewmember
Shoulder
Herness
4
2
1.730TGLLeaflet26
i.a.w.JAR-OPS
25-11-1 FlightCrewSeats
1 ) PowerAdjustment
Any in excess of those requiredfor flight deck crew
members (including official observer in foMard
observer'sseat)maybe inoperative.
0
for eachflightcrewmember.
Maybe inoperative
-
Mustbe operativefor eachflightcrewmember.
system(if installed)
tl
ManualAdjustment
System
a) Horizontal
Adjustment
b) Verticaland
ReclineAdjustment
provided,for
(M) Oneor moremaybe inoperative
eachflightcrewmember:
(a) The associatedpowercontrolis operative.
OR
(b) The associatedseatis securedor lockedin a
positionacceptable
to the flightcrewmember.
c) Other
Adjustment
providedthe
(M) Oneor moremaybe inoperative
associatedseatis securedin a positionacceptable
to the flightcrewmember.
armrestwill hinderan
Note:lf an inooerative
evacuation
or anyotherflight
emergency
dutiesit shouldbe removed.
Thigh
d) Lumbar,
Supports,and
Headrests
(M) May be inop€rativeprovidedseat is acceptableto
affectedcrewmember.
25-11-2 ObserverSeats
i.a.w.JAR-OPS1.730TGLLeaflet26
providedthe seat
Oneor moremaybe inoperative
is not requiredand is correctlystowed.
NOTE : The pilot in commandwill determineif the
minimumsafety equipmentis functionalfor other
personsauthorized
to occupyanyobserverseat.
Page25-1
REV 17.MAR10/2007
t+MaEV
Hungarian Airlines
fi
787
EOE'YE
LIST
EQUIPMENT
MINIMUM
25,ESUIPMENT/FURNISHINGS
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
25-25-l CebinCrew Seats
i.a.w.JAR-OPS1.730TGLLeaflet26
(M)(O)Oneseator seatassemblymaybe
provided:
inoperative
(a) Inoperative
seator seatassemblyis not
occupied,
(b) Cabincrewdisplacedby inoperative
seat
occupiesthe passengerseat mostaccessible
exits,
to hisor herassigned
(c) Alternateprocedures
/
are established
approvedand usedfor displacedcabin
crew,
(d) Foldingtypeseatis stowedor securedin the
retractedDosition.
and
(e) Passengerseatassignedto cabincrew
"FORCABINCREWUSE
is placarded
ONL\/".
or missingseat
NOTE1:A seatwithan inoperative
beltor harnessis consideredinoperative.
useof
doesnotpreclude
NOTE2: Thisrequirement
passengerseatsby cabincrew
memberscaniedin excessof the required
cabincrewcomplement.
NOTE3: Anyaeroplanewhichis subjectto the direct
may
viewrequirements
of JAR25.783(h),
haveone of the requiredcabincrew
providedthe aeroplane
seatsinoperative,
base
doesnotdeoarta maintenance
can be
wherereoairsor replacements
maoe.
NOTE 4: lf one side of a dual seat assemblyis
inoperativeand a flightattendantis displacedto
the adjacentseat,the adjacentseatmustoperate
normaIy.
2) ExcessFlight
AttendantSeats
provided:
(M) Maybe inoperative
a) Affected seat position or seat assembly is not
and
occuDied.
or is secured
b) Foldingtype seat stowsautomatically
in the retractedoosition.
Page25-2
REV 17 MAR10/2007
.tufilEV
Hungarian Airlines
4
787
EZEU,UE
LIST
EQUIPMENT
MINIMUM
25,EOUIPMENT/FURNISHINGS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE 1: An automaticfoldingseat that will not stow
is consideredinoperative.
automatically
or missing
NOTE2: A seat positionwith an inoperative
restraintsystemis consideredinoperative.
PLACARD
lnoperativeseat- INOP
- FORFLIGHTATTENDANT
USEONLY
Passenger
seat(s)as required
(O}
OPERATIONS
The cabinattendantassignedto the affectedseat mustoccupya passengerseatas closeto or closer
thanthe nearestseatedpassengerto the associatedexit.The cabinattendantmustbe ableto reach
assigned
seat,i.e.,a 2
theassigned
emergency
exitin essentially
thesametimeas fromthe normally
"essentiallv
the sametime".
or 3 secondtimediffer€nceis considered
i.a,w.JAR-OPS1.730TGLLeaflet26
25-25-2 PassengerSeats
1) Underseat
Baggage
Bars
Restraining
D
(M) Oneor moremaybe inoperative
securedin the
uprightposition.
D
providedthe
(M) Oneor moremaybe inoperative
inoperative
seat:
(a) Doesnot blockan emergencyexit,
(b) Doesnot restrictanypassengerfrom
aisle,and
accessto themainaeroplane
(c) ls blocked
andplacarded
"DONOTOCCUPY".
or missingseat
NOTE:A seatwithan inoperative
beltrsconsideredinoperative.
provided:
(O) Maybe inoperative
(a) Baggageis not stowedunderseatwith
restraining
bar,
inoperative
"DO
(b) Associated
seat is placarded NOT
UNDERTHISSEAT",ANd
STOWBAGGAGE
(c) Procedures
to alertcabin
areestablished
bar.
restraining
crewof inoperative
Page25-3
REV.'17.MAR10/2007
:'|:'tAlEV Hungarian Anrlines
4
BZET'UE
787
LIST
MINIMUM
EOUIPMENT
25.EQUIPMENT/FURNISHINGS
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
2) Armrest
D
-
-
(M) (O) May be inoperativeor missing and seat
occupiedprovided:
Exit,
a) Armrestdoesnot blockan Emergency
b) Armrestdoesnot restrictany passengerfromaccess
to the mainaircraftaisle,and
c) For an armrestwith a reclinemechanism,seat is
securedin theuprightposition.
PLACARD
Atfectedseat- DO NOTOCCUPY
UNDERTHISSEAT
Baggage
Restraining
Bars- DO NOTSTOWBAGGAGE
Underseat
(O)
OPERATIONS
1. Foran inoperative
RESTRAINING
BAR,ensurecabincrewis
UNDERSEAT
BAGGAGE
notifiedof the inoperative
restraining
barandthat baggageis notto be placedunderthe
associatedseat.
armrestand
2. Foran inoperative
ARMREST,ensurecabincrewis notifiedof the inoperative
MEL
remarks
that
are met.
C 5
0
25-25-5 CrewrestBunk
Restraint
PLACARD
Bunk- DO NOTOCCUPY
Associated
I
(M) May be inoperativeprovidedassociatedbunk is
- DO NoT USE.
INOPERATIVE
blocked
andDlac€rded
25-28-1 OverheadStorage
Bin(s)/Cabin
and
GalleyStorage
Compartment€,/
Closets
C
-
-
provided:
(M) Maybe inoperative
to securecompartment
a) Proceduresare established
CLOSED,
is not usedfor storageof emergency
b) Compartment
equipment,
and
is not usedfor storageof any
c) Affectedcompartment
affixed.
item(s)exceptfor thosepermanently
NOTE:lf no partitionsare installed,the entireoverhead
one bin.
areconsidered
storagecompartments
'1)Multi
Latch/Ouarter
Turn
Lug Installations
C
-
-
One latch./lugper compartmentmay be inoperative
provided:
affected
Remaining latch(es/lug(s) on
a)
compartmentsoperatenormally, and
is usedfor a galleycart,the
b) If affectedcompartment
cart rcmainsempty.
PLACARD
COMPARTMENTINOPERATIVE- DO NOT USEFOR STORAGE
Page254
REV.17.MAR10/2007
;*'HIEW
Hungarian Airlines
4
EZETUE
787
EQUIPMENT
LIST
MINIMUM
25. EQUIPMENT/FURNISHINGS
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
25-38-1 LavatoryDoor
Ashtrays
B767-200
8767-300
a
t
7
-
?
o
J
-
25-38-2 GelleyWaste
Access
Receptacle
Doors/Covers
provided:
(M) (O) Maybe inoperative
a) Containeris empty and the access is securedto
preventwaste introductioninto the cimpartment,
ano
b) Proceduresare esteblishedto ensure sufficient
galley waste receptacles arc available to
accommodate
all wastethat may be generatedon
the flight.
(OI
OPERATIONS
all wastethatmaybe
Ensurethatsufficientgalleywastereceptacles
are availableto accommodate
generatedon the flight.
25-d1-1 LavatoryWaste
Container
Flapper/Access
Doors
4
provided:
(M) Maybe inoperative
a) Associatedlavatorywaste containeris emptyand
into
accessis securedto preventwasteintroduction
thewastecontainer,
and
b) Lavatoryis onlyusedby crewmembers,
c) Associatedlavatoryentrancedoor is lockedclosed
- DO NOTENTER.
and placardedINOPERATIVE
NOTE: These provisionsare not intendedto prohibit
by crewmembers.
lavatoryuseor inspections
PLACARD
As appropriate
C
25-50-1 LowerCargo
Compartment
LiningPanels,Floor
Panels,and
Walkways
-
or missingprovidedprocedures
May be damaged
remalnsempry
a) Associatedcompartment
OR
arecarried.
materials
b) Onlynoncombustible
25-53-1 CargoLoading
System
1
NOTE:Any portionof system(s)that op€ratesnormally
mavbe used.
D
Page25-5
REV.17.MAR10/2007
,.+'LA,EV Hungarian anrfines
4
7A7
E?EtlvE
LIST
EQUIPMENT
MINIMUM
25. EQUIPMENT/FURNISHINGS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(M) May be inoperative
or missingprovidedacceptable
cargo loadinglimitsfrom an approvedsource,i.e., an
ApprovedCargo LoadingManual, Cargo handling
Manual, or Weight and Balance Documentare
observed.
May be inoperativeor missing providedassociated
remainsempty.
cargocompartment
25-54-1CargoRestraint
System/Devices
25-60-1 PortableProtective D
Breathing
Equipment
(PBE)
-
-
i.a.w.JAR-OPS1.780TGLLeaflet26
(M)Any in excessof thatrequiredmaybe
inoperative
or missingprovidedthe inoperative
removedfromthe
PBEis placardedinoperative,
location,
andplacedoutof sightso it
installed
cannotbe mistakenfor a functionalunit.
i.a.w.JAR-OPS1.825TGLLeaflet26
Any in exessof the minimumrequiredmay be missing
provided:
or inoperative,
lifejacketis placarded
a) Inoperative
removedfromthe installed
inoperative,
locationand placedout of sightso it cannot
unit,and
fora functional
be mistaken
25-62-1 FlotationEquipment
(Crewand
Passengers)
(b) Requireddistribution
of serviceable
lifeiacketsis maintained-
25-63-1Megaphones
D
.
Any in excess of the required quantity, may be
inoperative
or missingprovided:
a) Inoperative megaphone is removed from the
passenger
cabin,and
b) Requireddistributionis maintainedthroughoutthe
entirepaxcabin:
- one in the fwdwardrobetop box,and
- one in the aft zoneof f,^,dDaxcabin,
25-63-2 Emergency
Evacuation
Signal
System
D
1
May b€ inoperativeprovidedalternateproceduresare
used as the primarymeansof initiatingan emergency
evacuation.
Page25-6
REV.17.MAR10/2007
t!#lEW
Hungarian Airlinesh
EZElUE
7A7
LIST
MINIMUM
EQUIPMENT
25. EQUIPMENT/FURNISHINGS
REPAIRINTERVAL
NUiNBERREQUIREDFORDISPATCH
REMARKOR/ANDEXGEPTIONS
NOTE
OPERATIONS
Evacuationproceduresvary considerably
betweenoperators.The individualoperatorshoulddevelop
procedureswith the EmergencyEvacuationSignal System inoperative.These procedureswould
probablymake use of the P.A. and/orCabin/Service
Interphonesystems.Priorto flightthe pilot an
thatwill be used.
commandshouldbriefcabincrewmemberson the emergencyprocedures
-
25.63-3 FASTENSEAT
BELTWHILE
SEATED
Signsor Placards
25-634 Flightattendant
Flashlight
Holder
Assemblies
U
C
Locator
25-63-5 Emergency
(LTD)
Transmifter
D
-
25-64-1 EmergencyMedical
Equipment
One or more signs or placardsmay be illegibleor
missingprovideda legiblesign or placardis readable
fromeachoccupiedpassengerseat.
May be inoperativeor missingprovidedcrewmember
assigned to associated seat has a flashlight of
readilyavailable.
equivalentcharacteristics
i.a.w.JAR-OPS1.820TGLLeaflet26.
providedrepairsare made
Maybe inoperative
within6 furtherflightsor 25 flyinghours,whichever
occursfirst.
Any in excessof thoserequiredmaybe
inoperative.
1.755TGLLeaflet26.
i.a.w.JAR-OPS
Any in excessof thoserequiredmaybe
inooerative.
i.a.w.JAR-OPS1.745TGLLeaflet26.
lf morethanone is required,onlyone of the
for a
requiredflrstaid kits maybe incomplete
days.
maxrmum
of 2 calendar
1) FirstAidKits
A
3
2) Emergency
MedicalKits
A
1
i.a.w.JAR-OPS1.755TGLLeaflet26,
The requiredemergencymedicalkits maybe
whererepairs
for flightto a destination
incomplete
not
to exceeda
made
but
replacements
can
be
or
days.
maximum
of 2 calendar
3) Automated
A
External
(AED)
Defibrillators
and/orAssociated
Equipment
1
maybe
The requireddeflbrillator
whererepairs
for flightto a destination
incomplete
can be madebut notto exceeda
or replacements
days.
maximum
of 2 calendar
Page25-7
REV.17.MAR10/2007
,I*MIEW Hungarian Airlinesfi
.AAEIIYE
Zez
LIST
EQUIPMENT
MINIMUM
25.EQUIPMENT/FURNISHINGS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
25-66-3 OverwingEscape A
SquibTestSystem
1
0
provided:
(M) Maybe inoperative
a) The overwingescapesystemis verifiedto operate
normally,
and
b) Operationsare limitedto not more than 50 flight
hoursbeforereDairsare made.
Page25-8
REV.17.MAR10/2007
;*'AIEW
Hungarian Airlines
4
.787
.azrEtlvGF
EQUIPMENT
LIST
MINIMUM
26. FIREPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
26-10-1CrewRestSmoke C
DetectionSvstems
2
0
provided:
(M) Maybe inoperative
a) Associatedcrew rest area is not usedand personal
itemsare removed,and
b) Associatedcrewdooris lockedclosedand placarded
- DO NOTENTER
INOPERATIVE
NOTE:Theseprovisosare not intendedto prohibitcrew
by crewmembers.
restareainspections
PLACARD
Associateddoor- INOPEARATIVE
26-11-'l EngineFire
DetectionSystem
2
Exceptfor ETOPSoperationsbeyond120 minutes,one
loopperenginemaybe inoperative.
4
2
Exceptfor ETOPSoperationsbeyond120 minutes,one
loopperenginemaybe inoperatlve.
4
4
ETOPSbeyond120minutes.
1) DetectionLoops
EICASSTATUSMESSAGES
L ENGFIRELP .1
L ENGFIRELP2
R ENGFIRELP 1
R ENGFIRELP2
PLACARD
As appropriate
26-'ll-2 EngineOverheat
DetectionSystems
1) DetectionLoops
C
EICASSTATUSMESSAGES
(R) L ENGOH LP 1
(R) L ENGOH LP2
Page26-1
REV.17.
MAR10/2007.
Hungarian Airlines
/lMlEV
B
.7Az
.ZZTGt''YZF
MINIMUM
EOUIPMENT
LIST
26, FIREPROTECTION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACARD
As appropriate
26-14.1 CARGODETAIR C
IndicatingSystem
1
(M) Indicationmay be inoperetiveprovidedthe smoke
sampling system integrity is verified before each
deoarture.
EICASSTATUSMESSAGES
CARGODETAtR (-200/-300)
PLACARD
As appropriate
26-15-1 APU FireDetection
System
1), Detection
, Looos c
2
c
2
Exceptfor ETOPSbeyond120minutes,one loopmay
be inoperative.
provided:
(M) Maybe inoperative
a) APU is operatedon the groundonly,
monitored,
b) APUis continuously
c) APUexternalcontrolsystemoperatesnormallyand
d) APU is shutdownbeioretaxi.
for ETOPSdispatch,
NOTE: 1.TheAPUandAPUgenerator,
maybe required
2. Proceduresfor an operationalAPU generatorrequirean operativeAPU,thereis
Formore
no MELreliefbeyond120minutesETOPSwithoutthe APUavailable.
informationon reliefwithoutAPU generatoravailable,regardingto ETOPS,see
MELitem24-00-2.
EICASSTATUSMESSAGES
APUFIRELP ,1
APUFIRELP2
PLACARD
NearEICAS- APUFIRELOOP1 (2)INOP
Page26-2
REV.17MAR10/2007.
:!'l/iIEV
Hungarian Airlines4
.garEtt'vzF
.7Ez
LIST
EQUIPMENT
MINIMUM
26. FIREPROTECTION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
26-16-1 LowerCargo
Compartment
Fire
DetectionSystems
(FWDandAFT)
2
0
provided:
Oneor bothsystemsmaybe inoperative
remains
empty.
a) The associated compartment
or
materialsare carried.
b) Onlynon-combustible
(M) One may be inoperativein each compartment
provided remainingdetector is verified to operate
normallybeforeeachdeparture.
in eachcompartment.
Onemaybe inoperative
1) Detectors
C
4
2
2) DetectorFans
C
4
2
EICASSTATUSMESSAGES
AFT CARGODET,1
AFT CARGODET2
CARGODETAIR
FWDCARGODET,1
FWDCARGODET2
PLACARD
As appropriate
(O)
oPERATTONS
procedures
remainsemptyor
Usethe established
to verifythe associatedcompartment
(ballast
maybe loadedin ULDs),
equipment
contains
onlyballast,
emptycargohandling
or fly awaykits.The operator'sMELmustdefinewhichitemsare approvedfor inclusion
in the fly awaykitsandwhichmaterialscan be usedas ballast.(seeCombustible
Materials)
26-17-1WheelWellFire
DetectionSystem
8767-300
C
1
0
providedBrakeTemperature
(M)(O)Maybe inoperative
(BTMS)operates
normally.
lndications
of retracttngan overheated
NOTE: Avoidthe possibility
wheel by monitoring brake temperature
indications.
(continued)
Page26-3
REV.17.
MAR10/2007.
t!'lAlEV
.AZEttlYZF
Hungarian Airlines,fi
.7Ez
LIST
MINIMUM
EOUIPMENT
26. FIREPROTECTION
REPAIR INTERVAL
NUMBERREQUIRED
FORDISPATCH
REMARKOR/ANDEXCEPTIONS
8767-200
C
1
0
providedan accepted
(M) Maybe inoperative
orocedureis usedto ensurebrakesare cool
beforeenginestart.
of retractingan overheated
NOTE: Avoidthe possibility
wheelby leavingthe landinggearextendedfor
ten minutesaftertakeoff.In caseof engine
gearshouldbe
failureafterV1, landing
retracteduntiltakeotfobstaclesare cleared.
of ice
Pilotsmustconsiderthe possibility
gearextended
during
withlanding
accumulation
winterooerations.
PLACARD
then,placardadjacentto WHL
In the eventall fourfiredetectorsensorsare inoperative,
lf
of
sensorsare
WELLFIRElight WHLWELLFIREDETINOP. any thefiredetector
FIRE
lightwill
the
WHL
WELL
operative,
thenthatsensorwill
normally,
and
operate
illuminateif that sensordetectsa fire.
OPERATIONS
NOTE
1. A conservalive
deltafuel burnincreasefor leavingthe landinggearextendedfor 10
minutesis 970k9.
whendispatching
adjustments
2. lt is not necessary
to applygeardownperformance
underthisitem.
Page264
MAR10/2007.
REV.17.
I+U,EV
Hungarian Airlines,fi
EarEtjuaF
.74-
LIST
EQUIPMENT
MINIMUM
26, FIREPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
25-18-1 DUCTLEAK
DetectionSystems
1) L or R Loop
C
1
1
4
2
Oneloopin eachsystemmaybe inoperative.
-
1
provided:
M) (O) Maybe inoperative
ENGBLEEDswitchremainsOFF,
a) Associated
b) Associatedbleed ISLN valve remainsclosed
exceptfor enginestart,
c) Airplaneis not operatedin known or forecast
icingconditions,
remainsat or belowFL 270
d) Airplane
e) APUis usedas an air sourceduringtakeoffand
landing.
f) Onebodyloopsoperatesnormally,and
fan air modulation
g) For GE engines,associated
position,
valveis securedin the intermediate
h) For GE engines, appropriate performance
and
areapplied,
adjustments
i) Operationis limitedto one flight only, before
repairsare made.
provided:
(M) (O) Maybe inoperative
a) Associated
ENGBLEEDswitchremainsOFF,
b) AssociatedbleedISLNvalveremainsclosedexcept
for enginestart,
c) Airplaneis not operatedin knownor forecasticing
conditions,
remains
at or belowFL270,
d ) Airplane
penalties
areapplied
ADPinoperative
f) Center HydraulicMotor Generatoris considered
inoperative,
One
bodyloopoperatesnormallY,
s)
h ) For GE engines, associatedfan air modulation
position,
valveis securedin the intermediate
performance
appropriate
D For GE engines,
and
adjustments
are applied,
i) Operationis limitedto oneflightonly,beforerepairs
aremaoe.
Page26-5
REV.17.
MAY30/2007.
tVUaEV Hungarian Airlines
fi
78.7
EArEtjve
LIST
EQUIPMENT
MINIMUM
26. FIREPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
A
-
1
provided:
(O) Maybe inoperative
switchremainsOFF,
Associated
ENG
BLEED
a)
b) AssociatedbleedISLNvalveremainsclosedexcept
for enginestart,
c) Airplaneis not operatedin knownor forecasticing
conditions,
remainsat or belowFL270,
d ) Airplane
e) APU is used as an air sourceduringtakeoffand
randrng
One
bodyloopoperatesnormally,
0
g) For GE engines, appropriate performance
adjustmentsare applied for an open fan air
modulation
valve,and
h) Operationis limitedto one flightonly,beforerepairs
aremade.
1
provided:
(O) Maybe inoperative
ENGBLEEDswitchremeinsOFF,
a) Associated
b) AssociatedbleedISLNvalveremainsclosedexcept
for enginestart,
c) Airplaneis not operatedin knownor forecasticing
conditions,
d ) Airplaneremainsat or belowFL 270,
penaltiesare applied,
ADP inoperative
f) Center HydraulicMotor Generatoris considered
inooerative,
s) Onebodyloopoperatesnormally, performance
h ) For GE engines, appropriate
adjustmentsare applied for an open fian air
valve,and
modulation
i) Operationis limitedto one flightonly,beforerepairs
aremaoe.
(continued)
Page 26-6
REV.17.MAR 10/2007.
:fr4lEW
HungarianAirlines,rt
.AarEtlUZF
.78-
EQUIPMENT
LIST
MINIMUM
26. FIREPROTECTION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2) BodyLoop
provided:
(O) Maybe inoperative
a) APU is not usedas a pneumaticsourceexceptas
requiredfor enginestart,
b) APU bleedair switchremainsoff exceptrequiredfor
enginestart,
c) CenterbleedISLNvalveremainsclosedexceptas
requiredfor enginestart,
penaltiesare applied,
performance
d) ADP inoperative
e) Both center system electric pumps operate
normally,
f) Airplaneremains
at or belowFL270,
g) Center HydraulicMotor Generatoris considered
inoperative,
and
h) OneL andone R loopoperatenormally.
3) TestFunction
(M) May be inoperativeprovideddetectionsystem is
verifiedoperativeonceeachflightday.
NOTE1: The 767airplaneshaveeithera singleloopor dualloopDuctLeakDetection
system.Bothsystemshavea testfunction.
NOTE2: On the singleloopsystem,MMELreliefexistsfor (a) up to threeof the four loopsin
the (1, R) system,(b) bothbodyloops,and (c) the testfunction.
NOTE3: On the dualloopsystem,MMELreliefexistsfor (a) up to threeof the four loopsin
the (1, R) system,(b) bothbodyloops,and (c) the testfunction.
valve(FAMV)canbe (1)
NOTE4: ForL or R loopInoperative:
Thefanair modulation
position,or (2) allowedto be drivenfull
securedby maintenance
in the intermediate
BLEEDswitchoFF - no
Regulating
Valve(ENGINE
openbytheclosedPressure
penalty
withthe FAMVin the
maintenance).
The performance
associated
positionis lessthanthe penaltyassociated
withthe FAMVin the full
intermediate
openposition.
is inoperative.
NOTE5: TheHMGis required
for ETOPSroutesif an IDGor APUgenerator
The HMGis notrequired
for nonETOPS:
NOTE6: The HMGis requiredfor ETOPSroutesif an IDGor APUgeneratoris inoperative.
The HMGis not reouiredfor non-ETOP
Page26-7
MAR10/2007.
REV.17.
.;*MLEV Hungarian Airlines
B
.7Ez
^aaTEttlYZF
LIST
EQUIPMENT
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
EICASSTATUSMESSAGES
L STRUTDCTLP 1
L STRUTDCTLP2
L DUCTLEAKLP 1
L DUCTLEAKLP 2
BODYDUCTLP 1
DUCTLEAKLP
R STRUTDCT LP ,I
R STRUTDCT LP 2
R DUCTLEAKLP 1
R DUCTLEAKLP 2
BODYDUCTLP2
PLACKARD
- DUCTLEAKDETLOOP/TEST
INOP
As appropriate
OPERATIONS
{OI
Valvesecured
maintenance
has FanAir Modulation
1. For Leftor RightLoopsinoperative,
position,
in intermediate
andAPUis available:
off,thereforeusetheAPUas the
A. The affectedENGBLEEDvalvemustbe maintained
airsourcefortheADP.
B. CF6:Reduceperformance
limitedweightsfor takeoff,landingand enrouteclimbin
(O) procedurefor a FAMVsecuredin the
withltem 36-12-2Operations
accordance
position.
intermediate
Valvesecured
hasFanAir Modulation
maintenance
2. For Leftor RightLoopsinoperative,
position,
in intermediate
andAPUir notavailable:
off,thereforeapplyADP
A. The affectedENGBLEEDvalvemustbe maintained
penalties
(available
inoperative
in ltem29-11-3).
andenrouteclimbin
limitedweightsfor takeoff,landing
B. CF6:Reduceperformance
for a FAMVsecuredin the
withltem 36-12-2Operations(O) procedure
accordance
intermediate
oosition.
C. TheADPwill notoperate,thereforethe HMGwill notoperate.ETOPSflightsrequire
threeelectricalsourcesto be available.The HMG cannotbe countedasoneofthe
ETOPSelectricalsourcesin this MEL situation.
(ENGINE
BLEEDswitchOFF- no maintenance
3. ForLeftor RightLoopsinoperative,
actiontaken),andAPUis available:
off,thereforeusetheAPU as the
A. The affectedENGBLEEDvalvemustbe maintained
air sourcefor the ADP.
B. CF6-80C2:TheFanAir ModulationValveis drivenfull openby a closedPressure
limited
RegulationValve(ENGINEBLEED s\i/itchOFF).Reduceperformance
withltem 36-12'2
weightsfor takeoff,landingandenrouteclimb in accordance
(O) procedurefor a full openFAMV.
operations
Page26-8
MAY30/2007.
REV.17.
,;*EIEW
^aarEtlve
Hungarian Airlines
4
.787
LIST
EQUIPMENT
MINTMUM
26. FIREPROTECTION
REPAIRINTERVAL
NUMBERREQUIRED
FORDISPATCH
REMARKOR/ANDEXCEPTIONS
(ENGINE
BLEEDswitchOFF- no maintenance
4. ForLeftor RightLoopsinoperative,
actiontaken).andAPUis notavailable:
off, thereforeapplyADP
A. The affectedENGBLEEDvalvemustbe maintained
penalties
(available
inoperative
in ltem29-11-3).
B. CF6-80C2:The FanAir Modulation
Valveis drivenfull openby a closedPressure
limitedweights
Regulating
Valve(ENGINE
BLEEDswitchOFF).Reduceperformance
with ltem36-12-2operations(O)
for takeoff,landingand enrouteclimbin accordance
procedure
for a full ooenFAMV.
C. The ADPwillnot operate,thereforethe HMGwill notoperate.ETOPSflightsrequire
threeelectricalsourcesto be available.The HMGcannotbe countedas one of the
ETOPSelectricalsourcesin this MELsituation.
5. For BodyLoopinoperative:
penaltiesin accordance
with
A. TheADPwill notoperate,applyADP inoperative
(O) procedure.
Item29-11-3Operations
B. TheAPUshallnot be usedas a pneumaticsourceexceptas requiredfor enginestart.
The APUcan be usedas an electricalsource.
C. TheADPwill notoperate,thereforethe HMGwill notoperate.ETOPSflightsrequire
threeelectricalsourcesto be available.The HMGcannotbe countedas one of the
ETOPSelectricalsourcesin this MELsituation,Thetwo lDGsandAPUgeneratordo
fulfillthisETOPSreouirement.
D. With bothbodyloopsinoperative,
the APU BLEEDair valveis OFFand Centerbleed
ISLNvalveis closedso heatis notavailableto theAFT and BULKcargo
maybe impacted.
compartments.
Carriage
of animalsand/or perishables
Page26-9
MAY30/2007.
REV.17.
tyUaEV
Hungarian Airlines
4
.?aTEt'yzF
-a.7
EQUIPMENT
LIST
MINIMUM
26. FIREPROTECTION
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
FireBTLDISCH
Lights
(M) May be inoperativeprovidedthe test procedureis
used once each flight day to verify that associated
bottle(s)is properlycharged.
1 ) Engine,
APU,
LowerCargo
Compartments
providedfire extinguisher
systemfor
Maybe inoperative
is inoperative.
lowercompartment
z l LowerCargo
Compartments
(O) May be inoperative provided procs),.edores
established and used to ensure the associated
compartmentremainsempty,or is verifiedto contain
ballast(ballast
only emptycargohandlingequipment,
associated
Fly Away
and/or
in
ULDS)
may be loaded
Kits.0
materials"in the Preamble
NOTE:see"non-combustible
3) APU
c
2
C
2
0
providedAPU is not used.
Maybe inoperative
Procedures
may be requiredfor ETOPSdispatch.
NOTE: The APU,and APU generator,
I
APU,thereis no MELreliefI
requirean operative
APUgenerator
for an operational
For moreinformation
on I
beyond120minutesETOPSwithoutthe APU available.
reliefwithoutAPUgeneratoravailable,regardingto EToPS,see MELitem24-00-2
PLACARD
Atfectedlight- LIGHTINOP
26-20-2 FireExtinguisher
SQUIBTEST
System
1 ) APUSquibLight
0
(M) May be inoperativeprovidedthe squib circuit is
verifiedto operatenormallyonceeachflightday .
0
May be inoperative provided APU is considered
and not used.
inoperative
I
(continued)
Page26-10
REV17.MAR10/2007.
I*MIEW Hungarian Airlines
fi
.7e,7
.??Et'yzF
EQUIPMENT
LIST
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2) CargoSquibLights C
3
0
C
3
0
C
1
0
3) CargoSquibTest
system
systemis
May be inoperativeprovidedfire extinguisher
inoperative.
(O) May be Inoperativeprovidedassociatedcargo
remainsemptyor only non-combustible
compartment
materialsarecarried.
(O) May be inoperativeprovided proceduresarel
established and used to ensure the associated
I
compartmentremainsempty,or is verifledto containI
ballast(ballast
only emptycargohandlingequipment,
I
maybe loadedin ULDS,and /or FlyAwayKits.
I
"non-combustible
materials"in the MELI
\!qlE: see
Preamble
I
Procedures
for ETOPSdispatch.
NOTE: The APU,andAPUgenerator,
maybe required
I
for an operational
APU generatorrequirean operativeAPU,thereis no MELreliefI
beyond120 minutesETOPSwithoutthe APU available.For more informationon I
regarding
to ETOPS,
reliefwithoutAPUgenerator
available,
seeMELitem24-00-2.
PLACARD
- INOP
Testswitchat P61whenthe systemis inoperative
Affectedlight- LIGHTINOP
26-22-1APUFire
Extinguisher
System
0
A
Except for ETOPS operations,may be inoperative
Drovided
theAPUis notused.
(M) Exceptfor ETOPSoperationsbeyond12ominutes,
provided:
maybe inoperetive
a) APUis notused,
b) Bothenginedrivengeneratorsoperatenormally,
c) At leastone HydraulicMotorGeneratoris verifiedto
operatenormally,and
d) Repairsare madewithinthreeflightdays.
(continued)
Page26-11
MAR10/2007.
REV.17.
rtElEW
Hungarian Airlines4
^az7EtjvzF
.747
LIST
EQUIPMENT
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
for an
may be requiredfor ETOPSdispatchProcedures
NOTE: The APU, and APU generator,
'120
operationalAPU generatorrequirean operativeAPU, there is no MEL reliefbeyond
minutesETOPSwithoutthe APU evailable.For more informationon reliefwithoutAPU
generatoravailable,regardingto ETOPS,see MELitem24-00-2.
PLACARD
As appropriate
26-23-1 LowerCargo
Fire
Compartment
Extinguisher
System
(Meteredor Non
MeteredSystem)
1) TwoandThree
BottleSystems
0
providedprocedures
are
(O) Maybe inoperative
and usedto ensurethe lowercargo
established
remainempty,or are verifledto contain
compartments
materials.
onlynon-combustible
"non-combustible
materials"in the MEL
AIqtE: see
Preamble
-
(O) Extinguisherbottle No. 2 or 2A and associated
indicationsmay be inoperative,with cargo carried in
compartmentsprovided:
and
a) Airplaneis operatedpressurized,
provided
determine
the
timethe airline
to
A
chart
is
b)
to a suitable
airport..
mustremainin proximity
PLACARD
As appropriate
(O)
oPERATTONS
to verifythe associatedcompartment
I . Operatorsmustestablishand use procedures
(ballast
equipment
cargo
handling
empty
remains
emptyor contains
onlyballast,
maybe loadedin ULDs),or fly awaykits.The operator'sMELmustdefinewhich
itemsare approvedfor inclusionin the fly awaykitsandwhichmaterialscan be used
as ballast.
NOTE1: The 767 passengeraircrafthavetwelvedifferentLowerCargo
The followingpages
FireExtinguisher
SystemCombinations.
Compartment
The
DESIGNATED
systems
operate.
the
various
haveinformation
on how
whichmaydifferfromthe
NAMEcolumnhasthe assignednomenclature,
TIME
PROTECTION
actualcertified
timelimitsin theFAAAPPROVED
BOTTLE
column(seeDDG# C, F, G, H, andJ).TheBOTTLENUMBER,
howa fully
METHOD
columnsindicate
TYPE,andDISCHARGE
bottle
operational
systemworks,The lastcolumnindicatesthe inoperative
Page26-12
REV.17.
MAR10/2007.
tVUIEV Hungarian Airlines
4
.7Ez
.?ZEtrtYZt
LIST
MINIMUM
EQUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
airport.
andmaximumnumberof minutesa flightcanbe froma suitable
rangetime(AFM
NOTE2: ForETOPSairplanes,
theAFMhasan approved
*'*
Limitation
sectionstatesthatthe flightshallremainwithin minutesof a
a 15 minute
rangetimeconsiders
TheAFMapproved
suitable
airport).
Timeequatesto
diversion,thusa 157minuteFAAApprovedProtection
(157-15\142minuterangetimefroma suitable
airport.
NOTE3: The BOTTLEryPE columnrefersto threetypesof bottles.KNOCK
agentthroughan open
DOWNbottlesprovidea dischergeof suppression
nozzlefor initialfire knockdown.DUMPbottlesarethe sameas KNOCK
DOWNbutareactivatedaftera timedelay.METEREDbottlesmaintaina
prescribedlevelof suppression
througha metered
agentconcentration
nozzlesystemfor noteddurationof fire suppression.
NOTE4: The tablesarewrittenfor airplaneswithoutforwardcargoair conditioning
(in DESIGNATED
NAMEcolumn)
otherwise
unlessspecified
JCErql&lE&
LliEr8n.[hd
Hunc
3
t ll||nui.
lystcrn
Bsttlc Typ.
)y5Etr
Appmvcd
Pmtc tion
Iirnc
Trpc
I
SFtcm
g0
MiDuler
(ll
Du.tlSwihh
Dirchrgc
55 LBS.
Knoclt
Do*n
Llunl Sr'.lEt
Dircftrryc
I
l3 LBS.
Dump
Scc,lrrdBsttlc
Dirche€c Sv.itch 30
MinutcrshcrKnelc
Dcvm Dircharge
(.4 - 10 Minub6
TA
J5 LBSDunp
Ttitd Botdc
Dirchrrgc-t0
Minute Timc Dcl.ry
aftcr SccondEottlc
DircIrrgc
(?A) - 60 Minutcr
Macrcd
I
B ll0 Mituk
llopsriv. gdttE { r
Prtnhcris - Fligllt
Rcmrins rA'ithin3
Minutsr b SuiEblc
AuFofi
lt Lus.
Knock
Do*n
3t LBS.
D*"p
6U
It{inntcs
DlschEBc M.thod
NonMdclEd
lnd Dischtgc
S$/iht lrl lvliourca
aftcr Kaock Dornt
Dirdrrtgs
lJj - l0luiltuEi
(lt
Page26-13
MAR10/2007.
REV.17.
.ttfrLEW Hungarian eirfines4
.7A7
.?zrEttyaF
LIST
MINIMUM
EQUIPMENT
26. FIREPROTECTION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIREO
REMARKOR/ANDEXCEPTIONS
767.lmflooEn
l..l'crlgfthd
Narnc
!3
C IJU Mmrdc
Syrhlm
BsttL fyp(
FAA
li',!tm
Trp
Approrcd
PrDfrcctio]r
Timc
t:/
M inucs
MrErcd
I
:A
2
D lvf M nutc
t9:
Syrlcm
Minutcc
IUct!rcd
l
E l9l Mnuc
SI"t"-
Mctcr(d
I
MinrE!
On
A irplanc:
Dirdargc Mcthod
J! Ltss.
KnocL
Down
55LBS.
Ntctcrrd
ll LBs.
McEr€d
Erlglc 5*tch
Dischugc
l5 L BS.
Knock
Down
lrurlc Ss tch
DireItgc
All Bctdc! (KrocL
Dovm tnd Botlr
Mctcrcd Eoftlcsl
DircluEc d thi
SsrncTlrnc
80 LBS, All EottLc, (Xno{k
Ir{ctcced Do*a sJd Bot[
M.rscJ Botrl.r)
t3 LBti. Disctr+c t rhc
McErrd
Ss!. Timc
:: Ltts.
Knoclc
Dovn
5irg]. Swdch
I
For*srd
Cigo
Conditioncd
Ar
All Bonlcr(Knock
Dcpn urd Eoth
M€ldrd Bottlcai
_11LBS. llircluE d th.
Mcrtftd
Ssnc Trmc
E;I!!4!!IB
urrrSndkd
I5
Nffi.
Bottlc TyF
l)sEm
Apguwd
PrpEcti,:n
Dischrgc Mcdrod
Trr.
l
B
F 60 Mrnuk
sl'!tEm
PRR
Bl186-r.5
incorpontrd
9u
Minuica
MctEr.d
2
TUL 85.
Krlod(
Dowr
3:TLBS.
IMcEtd
(ll-N,A
(lA)-60 Minutcr
(2) - 90 Minutr
NrA
(2A)-60Minutt
(!) - 110Minrncr
r)
Dirchrrgc
92 LBS.
McierEd
\rt$
ldopaarirwBot r#r!
Purn}crb - Flight
Rcfleill' Withitr #
Mirlrtcg ts Suitrbh
AttFofi
Si'lgh S\r'nch
Dirchr4e
Mctred Bottl<
Dirclcgcs l0
M inttcr Trmc Dclay
aft6 First Bottlc
r.?A)- -t0Miruut
(21-110Minucr
InoFcrriv. got{c # ln
Parrdrcris - Flight
Rcmrinr Within #
MituEi io Suitrbl€
futFort
(l) - NJ
(21. -10Miruts
Page26-14
MAR10/2007.
REV.17.
ztElEV
Hungarian Airlines,fi
.787
.?27Et/u2F
LIST
EQUIPMENT
MINIMUM
26. FIREPROTECT]ON
REPAIR INTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
76?-300/r{10m
Ir.l€n.rt6d
Nlrne
{
-
Approwd
P!!bction
Timc
flJ Mmulc
S'rEm
Bottl€ Typ(
SysEm
Trpc
I
Mctcftd
Minutct
PRR
B I1863-5
1A
UULBs. luglt le tch
Knock Dirclffg.
Down
33LBS. lrleercd Eonlc
McicrEd
incorFord.d
H
l,al.lMlntrc
Slstcm
tvl rflmutc
Sltten
Metcrcd
Minutca
l9:
hlinuter
Mct$rd
I
:
]A
6l Mrmrtc
Syatcm
9U
McErtd
Minrte!
On
A irplancs
DirchsE. M.drod
l
6{JLB5.
Knoclr
Down
SirylE St tch
Diachugc
!t LBS.
Mcicrcd
Mclcrcd Botth
Discl a4sr !0
Min1n.6 Timc D.lry
en<r Fird Batth
5ULEs.
Knocl
Dov'n
Si|rgL Sl* ch
t0LBs.
tr{ctccd BottLcs
TULIiI.
Knoch
Do*n
SinAL$n'ltch
Dirchlgc
tr LBs.
It{emd Bottlc
Dirchrrgrs10
Minucr Tim. Dclsy
aftcr Firet Bonlc
Farv/Erd
Carfo
Conditioncd
l
(2Ai - l0Mirutt
(ll - NIA
(l) - 30Ilinuus
(r) - NrA
DircIrrgc
lvhtcrEd Dirclrrgc -10
Minrtcr Trmt Dclay
]ILBS. aficr Firn Botlc
Mcte$d
MCEtld
\+lth
Disc[ffgcr !0
Minrtcr linc Dchy
rftcr First Botttc
lnoFcrrhtt tsollE # ln
PrlEdcair - Flight
Rcmaiu Withia#
MinuE b SuitEblc
Aipst
(! - 70Mirurer
llA) - Lr0Minutcr
(tl-NrA
(D - 10 Minuts
Ar
K
195 Mmuc
SFtcm
Oh
Airplsncs
\thh
Caqs
Conditiorcd
Air
l9:
Miottcl
Mctercd
?
:A
EOLtts.
Knocl
Down
q: LBS.
Mct€ttd
tt LBs.
MGEIEd
SinglcS$"nch
Diechrrgc
Mccrrd Bottlcr
Dbchugc -10
Minutir lirDc Dckv
sfis Fir* BcttL
{l) - NrA
(l! -60 Minutr
(3Al - ll0 Minucr
Page26-15
MAR10/2007.
REV.17.
:!M)EV
Hungarian Airlinesh
.ezrEtttYaF
.787
LIST
MINIMUM
EQUIPMENT
26. FIREPROTECTION
REPAIR INTERVAL
NUMBERREQUIREDFORDISPATCH
REMARKOR/ANDEXCEPTIONS
PLACARD
- FWDor AFTCARGOFIRE
Associated
CargoFirePanel(P5)CargoFireArmswitch(es)
ARMINOP
26-26-1 PortebleFire
Extinguishers
(8767-200)
(B767-300)
i.a.w.JAROPS1.790
D
6
or missingprovided:
Onemaybe unserviceable
for the flight
is available
a) One Halonfireextinguisher
deck,
is availablefor each of three
b) One extinguisher
galleyarea,and
c) The inoperative extinguishe(s) is tagged
inoperative,removedfrom its locationand placed
outof sight.
D
10 8
or missingprovided:
one maybe unserviceable
for theflight
is available
a) One Halonfireextinguisher
deck,and
must be locatedin, or readily
b) One extinguisher
in,
for
use
eachgalley,and
accessible
c) The inoperative extinguishe(s) is tagged
inoperative,removedfrom its locationand placed
outof sight.
Page26-16
MAR10/2007.
REV.17.
.ltMlEV Hungarian Airlines,fi
.78.gz}EttryAF
LIST
MINIMUM
EQUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
26-26-2 LavatoryFire
Extinguisher
System
systemI
For each lavatory,the lavatoryfire extinguisher
may be inoperativeprovidedlavatorysmoke detectionI
systemoperatesnormally.
I
(M) (O) For each lavatory,the lavatoryfire extinguisher
provided:
systemmaybe inoperative
a) Lavatorywastereceptacleis empty,
b) Lavatorydoor is locked closed and placarded,
"INOPERATIVE
- DO NOTENTER",
and
purpose.
for
any
c) Lavatoryis not used
1) 8767-200
2) 8767-300
C
6
5
(M) (O) For each lavatory,the lavatoryfire extinguisher
provided:
systemmaybe inoperative
d) Lavatorywastereceptacleis empty,
e) Lavatorydoor is locked closed and placarded,
'INOPERATIVE
- DO NOTENTER",
and
Lavatoryis not usedfor any purpose.
NOTE 1: These provisosare not intendedto prohibit
by crewmembers.
lavatoryuseor inspections
NOTE 2: A lavatoryfire extinguishersystem is not
requiredfor all cargooperations.
PLACARD
Placardatfectedlavatorydoor- INOPEMTIVE- DO NOTENTER
(O)
OPERATIONS
lf lavatorysmokedetectorsystemdoesnotoperatenormally,ensurethatthe associated
lavatorydoorremainslockedand is not enteredexceptfor inspectionby crewmembers.
Page26-17
MAR10/2007.
REV.17.
;+U,EV Hungarian Airlines
fi
.7Ez
.?SrEtttUE
MINIMUM
EQUIPMENT
LIST
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
26-263 Lavatory
Smoke
Detection
System
For each lavatory,the lavatorysmokedetectionsystemI
may be inoperativeprovidedlavatoryfrre extinguisherl
systemoperatesnormally.
I
1) 8767-200
c
7
2) 8767-300
C
6
(M) (O) For eachlavatory,the lavatorysmokedetection
provided:
systemmaybe inoperative
is empty,
receptacle
Lavatory
waste
a)
b) Lavatorydoor is locked closed and placarded,
'INOPERATIVE
- DO NoT ENTER",
and
c) Lavatoryis not usedfor anypurpose.
5
(M) (O) For each lavatory,the lavatorysmokedetection
provided:
systemmaybe inoperative
is empty,
waste
receptacle
Lavatory
d)
e) Lavatorydoor is locked closed and placarded,
'INOPERATIVE
- DO NOTENTER".
and
f) Lavatoryis not usedf,oranypurpose.
NOTE 1: These provisosare not intendedto prohibit
by crewmembers.
lavatoryinspections
NOTE2:: A lavatorysmokedetectionis not requiredfor
all cargooperations
PLACARD
Placardaffectedlavatorydoor- INOPEMTIVE- DO NOTENTER
OPERATIONS
{OI
lf lavatorysmokedetectorsystemdoesnotoperatenormally,ensurethatthe associated
lavatorydoorremainslockedand is notenteredexceptfor useor inspectionby
crewmemDers.
Page26-'18
MAR10/2007.
REV.17.
t*AdEW
Hungarian Airlines
fi
.7A'7
,AzrEttvZF
LIST
MINIMUM
EOUIPMENT
27. FLIGHTCONTROLS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
c
27{'3.1 FLTCONTROL
SHUTOFF
VaIVes
6
0
(M)Maybe inoperative
open.
c
6
0
providedthe associatedvalveis
(M) May be inoperative
verifiedopenbeforeeachdeparture.
0
(M) May be inoperativeprovideda visualflight control
beforeeachdeparture.
checkis accomplished
27-03-2 FLTCONTROL
SHUTOFF
OFF
ValveLights
PLACARD
Affectedlight- LIGHTINOP
27-08-1 ControlSurface
Position
Indicating
System
NOTE:For-200i300,this itemcoversthe flightcontroldisplayon the EICASStatuspage.
27-08-2 FlaoPosition
IndicatorSystem
1) Position
Needles
C
2
1
PLACARD
- L (R)FLAPPOSINDINOP
Nearindicator(-200l-300)
as appropriate
27-09-l YawDamDer
Trim
Stabilizer
Module(YSM)
B
2
1 (M) (O) Onemaybe inoperative.
NOTE: YSM's replaceStabilizerTrim AileronLockoutModules,Yaw DamperModules,andRudder
new functionality.
YSM's alsoincorporate
RatioChang€rModuleson tlese airplanes.
EICAS STATUSMESSAGES
YSM
PLACARD
AirplaneFlight Log - L (R) YSM INOP
Page27-1
REV'17MAR10/2007.
:*MIEV
,azrEt'Ye
Hungarian Airlinesfi
.7ez
LIST
MINIMUM
ESUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS(O)
An inoperativeYSM will result in inability to manuallyselectthe associated(L or R) autopilot
whenusingoneof tle remainingchannels
channel.This channelis still ableto engageautomatically
in Approachmode,so autolandstatusis not affected.
27-ll-1 AileronTrim
System
C
I
0
provided:
(M) Maybe inoperative
a) Oneautopilotoperatesnormally,and
b) Ailerontrim systemis verifiedcentered.
PLACARD
-AILERONTRIMINOP
Ailerontrimswitches
Aileron
27-11-2Outboard
LockoutSystem
1) Indication
System
C
1
0
(M) (O) May be inoperative unlocked provided
is limitedto 270 KIASor 0.73Mach,
maximum
airspeed
whicheveris less.
C
'1
0
(MXO) May be inoperativeprovidedaileron lockout
system is verified to operate normally before each
deDarture.
PLACARD
Pilot'spanels- DO NOTEXCEED
270KIASOR 0.73MACH
INOP
Pilot'scenteroanel- OUTBOARD
AILERONLOCKOUT
OPERATIONS
{O)
DO NOTEXCEED
270KIASOR 0,73MACH
Avoidlargeor abruptaileroncontrolinputsabovemaximumflapextensionspeed.Excersizecaution
to preventexcessiveroll response.
27-21-1 RudderRatioLight C
0
(M) Maybe inoperative
OFFprovided:
a) RUDDERRATIOmessageon the EICASis verified
to operatenormally,and
b) Bothcontrolchannelsoperatenormally.
Page27-2
REV17 MAR10/2007.
Hungarian Airlines
:tMlEV
B
.7Az
^SaTEttYat
LIST
MINIMUM
EQUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
the amber
NOTE:One channelmust operatefor dispatch.lf both channelsare inoperative,
permitted.
is
not
RUDDERRATIOmessage
willappearanddispatch
PLACARD
Affectedlight- LIGHTINOP
27-32-1 StallWarningTest
Systems
C
2
0
providedoperationof associated
(M) Maybe inoperative
systems is verifiedto operate normallybefore each
deoarture.
PLACARD
- L (R) STALLWARNINGTEST INOP
As appropriate
27.41-1 ControlWheelTrim B
SwitchSystems
2
on the non-flyingpilot'sside
1 (M) One maybe inoperative
providedstabilizertrim system is verifiedto operate
normallv.
2741-2 Horizontal
StabilizerPrimary
TrimChannels
2
1
C
provided:
(M)(O)Onemaybe inoperative
a) Horizontalstabilizertrim operatesnormallyusing
stabilizer trim levers (Alternate Stabilizer Trim
Switches),
to CategorylllA Landing
b) The aircraftis re-classified
Minima.
c) No arm or controlvalvesare failedin the energized
position.
OPERATIONS
{OI
rate.
to halfthesignaled
willbe reduced
trimming
STABTRIMlightmayilluminate.
lf lightilluminates,
alternete
trim
system
procedure
from
the
(M)
rate
is
available
full
trim
NOTE:Maintenance
confirms
priorto dispatch.
2748-1 STABTRIM
lndicators
1 One may be inoperativeprovidedfaultyindicetoris not
visible.
PLACARD
- STABTRIMINDICATOR
INOP
indicator
Overassociated
Page27-3
REV17 MAR10/2007.
,y'lAaEV Hungarian Airlines
4
.7e.7
.?ZEtJUE
LIST
MINIMUM
EOUIPMENT
27. FLIGHTCONTROLS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
27-51-1 AutomaticFlap
LoadRelief
Retraction
1) -200/-300
(ActuatorRodEnd
Down)
c
2) -300(ActuatorRod C
EndUp)
1
(M) May be inoperativein the normal (actuator
extended)positionprovidedflaps30 are not used.
1
NOTE:Flaps25 may be used to maximumlanding
weight.
(M) (O) May be inoperativein the normal (actuator
retracted)positionprovidedthe flaps 25 and flaps 30
adjustedmaximumlandingweightsareobserved.
0
PLACARD
Near flap handle- AUTO FLAP LOAD RELIEF INOP
- DO NOT USEFLAPS30
As appropriate
OPERATTONS(O)
Maximumlandingweightmustbe equalto or lessthanthe valueslistedin the followingtable:
Model
(md end
767-200ER
down)
767-3008R(rodend
up)
27-62-1 AutoSpeedBrake
Svstem
25MLW
seeAFM
30 MLW
Not used
257,400
lbs.
(116,760
kgs)
236,600lbs.
(107,320
kgs)
C
1
0
20 MLW
not applicable
not applicable
(MXO) May be inoperative provided system is
areappliedif landing
andAFMdecrements
deactivated,
performance
requiresuseof autospeedbrakes.
PLACARD
Auto speedbrake
light - AUTO SPDBRK INOP
Nearsoeedbrake
handle- AUTO SPDBRK INOP
(OI
OPERATIONS
1. The FAA ApprovedAirplaneFlightManualprovidesperformancepenaltiesfor airplanescertified
withlandingfieldlengthcreditfor autospeedbrakes,
2. Forlandingdeployspeedbrakesmanually.
Page274
REV17 MAR10/2007.
.ah'AIEW Hungarian AirlinesB
,sarEtjve
.787
EQUIPMENT
LIST
MINIMUM
27. FLIGHTCONTROLS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
27-62-2 Speedbrake
CautionLight
System
a
1
27-63-1AUTOSPDBRK, C
SPOILERS,
and
STABTRIMLights
PLACARD
Affectedlight- LIGHTINOP
3
0
(M) May be inoperativeprovidedassociatedEICAS
messageis verifiedto operateonceeachflightday.
27-81-1 Leading
edgeSlat
Skew/ Loss
DetectionSystem
1
0
(M) May be inoperativedeactivatedprovidedleadingI
edgeslatsystemis verifiedto operatenormally.
I
C
Page27-5
REV17 MAR'10/2007.
I+UIEV
Hungarian Airlinesfi
EOEIaUG
7Az
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
28-11-1SumDDrainValves C
8
7
(M)Onemaybe inoperative
closed.
(M) May be inoperativeprovidedalternateprocedures
andused.
areestablished
28-21-1 PressureFueling
System
1) FuelShutoffValves C
6
0
(M) Maybe inoperative
closed.
c
6
0
(M) May be inoperativeopen if fuel iettisonsystemis
deactivated.
28-21-2 FuelingReceptacle C
Cao
2
0
(missing)provided
(M) Maybe inoperative
a) Refueling receptacle is vitually checked for
beforeeachrefuelingand
contamination
b) No leakage can be detected after refuelingis
complete.
PLACARD
Fueling panel door - FUEL CAP MISSING
28-22-'l MainTank Fuel
Pumps
C
4
3
(M) (O) Except for ETOPS operations,beyond 120
provided:
deactivated
minutesone maybe inoperative
quantity
indications
operate
a) Both main tank
normally,
and
b) The followingminimumfuel quantitiesare retained
in the affectedtankfor the flightconditionshown:
- 4,540kg (10,000lbs)
TAKEOFF
LANDING-2,270kg ( 5,000lbs)
1) AutomaticFunction C
of LeftFWDPump
1
0
(O) May be inoperativeprovidedalternateprocedures
and used.
are established
maintank
providesutficient
fuelto ensuretheoperable
NOTE:The minimum
fuelquantities
specified
pump'sinletand suctionbypassinletwill remaincoveredat expectedpitchattitudesduring
takeoffandlanding.
PLACARD
Associatedswitch as appropriate- L (or R) FWD (or AFT) PUMP INOP
PAGE28.1
REV17 MAR10/2007
:IMIEW
Hungarian Airlines,fi
E?E'IUE
787
MINIMUMEOUIPMENTLIST
28, FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
(O}
OPERATIONS
1. Foran inoperative
maintankfuelpump:
for takeoffandlanding:
minimum
fuelvaluesareavailable
a) Ensurethefollowing
- 4,540kg (10,000lbs)
TAKEOFF
LANDING- 2,270kg ( 5,000lbs)
unusable.
b) Thelandingminimum
fuelquantity
mustbe considered
2. Foran inoperative
automaticfunctionof the leftforwardfu€lpump:
Startthe APU.
selecttheleftfoMardfuelpumpON.
b) OncetheAPUis running
andAC poweris available,
NOTE: Fuel for the APU operationis suppliedfrom the left main tank. When AC poweris
by a DCfuelpump.WhenAC poweris applied,
unavailable,
fuelpressure
is provided
the left forwardAC fuel pumpis signaledto start regardlessof its position.lt is this
automaticfunctionwhichmaybe inoperative.
28-22-2 CenterTankFuel
Pumps
C
2
I
provided:
(M)Onemaybe inoperative
a) Centertankremainsempty,and
b) Associatedcentertankfuelpumpis deactivated.
1
(M) (O) May be inoperativewith center tank fueled
provided:
a) Fuel quantityin main tanks is adequateto reach
pumpfailsat anytime,
airportif remaining
suitable
b\ Zero fuel weight calculationsare adjustedby the
weightof centertank fuel,
c) The effect on airplanebalance,in the event fuel
cannotbe used,is accountedfor,
d) Low PRESSlightoperatesnormallyon remaining
pump,
e) Centertankquantityindicationoperatesnormally,
f) One crossfeedvalve is open priorto take off and
remainsopenuntilcentertank is selectedOFF,and
g) Associatedcentertankfuel pumpis deactivated.
PAGE28-2
REV17 MAR10/2007
;+UIEV
Hungarian Airlines4
EAEIIYE
787
MINIMUMEQUIPMENTLIST
28, FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
provided:
(M) Maybe inoperative
a) Centertankremainsempty,
b) Centertank quantityindicationoperatesnormally,
and
c) Centertankpumpsare deactivated.
provided:
(M) Maybe inoperative
C 2
l) Airplaneswith
tank
empty,
a)
Center
remains
ServiceBulletins
system operatesnormally,
tank
b)
Center
scavenge
767-28-0052
or
ano
767-28-0062
c) Centertank Pumpsare deactivated.
installed
NOTE:
for Malev8767-200ER.
SB 767-28-0062had
beenaccomolished
2) Airplanes
subjectto
Airworthiness
Directive200115-08in effect
C
2
0
(M) May be inoperativeprovided:
a) Boeing Alternate Means of Compliance to
AirworthinessDirective2001-15-08arefollowed,
b) Centertank containslessthan 5000poundsof fuel,
c) Centertankfuel is not used,and
d) Aflected pump(s)is deactivated.
NOTE:
ER.
AD 2001-15-08
hadbeenaccomplished
for Malev8767-200
PLACARD
- L (R) PUMPINOP
Centertankpumpswitch(es)asappropriate
(O)
OPERATIONS
-Ensurethat grossweightandfuel limitationhavebeensatisfied.
A. Adjustthezerofuel weightofthe airplaneby includingthe weightofcentertank fuel, or
adjustthemaximumzerofirel weightby subtracting
the weightofcentertankfuel.
empty.
NOTE:130to 230kgsof fuelin centertankis considered
PAGE28-3
REV 17 MAR 1Oi2OO7
,*'lAlEW
Hungarian Airlinesfi
787
BAEfiUE
MINIMUMEQUIPMENTLIST
28, FUELSYSTEM
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
28-22-3 DualFuel
CrossfeedValves
C
2
provided:
1 (M) (O) Maybe inoperative
a) Atfectedvalveis securedclosed,
valveoperates
normally
and
b) Remaining
c) For ETOPS operations, remaining valve is
duringthe lasthourof flight.
exercised
OPERATIONS
{OI
Duringthe last hour of cruiseon all extendedrange flights,exercisethe operativevalve per the
following.
1. Selectthe crossfeedvalveswitchON.VerifyVALVElightilluminates
and extinguishes.
and extinguishes.
2. SelectcrossfeedvalveswitchOFF.VerifyVALVElightilluminates
28-224 Centerfank Float
OoeratedShutoff
Valves
c
2
0
May be inoperativeprovidedthe centertank remains
empty.
PLACARD
Indicating
FuelQuantity
SystemCenterTank- CENTERTANKUNUSABLE
28-25-'l APUFuelPump
(Dc)
28-25-2 APUFuelShutoff
Valve
C
1
0
(M) May be inoperativedeactivatedprovidedboth bft |
whenAPU is I
fueltank boostpumpsoperatenormally,
requiredfor dispatch.
I
0
provided:
(M) Maybe inoperative
APU
is
not
used,
and
a)
b) Valveis securedclosed.
PLACARD
APU controlpanel- APU FUEL VLV INOP
28-25-3APUFuellsolation C
Valve
(if installed)
EICAS STATUSMESSAGES
APU ISLN VAL
(M) May be inoperativeprovidedthe valve is secured
closed.
PAGE284
REV17 MAR,10/2007
:!frlEV
Hungarian Airlinesfi
BOE
TUE 7A7
MINIMUMEQUIPMENTLIST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACARD
APU controlpanel- INOP
NOTE:Withthe APUfuel isolationvalveinoperative
closed,the DC FuelPumpwill not be availablefor
inflight
enginestart.
28-26-1 DefuelValves
r . e
0
(M) Maybe inoperative
closed.
28-313 FuelJettison
System
C
0
provided:
(MXO)Maybe inoperative
a) Jettisonnozzlevalvesare securedclosed,and
b) Jettisontransfervalvesare securedclosed.
1
'1) CenterTank
0 (MXO) May be inoperativeprovidedboth centertank
C 2
Jettison
Pumps
fuelpumpsoperatenormallyif centertankis used.
PLACAR,D
- FUEL JETTISONSYSINOPor CTR JET PUMP(S)INOP
Fueljettisonpanelasappropriate
(O)
OPERATIONS
and both centertank fuel pumpsoperative,fuel
NOTE:With centertank jettisonpumpsinoperative
jettisoncapabilityremainsavailableat 50%normaljettisonrate.
and
by using normallandingprocedures
1. OveMeightlandingsmay be safelyaccomplished
techniques.
associatedwith heavierthan normal landing
2. There are no adversehandlingcharacteristics
weights.
autolands.
3. Boeingdoesnotrecommend
overweight
4. Referto the BoeingFlightCrewTrainingManualfor furtherinformationconcerningOveMeight
Landing
Autoland
Policy.
and/orOveMeight
2840-l CrossfeedVALVE
Light(s)
1)SingleVALVE
Installation
2) DualVALVE
Installation
(M) Exceptfor ETOPSoperations
may be inoperativel
providedcrossfeedvelve and both main fuel quantityl
indications
operatenormally.
I
C
1
0
C
2
provided:
1 (M) On€maybe inoperative
valve
is
verified
to operatenormally,
a) One crossfeed
and
PAGE28-5
REV17 MAR10/2007
:|'lAlEV
Hungarian Airlinesfi
EAEaUE
787
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
operatenormally.
b) Bothmainfuelquantityindications
C
2
0
(M) Exceptfor ETOPSoperationsmay be inoperative
provided:
a) Crossfeedvalvesare verifiedto operatenormally,
ano
operatenormally.
b) Bothmainfuelquantityindications
0
providedsparvalveoperationis
(M) May be inoperative
flight
day
verifiedonceeach
PLACARD
Affectedlight- LIGHTINOP
28"{0-2 SPARVALVE
Lights
PLACARD
Affected
light- LIGHTINOP
28-41-l FuelOuantity
Indication
System
(FlightDeck)
1) MainTank
lndicators
c
2
(M)(O) Except for ETOPS operationsone may be
provided:
inoperative
a) Fuel quantityin associatedtank is verifiedby an
means,
alternate
b) FMC CALCULATED fuel quantity operates
normally,
and
c) FMC FUEL is initializedwith the knowntotal fuel
quantity,
to identifycontainan inflightenginefuel
d) Procedures
leakareused
e) Both boost pumps in associatedtank operate
normally,
and.
0 Fuel pump Low pressure warning lights in
associatedtankoperatenormally.
g) Centertankremainsempty.
operatenormally,
h) Fuelflowindications
NOTE:FUEL CONFIGadvisorymessagefor lateral
maybe inhibited.
imbalance
PAGE28-6
REV17 MAR10/2007
t+UaEV
Hungarian Airlines,fi
EoEttUE
7Az
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
provided:
2) CenterTank
0 (M) Maybe inoperative
empty,
lndicator
a) Centertankremains
b) Center tiankscavengesystem operatesnormally,
(Airplaneswith
ano
ServiceBulletins
c)
Centertankfuel pumpsare deactivated.
-28-0052
767
or
767-28-0062
installed)
NOTE:
for Malev8767-200ER.(LHA,LHB)
SB 767-28-0062had
beenaccomolished
3) CenterTank
C
lndicator
(Airplanessubject
to Airworthiness
Directive2001-l508)
0
provided:
(M) May be inoperative
a) Boeing Altemate Means of Compliance to
AirworthinessDirective2001-15-08is followed,
b) Centertank is verifiedto havelessthan5000pounds
of fuel,
c) Centertankfuel is not used,and
d) Centertankfuel pumpsaredeactivated.
NOTE:
AD 2001-15-08
hadbeenaccomplished
for Malev8767-200ER.(LHA,LHB)
4) FuelQuentity
Densitometers
a) Honeyruell
b) B.F. Goodrich
(Simmonds)
c
3
0
c
3
0
(M) May be inoperative provided
densitometer{s)is deactivated.
associated
NOTEI: Subitem 3: Fuel Quantity Densitometershave in the past caused l) blanking of the flight
deck fuel quantity indicators and, 2) fluctuation of flight deck fuel quantity indicators. Ifa
FQIS processorunit will utilize
densitcmeteris inoperative or deactivated,the Honey"rrvell
to
indications from another firnctional densitometer or revert an intemal density standard of
6.7 lb per gallon. B. F. Goodrich (Simmonds) FQIS system, with an inoperative
densitometerwill revert to an intemal densif standardof6.725 lb per gallon. Both systems
will continually meet accuracyspecificationswith failed densitometers.
maybe
equipment
of FQISandanotherinoperative
NOTE2:MELreliefforthefollowing
combinations
limitedor notallowed.
Referto eachMELitem.
PAGE28-7
REV 17 MAR 10/2007
ztAlEV
Hungarian Airlines
rrt
EAETG
787
MINIMUMEAUIPMENTLIST
28. FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2841-1 FuelQuantityIndication
System(FlightDeck)
(continued
NOTE2)
FQIS& 28-22-1
MainTankFuelPumps
FQIS& 28-22-2
CenterTankFuelPumos
FQIS& 2841-2FuelQtyProcessor
Channels
FQIS& 73-31-1
FuelFlowIndications
Limitedor not allowed
Limitedor not allowed
Notallowed
Notallowed-(thisresultsfromthe FMC
fuelquantityrequirement)
CALCULATED
NOTE 3: ServiceBulletin767-28-0052,
andproductionequivalentPRRB 12778,is the FuelPumpWithout
Installationof a CenterAuxiliary TankOverridePumpor Ovenide/Jettison
an Inlet Diffuser.ServiceBulletin767-28-0062,
andproductionequivalentPRRBl277E-2,
is the Fuel-Installation
ofa CenterAuxiliary TankOverridePumpor Override/Jettison
ManualBulletinsfor Fuel
PumpWith a Cast-inlnlet Diffuser.The BoeingOperations
SystemImbalanceAnomalyprovidefurtherinformation.
NOTE 4: TheFMC OperationalProgramSoftware(OPS)partnumberis displayedon the FMC
IDENT page.
EICAS STATUSMESSAGES
FUEL QTY BITE
FUEL QTY IND
PLACARD
Fuel Quantity Indicator- ToTAL FUEL QUANTITY INOP
- L (R) TANK FQISINOP or CTR TANK FQISINOP
FuelQuantityIndicatorasappropriate
- CTR TANK FUEL PUMPSDEACTIVATED
CenterTankFuelPumpSwitchesasappropriate
(O)
OPERATIONS
Reviewthe Log book to verify that FMC calculatedfuel quantityis operatingnormally.Total fuel
page.Flight
quantity
Initialization
mustbe calculated
initialized
on the FMCPerformance
andmanually
crew should monitor FMC Fuel Used an CalculatedFuel and the op€rativefuel tank quantity
indications
to ensureusageare normal.
1. Operatethe flightwiththe fuelcrossfeedvalve(s)closed(unlessdirectedotherwisebelow)
PAGE28-8
REV17 MAR10/2007
rtMlEW
Hungarian Airlines,fi
EZE'TUE
7A7
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2. Comparethe FMC CalculatedFuelwith the flightplanfuel remainingat eachway-pointor fix for
whichpredictedfuel useis available.
Monitorfuel usagefor anyunusualdecreasein fuelquantityand/ora fuel imbalance.
4 . A fuelleakmaybe evidencedby one or moreof the following:
rate.
A. Fuelquantity
decreasing
at an abnormal
B. Excessivefuelflow.
900kg perhour(2000lbihr)or
An increasing
fuelimbalence
of approximately
C. Fuelimbalance.
moreshouldbe considered
a fuelleak.
NOTE: "FUELCONFIG"advisorymessegeor lightwill not displayfor a fuel imbalance
condition
whenIeftor rightFQISis inoperative.
one unit
D. Excessive
lateraltrim- an imbalance
of 1,800kg (4,000lb)willrequireapproximately
level.
of ailerondisplacement
to holdthewings
E. Visualobservation
of fuelsprayfromthe struVengine.
F. An engineflameout.
5. For operationwith centertank fuel, when centertank fuel is depleted,verifythat airplaneat the
pointpredicted
bytheflightplan.
NOTE:lf centertankexhaustionprecedesthe pointpredicted,a fuelleakshouldbe suspected.
6. lf an enginefuel leak is confirmed,shutdownthe affectedengineto stop the leak.After engine
engine.
fuelmaybe usedfortheoperating
shutdown,
all remaining
28.41-2 FuelQuantity
ProcessorChannels
1) Hone)ryrell
FQIS
B
2
1 (M) (O) Exceptfor ETOPSoperations
onechannelmay
be inoperativeprovided:
by measuringsticks
a) Total fuel quantityis determined
or other acceptablemeansafter each refueling, and
agreeswith the fuel quantityindications,
by an acceptable
b) Inoperativechannelis deactivated
procedure,
c) All flight deckfuel indicationsoperatenomally,
d) FMC calculatedfuel quantity operatesnormally,
e) Fuelflow indicationsoperatenormally,
PAGE28-9
REV17 MAR10/2007
;tUlEV
Hungarian AirlinesB
AOEIIUE
7A7
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
0 FMC TOTALIZER FUEL quantitya$ees with tuel
quantityindications,and
g) For PegasusFMC installationswith Operational
or
ProgramSoftwarepart number3418-HNP-02C-0E
System
operates
normally.
earlier,ThrustManagement
2) Simmonds
FQIS
B
2
I
(O) Exceptfor ETOPSoperations,one channelmay be
provided:
inoperative
operates
normally,
a) All flightdeckfuelrndications
b) FMC CALCULATED fuel quantity operates
normally,
and
operatenormally
c) Fuelflowindications
d) FMC TOTALIZERFUEL quantityagreeswith the
fuelquantityindications.
e) For PegasusFMC installationswith Operational
ProgramSoftwarepart number3418-HNP-02C-08
or earlier, Thrust ManagementSystem operates
normallY.
IDF*'- |
--"
is urrPr4Jwu
displayed-on the
*
tFMC
*
numberrJ
NOTE: The FMC OperationalProgram
uBlall Dultw'llr'
Software(OPS)
(vrD/ part
P4rr uurlrusr
page.
I
EICAS STATUSMESSAGES
FUEL QTY BITE
FUEL QTY CHANNEL
PLACARD
Fuelquantityindicator- PROCESSOR
CIIANNEL INOP
OPERATIONS
{OI
'1. Prior to each enginestart, confirmthat the FMC Performance
Page, FUEL is
Initialization
quantity.
(i.e.
boxes
appear),
DO NOT
lf
not,
fuel
automatically
initializedwith the knowntotal
manuallyenterfuelquantity,repairsmustbe madebeforedispatch.
3. Priorto each enginestart,confirmthat fuel flow systemInputsare valid on the FMC SENSOR
STATUSPage1 (PlP FMC- LEFTand RIGHTEICASOK or NON-PIPFMC- Leftand Right
FUELFLO).
PAGE28.10
REV17 MAR10/2007
tlMlEV
Hungarian Airlines
fi
EAEflUE
787
MINIMUMEAUIPMENTLIST
28. FUELSYSTEM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
28.11-6 FuelOuantity
(Fueling
Indications
Panel)
0
(M) May be inoperativeprovided alternate fueling
and used.
are established
orocedures
PLACARD
-RIGHT(LEFTand/orCENTER)
,UEL artl
Fuelingcontrol panel indication(s)asappropriate
INOP
2841-7 TotalFuelQuantity C
lndication
1
0
provided:
(O) Maybe inoperative
withthe knowntotalfuelquantity,
a) FMCis initialized
b) FMC CALCULATEDfuel used for each engine
operatesnormally,
c) BothFMC's operatenormally.
operatenormally,and
d) Fuelflowindications
e) For PegasusFMC installationswith Operational
ProgramSoftwarepart number3418-HNP-02C-08
or earlier, Thrust ManagementSystemoperates
normallY.
NOTE:The FMC OperationalProgramSoftware(OPS)partnumberis displayedon the FMC
IDENT page.
PLACARD
FuelQuantityIndicator- TOTAL FUEL QUANTITY INOP
(O)
OPERATIONS
1. Total fuel quantitymust be calculatedand manuallyinitializedon the FMC Performance
Pagepriorto enginestart.
Initialization
2 lt total fuel quantityis inoperativeas a result of an individualtank quantityindication,MEL
restrictions
for that itemmustbe observed.
3- Priorto eachenginestart,confirmthat fuel flowsysteminputsare validon the FMCSENSOR
STATUSPage1 - LEFTandRIGHTEICASOK .
FUELOTY.Forflightsnot
4. (Optional)
Priorto eachengineshutdown,recordFMCCALCULATED
totalfuelquantity.
means
of
determining
requiring
fuel,thisvaluemaybe usedas a
additional
PAGE28-11
REV17 MAR10/2007
I!'AIEV
Hungarian Airlinesfi
EZE
IUE
787
MINIMUMEQUIPMENTLIST
28. FUELSYSTEM
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR'ANDEXCEPTIONS
with the fue
lf it is necessaryto jettisonfuel enroute,FMCtotalfuel quantitymustbe reinitialized
quantityremainingat the completionof jettison.
In caseof enroutefailureof the FMCcalculatedtotalfuelquantity,flightcrewmustkeepa fuel log
for the remainderof the flight.
NOTE:The PROGRESSpage 1 displayof FUELquantityand ATA at the LastWaypointpriorto
page2 FUEL
failuremaybe usedas a startingpoint.In somefailuremodes,PROGRESS
USEDdatamaybe available.
NOTE:Ailerontrim indicationon the controlwheelcan be usedto determineif a fuel imbalance
of 1,800kg (4,000pounds)will require
condition
exists.At cruisespeedsan imbalance
to holdthewingslevel.
approximately
oneunitof ailerondisplacement
28-42-l FuelPumpLow
PRESSLights
c
6
pump.
for an associatedinoperative
Maybe inoperative
c
6
(M) May be inoperativeprovidedassociatedEICAS
messageis verifiedto operateonceeachflightday.
C
1
PLACARD
Affectedlight- LIGHTINOP
28.43-1 FUELTEMP
Indicating
System
0
(O) May be inoperativeprovidedTotalAir Temperature
(TAT)is usedas an indicationof fueltemperature.
NOTE:StaticAir Tempereturemay be used provided
ram risefactoris applied.
appropriate
PLACARD
Airplaneflight log - FUEL TEMP IND INOP
(O}
OPERATIONS
(TAT)for fueltemperature.
UseTotalAir Temperature
(SAT)conversion.
SeeMEL3413-7 for StaticAir Temperature
28-44-1 MeasuringSticks
C
16
0
May be inoperativeprovidedfuel quantityis determined
means.
byotherapproved
PAGE28-12
REV 17 MAR 1Ol2007
;?MIEV
Hungarian Airlinesfi
EOETE
787
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIC
REPAIRINTERVAL
NUMBERREQUIREDFORDISPATCH
REMARKOR/ANDEXCEPTIONS
29-11-1 EngineDriven
Hydraulic
Pumps
1) Depressurization c
Function
2
C
29-11-2 CenterSystem
(Electric)
Hydraulic
Pumps
2
providedthe Air
1 (M)onlypumpNo.2maybe inoperative
DrivenPumpoperatesnormally.
29-11-3Air DrivenPump
(ADP)
1
0
C
provided:
(M) (O) Maybe inoperative
(HMG)is notrequired,
Motor
Generator
a) Hydraulic
pumps operate
system
electric
Both
center
b)
normally,
and
c) Takeoffand landingperformancelimitedweightis
(40,0001b)
OR 318k9(7001b)
reducedby 18,143k9
are
when specialobstaclecl€arancerequirements
meI.
The
NOTE: TheHMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.
HMG is not requiredfor non-ETOPS.
PLACARD
- ADP INOP
Hydrauliccontrolpanelasappropriate
(OI
OPERATIONS
andC HYDSYSMAINTstatus
NOTE:Duringperiodsof highdemand,C HYDSYSPRESScaution,
messagemay display.lf centerhydraulicsystempressureremainsbelow2800 psi for 60
willlatch.
thentheC HYDSYSMAINTmessage
secondsor more,withbothenginesrunning,
1. lt is normalfor the landingGEAR DISAGREEmessageto be displayedif the gear is not
retracted/extended
within the time delay on the landinggear monitorcircuit,With the ADP
2y2tines
inoperative,
the landinggear retraction/extension
times will increaseto approximately
normaland mayexceedthe timedelayresultingin displayof the GEARDISAGREEmessageuntil
gearretractionis complete.
30%.
2. Flapretractionand extensiontimeswillincreaseby approximately
PAGE29-1
REV17 MAR10/2007
z!'lAlEW
Hungarian Airlines4
AOE
TUE 7A7
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
The ADP will not operate,thereforethe HMG will not operate.
Specialobstacleclearancetiakeoffperformance:
timeswhich,in turns,causesa
NOTE:An inoperative
ADP causeslongerlandinggearretraction
degradedflight profile.Beforeapplyingthe appropriatesmallertakeoffweight penalty,
ensurethat no obstaclesexist abovethe obstacleclearanceplanedefinedby the table
below.
a) Reduceperformancelimitedweightby 18,143k9if an obstacleprotrudesabovethe obstacle
clearanceplaneas definedbythe tablebelow,OR
b) Reduceperformancelimitedweightby 318kgif NO obstacleprotrudesabovethe obstacle
clearanceolaneas definedbv thetablebelow.
PLANE
OBSTACLECLEARANGE
*Horizontal distance (in
feet)fromreferencezero
0
5.000
6.500
7.000
8.000
10.000
20.000
30.000
40,000
50,000
60.000
66,000
andon
' Height (in feet) above
referencezero
cF6-80c2
0
29
cz
37
50
195
340
484
630
775
854
854
*This tableassumes
referencezerois locatedat the departureendofthe runway(clearwayis not
usedfor takeoff analysis).Altematelythe Airplane Flight Manual may be usedto determine
referencezeropoint.
t'ttttc,
zJ-z
REV 17 MAR 1Oi2OO7
^rYUaEV Hungarian Airlines
4
EOEfrE
787
MINIMUMEQUIPMENTLIST
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
planeas definedby the tableabove,reduce
A. If an obstacleprotrudesabovethe obstacleclearance
performance
limitedweishtasfollows:
Model/ Enqine
IAKEOII
-200&-300/-cF6-80c2 18143kq /40.000lb
planeasdefinedby the tableabove,reduce
B. Ifno obstacleprotrudesabovethe obstacleclearance
performance
limitedweightasfollows:
Model/ Enqine
I aKeofi
-200&-300/-cF6-80c2
318 kq / 700 lb
29-11.4 ADPController
1) AUTOFunction
C
'1
0
provided:
(O) Maybe inoperative
a) Controlis ON for takeotfand landing.
b) HydraulicMotorGenerator(HMG)is not required,or
whenHMGis required,
controlis ONcontinuously
c) Takeoffand landingclimblimitedgrossweightsare
reducedby 1,633kg(3,6001b).
d) OFFpositionoperatesnormally,and
2) ON Function
C
1
0
provided:
Maybe inoperative
a) The AUTO and OFF functionsof the ADP operate
normally,and
b) HMGis notreguired.
The
NOTE: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.
HMG is not requiredfor non-ETOPS.
(O}
OPERATIONS
1. WithAUTOinoperative
turntheADPon at thefollowingtimes:
a) On the groundpriorto takeoff.
priorto flapextension.
b) Inflight
c) At all timesif hydraulicdrivengeneratoris requiredfor dispatch.
by 1,633kg(3,6001b).
2. Takeolfandgo-around
climblimitedgrossweightsarereduced
PAGE29.3
REV17 MAR10/2007
z*MIEV
Hungarian Airlines
fi
EOE
IUE
7A7
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIC
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
29-11-5 ElectricDemand
Pump(ACMP)
1) AUTOFunction
29-18-1 ReservoirService
Indication
Quantity
B
2
provided:
1 One maybe inoperative
and
normally,
a) Pumpoperates
b) Associatedpumpis selectedON and remainson.
U
LowSYS
29-31-1 Hydraulic
PRESSLights
1) LeftLowSYS
PRESSLight
provided:
(M) Maybe inoperative
a) Pump low PRESS lights and all HYD PRESS
in the leftsystemoperatenormelly,and
indications
signalwireof the PTUsystem
The
left
low-pressure
b)
is cappedand stowed.
2) RightLowSYS
PRESSLight
May be inoperativeprovidedpump low PRESSlights
in the right system
and all HYD PRESSindications
operatenormally,
PLACARD
Affected
light- LIGHTINOP
29-31-2 PumpLowPRESS
Lights
1) Left,Center,
RightandAir
DrivenPump,
provided:
(M) Onein eachsystemmaybe inoperative
a) Associated low SYS PRESS light operates
normally,
and
b) Associatedpump operationis verifiedbeforeeach
departure.
2) Centersystem
No.2Electric
Pump
provided:
Maybe inoperative
Driven
Pump
operatesnormally,and
Air
a)
b) Associatedpumpis selectedOFF.
PAGE294
REV17 MAR10/2007
;VUIEV
Hungarian Airlinesfi
EAE
lYG
787
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
3) Air DrivenPump C
(ADP)
I
0
provided:
(O) Maybe inoperative
Electric Pumps operate
Both
center
system
a)
normally,
OFF,
b) ADPis selected
c) Center HydraulicMotor Generator(HMG) is not
required.
and
performance
adjustments
areapplied.
d) Appropriate
NOTE 1: Crew shouldbe aware,in case of emergency,that the CenterSystemNo.2
ElectricPumpandAir DrivenPumphavebeenselectedOFF as a precautionary
lowpressure
measureto precludeun-announced
NOTE2: The HMGis requiredfor ETOPSroutesif an IDGor APUgeneratoris inoperative.
The HMGis notrequiredfor non-ETOPS.
PLACARD
-_ LOW PRESSLIGHT INOP
Hydrauliccontrolpanelasappropriate
OPERATIONS (O)
normallyasfollows:
1.
Checkaffectedpumpandverifo SYSPRESSlight operates
CAUTION: TO PREVENT HYDRAULIC PUMP DAMAGE FROM OVERT{EAT, DO NOT
OPERATE PUMPS WITHOUT MINIMUM QUANTITIES OF FUEL IN TANKS
(REF.AMM 29-11-00).
NOTE l:The pumpbeingtestedmustbe the only pumpoperatingwithin the relatedhydraulicsystem
at the time of thetest.
below varies
NOTE 2:Thesourceof EICAShydraulicpressurereadingsrequiredin the procedures
-200f300,
HYD PRESSreadingsare availableon the ELEC/IIYD
by model. For
pageor optionallyon the EICASstatuspage.
maintenance
A. Air DrivenPump(ADP):
l) Associated
SYSPRESSlight mustbe illuminated.
2) Ensurethatpersonnelareclearof flight controls.
turn air
3) With electricalpoweron the airplaneand pneumaticsystemprcssurepressurized,
pumpswitchto AUTO or ON.
4) C HYD PRESSreadingon EICASmustbe 2800to 3200psig.
5) SYSPRESSlight mustextinguish.
6) Restoreairplaneto its requiredconfiguration.
PAGE29.5
REV17 MAR10/2007
ttUViV
Hungarian Airlines4
EOE
IUE
7A7
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIG
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
B. EngineDrivenPump(EDP):
NOTE: An activebrakesourceis requiredwhenoperatingan engine.
I ) Associated
SYSPRESSlight mustbe illuminated.
2) Ensurethatpersonnelareclearofflight controls.
3) With affectedenginerunning,turn ENG pumpswitchON.
4) IIYD PRESSreadingon EICASmustbe 2800to 3200psig.
5) SYSPRESSlight mustextinguish.
6) Restoreairplaneto its requiredconfiguration.
C. Alternatingcunentmotorpump(ACMP):
l) AssociatedSYSPRESSlight mustbe illuminated.
2) Ensurethat personnelareclearofflight controls.
3) With electricalpoweron the airplale,pressaffectedELEC pumpswitchto ON.
4) I{YD PRESSreadingon EICASmustbe 2800to 3200psig
5) SYSPRESSlight mustextinguish.
6) Restoreairplaneto its requiredconfiguration.
2. WhentheADP is OFF:
A. Seeitem 29-11-3for ADP OFF (inoperative)performancepenalties,landinggearextensiot/
retractionaffects,and flap extension/retructionaffects.
B. The HMG is poweredby the centerhydraulicsystem.The ADP hasbeenselectedOFF dueto
the (inoperative)indicationsystemsinability to identifr a potentialproblem.If a complete
electricalfailureoccurs(an emergencysituation),the HMG will operateif the ADP is selected
oN.
D
29-3I-3 HYDPRESS
(EICAS)
Indication
3
O
7
4
29-32-1 PumDOVHT
IndicationSystem
1) Left,Center,Right C
andAir Driven
PumpOVHTLights
provided:
(M) Onein eachsystemmaybe inoperative
pump low
light
or
PRESS
Associated
low
SYS
a)
normallY,
and
PRESSlightoperates
b) Associatedpump operationis verifiedbeforeeech
deoarture.
PAGE29.6
REV 17 MAR 1Ol2007
IIMIEV
Hungarian Airlinesfi
E?E
IUE
787
MINIMUMEQUIPMENTLIST
POWER
29. HYDRAULIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2) CenterSystem
No.2ElectricPump
lndicationSystem
provided:
Maybe inoperative
normally,
and
a) Air DrivenPumpoperates
b) Associatedpumpis selectedOFF.
3) Air DrivenPump
(ADP)lndication
System
provided:
(O) Maybe inoperative
a) Both center system Electric Pumps operate
normally,
OFF,
b) ADPis selected
c) Center HydraulicMotor generator(HMG) is not
reouired.
and
performance
adjustments
are applied
d) Appropriate
that the CenterSystemNo.2 ElectricPump
NOTE 1: Crew shouldbe aware,in caseof emergency,
measureto prccludea
and Air Driven Pumphavebeen selectedOFF as a precautionary
potentialoverheat.
NOTE 2: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inopetative.The
HMG is not requiredfor non-ETOPS.
PLACARD
- _ PUMPOVHT LIGHT(S)INOP
Hydrauliccontrolpanelasappropriate
OPf,RATIONS NOTE
1. WhentheADP is OFF:
penalties,landinggearextension/
A. Seeitem 29-11-3for ADP OFF (inoperative)performance
retractionaffects,and flap extension/retractionaffects.
B. TheHMG is poweredby the centerhydraulicsystem.The ADP hasbeenselectedOFFdueto
the (inoperative)indicationsystemsinability to identif, a potentialproblem.If a complete
electricalfailure occurs (an emergencysituation),the HMG will operateif the ADP is
selectedON.
29-33-1 HydraulicSystem
LowQTY
providedHYDQry indication(s)
(M) Maybe inoperative
operatesnormally.
provided:
(M) Maybe inoperative
a) Reservoir level(s) ve fied normal before each
departure,
b) The associated SYS PRESS lights operate
normally,
and
t'r\\tE
zY- |
REV17 MAR10/2007
TYMIEV Hungarian Airlines
fi
EZE
TYE 787
MINIMUMEQUIPMENTLIST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
c) With the left hydraulicsystem low QTY lights
inoperative,the left low quantitysignalwire of the
PTUsystemis cappedand stowed.
NOTE:With the centerhydraulicsystemlow QTY light inoperative,placethe ReserveBrakesand
positionpriorto
SteeringRESET/DISABLE
switchon the P61 panelto the RESETiDISABLE
valves.
isolation
Hydraulic
system
This
of
the
Center
dispatch.
inhibitsautomaticclosure
PLACARD
Affectedlight- LIGHTINOP
29.33-2 HYDQTY
lndications
C
3
0
provided:
(M) Maybe inoperative
level
is
verified normal before each
Reservoir
a)
deDarture.
b) Associated low SYS PRESS lights operate
and
normally,
c) On PTU equippedairplanes,with the left hydraulic
the left
systemlow QTY or RSVRlightsinoperative,
is
quantity
PRU
system
wire
of
the
low
signal
caooedand stowed.
NOTE:With the centerhydraulicsyslemlow QTY light inoperative,placethe ReserveBrakesand
positionpriorto
SteeringRESET/DISABLE
switchon the P61 panelto the RESET/DISABLE
dispatch.Thisinhibitsautomaticclosureof the CenterHydraulicsystemisolationvalves.
PAGE29-8
REV17 MAR10/2007
Hungarian Airlinesfi
.I!'AIEV
.787
.?A7Et/YZF
EQUIPMENT
LIST
MINIMUM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
30-11-1WingAnti-lce
Valves
0
(M) Exceptfor ETOPSoperationsbeyond120 minutes,
may be inoperativeclosedprovidedthe airplaneis not
operatedin knownor forecesticingconditions.
PLACARD
- L (R) WAI VLV INOP
Anti-icecontrolpatrelasappropriate
30-11-2WingAntilce
VALVELights
C
2
0
(O) May be inoperativeprovided associatedvalve
operatesnormally.
C
2
0
providedassociatedvalve(s)
(OXM)Maybe inoperative
is inooerative.
PLACARD
- L(R) WAI VLV LIGHT INOP
Anti-icecontrolpanelasappropriate
(O}
OPERATIONS
1. Valve operates normally:Observe pressure indicatorwhen repositioningswitch. Pressure
fluctuationis an indicationof valvemovement.
2. Valveinoperative
closed:EnsureWingAnti-lceswitchis selectedoff..
30-11-3WingAnti-lce
GroundTest
30-21-1 EngineAnti-lce
Valves
1)CowlValves
Closed
2) CowlValves
Open(CF6-80C2)
c
2
(M) Exceptfor ETOPSoperationsbeyond120 minutes,
one may be inoperativeclosedprovidedthe airplaneis
notoperatedin knownor forecasticingconditions,
openprovided:
(M) (O) Maybe inoperative
pressure
valve
is securedclosed,
shutoff
a) High
engineremainsOFF
for
associated
Bleed
air
switch
b)
exceptwhenTATis lessthan10Celsius(50F),
c) Remaining(opposite)enginebleedsystemoperates
normarry,
'10,000feet
d) A minimumof 70% Nl (557obelow
enginein icing
on associated
MSL) is maintained
conditions,
Page30-1
REV17 MAR10/2007.
Hungarian Airlinesrfi
I*MIEV
.787
EZTE'|VGF
EQUIPMENT
LIST
MINIMUM
30. ICEAND RAINPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
operatesnormally,
AssociatedPRV/FWSOV
generator
is not required,
hydraulic
motor
Center
D
s) Associatedthrustreverseris securedin the forward
and
thrustoosition.
performance
adjustments
are applied.
h ) Appropriate
The
NOTE: TheHMG is requiredfot ETOPSroutesif an IDG cr APU generatoris inoperative.
HMG is not requiredfor non-ETOPS.
f,ICAS STATUSMESSAGES
L (R) ENG TAI VALVE L (R) COWL DUCT LEAK
PLACARD
- L(R) TAI COWL VLV INOPOPEN(CLOSED)
Anti-icecontrolpanelasappropriate
- L(R) HPSOVINOP
panel
Pneumatic
control
asappropriate
OPERATIONS
{OI
1 . Forcowlvalvesclosed,avoidflightintoknownicingconditions.
2. Forcowlvalvesopen:
A. Selectengineanti-ice
switchOFF.
will nottakeintoaccountEPR
NOTE1: Withthe engineanti-iceOFF,the autothrottle
reductions
for the cowlvalveoDen.
NOTE2: The anti-icecapabilityis addressedby useof bleedair switchpositionand engineN1
speeo.
limitweightreductions.
B- Observethe followingperformance
Model/Enqine
Takeoffand Landino
Climb
En-route
-200&-300icF6-80c2
1,497kq (3,300lb)
1 , 8 6 0k q ( 4 , 1 0 0l b )
hasbeenlockedout.
1)On CF6-80C2
enginestheassociated
thrustreverser
a) Takeoffperformance
for FAArulesdoesnot providefor anythrustreversecredits.
penaltyis zero.
The performance
performance
for the acceleratestopscenanoundersome
Wet
runway
takeoff
b)
for zerothrust
regulatory
agencyrules,otherthanthe FAArules,mustbe calculated
Performance
reversecreditratherthanone thrutt reverser.Referto the JAAOperational
Supplement
or BoerngPerformane€
Software.
Page30-2
REV17 MAR10/2007.
;lGlEW
Hungarian Airlinesh
EarEttrvaF
'78.7
EQUIPMENT
LIST
MINIMUM
30. ICEAND RAINPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C, Planfor fuel burnincreaseas follows:
Model/Enqine
FuelBurnlncrease
-200& -300/cF6-80c2
1.0 o/o
F):
D. For CF6-80C2,andTAT equalto or greaterthan 10degreesC (50 degrees
1l For CF6-80C2.selectBleedAir SwitchOFF.
AC packwill
2) The bleedair switchOFFpositiondrivesthe PRV closedandthe associated
andconditionthe airplane.
not receiveair. Theremaining(opposite)AC packwill pressurize
Altematively,selectAPU ON to drivethe AC pack.SelectAPU OFFafterthe BleedAir
SwitchoN is available.
F), selectBleed
3) After flap retraction,andafterTAT is lessthan 10degteesC (50 degrees
Air SwitchON.
E. ForCF6-80C2,andTAT lessthan 10 degreesC (50degreesF):selectBleedAir SwitchON.
MSL,exceptas
F. lf icingconditions
maintain
70%Nl (55%below10,000feet
areencountered,
requiredfor landing)on affectedengineto ensurethatadequatebleedair is availablefor antircesysEms.
G. With the High Stage BleedValve or HPSOVlockedclosed,it is normalfor the Pressure
at idle.Consequently,
Regulating
andShutotfValve(PRSOV)
to closeduringengineoperation
whenever
the PRSOis closed.
theassociated
EngineBleedAir OFFlightwillilluminate
the
75% N2 will open the PRSOVand extanguish
Advancingpoweroff idle to approxrmately
EngineBleedAir OFFlight.
30-21-2 a) EngineAnti-lce
VALVELights
b)
I
providedvalveoperationis
(M) One may be inoperative
verifiednormalbeforeoDerationin knownor forecast
icingconditions.
1 (MXO) One may be inoperativeprovidedassociated
valveis inooerative.
1 One may be inoperativeprovidedassociatedEICAS
Advisory messagef../R ENG ANTI-ICE operates
normally.
PLACARD
Anti-ice control panelasappropriate- L (R) EAI VLV LIGHT INOP
Page30-3
REV17 MAR10/2007.
I*MIEW
Hungarian Airlines
fi
^aarEttye
.7e,7
EQUIPMENT
LIST
MINIMUM
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS(O)
1.-200l-300
procedurehas beenaccomplished
A. Engineanti-icevalve operative:Ensuremaintenance
prior to eachdepartureinto knownor forecasticing.
MEL restriclions
B. Engineanti-icevalveinoperative:Referto item 30-21-1for appropriate
andprocedures.
Probe
30-31-1 Pitot-Static
HeaterSystem
- HeaterElement
B
4
3
Exceptfor ETOPSoperationsbeyond120 minutes,a
heater element in one probe may be inoperative
orovided:
a) RVSMoperationsare notconducted,and
b) The airplaneis not operatedin visiblemoisture,in
knownor forecasticingconditions.
30-31-2 ProbeHeatLights
(ExceptCAPTand
F/O PrTOT)
B
4
0
May be inoperativeprovidedassociatedprobe heater
operatesnormally.
1) DualTATLights C
2
I
2
0
PLACARD
Affectedlight- LIGHTINOP
30-31-5CAPTPITOT,and
F/OPITOTHeat
IndicatingSystem
(HeaterOFF
Monitor)
B
(O) Exceptfor ETOPSoperationsbeyond120 minutes,
provided:
maybe inoperative
a) All other elements of the Pitot heat systems
normally,
and
operates
b) The airplaneis not operatedin knownor forecast
icingconditions.
PLACARD
- CAPT(F/O)PITOTHEAT IND INOP
NearEICASasappropriate
(OI
OPERATIONS
Avoidicingconditions.
Page30-4
REV17MAR10/2007.
)V'AIEV
Hungarian Airlinesfi
.eZrEt'YGt
.7Az
EQUIPMENT
LIST
MINIMUM
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
30-32-1 Angleof Attack
SensorHeater
Systems
c
2
1
provided:
(M) Maybe inoperative
a) AssociatedAOAvaneis verifiedintact,and
b) Airplaneis not operatedin knownor foreeasticing
conditions.
PLACARD
- L(R) AOA IIEAT INOP
Overheadpanelasappropriate
(TAT) C
30-33-1 Temperature
ProbeHeater
System
1
0
(O) Exceptfor ETOPSoperationsbeyond120 minutes,
providedthe airplaneis notoperated
maybe inoperative
in knownor forecasticingconditions.
oPERATTONS(O)
(RefMELitem22-30-1).
Observe
MELexceptions
fromthe TAT to
NOTE:Whenthe TAT heatersystemis inoperative,
the TMCconsiderstemperature
be invalidand disconnectsthe autothrottle.
Sinceproceduresfor operatingto CategorylllB
LandingMinimarequireoperativeTMC,there is no MEL relieffor operationto CategorylllB
LandingMinimafor inoperative
TAT probeheater.
30-41-1 FlightDeck
WindowHeat
Systems
1) No.l (n/vd)
Windows
2) No.2 (side)
Windows
2
C
2
provided:
(M) One maybe inoperative
a) Both No.1 (fwd)windowheatersoperetenormally,
ano
b) Associated
windowheatis deactivated.
(M) May be inoperativeprovidedassociatedwindow
heatis deactivated.
c
4
(M) May be inoperativeprovidedassociatedwindow
heatsystemis verifiedto operatenormallybeforeeach
deoarture.
3) No.3
Windows
30.{1-2 WindowHeat
INOPLights
1
(M) Exceptfor ETOPSoperationsbeyond120 minutes,
providedl
one maybe rnoperative
a) Airplaneis not operatedin knownor forecasticing
conditions,
b) BothNo.2(side)windowheatersoperatenormally,
c) Associatedwindshieldpneumaticanti-fogsystem
operatesnormally,and
windowheatis deactivated.
d) Associated
C
Page30-5
REV17 MAR10/2007.
.r+'lAlE|l/ Hungarian Airlinesfi
.aarEtjve
787
LIST
MINIMUM
EOUIPMENT
30, ICEAND RAINPROTECTION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
4
1
May be inoperativeprovidedassociatedwindol heat
systemis inoperative.
MELrestrictions.
NOTE:lf windowheatis inoperative,
referto item30.41-1for appropriate
PLACARD
Affectedlight- LIGHTINOP
30.413WTNDOWPROBEC
HEATGroundTest
Svstem
1
30.f2-1 Windshield
Wipers C
2
0
providedthe airplaneis notoperatedI
Maybe inoperative
within 5 statutemiles of the airportof I
in precipitation
landing.
takeoffor intended
I
1) HighSpeed
May be inoperativeprovidedassociatedlow speed
operatesnormally.
2) LowSpeed
May be inoperativeprovidedassociatedhigh speed
operatesnormally.
30-{3-1 RainRepellent
System
D
30-71-1 DrainMastHeaters C
NOTE:lf is installed.
I
(M) May be inoperativeprovidedwater supplyto the
associatedgalley,lavatorysink and drinkingfountainis
securedOFF.
30-72-l WasteSystem
Heaters
1) DrainCapGasket
Heater
2) RinseHoseHeater
Boot
Page306
REV17MAR10/2007.
/hAlEV
Hungarian Airlines
fi
.?A7EI]IYAF
.78?
EOUIPMENT
LIST
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
31-25-1 Clocks
31-31-1 FlightData
(FDR)
Recorder
System
(includes
Digital
FlightData
Acquisition
Unit)
C
2
26.
i.a.w.JAROPS1'715& 1.720,leaflet
provided:
Maybe inoperative
a) The aeroolanedoesnotexceed8 further
flightswiththe flightdatarecorder
consecutive
unserviceable,
b) Notmorethan72 hourshaveelapsedsincethe
flightdatarecorderwasfoundto be unserviceable,
and
c) Anycockpitvoicerecorderrequiredto becarriedis
ooeratve.
to be
Note1: The flightdatarecorderis considered
whenanyof the following
inoperative
conditionsexist:
a) Lossof the flightrecordingfunctionis evidentto the
checke.g.by means
flightcrewduringthe pre-flight
of a systemstatusmonitor;or
has beenidentifiedby
b) The needfor maintenance
the systemmonitors,whereavailable,withthe
settingof an indicatorand the causeof thatsetting
or
hasnot beendetermined;
actions
c) Analysesof recordeddataor maintenance
haveshownthat morethan5oloof the totalnumber
(variableand discrete)
of individualparameters
requiredto be recordedfor the particularaircraft,
are not beingrecordedproperly.
Note2: Whereimproperrecordingaffects5oloof the
parameters
or less,timelycorrectiveactionwill
needto be takenbythe aeroplaneoperatorin
withapprovedmaintenance
accordance
procedures.
(continued)
Page31-1
REV17 MAR10i2007.
ztallEV
Hungarian Airlines
fi
.?ZE''YZF
.787
LIST
MINIMUM
EQUIPMENT
SYSTEMS
31. INDICATING/RECORDING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
1) FDRRecording
Parameters
requiredby FAR
(see31-31-1NOTE2)
Deleted
2) DFDR
Recording
ParametersNOT
requiredby FAR
(see31-31-1NOTE2)
Deleted
3) QuickAccess
Recorder(QAR)
D
1
0
EICASSTATUSMESSAGES
FLT DATAACQ
FLTDATAREC
PLACARD
As appropriate
MAINTENANCE
NOTE
Installonboardan Instrument
Readingformbook.
(O)
OPERATIONS
UsestandardInstrumentReadingformsfor recordingengineparameters.
and
31-35-1 Performance
Maintenance
(PMR)
Recorder
D
1
0
31-35-2 AirplaneIntegrated D
DataSystem
(AtDS)
1
0
NOTE:AirplaneIntegratedData System is the storing,computingand reportingfunctionof the
DFDAUCPU2with its floppy disk drive and also known as AircraftConditionMonitoring
System(ACMS).
3'l-353 AircraftCondition
Monitoring
System
(ACMS)
Page31-2
REV17 MAR10/2007.
:*'AIEV Hungarian Airlines
fi
.78?
.A2}Et/vZF
EQUIPMENT
LIST
MINIMUM
SYSTEMS
31. INDICATING/RECORDING
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
31-,f1-1EngineIndication
andCrewAlerting
Systems(EICAS)
1) DisplayUnit(DU)
Airplane
A
2
(MXO) Except for ETOPS, one may be inoperative
orovlded:
operatenormallyand
a) StandbyEngineInstruments
areturnedON,
test is performedbeforeeach
b) CargoFIRE/OVHT
depafiure,
system
c) ElectronicEngineControlor autothrottle
operatesnormally,
d) At leastone autopilotoperatesnormally,
e) All EICAScomputersoperatenormally,and
are madewithinoneflight
f) Repairsor replacements
day.
DU failureenroute,
NOTE:In the eventof an additional
the flight crew should considerlandingas soon as
oractical.
2) Computer
(M) XO) Exceptfor ETOPS,one may be inoperative
orovided:
areturnedON,
EngineInstruments
a) Standby
b) ElectronicEngineControland autothrottleopeftltes
normafiy
c) At leastone autopilotoperatesnormally,
sensorsareinstalled,
d) Dualoiltemperature
and
e) Bothdisplayunitsoperatenormally,
0 Repaksor replacementare madewithinone flight
dav.
NOTE:In the eventof an additionalenroutecomputer
failure,flight crew shouldconsiderlandingas soon as
oractical.
sensors.
NOTE'1: HA-LHA,HA-LHB,HA-LHCareconfigured
withdualoil temperature
(continued)
Page31-3
REV17 MAR10/2007.
;|EIEV
Hungarian eirinesh
.ezEttvaF
.787
LIST
MINIMUM
EQUIPMENT
SYSTEMS
3I. INDICATING/RECORDING
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
(version
on the
numbernotindicated
NOTE2: Forahplanes
containing
the Non-PlPFMCinstallation
inoperative,
the FMC'swillnotbe ableto
FMCIDENTpage),withoneEICAScomputer
fuel
comparefuelflowdatabetweenthe EICAScomputers.Thiswillcausethe calculated
quantityvalue,normallydisplayedon the progresspage(212),to go blank.Airplaneswith PIP
rather,thePIPandPegasus
do notexhibitthisblanking;
or Pegasusinstallations
installations
will utilizethe remainingEICAScomputerfuelflowdataandwill providethe
calculatedfuelquantity.
the FMCmaydetermineflight
NOTE3: Followinga flightwithone EICAScomputerinoperative,
groundspeedto setat
completion
duringhighspeedtaxi.ThismaycausetheIRUresidual
greater.
thresholdto identifya
knots
as
the
The FaultlsolationManualuses21
21 knotsor
replacement.
Manualmaypreclude
faultylUR.TestingtheIRUpertheMaintenance
EICASSTATUSMESSAGES
EICASDISAGREE
L EICASCMPTR
R EICASCMPTR
PLACARD
Associateddisplayunit(CRT)or computerselectswitchas appropriate.
(OI
OPERATIONS
1.
c.
4.
Foran EICAScomputerinoperative,
beforetakeoff,withenginesrunning,compareenginedisplay
enginedisplaycross-compare
TheEICAS/SEI
on EICASwiththeStandbyEngineInstrument.
tolerancesareas follows:
Er8r|re
Disphy
ElcAS/SEIEn8ineDi6phy
Cros3-Comlere
Tder!nc€
EPR
.0t
ECT
l:.0'c
NI
.t.!i
N2
l.Oir'i'
Powersettingfor Takeoffmustbe madewith EICAS.
lf remaining
EICASfails:
A. UseSEIto observeengineparameters.
panelfor possible
indications.
abnormal
B. Priorto descent- scanoverhead
Performthe cargoFIRE/OVHT
testpriorto eachflightby pushingthe ENG/APU/CARGO
switchon theAft ElectronicControlPanel.
Page31'4
REV17 MAR10/2007.
I*MIEV
Hungarian AirlinesB
^aa-Ettve
.747
LIST
EQUIPMENT
MINIMUM
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
/
31-51-1 MasterCaution
WarningSyslems
1) MasterWarning
Lights(Pilot'sGlare
Shield)
providedmasterwarningaural
One may be inoperative
system,and all discretewarninglightsoperatenormally.
2) MasterCaution
Lights(Pilot'sGlare
Shield)l
One may be inoperativeprovidedmastercautionaural
system,and all discretecautionlightsoperatenormally.
PLACCARD
As appropriate
deletedaccto MMELRev31.
3141-1 CockpitDoor
Surveillance
System(CDSS)
31-61.4 EICASStatus
Messages
C
C
0
-
0
(M) (O) May be inoperativeprovided associated
equipmentis verifledto operatenormallybeforeeach
deoarture.
provideddispatchdeviations
(M) (O) Maybe inoperative
for associatedequiomentare observed.
MAINTENANCE/OPERATIONS
NOTE
(nuisance)Statuslevelmessagesis allowedby the provisionsof this MEDispatchwithinoperative
Item.
fault.lf suchan
whenthereis no actualequipment
An inoperative
messageis onewhichis displayed
equipment
verifying
that
the
by
EICASmessageis suspected,dispatchmaystillbe accomplished
(proviso
if MMEL
a);
or,
normally
operates
associated
withthe inoperative
EICASstatusmessage
for the associatedinoperative
reliefis available,by observingthe MMELremarksor exceptions
equipment(provisob). The EICASCrossReferenceList(Section1) can be usedto locatethe
itemfor possibleMMELrelief.
appropriate
(M) procedures
Maintenance
are presentedto verifynormaloperationof equipmentfor selected
The messagelistthatfollowsis not intendedto be all inclusive:
nuisancestatusmessages.
EICASSTATUSMESSAGE
EICASSCC
EICASSCCUF
(continued)
Page31-5
REV17 MAR10/2007
.tYUlEV
Hungarian Airlines
fi
.azEttue.7e7
LIST
MINIMUM
EQUIPIIIENT
SYSTEMS
31, INDICATING/RECORDING
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACCARD
As appropriate
C
31-61-5 EICASSignal
Consolidation
Card
(scc)
provided:
(M) Maybe inoperative
a) Fuel quantity indication is verified to operate
normallybeforeeachflight,and
b) Dispatchdeviationsfor associatedequipmentare
observed.
EICASSTATUSMESSAGE
EICASSCC
EICASSCCUF
PLACCARD
As appropriate
Page31-6
REV'17MAR10/2007.
,/VUaEV
Hungarian Airlines,$
.787
.sQuEtwzF
LIST
EQUIPMENT
MINIMUM
32. LANDINGGEAR
REPAIRINTERVAL
NUIIIIBER
REQUIREDFORDISPATCH
REMARKOR/ANDEXCEPTIONS
32-30-1 LandingGear
C
RehactingSystem
1
0
provided:
(M) (O) Maybe inoperative
components
are properlysecuredby an
a) Inoperative
procedure,
and
approved
b) The airplaneis dispatchedin accordancewith the
AFMGearExtendedAppendix.
appropriate
PLACARD
Landinggearlever- LANDING GEARLOCKED DOWN
(O)
OPERATIONS
NOTE:Dispatchrequiresauthorization
by theAFM LandingGearExtendedAppendix.
limits.
and operational
1. ObserveAFM LandingGearExtendedcertificatelimitations
2. Baseflightplanon landinggearextended.
3. TheALT Vmo/Mmoswitchto the Air DataComputethasbeensetto providegeardown
Vmo,4VImo
datafor displayon airspeedindicators.The auralwaming,redwaminglightson the
glareshield,
andthe RED OVSPDwaminglight on thecaptain'spanelwill comeon whenthe
geardownVmo/I\{mois exceeded.
4. The followingflight deckaffectswill occurwhile the gearis extended:
A. Geardown liglts (NOSE,LEFT, RIGHT)will remainilluminated.
ALT Vmo,4Umo
hasbeenselected).
B. Altitudealertingwill be available(because
GPWSMode3("Don't Sink") and
C. If flapsareloweredflaps30 (retumto base),Enhanced
Mode4 ("Too Low Terrain")will not be available.
D. CollinsTCAS lowerantennawill not switchto omnidirectional.
E. AlliedSignalTCAS lowerantennawill switchto omindirectional.
F. HoneywellTCAS lowerantennawill switchto omnidirectional..
Gear
32-31-1 Landing
LatchSolenoid
C
1
0
(M) (O) May be inoperativein the latched position
providedthe overridemechanismoperatesnormally.
PLACARD
Landinggearlever- GEARLATCH SOLENOIDINOP
(OI
OPERATIONS
Forgearretractionusethe followingprocedure:
gearLOCKOVRDswitch.
1. Pushlanding
2. Position
landinggearleverto UP.
position
gearleverto OFF.
landing
3. For-200f300afterGEARLightextinguishes,
Page32-1
REV17 MAR10/2007,
tVUaEV Hungarian Amines
fi
.zez
.gZTEtjUZF
LIST
MINIMUM
EOUIPMENT
32. LANDINGGEAR
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
32-32-1MainGearDoor
UplockSprings
B
4
3
(M) (O) One springon one door uplockmechaniusm
maybe missingprovidedspeeddoesnotexceed
270 KIAS/ 0.82Mach.
OPEMTIONS(O)
Observegearextendedplacardspeedlimit.
32-41-1WheelBrakes
c
8
C
8
(MXO)(PREFERRED)
One brakemay be deactivated
tool provided:
witha deactivation
a) Performancecomplieswith AFM for ONE BRAKE
and
DEACTIVATED,
b) Anti-skid operates normally on the remaining
wheels.
7 (MXO)(OPTIONAL)One brakemay be deactivatedby
cappingoffthebrakelineprovided:
a) Takeoff performanceis based on LandingGear
Extended,
complieswiththe
b) Takeoffand Landingperformance
AFMfor one brakeinooerative.
c) After takeoff, gear remains extended for two
minutespriorto retraction,
and
wheels.
normally
on remaining
operates
d) Anti-skid
OPERATIONS
IOI
1. BrakeDisconnect
Toollnstalled:
Adjustlakeoffand landing
Stoppingdistanceswill be increased
witha brakedeactivated.
performance
in comoliance
withtheAFMdatafor BrakeDeactivated.
2. BrakeLineCapped:
A. Aftertakeoff,leavethe landinggearextendedfor a minimumof two minutesto allowthe
wheelsto spindownpriorto gearretraction.
Thefollowingflightdeckaffectswilloccurwhilethe gearis extended:
Geardownlight(NOSE,LEFT,RIGT)willremainilluminated.
Altitude
willnotbe available.
alerting
lf flapsare loweredto flaps30, EnhancedGPWSMode3 ("Don'tSink")and Mode4 ("Too
LowTerrain")
willnotbe available,
4) CollinsTCASlowerantennawill notswitchto omnidirectional.
5) AlliedsignalTCASlowerantennawillswitchto omindirectional.
6) Honeywell
TCASlowerantennawill switchto omnidirectional.
B.
1)
2)
3)
Page32-z
REV17 MAR10/2007.
.ttMlEV
Hungarian Airlinesfi
.ezEtze.787
MINIMUMEQUIPMENT
LIST
32. LANDINGGEAR
REPAIRINTERVAL
NUMBERREOUIRED
FORDISPATCH
REMARKOR/ANDEXCEPTIONS
C. Takeoffperfomance:for all 767airplanes,
the allowabletakeoffweightis the lowestof the
brakedeactivated
field length,adjustedclimb or the adjustedobstaclelimitedweight.
l) Adjusttakeoffandlandingfield lengthperformance
in compliance
with AFM datafor one
BrakeDeactivated.
Do not useimprovedclimb performance.
2) ReduceAFM secondsegment(gearup) climb limitedweightwith the Climb Limit
Decrementshownin thetablebelow.
3) Reducethe obstacleclearance
shownin the
limitedweightby the ObstacleLimit Decrement
use
of
extended
segment
tablebelow.Obstacleclearance
assume
second
adjustments
procedures
with MCT cleanup.All obstacles
mustbe clearedby the heightachievedat the
in
endof extendedsecondsegmentclimb.Adjusttakeoffand landingfiledperformance
comoliance
withAFM datafor BrakeDeactivated.
Model/Enqine
-200i-cF6-80c2
-300/ cF6-80c2
32-41.2 BRAKESOURCE
Lioht
1
TakeoffClimb
5 1. 0 0 0l b ( 2 3 , 1 3 4k q )
44.000lb (19.959ko)
TakeoffObstacleClearance
kq)
51.000lb (23,134
15
37.000lb (16,784kq)
ko)
39.000tb (17,69'1
32.000lb (14.516kq)
36.000lb (14,516kq)
l)
ke)
s3.000
lb (24,041
lb (19.9s9
ks)
44.000
s4.000lb (24.495ke)
ke)
lb (22,680
50.000
20
38"000lb (17,237ks)
45,000lb (20,412kg)
Flap
5
44.000lb {19,959kq)
0
providedassociatedEICAS
(M) (O) May be inoperative
advisorymessageis verifiedto operatenormally.
0
provided:
(M) Maybe inoperative
a) C and R hydrauliclow SYS PRESSlightsoperate
normally,
and
b) Brakehydraulicsourceand alternatesourcesystem
are verifiedto operatenormally.
PLACARD
Affectedlight- LIGHTINOP
OPERATIONS(O)
Usethe EICASadvisorylevelBRAKE SOURCEmessage
for the non-normalchecklistprocedurein
lieuof theBRAKESOUCElishl.
Page32-3
REV17 MAR10/2007.
:tMlEV
Hungarian Airlines
A
.aa7Et/vaF
.7A.7
LIST
EQUIPMENT
MINIMUM
32. LANDINGGEAR
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
3241-3 GearRetraction
BrakingSystem
C
1
0
provided:
(O) Maybe inoperative
a) After takeoff, gear remains extended for trrvo
and
minutespriorto retraction,
b) Takeoff performanceis based on LandingGear
Extended
PLACARD
Near gearhandle- INFLT WHEEL BRAKING INOP
(O)
OPERATIONS
1. Takeoffperformancemust be basedon the AFM Gear DownAppendixperformancedatiafor
limited
reduceperformance
TakeotfClimband ObstacleClearance.In lieu of theseadjustments,
(O) procedurefor BrakeLine Capped.
weightsasshownin the Item32-41-1Operations
2. After takeoffthe landinggear must be left extendedfor a minimumof 2 minutesto allowthe
wheelsto spindownpriorto gearretraction.
3242-1 ANTISKIDSystem C
1) Channels
C
1
0
(O) May be inoperativeprovidedAFM decrementsare
operations.
appliedfor antiskidinoperative
8
7
brakemay be
(MXO)One channeland the associated
(brakedeactivated
or linec€pped)provided:
inoperative
a) Brake is deactivatedby an acceptableprocedure,
ano
b) AFM decrementsare applied for the selected
orocedure.
NOTE 1 : For antiskidsystem inoperativedispatch,it is recommendedthat inoperativeantiskid
channelsare deactivatedand that operativechannelsremainoperativeMAINTENANCE
(M) step2 is providedto deactivateonly the inoperativechannelsfor dispatch.Altemately,
the entireAntiskid System
MAINTENANCE(M) step3 is providedto deactivate
NOTE 2: MEL ltem 3242-1 covers all Normal and AlternateAntiskid System faults (including
transducerfaults)exceptfor AlternateAntiskidValve Faults.For AlternateAntiskidValve
faults,consultMELitem3242-2 tor possibledispatchrelief.
EICAS STATUSMESSAGES
ALTN ANTISKID
NORM ANTISKID
Page32'4
10/2007.
17
MAR
REV
Hungarian Airlines,f
fuAlEV
.78.7
.?zEtjyzF
LIST
MINIMUM
EQUIPMENT
32, LANDINGGEAR
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACARD
Autobrakesswitch as appropriate- AUTO BRAKES INOP
(O)
OPERATIONS
(twoor morechannelsinoperative)
1. Forantiskidsysteminoperative
withAFMfor antiskidinoperative.
mustbe in compliance
a) Takeoffand landingperformance
b) SelectAUTOBRAKESOFF.
c) Whenstoppingafterlandingand for refusedtakeoffs:
- Closethrustleversand raisespeedbrakes.
- Initietewheel brekingusing light pedal pressureand increaseas groundspeed
oecreases.
d) CategoryIII weatherminima operationsmay requirean operativeautobrakesystem.
(oneantiskidchannelinoperative)
2. Forone brakedeactivated
Adjusttakeotfand landing
a) Stoppingdistanceswill be increasedwith one brakedeactivated.
performance
in compliance
withtheAFMfor One BrakeDeactivated.
b) lf a brakeline is capped,aftertakeoffthe landinggearmustremainextendedfor a minimum
of two minutesto allowthe wheelto spin down priorto gear retraction.Takeoffclimb and
obstructionclearanceperformancewill be limited by the requirementto keep the gear
extended.Adjust takeotf and landingperformancein compliancewith the AFM for both
reducel
In lieu of theseadjustments,
LandingGear Extendedand One Brake Deactivated.
performancelimited weightsas shownin the Item 32-41-1Operations(O) procedureforl
BrakeLine Capped.
NOTE:lf a transducer
fault exists,EICASstatusmessageALTN ANTISKIDwill remain
displayed.Flightcrewsshouldbe awarethatlossof the righthydraulicsystemenroute
will resultin annunciation
of the ANTISKIDlightand message.Brakingetfectiveness
on the alternatesvstemis reduced- brakewithcaution.
3242-2 AlternateAntiskid c
Valves
4
0
provided:
(M) (O) Maybe inoperative
a) Manual brakingcapabilityon the alternatebrake
systemis verifiedon associatedwheels,and
b) lf failure affects normal antiskid system, AFM
antiskid inoperative performance decrements
applied.
Page32-5
REV17 MAR10/2007.
,VU,EV
Hungarian Airlines,fi
.azEtjyaF
.7e7
LIST
MINIMUM
EQUIPMENT
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE: For NormalandAltemateAntiskid SystemfaultsotherthanAlternateAntiskidValvefaults,
consultMMEL iten32-42-1for possibledispatchrelief.
EICAS STATUSMESSAGES
ALTN ANTISKID
OPERATIONS
{O}
1. Inop€rativeAlternateAntiskidValvesdo not affectthe normalbrakingsystem.However,flight
of
crewsshouldbe awarethat lossof the righthydraulicsystemenroutewill resultin illumination
on the alternetesystemis
the ANTISKIDLightand message,indicatingbrakingeffectiveness
reduced.lf thisoccurs,brakewithcaution.
2. lf anti-skid
systemis inoperative:
performance
a ) UseAFMAnti-skidInoperative
decrements
as applicable.
b) SelectAUTOBRAKESOFF.
for stopping.
c) Usemoderatebrakingaction,consistent
withrunwayconditions,
Light
3242-3 ANTISKID
C
1
0
(M) May be inoperativeprovidedantiskid system is
verifiedto operatenormally.
C
1
0
(O) May be inoperativeprovidedAFM decrementsare
operations.
appliedfor antiskidinoperative
PLACARD
Affectedlight- LIGHTINOP
OPERATIONS
{O}
1. Forantiskid
systeminoperative
a) Takeoffand landingperformance
mustbe in compliance
withAFMfor antiskidinoperative.
(all
with
all
antiskid
channels
deactivatedor Antiskid Switchl
bi
s=ystem
channelsinoperative
OFF), the autobrakesystemis also inoperative.Do not use autobrakes.Select AUTOI
BRAKES
OFF.
c) Whenstoppingafterlandingand for refusedtakeotfs:
- Closethrustleversand raisespeedbrakes.
- Initiatewheel brakingusing light pedal pressure and increase as ground speed
oecreases.
3242.4 Autobrakesystem
provided:
Maybe inoperative
AUTO
BRAKES
light is not illuminatedwith the
a)
autobrake
switchOFF,and
minimums
do notrequireitsuse.
b) Approach
Page32-6
REV17 MAR10/2007.
;*'lAlEW
Hungarian Airlines4
^eaTEt'YZt
.78.7
EQUIPMENT
LIST
MINIMUM
32. LANDINGGEAR
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
n
(M) May be inoperativewith AUTO BRAKES light
andthe autobrakeswitchOFFprovided:
illuminated
a) Autobrakesolenoidvalve must be verifiedclosed,
and
do notrequireitsuse.
b) Approach
minimums
(M) May be inoperativewith AUTO BRAKES Light
illuminated
andthe autobrakeswitchOFFprovided:
a) Module is deactivatedin accordancewith an
and
acceptedprocedure,
b) Approachminimumsdo not requireits use.
PLACARD
Auto brakesselector- AUTO BRAKESINOP
32-,42-5TaxiSpeed
Indication
32-44-2 ParkingBrake
Valve
C
1
0
(M) (O) May be inoperativeclosed providedAFM
areapplied.
decrements
antiskidinoperative
PLACARD
ParkingBrakelight- INOP
Autobrakeswitch - INOP
(O)
OPERATIONS
1. Takeoffandlandingperformance
withAFMforantiskidinoperative.
mustbe in compliance
2. Se|ectAUTOBRAKESOFF.
3. Whenstoppingafterlandingand for refusedtakeoffs:
a) Closethrustleversand raisespeedbrakes.
b) Initiatewheelbrakingusinglightpedalpressureand increaseas groundspeeddecreases
32.44-3 ParkingBrake
Lights
provided:
(M) Maybe inoperative
a) Parkingbrakevalveoperatesnormally,and
b) Antiskidlight is verifiedoperationalonceeachflight
day.
(O) May be inoperatrveprovided AFM Antiskid
decrements
are applied.
inoperative
Page32-7
REV17 MAR10/2007.
:IMIEV
Hungarian Airlines4
.78.7
.?zEtjvat
MINIIIIIUM
EQUIPMENT
LIST
32. LANDINGGEAR
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
1
0
(O) May be inoperativeprovided EICAS message
normallY.
BRAKEoperates
PARKING
PLACARD
Affectedlight- LIGHTINOP
(O)
OPERATIONS
1. Whenparkingbrakeis set,ensureadvisory
PARKING
BMKE is displayed.
EICASmessage
parkingbrake:
2. Whenreleasing
a) CheckthatANTISKID
indicator
lighton P5 panelis extinguished.
b) lf ANTISKIDlight is illuminated,
but leave
dispatchwill be with the antiskidinoperative,
antiskidswitchselectedON.
3. Forantiskidsysteminoperative:
a) Takeoffand lendingperformance
withAFMfor entiskidinoperative.
mustbe in compliance
b) Initiate
wheelbrakingusinglightpedalpressure.
3244.4 BrakeAccumulator C
Pressure
Gauge
(WheelWell)
I
3244.5 BRAKEPRESS
Gauge
(FlightDeck)
0
May be inoperetiveprovidedassociatedflight deck
indicationoperatesnormally.
0
provided:
(M) Maybe inoperative
a) Brake accumulatorair charge is verified normal
onceeachflightday,and
normally.
b) RightlowSYSPRESSlightoperates
PLACARD
Parkbrakeindicatorlight on quadrantstand-PARK BRAKE LIGHT INOP
32*45-'l Tire Pressure
Indicators
D 1 0 0
3245-2 NoseWheelSDin C
Brakes(Snubbers)
2
0
32.f5-3 Tire Pressure
IndicationSystem
1
0
D
(M)Maybe damaged
or missing.
(rPrs)
NOTE: For -2001300,
this item coversthe tire pressureindicationson the lowerEICASdisplay.
Page32-8
REV17 MAR10/2007.
Hungarian Airlines
I!'AIEV
rt
,78.7
.?a7Et/vaF
EQUIPMENT
LIST
MINIMUM
32. LANDINGGEAR
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
D
32.46-1 Wheel Brake
Temperature
Monitoring System
(BTMS)
1
0
NOTE: Brakecoolingfanswill be inoperativewhenall
eight braketemperaturereadingsare inoperative.
NOTE: For -2001300,
this item coversthe braketemperature
indicationson the lower EICASdisplay,
aswell asthe BRAKE TEMP light abovethe landinggearhandle.
32-51-1 RudderPedal
NoseWheel
Steering
0
provided:
(M) (O) Maybe inoperative
a) Operationof other systemson the airplaneis not
impaired,
minimums
do notrequireitsuse,and
b) Approach
c) All takeoffsand landingsare madeby the pilotwith
accessto an operatingtiller.
PLACARD
Neareachpilot's airspeedindicator- RUDDERPEDALNOSEWHL STEERINOP
OPERATIONS
{OI
CAUTION: PILOTS MUST USE CAUTION WHEN USING TIIE NOSE WHEEL STEERING
TILLER (WHEEL) ABOVE 20 KNOTS TO AVOID OVER-CONTROLLINGTIIE
NOSEWHEELSRESULTINGIN POSSIBLELOSSOF DIRECTIONALCONTROL.
procedures
shallbe used.
Flightcrewmemberwithaccersto thetillerwillbeflying,andthefollowing
Takeotf:
The crewmembershouldsteer the airplane,manipulatingthe steeringwheel controlwith his
notflying
40 to 50 kts).The crewmember
hand,untilthe rudderbecomesetfective(approximately
on the controlcolumnuntil
shouldassistby keepingthewingslevelanda lightfoMardpressure
forsteering.
thetilleris no longerrequired
Landing:
with accessto the tiller shoulduse the rudderand steeringwheelcontrolas
The crewmember
shouldassistby keepingthewingslevel
required
duringthe landingroll.The othercrewmember
andforwardpressureon the controlcolumn.
Page32-9
REV17 MAR10/2007.
t!'lAlEV
BzrEttyzF
Hungarian Airlinesfi
.787
LIST
EQUIPMENT
MINIMUM
32. LANDINGGEAR
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Gear
32-61-1 Landing
DOORSLight
System
0
(M) May be inoperativeprovided EICAS Advisory|
messageGEARDOORS(LevelC) is verifiedto operateI
normally.
I
PLACARD
Affectedlight- LIGHTINOP
GearDoor
32-61-2 Landing
LatchProximity
Sensor
1) SystemOne
C
4
provided:
(M)(O)Onemaybe inoperative
a) Appropriateperformanceadjustmentsare applied,
and
b) RemainingSystem One and all System Two
sensorsare verifiedto operatenormallybeforeeach
deoarture.
2) SystemTwo
C
4
provided:
(M)(O)Onemaybe inoperative
a) Manualfunctionof the PassengerNoticeSystem
operatesnormallyand proceduresfor its use are
andused,and
established
b) RemainingSystem Two and all System One
sensorsare verifiedto operatenormallybeforeeach
deoarture.
NOTE:An inoperativeSystem2 sensorwill renderthe
FlightDeckAutomaticFunctionof the PassengerNotice
Systeminoperative.
to display.
LDGGEARMONITOR
NOTE:Oneor moreinoperative
willcausestatusmessage
sensors
Two or more inoperative
sensorswill causeNo DispatchadvisorymessageGEARDOORS
and cautionmessageGEAR DISAGREEto display,Note that nose gear door sensorsare
inhibited
withoearextended.
EICAS STATUSMESSAGES
LDG GEARMONITOR
Page32-10
REV17 MAR10/2007,
ttU,EV
zzrEtlvzF
Hungarian Airlinesfi
.787
EQUIPMENT
LIST
MINIMUM
32. LANDINGGEAR
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O)
OPERATIONS
1. ForSystemOneinoperative:
withthe
NOTE: lf a SystemOne(SYS'1)sensoris inoperative,
theADPwilloperatecontinuously
ADP switchin the AUTODosition.
A. Reduceperformance
limitedweightsas follows:
Takeoff,En-routeClimband Landing
Model/Enqine
-200& -300/All
3 . 6 0 0l b ( 1 , 6 3 3k q )
B. The enrouteclimbweightpenaltieslistedaboveare basedon singleengineoperatingspeeds
meximumlift-to-drag
thatapproximate
ratiospeed.To accountfor the differencein leveloff
altitudewhenoperatingat otherspeeds,multiplythe enrouteclimbweightpenaltylistedabove
SPEED
in theENROUTE
DIVERSION
bytheappropriate
factorlistedon page3-01-0.0
paragraph.
EFFECTS
for use
eachoperatormustestablishprocedures
lfa SystemTwo (SYS2) sensoris inoperative,
of the flightdeckmanualfunctionof the PassengerNoticeSystem.
32-7'l-1 TailSkid
(767-300)
0
provided:
(M) (O) May be inoperative
a) Tail skidis securedin the extendedposition,
b) Water suppliesassociatedwith aft drain mast are
securedOFF,and
adjustments
areapplied.
c) Appropriateperformance
PLACARD
Tail Skidlight - TAIL SKID INOP
Affected lavatorydrains,sinksand fountainsasappropriate- INOP
OPf,RATIONS (O)
limitedweightsasfollows:
1. Reduceperformance
Model / Engine
-300/ Alt
TakeoffandLandine
1.400lb (635ksi
EnrouteClimb
( l,l 79kg )
2,6001b
Page32-11
REV17 MAR10/2007.
Hungarian Airlinesfi
ttAlEW
.787
.azTEtjyzF
LIST
MINIMUM
EOUIPMENT
32. LANDINGGEAR
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2. The enrouteclimb weightpenaltieslistedabovearebasedon singleengineoperatingspeedsthat
approximate
maximumlift-to-dragratio speed.To accountfor the differencein level off altitude
when operatingat other speeds,multiply the enrouteclimb weight penaltylisted aboveby the
appropriatefactor listed on page3-01-0.1in the ENROUTE DIVERSION SPEEDEFFECTS
paragraph.
3. Enroutefuel consumption
will increaseby 1.4%with thetail skid securedin theextendedpositron.
32-71-2 fatl Skidlndication C
System
(767-300)
'l
(M) May be inoperative provided tail skid
function is verified to operatenormally
extend/retract
onceeachflight day.
c
l
(M) (O) May be inoperativeprovided:
a) Tall skid is securedin the extendedposition,
b) Water suppliesassociatedwith aft drain mast are
securedOFF,and
areapplied.
adjustments
c) Appropriateperformance
1) TAIL SKID Light
(-300)
C
1
May be inoperative provided altemate indication
normally.
operates
2) ProximirySwitch
System
c
1
(M) May be inoperative provided tail skid
extend/retractfunction is verified to operatenomally
onceeachflight day.
PLACARD
TAIL SKID light (abovelandinggearlever)TAIL SKID LIGHT INOP
Affected sinksand drains- INOPERATIVE
OPERATIONS(O)
For tailskidextended,
reduceperformance
limitedgrossweightsasshownin l1em32-7l-l Operations
(O) procedure.
Enroutefuel consumptionwill increaseby approximately1.4% with the tailskid securedin the
extendedoosition.
Page32-12
REV17 MAR10/2007.
tlHlEW
Hungarian Airlines4
.?zEtjYE.787
LIST
MINIMUM
EQUIPMENT
33. LIGHTS
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
33-11-1 Flight
C
Compartment
and
Instrument
Lighting
System
-
for nightoperations
Individuallightsmay be inoperative
provided
remaining
lightsare
a) Sutflcientto clearlyilluminateall requireinstruments,
control,andotherdevicesfor whichit is provided,
b) Positionedso direct rays are shieldedfrom flight
eyes,and
crewmembers
and intensityis acceptableto
c) Lightingconfiguration
the flightcrew.
1) Crewentrylight
PLACCARD
As appropriate
33-14-1Supernumerary
Reading
Lights
PLACCARD
As appropriate
33-16-1MasterDimand
TestSystem
providedthe intendedfunctionof
(M) Maybe inoperative
light(s)
is
verified.
associated
PLACCARD
As appropriate
33-21-1CabinInterior
lllumination
System
1) Passenger
Configurations
WithIncandescent
Emergency
EscapePath
MarkingSystems
i.a.w,JAROPS1.815,leaflet26.
provided:
Individuallightsmaybe inoperative
a) Remaininglightingis sufflcientfor cabinattendants
to Derformtheirduties.and
b) For night ETOPSoperations,at least 75% of the
NightLightsmustoperate.
(continued)
Page33-1
REV17 MAR10/2007.
rtailEW
Hungarian Airlines,fi
.aa7EtlvaF
.78?
LIST
MINIMUMEQUIPMENT
33. LIGHTS
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2) Passenger
Configurations
With PhotoLuminescent
Emergency
EscapePath
MarkingSystem
Everytwoadjacentgenerallightingceilingfluorescent
provided:
tubesmaybe inoperative
a) At leasttwo tubesare operativebetween,
and adjacent
b) The tubesatthe samebodystation
in otherceilinglightsstripare operative,
and adjacent
c) The tubesatthe samebodystation
in othersidewalllightsskip areoperative.
Everytwo adjacentgenerallightingsidewallfluorescent
provided:
tubesmaybe inoperative
a) At leasttwotubesareoperativein between,
b) The tubes at the same bodystationin all other
sidewalllightsstripare operative.
General lighting window fluorescenttubes may be
inoDerative.
a) For night ETOPS,et least 75oloof the Night
Lightsmustoperate.
PLACCARD
As appropriate
33-24-1 PassengerNotice
System
('NOSMOKTNG,
FASTENSEAT
BELT,
RETURN
TO
cABlN")Signs
(M) (O), No passengerseat, cabin attendantseat,
"No
lavatory, or may be occupied from which a
to Cabin"sign i3 not
Seat BelUReturn
Smoking/Fasten
visible.(Theseet,lavatory,or bunkmustbe blockedand
- "DONOTOCCUPY').
placarded
(o) "No Smoking/Fasten
Seat Belv Return to Cabin'
signs may be inoperativeand the atfectedpassenger
seat(s),cabin attendantseat(s),lavatoriesor crew rest
areabunkmaybe oc.upiedprovided:
PA System operates normally and cen be
a)
the cabinduringflight,
clearlyheardthroughout
and
PA systemis usedto alertthe cabincrewand to
b)
and crewrestareaoccupants
notifypassengers
when seat belts should be fastened, and
smokingis prohibited.
(continued)
Page33-2
REV17 MAR10/2007.
;+UIEV
Hungarian Airlinesfi
.earEttuzt
.787
LIST
MINIII,IUM
EQUIPMENT
33. LIGHTS
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
1) AuralToneSystem c
l
0
2) FlightDeck
c
AutomaticFunction
1
0
provided:
(O) Maybe inoperative
a) Manualcontrolfunctionoperatesnormally,and
and used.
b) Procedurefor its useare established
PLACARD
Blocked
seat- DO NOTOCCUPY
OPER.ATIONS
{OI
whenseat beltsshouldbe fastenedand smoking
Whenthe pilotin commandshallnotifypassengers
prohibited.
on takeoffwhenthe landinggearis retracted
NOTE:The NO SMOKINGsignsnormally
extinguish
gearis extended.
TheFASTENSEATBELTsigns
andilluminate
duringlandingas thelanding
whenthe
normally
extinguish
on takeoffwhentheflapsandlandinggearareup andilluminate
flapsor landinggearareextended.
33-31-1WheelWell Lights C
6
0
D
-
0
C
I
0
9
0
PLACCARD
As appropriate
33-31-2 ExteriorCargo
Loading
Area
Lights
PLACCARD
As appropriate
33-31-3ServiceLights
PLACCARD
As appropriate
C
33-31.4 Electrical
Equipment
Center
Lights
PLACCARD
As appropriate
Page33-3
REV17 MAR10/2007.
,',/aA|'EV Hungarian Airlines'fi
.eaTEttvaF
.78-
LIST
EQUIPMENT
MINIMUM
33. LIGHTS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
33-37-1 Cargo
Compartment
Lights(Lower)
1) StillLights
0
2) LowerCargo
Compartments
0
3) LightLens
providedprocedures
do
(O) Maybe inoperative
not reouiretheiruse.
providedassociatedlightis
(M) Maybe broken/missing
deactivated.
PLACCARD
As appropriate
(O)
OPERATIONS
materialis carriedin accordance
with FAR 25.857,US HMR 175.25
Ensurehazardous
regulations.
through175.90andotherappropriate
Page334
REV 17 MAY30/2007.
:*MIEW Hungarian Airlines
fi
.78,?z7Et'ye
LIST
EQUIPMENT
MINIMUM
33. LIGHTS
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
33.41-1 Winglllumination C
Lights
2
0
(O) May be inoperativeprovided ground de-icing
do not requiretheiruse.
orocedures
PLACCARD
Winglllumination
Lights- WINGLIGHSINOP
(O)
OPERATIONS
Ensurethatde-icing
is complete,
whenused.
33.f2-1 LandingLights
c
4
One nosegearand/orone wingmountedlightmay
for nightoperations.
inoperative
c
4
for dayoperations.
Maybe inoperative
PLACCARD
As appropriate
3342-2 TaxiLight
PLACCARD
TaxiLightswitch- INOP
RunwayTurnoff
Lights
PLACCARD
Associatedlight switch(es)- INOP
33.43-1 PositionLights
(Bulbs)
c
c
8
all exceptthe followingminimum
For nightoperations,
maybe inoperative:
b) Onestationaryredwingtip bulb,
greenwingtip bulb,and
c) Onestationary
whitebulbperwingtip.
d) Onestationary
for dayoperations.
Maybe inoperative
PLACCARD
As appropriate
Page33-5
REV'17MAR10/2007.
Hungarian Airlines4
IIMIEV
.787
,Z2TEI]VJF
EQUIPMENT
LIST
MINIMUM
33. LIGHTS
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
33.44-1 Anti-Collision
Lights
(RedStrobes/
WhiteStrobes)
C
4
0
for dayoperations.
Maybe inoperative
For night operations,upper and lower red fuselage
providedwingtip whitestrobe
lightsmay be inoperative
lightsoperatenormally.
C
4
D
4
wingtip whitestrobelightsmay be
For nightoperations,
providedupperand lowerredfuselagelights
inoperative
ooeratenormallv.
PLACCARD
As appropriate
3345-1 LogoLights
PLACCARD
As appropriate
Light assembliesinstalled above either main aisle
(curved edge of stowage bins) may be inoperative
providedno two adjacentoppositeside lightassemblies
are inoperative.
33-51-1 InteriorEmergency
LightingSystem
(BatteryPowered)
PLACCARD
As appropriate
33-51-2Exterior
Emergency
LightingSystem
i.a.w.JAR OPS 1815,leaflet26,
0
May be inoperativefor daylightoperations.
1) EscapeSlide
Lighting
PLACCARD
As appropriate
Page33S
REV17 MAR10/2007.
.I+UIEV
,ezrEttve
Hungarian AirlinesB
.78,7
LIST
MINIIII|UM
EQUIPMENT
33. LIGHTS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
33-51i EmergencyEscape
PathMarking
System
1) Incandescent
LightingSystem
C
2) Photo-Luminescent
C
Lighting
System
-
May be inoperative provided approved minimum
acceptablelightinglevelsspecifiedbeloware complied
with:
a) FloorMarkerLights- MainAisle:
(1) Allarrowlightsmustbe operative.
(2) All lights adjacentto arrow lights must be
operatlve.
lightsmust
(3) Lightadiacentto an inoperative
operatenormally.
b) FloorMarkerLights- CrossAisle:
(Electroluminescent)
Mustbe operative.
c) SidewallExitIndicator
At least two of five lamps in each exit indicator
mustbe oDerative.
d) At least one light must be operativeevery meter
betweenthe farthestandfarthestaft pathlights.
-
stripsof an aisle may
Each of the Photo-Luminescent
be partlyinoperativeup to a lengthof 0,25m provided
partsare not directlyoppositeeachother
the inoperative
than2,0m.
andarenotclosertogether
partsare allowed.
No morethan4 suchinoperative
PLACCARD
As appropriate
OPERATIONS
NOTE
forthe BoeingDesigned
requirements
1. Thefollowing
arethe minimumFAAdispatch
systems:
on thecabin
NOTE'1:Thenumberof floormounted
aislemarkerlightsmayvarydepending
mayhavelightedanowsin placeof red lenses
configuration,
Someconfigurations
at the midcabinexits.
of floor
NOTE2: Emergency
EscapePathMarkingSystemsareoftena combination
mounted,seatmounted,and monumentmountedlights.Eachsystemmayvary
due to ditferingcabinconfigurations.
Page33-7
REV17 MAR10/2007.
I+UIEV
Hungarian AirlinesB
.azrEttvat
.787
LIST
EQUIPMENT
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Source C
34-00-'l Instrument
SelectSwitches
-
provided:
(O) Maybe inoperative
a) Associated instruments operate from isolated
sources,
switchesare not movedin flight,
b) Inoperative
at leastone FMC,EFISand
c) For ETOPSoperations,
IRSswitchmustoperatenormally.
PLACARD
Associatedswitch- INOP
(OI
OPERATIONS
Ensureinstruments
areoperatingfromisolatedsourcesas follows:
NOTE:Do notmoveinoperative
switchduringflight.
1.
FMCSwitch:
WarningSystem(EGPWS)
A. PIPand PegasusFMC'SwithoutEnhancedGroundProximity
upgrade:
circuitbreaker(P'11) panel.
1) OpencircuitbreakerFMCR on theoverhead
2) Observe
thatmapdisplayfailson rightHSIonly.
circuitbreaker(P11) panel.
3) ClosecircuitbreakerFMCR on theoverhead
WarningSystem(EGPWS)upgrade:
B. Pegasus
FMC'swithEnhanced
GroundProximity
NAV
select
switch
to the offsideFMC.
1) Positionan operative
source
will
2) lf bothpilotsareoperating
fromthesameFMC,a greenFMCL or FMCR annunciation
appearin the lowercenterportionof the HSl.
3) Returnthe NAVsourceselectswitchto the originalselection,
2.
EFISSwitch
side,ILSmodeon FirstOfficer's
A. UsingHSIcontrolpanels,selectVORmodeon Captain's
side.
modesaredisDlaved
on eachHSl.
B. Observe
thatselected
3.
IRSSwitch
A. Placeonlythe centerIRS modeselectorswitchin ALIGNposition.
(shadedsky andground)lf
B. Observethatat Leastone ADI hasa normalbackground
the
shadingis loston bothADI's,bothare using centerIRS
background
4.
AIR DATASwitch
A. Ptacethe L AtR DATACOMPTRTESTSWITCH(P61)in the testpositionand observethat
testdata(airspeed,altitude,etc.)are displayedonlyone pilot'sinstruments.
Page34-1
REV17 MAR10/2007
.ttMlEW
.aarEttve
Hungarian Airlines
fi
.7e-
LIST
IIIINIMUMEQUIPMENT
34. NAVIGATION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-10-1 AirsoeedIndicators C
2
Any in excessof one may be inoperativeprovidedthe
side
operativeairspeedindicatoris on the commander's
NOTE: For aeroplanesfittedwith EFIS, both airspeed
indicatordisplays(tape)mustbe operative.
1) Standby
airspeedindicator
34-10-2 Altimeters
0
May be inoperativeprovided both main airspeed
indicatorsareoperative.
2
provided:
Any in excessof two maybe inoperative
a) Onealtimeteris operativefor eachpilot.
and
b) The requiredaltimetersoperateindependently,
or servo
c) At lleastoneof the aboveis pneumatic,
pneumaticaltimeter.
fiftedwith EFIS,the altimeter
NOTE: Foraeroplanes
displays(tape)mustbe operative.
measurement
altitude
NOTE2: Twoindependent
systemsare requiredto be operativefor RVSM
ooerations.
34-13-'l Mach/Airspeed
lndicators
1) MachIndicators
1
c
2
0
providedEFISMachindications
are
May be inoperative
installedand operatingnormallyat the respectivepilot's
station.
provided:
Maybe inoperative
remainsat or belowFL 300,and
a) Theairplane
b) A placard with this limitationis affixed to the
panel.
instrument
2) Command
AirspeedCursors
3) AirspeedIndicators
May be inoperativeprovidedEFISAirspeedindications
operatenormallyat the respeclivepilot'sstation.
(continued)
Page34-2
REV17 MAR10/2007
.:lMlEW Hungarian AirlinesA
.78?
.?aTEtJUZt
LIST
EQUIPMENT
MINIMUM
34, NAVIGATION
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
4) ExternalAirspeed
Markers(Bugs)
C
0
(O) May be inoperativeor missingprovidedalternate
and used
Drocedures
areestablished
PLACARD
- INOP.
Appropriate
indicator
lf bothmachindications
are inoperative
attacha placardon the instrumentpanel
- ALTITUDE
LIMITED
TO FL 3OO
placardnearairspeedindicator
lf the CommandAirspeedcursoris inoperative,
- COMMAND
AIRSPEED
CURSORINOP
(O)
OPERATIONS
Usealternateprocedures
to assureflightcrewawarenessof operationalreferencespeeds.
This mayincludeuseof takeoff cardsor placards,
34-13-2 Mach/Airsoeed
WarningSystems
(VisualandAural)
B
2
1 (Ol May be inoperativeprovidedan autopilotwith an
holdis ooerative.
altitude
NOTE: One altitudealertingsystemis requiredto be
ooerativefor RvSM operations,
PLACARD
As appropriate
34-13-6 StandbyAltimeter
Vibrator
providedVMC existat the departure
Maybe inoperative
and arrivalairports.
PLACARD
As appropriate
34-'l3-7 TotelAir
Temperature
(TAT)
Indication
providedone othertemperature
(O) May be inoperative
(RATor SAT)is available.
indication
PLACARD
NearEICASdisplay- TATINOP
(continued)
Page34-3
REV17 MAR10/2007
.tt'VIEV
Hungarian Airlines4
.az7EtivzF
.787
LIST
EQUIPMENT
MINIMUM
34. NAVIGATION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS
IOI
See SAT/TATconversionchart (SAT is availableon FMC ProgressPage 212)BoeingOperations
Manualperformance
section4.1 page25 or the tablebelowshoesto convertSATto TAT.
SAT
40
35
25
20
15
10
c
0
-5
-15
-20
-25
-JU
-35
40
TAT
M.50 M.60 M.68 M.70 M.72 M.74 M,76 M.78 M.80 M.82 M.84 M.86
0z
70
56
69
70
51
57
64
65
66
68
oo
oc
6T
OJ
45
52
58
59
61
68
OJ
66
64
6'1
40
52
54
56
57
59
6e
60
c
l
53
55
41
47
48
CU
51
f,J
ac
57
51
49
JO
42
43
44
46
48
30
49
51
44
46
J
O
3
I
40
24
31
38
43
45
40
4
1
I
J
35
37
38
19
31
JO
40
38
33
34
zo
31
13
20
25
28
34
29
30
32
zo
27
14
8
20
21
o
to
28
ZJ
lc
20
3
14
15
17
19
-2
IJ
19
21
13
14
16
10
11
3
I
15
10
12
13
o
4
7
't1
-7
-c
o
8
J
5
u
1
n
-2
-18
.U
o
4
1
2
4
-2
-9
-tt
-25
-17
-13
-10
0
4
-Y
-11
-13
-28
-18
-16
-15
€
Page 344
REV 17 MAR 10/2007
t%lEV
Hungarian Airlines
fi
.EZEtttyaF
.7A.7
LIST
MINIMUM
EQUIPMENT
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
i.a.w.JAROPS 1.660,leaflet26.
34-16-'l AltitudeAlerting
System
B
1
0
(O) Except for RVSM operation,may be inoperative
Drovided:
a) Autopilotwithaltitudeholdoperatesnormally,
1
1
One altitudealertingsystemis requiredto be operative
for RVSMoperations.
OPERATIONS
IOI
The PilotNonFlying(PNF)should
The PilotFlying(PF)shouldfocusattention
on flyingthe airplane.
focusattentionon airspeed,verticalspeed,altitude,altitudedeviation,pitchattitudeand thrust.lf any
calloutdeviation.
the PNFshouldimmediately
fromnormalindication
is detected,
significant
deviation
34-21-1 InertialReference
Systems
1) IRU
a) Without
Hydraulic
Motor
(HMG)
Generator
Installed
b)with HMG
Installed
C
3
2
provided:
(M) Centerof Leftmaybe inoperative
minimums
do notrequireits use,and
a) Approach
centeris selectedand isolation
b) lf left is inoperative,
day.
flight
is verifiedoneeach
C
3
2
(Hl Right may be inoperativefor day VMC flight
providedcenteris selectedand isolationis verifledonce
eachflightday.
C
3
2
provided:
(MXO)Leftor rightmaybe inoperative
itsuse,
not
require
do
minimums
a) Approach
b) Centeris selectedand isolationis verifiedone each
flightday,
c) First officer'sIRS instrumentsourceselectswitch
operatesnormally,and
d) For RNPoperations,Left and Centermustoperate
(RNP-10,
PRNAV,BRNAV,and MNPS)in
normally
NAVmode.
(Refer to AFM Section 3.1 for demonstratedRNP
caPability)
2
for dayVMCflight.
Centermaybe inoperative
\
-
J
(continued)
Page34-5
REV17 MAR10/2007
I*IHiIEV
Hungarian Airlinesfi
aez
Z?EtttUZF
LIST
EQUIPMENT
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARK OR/AND EXCEPTIONS
2) IRSModeSelector C
Panel- Display
and Keyboard
Functions
-
0
For ETOPSoperationsmay be inoperative,provided
bothFMCSCDU'Soperatenormally.
C
-
0
For non-ETOPS operations, may be inoperative
providedone FMCSCDUoperatesnormally.
NOTE'1:lf the left IRU is inoperative,
Windshear
and AlertingSystemwill be inoperative.
Guidance
See MEL 34'46-2 dispatchrequirementsfor an inoperativeWindshearGuidenceand
AlertingSystem.
NOTE2: IRSunitsare interchangeable.
NOTE3:Followinga flightwithone EICAScomputerinoperative
or onefuelflowindicationinoperative,
high
may
determine
flight
completion
speed
taxi.Thiswillcausethe IRU
theFMC
during
residualgroundspeedto set at 21 knotsor greater.The FaultlsolationManualuses21
Manual
knotsas the thresholdto identitya faultylR. Testingthe IRUperthe Maintenance
maypreclude
replacement.
PLACARD
AssociatedIRS ModeSelector- INOP
OPERATIONS
{O)
1. ComplywithMMELremarks.
maybe
2. lf the airplaneis operatingon stendbybafterypower,thenthe Captain'sRDMIinformation
lost.lf the centerIRUis operatingnormally,the captain'sRDMIcan be restoredby switchingthe
firstofficer'sIRS instrument
sourceselectswitchto the alternate(ALTN)position.
selectthe centerCMDswitchto engagethe
3. Whendispatching
witha rightor left IRUinoperative,
autopilot.
34-22-3 RadioDistance
C
Indicators
Magnetic
(RDMr)
v
2
z
1
Rightmaybe inoperative.
Left may be inoperativeprovidedflight is restrictedto
dayVMC.
Right and left may be inoperativeprovidedstandby
po\,\,er
systempo\\,ersthe Captain'sinstrumentbus.
PLACARD
As appropriate
Page34-6
REV 17 MAR 1Oi2OO7
I!'t/lIEV
Hungarian Airlines,fi
,azEtlvaF
.7A?
LIST
EQUIPMENT
MINIMUM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
providedapproachminimumsdo not
Maybe inoperative
requiretheiruse.
34-224 FlightDirector
Systems
providedapproachminimumsdo not
Maybe inoperative
requiretheiruse.
1) Displays
guidance
maybe unavailable.
NOTE:Windshear
(M) Except for ETOPS, one may be inoperative
providedsymbol generatorisolationis verified once
eachflightday.
C
34-22-5 ElectronicFlight
lnstrument
(EFIS)
Systems
SymbolGenerators
(M) For ETOPS,L or R may be inoperativeprovided
symbolgeneratorisolationis verifiedonce each flight
day.
f-
NOTE:Symbolgenerators
areinterchangeable.
EICASSTATUSMESSAGES
COMPARATOR
BITE
PLACARD
- EFI NORMINOP
placardcaptain'sEFIswitch
lf leftEFISSymbolGeneratoris inoperative,
placardcaptain'sandfirstofficer'sEFIswitches EFIALTNINOP
lf centerEFISSG is inoperative,
placerdfirstotficer'sEFIswitch - EFINORMINOP
lf rightEFISSymbolGeneratoris inoperative,
34-22-6 EFISControlPanel
1) MAPSwitches
C
(NavAid
/ARPT/RTEDATA
^/VPTAA/XR/TERR)
-
One switch for each function may be inoperative
providedprocedures
do not requiretheiruse.
2) Decision
Height
Indication
2
provided:
Maybe inoperative
displayon bothEADIdisplays
a) DHnumerical
and
operatenormally,
b) BothDH selectorsoperatenormally.
C
(continued)
Page34-7
REV 17 MAR 1Oi2OO7
:*MIEV
Hungarian Airlinesfi
.ezEttuaF
.78-
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
c
2
providedapproachprocedures
do
Maybe inoperative
not reouireits use.
a) MAPPosition
B
2
provided:
(O) Maybe inoperative
normally,and
FMCS
operate
a) Both
and used.
are established
b) Alternateprocedures
b) PLANposition
B
2
provided:
(O) Maybe inoperative
al BothFMCSoperatenormally,and
and used.
are established
b) Alternateprocedures
HSIModeSelector
PLACCARD:
As appropriate
(O)
oPERATTONS
1. Useappropriate
HSImodeandFMCCDUpageto displaydesiredflightinformation.
34-22-7 EFISMach/Airspeed
lndications
1) Machindications C
2) Airspeed
lndications
2
1
u
May be inoperativeorovided Mach indicatorsare
normallyat the respectivepilot's
installed
andoperating
station.
v
z
C
2
0
provided:
Maybe inoperative
remainsat or belowFL 300,and
a) Theairplane
b) A Dlacardwith this limitationis affixed to the
panel.
instrument
C
2
0
May be inoperativeprovidedairspeedindicatorsare
installedand operatingat the respectivepilot'sstation.
indicators(rounddials).Some767airplaneshave
NOTE: Some767airplaneshaveMACH/Airspeed
and
havebothindicators
(EFISspeedtape).Some767airplanes
MACH/Airspeed
indications
only.Seeitem34-13-1for reliefof
indications.
This reliefis f,orthe speedtapeindications
(rounddial)MACH/Akspeed
indicators.
PLACARD
On the instrumentpanelas appropriate- ALTITUDELIMITEDTO FL 300
Page34-8
REV17 MAR10/2007
ttMlEW Hungarian Airlinesfi
.787
^g2rE-/YAF
LIST
EQUIPMENT
MINIMUM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-22-8 PitchLimit
lndicators
c
2
(O) May be inoperativeprovided three INS (lRS)
operatenormally.
34-23-l MagneticCompass B
(Standby)
B
1
provided:
(O) Maybe inoperative
a) Two INS(lRS)Systemsare operative,and
b) Airplane is operated with dual independent
navigation capability and under positive radar
controlby ATCon enrouteportionof flight.
for flightsthat are entirelywithin
(O) May be inoperative
providedat leasttwo INS
areasof magneticunreliability
(lRS) systemsare operative,and used in conjunction
techniques.
withapprovednavigation
(O)
OPERATION
Flightcrewmustinsurethetplennedroutescomplywithlimitations.
34-24-1 StandbyAftitude/
ILSlndicator
1) AttitudeDisplay
2) Approach Mode
i,a.w.
JAROPS1.650and1.652
May be inoperativefor day VMC only providedboth
attitudeindicatorsareoperative.
B
C
1
PLACCARD:
As appropriate
Page34-9
REV17 MAR10/2007
ttMlEW Hungarian Airlines4
787
.a27Et/v2F
EOUIPMENT
LIST
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-24-2 lnte$ated Standby
FlightDisplay
(ISFD)System
1)AttitudeDisplay B
provided:
Maybe inoperative
are
a) Operations conductedin DayVMConly,and
b) Operationr are not conducted into known
conditions.
forecastover-the-too
2) ApproachMode C
0
3) HeadingDisplay C
4) MetricAltimeter C
Display
0
(O) May be inoperativeprovidedalternateprocedures
areestablished
andused.
D
0
May be inoperativeprovidedoperationsdo not require
its use.
0
May be inoperativeexcept for ETOPS operations
beyond120minutes.
5) Dedicated
Battery
Charger
System
C
I
PLACCARD:
As appropriate
OPERATIONS
{OI
guidance
regulatory
1. Inoperative
attitude
display:
seeFAR121.305
andJAR-OPS1.650/1.652
material..
conversion
2. Inoperative
metricaltimeterdisplay:flightcrewsshouldbe providedwithconvenient
tablesfor correctingaltimeterreadingin feetto meters.
Page34-10
REV17 MAR10/2007
rt'AIEW
aarEttvaF
Hungarian Airlinesfi
.78.7
EQUIPMENT
LIST
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-25-1 Instrument
Comparator
Unit
(if installed)
D
1
0
B
3
2
The left or right may be inoperativeprovidedthe
lllA LandingMinima.
reclassified
to Category
airplane
1
The left and right may be inoperativeunlessapproach
minimums
do notrequiretheiruse.
EICASSTATUSMESSAGE
BITE
COMPARATOR
34-31-1 ILSSvstems
PLACARD
As appropriate
OPERATIONS
NOTE
at their
ILSSystemrequirements
depending
on weatherminimums
aredetermined
byoperators
airport.
SeeApproved
AirplaneFlightManual,FAR121.347through121.349,or JAR-OPS1.865
regulations.
34-32-1 MarkerBeacon
System
B
1
0
providedapproachminimumsdo not
Maybe inoperative
reouireits use.
PLACARD
As appropriate
OPERATIONSNOTE
Airlines must determinemarker beacon requirementsdependingon their route system. See FAR
121.349
or JAR-OPS
1.865regulation.
34-33-1 RadioAltimeters
(RA)
1) SingleSource
Datalink
to GPWS
A
1
0
provided:
(O) Maybe inoperative
do not
a) Approachminimumsor operatingprocedures
reouireits use.and
b) Repairsare madewithintwoflightdays-
RA C
b) Center/Right
2
0
providedapproachminimumsor
(O) Maybe inoperative
do not requireits use.
operatingprocedures
e)LeftRA
Page34-11
REV17 MAR10/2007
Hungarian Airlines
tt'AIEV
B
.78^?27E2/tvzF
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2) Multi-Source C
Datalink
to GPWS
3
provided:
(O) Maybe inoperative
withaltitude
data,and
a) GPWSis supplied
procedures
or operating
b) Approach
minimums
do not requireits use.
provided:
(O) Maybe inoperative
minimums
or operatingprocedures
a) Approach
do notreouireitsuse.and
b) Repairsare madewithintwoflightdays.
EICASMESSAGES
GNDPROXBITE
GNDPROXSYS
PLACCARD
As appropriate
MAINTENANCE
NOTE
lf left radioaltimeteris inoperative,
operationof the testswitchfor the landingconfiguration
modesof the landing
warningwill showthe functionto be faulty.However,flap-basedmonrtoring
configuration
remainoperational
and can be verified,if desired,as follows:
A. OpenLDGGEARPOSSYS1 and 2 circuitbreakers.
B.Withlandingflaps,allwarningindications
willbe activated.
willilluminate
EICASmessage
C. Withflapsup,theconfiguraiion
warninglightandassociated
withat leastone throttleat idle.
D. CloseLDGGEARPOSSYS1 and2 circuitbreakers.
2. Certainfailuresof the radioaltimetersystemwillcauseone or moreof the followingmessagesto
bedisplayed:
A. AUTOPILOT
B, R/ADISAGREE
C. GNDPROXBITE(leftR/Aonly)
3. lf the GroundProximityWarningSystemwithmulti-source
datalinkis not receivingradioaltitude
information
fromanyradioaltimeters,
the GNDPROXSYSstatusmessagewill be annunciated
1,
(O)
OPERATIONS
1.ObserveMELexceptions.
2. lf the left radioaltimeteris failed,the flightcrewshouldexpectto seethe followingflightdeck
effects:
A. lf the landinggearis notdownand locked,the flapsare retracted,and eitherenginethrottleis
Page34-12
REV17 MAR10/2007
tVUaEV Hungarian Airlines
fi
.78.AzEt'YaF
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
at idletheCONFIGwarninglightwillilluminate
andtheGEARNOTDOWNEICASwarning
message
willannunciate;
however,
thesirenwillnotsoundandthemasterwarninglightswillnot
illuminate.
B. lf the landinggearis notdownand locked,the flapsare notfullyretractedandeitherengine
Thatis,theCONFIGwarning
throttleis at idle,thegearnotdownwarningwilloperatenormally.
message
willannunciate,
thesiren
warning
lightwillilluminate,
theGEARNOTDOWNEICAS
willsoundandthe masterwarninglightswillilluminate.
C. lf the landinggearis notdownand locked,the flapsare set at 25 or 30, andthe throftlesareat
TheCONFIGwarninglightwill
anyposition,
thegearnotdownwarningwilloperatenormally.
thesirenwillsound
willannunciate,
illumiate,
theGEARNOTDOWNEICASwarningmessage
andthe masterwarninglightswillilluminate3. TCASrequiresonlyone radioaltimeterfor operation.lf one radioaltimeterfails,the flightcrewwill
see no effecton TCAS.
3443-1 WeatherRadar
System
C
2
0
providedthe
Oneor moresystem(s)maybe inoperative
weatherreoortsor forecastsavailableto the
cloudsor
commander
indicate
thatcumulo-nimbus
which
weetherconditions,
hazardous
otherpotentially
couldbe detectedby the system(s)whenin working
on the intended
order,are unlikelyto be encountered
routeor anyplanneddiversiontherefrom.
D
2
1
providedone weatherradarsystem
May be inoperative
operatesnormally.
NOTE
Required
for ETOPSbeyond120minutes
1)Autotilt
c
/Multiscan
Function
l
providedmanualtilt function
Maybe inoperative
operatesnormally.
2) WXRON Light
2
providedalternate
(O) Maybe inoperative
procedures
and used.
are established
D
(continued)
Page34-13
REV17 MAR10/2007
ttAilEV
.AArtttrYZF
Hungarian Airlines
fi
.78?
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR'ANDEXCEPTIONS
3) Predictive
WindshearAlert
provided:
(O) Maybe inoperative
and used,
are established
a) Alternateprocedures
and
System
b) WndshearWarningandGuidance
normally,
operates
provided:
(O) Maybe inoperative
and used,
areestablished
a) Alternateprocedures
and
b) Takeoffsand landingsare not conductedin
knownor forecastwindshearconditions.
EICASSTATUSMESSAGES
WINDSHEAR
PRED
WXR SYS
PLACCARD
As appropriate
(O)
OPERATIONS
(VFR/IFR)
and
1. Aidinesmustdetermine
radarrequirements
depending
on theirtypeof operation
regulations.
reportedweather.See FAR12'1.357
or otherappropriate
Windsheer,the Operatormustdevelopand
2. lf normalprocedures
are basedon usingPredictive
altitudeand
usealternateprocedures
to increaseflightcrewawarenessof airplaneconfiguration,
path.
flight
(reactive
windshear,
autopilot,
Thismayincludeflightcrewuseof all airplane
systemsavailable
Altitudes
andaltitude
callouts
Enroute
autoland,
lLS,FMCS)andflightcrewreviewof Minimum
for Windshear).
(referto OperationsManualSupplementary
NormalProcedures
3. WhenWXRON lightsare inoperative
or not installed,determinestatusof theweatherradarby
GAIN,MODE,andTILTon the
viewingthe EHSIdisplay.
Someweatherradarsannunciate
are notavailable,WXR statusmay
displaywhenthe weatherradaris ON. lf theseannunciations
lf no returnis indicated
be determinedby observingthe EHSIfor rastorand returnindications.
andthereis doubtaboutthe statusof the radar,the antennamaybe tilteddownwardto determine
if groundreturnis indic€ted
on theEHSI.
Modeof theGround
of theWindshear
4. Thewindshear
warningandguidance
systemconsists
ProximityWarningSystem(item3446-1),Go-AroundSwitches(item22-30-2)and FlightDirector
System(item34-22-4).Faultsin anyof thesesystemsmeyetfectthe operationof the windshear
warningandguidance
system.
Page34-14
REV17 MAR10/2007
;+AIEV
Hungarian Airlines
fi
.7e-
.aauEtlvaF
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
i.a.w.JAROPS1.665,leaflet26:
providedrepairsor replacements
Maybe inoperative
are carriedoutwithin6 furtherflightsor 25 flyinghours
or 2 calendardays,whicheveroccursfirst.
34"16-1 GroundProximity
WarningSystem
NOTE:
lf anyof theTenainAvoidanceModes1-4or the Test
thenthe GPWSis considered
Modeare inoperative,
inoperative.
1) Glideslope
Deviation(Mode5)
Maybe inoperative
or
c
2
2) Advisory
Callouts c
(Mode6)
1
0
for dayVMConly
Maybe inoperative
0 (O) May be inoperativeprovidedalternateprocedures
andused.
areestablished
NOTE:
approach
minimums.
CheckFIightManuallimitations
3) WindshearAlert
Mode
(Reactive)
(Mode7)
provided:
(O) Maybe inoperative
and used,and
are established
a) Alternateprocedures
WindshearDetectionandAvoidance
b) Predictive
Systemoperatesnormally.
provided:
(O) Maybe inoperative
and used,and
are established
a) Alternateprocedures
b) Takeoffsand landingsare notconductedin known
or forecastwindshearconditions..
4) TerrainAwareness
andWarning
System(TAWS)
(Enhanced
GPWS)
provided:
Maybe inoperative
a) The GPWSfunctionsare operative,and
arecarriedoutwithin10
b) Repairsand replacements
calendar
days.
EICASSTATUSMESSAGE
GNDPROXBITE
GNDPROXSYS
WINDSHEAR
REAC
(continued)
Page34-15
REV 17 MAR 1Oi2OO7
;+EIEV Hungarian Airlines,fi
.7Ez
.?ZEtjYE
LIST
MINIMUMEQUIPMENT
34, NAVIGATION
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACCARD
As appropriate
OPERATIONS
{OI
a)
Inoperative
TerrainAvoidanceMode1-4
The flightcrew makessharpbriefingfor everypart of flightespeciallywhen relationof terrainis
factor.They must knowthe placesof the highestobstaclesduringboth departureand arrival.
and belowMSA Do
Systematically
checkthe aircraftaltitudeby radioaltimeterjust approaching
not hesitateif necessaryfor makean escapemaneuveraccordingto 8767SOP.
b)
Inoperative
GlideslopeDeviationMode
+1 dotfromGS/LOCduringapproach,
ThePNFcallanyexcessive
deviation
Inoperative
AdvisoryCallouts
PNFwill announcerequiredRadioAltimetercalloutin additionto otherspecifiedcalls.Thesecalls
out havedeterminedin 8767 SOP.
0)
lnoDerative
Windshear
under34-46-2termination.
SeeOoerationProcedures
Page34-'16
REV17 MAR10/2007
*MIEV
Hungarian AirlinesA
,zaEttve.7E7
EOUIPMENT
LIST
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34106-2Windshear
Guidance
and
AlertingSystem
Deleted,FAAMMELRev25
under3446-1(5)
Reliefalreadyavailable
(OI
OPERATIONS
lf windshearGuidanceand AlertingSysteminoperative,crews shouldbe preparedto executethe
recommendedrecoveryprocedureimmediatelyif deviationfrom targetconditionin excessof the
followingoccur:
- Takeoff
1) 115knotsindiceted
airspeed,
2) 1500FPMverticalspeed,
3) 15opitchattitude,
- Approach
1) tl dotglideslope
displacement,
2) Unusualthroftlepositionfor significantperiodof time.
on flyingthe airplane.The PilotNon Flying(PNF)
1, The PilotFlying(PF)shouldfocusaftention
shouldfocusattentionon airspeed,verticelspeed,altitude,pitchattitude,glidepathdeviationand
thrust. lf any significantdeviationfrom normal indicationare detected,the PNF should
immediately
cellout deviation.
2. The recoveryprocedureas follows:
on ADl.Smoothly
fullthrust.PNFcheckFMAannunciation
a. PF pushG/Aswitchand advance
doesnot provide15"
rollwinglevel.lf autopilot
adjustpitchaftitude15' and simultaneously
attitudeor groundcontactis factortake over the airpleneand fly by manually.PNF observe
the recoverymaneuverand callfor anydeviation.
to windshearfeature
WARNING:lf WindshearGuidanceand AlertingSysteminoperative
mode does not work that is why not use F/D pitch indjcation,only the roll mode works
ProPerlY.
b. lf groundfactor is effect increasepitch as desired.Stick shakermust be respectedat all
times.lf stickshakeris activeted,pitchattitudeshouldbe reducedjust enoughto silencethe
stickshaker.
Page3417
REV17 MAR10/2007
:tMlEV
Hungarian Airlines
fi
.aarEtjvzP
.78.7
LIST
EQUIPMENT
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-51-l VORNavigation C
Systems
2
i,a.w.JAROPS1.865leaflet26.
1) Aeroplane
C
Equipped
withOne
OperativeFMS
2
provided:
(O)Any in excessof one maybe inoperative
(a) BothADF(whererequired)and DMEare
and
ooerative,
(b) The aeroplaneis equippedwithalternative
for the routebeingflown,
equipmentauthorized,
bythe Authority.
NOTE:Operatorsshouldconsiderif the in-flightfailure
withthe
of anyFMSsensorallowssafe navigation
sensorsand equipment.
remaining
serviceable
Aeroplane
C
EquippedwithTwo
OperativeFMS
-
wherenavigational
(O) Oneor moremaybe inoperative
can be assuredand the approachprocedures
capability
are not requiredto be baseduponVORsignals
(seeNOTEabove).
(RNP-10& PRNAV)oneVOR
NOTE For BRNAVor RNPoperations
NAV not powered by a StandbyBus may be inoperative
provided1 GPS is operative(if installed)(Referto AFM Section
RNPcapability).
3,1for demonstrated
-
2
2
(RNP-10)and BRNAVin
Required
for RNPoperations
not
installed.
or
caseGPSnotooerative
For RNP-10the duretionof the non radio updating
sectormustnotexceed6,2 hours.
then the
NOTE:lf a powersupplyanomalycausesthe L VOR navigationsystemto be inoperative,
Marker
See MEL 34-32-1for an inoperative
markerbeaconsystemmay also be inoperative.
BeaconSystem.
PLACCARD
As appropriate
Page34-18
REV 17 MAR 1Ol2007
:IMIEW
Hungarian Airlines4
azEtjvaF
.7A.-
LIST
MINIMUM
EOUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-53-1 ATCTransponder
AutomaticAltitude
Reporting
Function
i.a.w.JAROPS1.866.leaflet26.
D
Any in excessof thoserequiredfor the intendedroute,
provided:
maybe inoperative
a. En-routeoperationsdo not requireits use,and
b. Prior to flight, approvalis obtainedfrom ATC
facilitieshavingjurisdictionoverthe plannedroute
of flight.
Requiredto be operativefor RVSMoperations.
providedpermissionis
Oneor moremaybe inoperative
ServiceProvide(s)
obtainedfromtheAir Navigation
whenreouiredfor the intendedroute.
NOTE1:
An ooerativeATC ModeS transponder
is definedas a transponderwhichcan provideat least
capability.
Surveillance
Elementary
Altitudereporting,providedby an ATC
NOTE2:
is requiredfor ACASll operation.
ModeS Transponder,
tor
flight with ACAS/TCAS ll
Refer to 34-61-2
inooerative.
Altitude reporting, provided by ATC
EIEI:
Mode S Transponder,is requiredfor flight into RVSM
arrspace.
Referto MELJ34-01for flightintoRVSMairspace.
Enhanced
Surveillance
Capability
(DAP's),
AircraftParameters
Oneor moreDownlinked
maybe
Surveillance,
whichprovideEnhanced
inooerative
whennot requiredfor the intendedroute.
(DAP'S),
AircraftParameters
Oneor moreDownlinked
provide
maybe
EnhancedSurveillance,
which
whenrequiredfor the intendedroute.
inoperative
PLACCARD
As appropriate
Page34-19
REV17 MAR10/2007
.*MIEV
Hungarian Airlines
fi
aarEttuat
.7a7
LIST
MINIMUM
EQUIPMENT
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-55-1 Distance
Measuring
Equipment
Systems(DME)
i.a.w.JAROPS1.865,leaflet26.
provided:
Oneor moremaybe inoperative
(a) Alternative
equipment
approvednavigational
and
is oDerative.
(b) The DMEis not requiredfor the plannedroutes
to be flown.
if thein-flight
failure
shouldconsider
NOTE:Operator
safe
navigation
with
allows
of any FMSsensor
sensorsand
the remainingserviceable
equipment.
(RNP-10),PRNAVand
Requiredfor RNP operations
BRNAVin caseGPSnotoperativeor not installed.
of thenonradioupdating
ForRNP-10theduration
sectormustnotexceed6,2 hours
PLACCARD
As appropriate
34-57-1 RadioCompass
(ADF)Systems
PLACCARD
As appropriate
Page34-20
REV 17 MAR 1Oi2OO7
Hungarian Airlinesfi
tlElEV
.78?
,AarEttYZF
LIST
EQUIPMENT
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
34-60-1 GlobalPositioning C
System(GPS)
2
providedalternate
(O)Maybe inoperative
procedures
and used.
are established
D
2
providedprocedures
do not
Maybe inoperative
requireits use.
(RNP-10)
notrequired
NOTE:ForRNPoperations
orovided:
a. TwoVORandtwo DMEareoperative,and
b. The durationof the non radioupdatingsector
doesnotexceed6.2 hours.
Twoare requiredfor RNPoperations(RNP-10&
PRNAV)in caseVORand DMEcoveragefor the
selectedrouteis not availablefor morethen6,2 hours.
NOTE: Referto AFM Section3.1for demonstrated
RNPcapability.
c
2
(RNP-10
& PRNAV)
for RNPoperations
Oneis required
in caseVOR and DMEcoveragefor the selectedroute
is available.
NOTE: Referto AFMSection3.1for demonstrated
RNPcapability.
PLACCARD
As appropriate
34-61-1 FlightManagement
ComputerSystems
(FMCS)
1) FMC
(including
CDU/MCDU
and
HMCDU)
C
2
(O) Except for ETOPS operations,one may be
inoperativeprovideden-routeoperationsdo not require
its use.
NOTE: For BRNAV& PRNAVoperationsone FMC is
reouired.
(continued)
Page34-21
REV 17 MAR 1OI2OO7
Hungarian Airlines
ttElEV
4
.78?
.?2rEt/YZF
EQUIPMENT
LIST
MINIMUM
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(M)(O) Except for ETOPS operations, may be
provided:
inooerative
a) Both Fuel Quantity Indicating System (FQIS)
processorchannelsoperatenormally,
b) All flaghtdeck fuel quantity indicationsoperate
normally,
and
c) BRNAVoperationsare notallowed.
one
Navigation
operations,
(O) For ETOPS/Long-Range
may be inoperativeprovidedotherappmvedmeansof
areavailable.
navigation
NOTE:An associatedHMCDUor MCDU,if operative,
requirements.
maybe usedto meetnavigation
(RNP-10)may be
(o) For MNPSand RNPoperations
inoperativeprovided two HMCDU or MCDU are
operative.
NOTE
Refer to AFM Section 3.1 for demonstratedRNP
capability
(O) Maybe out of currencyprovided:
2) Navigation
Databases
3) FMCAnnunciator C
Light
a) Current aeronauticalcharts are used to verify
navigation
fixespriorto dispatch,
b) Proceduresare establishedand used to verify
statusand suitabilityof navigationfacilitiesusedto
definerouteof flight,and
c) Approachnavigationradiosare menuallytunedand
identified.
d) P-RNAVoperationsare notallowed
1
0
providedthe CDU MSG light
(M) May be inoperative
'FMC MESSAGE"
are
and EICASadvisorymessage
normally.
verifiedto operate
NOTE: For those airplaneswith the advancedstall warning computerand speed tape display,
dispatchwith a "WARN ELEX" status messageis allowedprovidedthe P51 WEU BITE
moduledisplaysonly faultcode D7 (FMC Invalid).This shouldbe checkedpriorto each
departure.
Page3/'-?'2
REV17 MAR10/2007
Hungarian Airlines
ttMlEV
4
.78?
,?zTEt'yzF
LIST
EOUIPMENT
MINIMUM
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
EICASSTATUSMESSAGES
WARNELEX
PLACCARD
As appropriate
OPER.ATIONS
IOI
1. Foralloperations
withoneFMCinoperative:
moves.
A. IRSalignment
muste completed
beforeairplane
NOTE: Some aircraftare configuredwith IRS'swithoutkeypads.When this type of airplaneis
dispatchedwithone FMCinoperative
and the secondFMCfails,therewill no longerbe a
meansto alignthe IRSoncethe electricalpoweris removedfromthe airplaneor the IRS
modeselectorswitchis movedfromthe NAVDosition.
B. Useof LNAVandVNAVwithflightdirector:
1)Airplanes
withHMCDU/MCDU:
FMC,selectthe oppositeFMCor the on-sideCDUwiththe
a) On the sidewiththe inoperative
NAVsourceselectswitch.
b) LEFTFMCINOPEMTIVE- Whenoperatingin flightdirectormodewithbothF/Dswitches
ON, LNAVandVNAVwill engageif the Captein'sNAVsourceswitchis selectedto R FMC
or L CDUposition.Otherwise,LNAVandVNAVwillengageif the rightautopilotis engaged
or onlythe right F/D is ON. Turningoff the lefr F/D switchwouldallowuse of LNAVand
VNAV,butonlythe rightflightdirectorwouldoperate.
Procedure:
After liftoff(withF/D in TO mode),use HDGSELand FL CH modesas desired
untilCaptain'sNAVselectoris movedto an alternatesource,or rightautopilotis engaged.
ThenuseLNAVandVNAVas desired.
- Whenoperatingin flightdirectormodewithbothF/Dswitches
c) RIGHTFMCINOPERTIVE
ON, LNAVandVNAVwill engage.lf the FirstOfficer'sNAVsourceswitchis selectedto the
L FMC or R CDU position,LNAVand VNAVwill engagewith any autopilotengaged.
OtheMise,LNAVand VNAVwill engageif the left or centeris engagedor the rightF/D is
oN.
(continued)
Page34-23
REV17 MAR10/2007
:t'lAlEV
Hungarian Airlinesfi
.azrEttvzt
.78.7
LIST
EQUIPMENT
MINIMUM
34, NAVIGATION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Procedure:
After liftoff(withF/D in TO mode)use HDGSELand FL CH modesas desired
untilFirstOfficer'sNAVselectoris movedto an alternatesource,or leftor centerautopilot
ThenuseLNAVandVNAVas desired.
is engaged.
C. With a singleoperationalFMC,monitoringof VOR rawdata is requiredno laterthenthe final
displayedon one EHSIin theVOR
approachfix. Useof theVORcourseand DMEinformation
modesatisfiesthis requirement.
FordispatchwithbothFMC'sinoperative,
enterairplanepresentpositionusingIRSModeSelector
Panel (reference Operations Manual, SupplementaryProcedures- Flight Management,
Navigation).
Forlong-rangenavigation
operations
withone FMCinoperative:
mustbe installed.
NOTE1: FMCNAVSourceSelectSwitchwithCDU-LandCDU-Rpositions
modeandtwo HMCDU'S
withtwo IRSsystemsin navigation
NOTE2: One FMC,in conjunction
AirplaneFlightManual,
for dispatch(reference
or MCDU'swill meetthe requirements
Section3, FMCS).
the followingas appropriate:
A. In additionto step 1 above,priorto kkeotf accomplish
1)
Foran inoperative
leftFMC:
a)
Selectthe FMC-Rpositionwiththe Captain'sFMCNAVSourceSelectSwitchto
loaddatafromthe rightFMCintothe leftCDU.
NOTE:The FMC switchshouldremainin this positionfor at leastone minute
after flight planningis completedor after any flight plan modificationspriorto
takeotf.
2)
b)
Aftera minimumof one minute,selectthe CDU-Lpositionwith the Captain's
FMCNAVSourceSelectswitch.
c)
routedisplay
Observethat Captein'sHSI Map displaychangesto a simplified
"CDU-L"shouldbe displayedon
withoutnormalnavigationdatabasesymbology.
system
Navigation
of theAlternate
the HSI/ND,
Thisconfirms
availability
d)
Priorto takeoff,selectthe FMC-Rpositionwith the Captain'sFMC NAV Source
selectSwitch.
Foran inoperative
rightFMC:
a)
Selectthe FMC-Lpositionwiththe FirstOfficer'sFMCNAVSourceSelectSwitch
to loaddatafromthe leftFMCintothe rightCDU
(continued)
Page34-24
REV17 MAR10/2007
t+UaEV
,azEtlyE
Hungarian Airlines
fi
.78.7
EQUIPMENT
MINIMUM
LIST
34. NAVIGATION
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE:The FMCswitchshouldremainin this positionfor at leastone minute
after flight plenningis completedor after any flight plan modifi€tions prior to
takeoff.
b)
Aftera minimumof one minute,selectthe CDU-Rpositionwiththe FirstOfficer's
FMCNAVSourceSelectswitch.
c)
Observethat FirstOfficer'sHSI Mapdisplaychangesto a simplifiedroutedisplay
'CDU-R'shouldbe displayedon
withoutnormalnavigationdatabasesymbology.
system.
of the AlternateNavigation
the HSI/ND.Thisconfirmsavailability
d)
Prior to takeoff,selectthe FMC-L positionwith the First Officefs FMC NAV
SourceSelectSwitch.
out of currency,observeMELrestrictions.
FordispatchwithnavigationDatabases
4.
A.
navigation
database.
CheckNOTAMSand chartsagainstthe out-of-date
B.
Manuallyinputroutestructure,if needed-
34-61-2 TrafficAlert
Collision
Avoidance
System
(ACAS/TCAS
il)
A
i.a.w.JAROPS1.668,leaflet26.
1
0
provided:
(MXO)Maybe inoperative
and secured,and
a) Systemis deactivated
b) lf the airplaneis intendedto be flownin airspacein
whichACASoperationis requiredit may not fly for
more than 10 calendardays with the equipment
completelyinoPerative.
may imposea more
NOTE: Localairspacerequirement
interval.
restrictiverectification
1) Combined
Traffic C
Alert(TA)
andResolution
Advisory(RA)
DualDisplay
2
pilotside
Maybe inoperative
on the non-flying
orovided:
are
andaudiofunctions
a) TA andRAelements
pilot
side,
and
on
the
flying
operative
arevisibleto thenonb) TA andRA displayindications
flyingpilot.
(continued)
Page34-25
REV17 MAR10/2007
:?MIEV
Hungarian Airlines
A
.ezEttutt
.787
EQUIPMENT
LIST
MINIMUM
34. NAVIGATION
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O) One maybe inoperative
on the nonflyingpilotside
2) (RA)Resolution
AdvisoryDisplay
System(s)
provided:
(O) Maybe inoperative
(TA)
displayelementsandvoice
a) TrafficAlert
commandaudiofunctionsare operative,and
b) TA onlymodeis selectedbythe crew.
3) (TA)TrafficAlert
C
DisplaySystem(s)
providedall
(O)Oneor moremaybe inoperative
installedRA displayandaudiofunctionsare operative.
2
PLACCARD
As appropriate
(O)
OPERATIONS
Monitorthe operativeindications
and advisoriesand respondas appropriate.
i.a.w.JAROPS1.872,leaflet26.
ReducedVertical
SeparationMinima
(RVSM)
1 ) Altimeters
3)
4)
5)
o.l
AltitudeAlerting
System
Autopilot
SSRTransponder
PitotHeater
StaticPortHeater
I
I
NOTE:An automaticaltitudecontrolsystemis required
,l
NOTE:Fuselagedamageto the areadefinedby the
relevantStructuralRepairManualmustbe assessedto
for operation
withthe requirements
ensurecompliance
in RVSMairsDece.
Page34-26
REV17 MAR10/2007
."+UaEV Hungarian Airlines
fi
.a?Ettve.7e7
EQUIPMENT
LIST
MINIMUM
35. OXYGEN
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
35-11-2CrewOxygen
System
1) Pressure
lndication
(ErcAS)
provideda procedureis usedto
(M) May be inoperative
verifythatoxygensupplyis abovethe minimumrequired
beforeeachdeparture.
2) BoftleGage
(oneboftlesystem)
May be inoperativeprovidedthe pressureindication
(EICAS)
normally
operates
BottleGage
(twobottlesystem)
4) Supernumerary
c
2
providedthe pressureindication
(M) May be inoperative
(EICAS)
operates
normally
C
-
May be inoperativeprovidedassociatedseat is not
occuoied,
OxygenMask
May be inoperativeprovidedflight is not conducted
above10,000feetMSL.
provided:
(M) One maybe inoperative
PressureRegulator
(twobottlesystem)
pressureregulatoris
a) Lineto inoperative
disconnected
andplugged.
b) Bottlegageon remainingboftleoperates
and
normally,
c) Oxygensupplyis verifiedto be abovethe
minimumrequiredbeforeeachdeparture.
o,|
OxygenThermal
ReliefIndikator
0
(O)Maybe damaged
or missing.
PLACCARD
INOPe
NearEICAS- 02 PRESINDICATION
(continued)
Page35-1
REV17 MAR10/2007.
IIMIEV
Hungarian Airlines
fi
.78?
.aa7Ett'vaF
EOUIPMENT
MINIMUM
LIST
35. OXYGEN
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O)
OPERATIONS
Verifythatoxygenpressureis adequatefor dispatch:
1. SelectEICASstatuspage;noteoxygenpressure.
switch.
2. Select100o/o
on the NORMAL/100%
SLIDElever.
3. Pushdownandholdthe RESET/TEST
in FLOWindicator.
4. Observeyellowcrossappearsmomentarily
selector.
5, Pushandholdthe EMERGENCY/TEST
A. WhileholdingRESET/TEST
SLIDEleverdown,puth EMERGENCY
TESTselectorandobserveyellowcrossappearsin FLOWindicator.
B. Observeoxygenpressuredid notdecreaseduringtest.
35-20-1 PBESmokeHoods
i.a.w.JAROPS1.770.
C
10
-
One requiredfor everyattendantcrewmemberon duty.
0
provided:
(O) Maybe inoperative
wherethe minimumenroute
a) Flightis notconducted
altitudeis above14,000f,eetMSL,
packsoperatenormally,
b) Bothairconditioning
system
c) All other componentsof the pressurization
operatenormally,
remainsat or belowFL 250,
d) Theajrplane
e) Portableoxygenunitsare providedfor 10% of the
passengers,
ano
are appropriately
briefed.
f) Passengers
0
May be inoperativeprovidedflight is conductedat or
below10,000feetMSL.
-
(M) May be inoperative
with no flightaltituderestriction
provided:
a) Affected seats are blocked and placarded to
preventoccuPancY,
and
b) Units operatenormallyfor all usablelavatoryand
flightattendantlocations
(continued)
PLACCARD
As appropriate
35-21-1 PassengerOxygen
System
1) Passenger
Service
Units(PSU)
Page35-2
REV17 MAR10/2007.
;+UIEV
.?arEttye
Hungarian Airlinesfi
7E?
LIST
MINIMUMEQUIPMENT
35. OXYGEN
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Automatic
Presentation
System
0
provided:
(M) Maybe inoperative
manual
deployment
systemoperatesnormally,
a) The
ano
remainsat or belowFL 300.
b) Theairplane
NOTE.
UseMELitem25-25-1,FlightAttendantSeatAssembly,for dispatchwhenan inoperative
oxygenserviceunitrendersa flightattendantseatunusable.
PLACARD
Placardthe blockedseat(s)- DO NOTOCCUPY
- DO NOTENTER
- INOPERATIVE
Placard
theblockedlavatory(s)
Withautomaticdeploysysteminop,placardnearthe upperEICASdisplay- PASSOXYAUTOINOP
- ALTITUDE
panelas appropriate
TO FL 300
LIMITED
On the instrument
panel
LIMITED
TO FL 250
ALTITUDE
the
instrument
as
appropriate
On
- ALTITUDE
panelas appropriate
TO 10,000FEETMSL
LIMITED
On theinstrument
(O}
OPERATIONS
PassengerOxygenSystemInoperative:
equalto or lowerthan14,000feet
1. Planflightoverroutewithminimum
enroutealtitude
F1250.
2. Maximum
flightaltitude
shallnotexceed
3. Priorto flight,the pilotin commandshallbriefcabincrewon the alternateemergency
procedures
thatwill be used.
Systemlnoperative:
AutomaticPresentation
1. Be preparedto deploypatsengermasksmanuallyusingthe PASSOXYswitch.
2. Fliohtaltitude
is limitedto F1300.
Page35-3
REV17 MAR10/2007.
tVUaEV
Hungarian Airlines
f
.?ZEtIIYE.78.7
EQUIPMENT
LIST
MINIMUM
35.OXYGEN
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
i.a.w. JAROPS1.760
35-31-1
1) PortableOxygen
Dispensing
Units
(Bottleand Mask)
8767-200
D
2) PortableOxygen
Dispensing
Units
(Bottleand Mask)
8767-300
D
9
or missingprovided:
Maybe unserviceable
bottlesis
of serviceable
a) The followingdistribution
maintained:
- 2 in the emergencyequipmentstowageunit,
- 1 at aft zoneof fwd passcabin,
- 2 at midgalleyarea,
- 3 at aft zoneof afr passcabin,
b) Bottlesnot properlyserviceare replaced,serviced
or removed at the next available maintenance
facility.
't7 15 a) Maybe unserviceeble
or missingprovided:
1) The following distribution of serviceable
bottlesis maintained:
2) ?haolille bottlesin the emergencyequipment
stowageunit,(G1)
bottlesat aft zoneof
and 1i310litre
3) 1/120litre
fwd Dasscabin.
4) 1l120litrcand 3/310litrebottlesat mid galley
area,
5) 2ll2olitre and 5/310litrebottlesat aft zoneof
aft oass.cabin,
b) Bottlesnot properlyserviceare replaced,serviced
or removed at the next available maintenance
facility
Page35-4
REV17 MAR1012007.
tt'AIEV
Hungarian Airlines,fi
.ezrEtt'vZF
.78.7
EQUIPMENT
MINIMUM
LIST
36. PNEUMATIC
REPAIR INTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
36-1I-1 ENGBLEED
Pressure
Regulating
and
ShutoffValves
(PRSov)
1 (M) (O) Except for ETOPS operationsbeyond 120
provided:
minutes,one maybe inoperative
a) PRSOVis securedclosed,
b) AssociatedEngineBLEEDswitchremainsOFF,
c) Associatedbleed isolationvalve is opened after
takeoff,and closedbeforeapproachand landing,
d) Airplaneis not operatedin knownor forecasticing
conditions,
e) APU is usedas air sourcefor the ADPfor takeoffor
penaltiesareapplied,
ADP inoperative
f) The remaining opposite engine bleed system
operatesnormallY,
The
s) airplaneremainsat or belowFL 350,
MotorGeneratoris not required,and
h ) Hydraulic
r) For CF6-80C2 engine appropriateperformance
adjustmentare appliedfor either of the following
conditionsareapDlied:
(1) The associatedfan air modulationvalve is
securedin the intermediateposition,and takeoff and landing performancelimited weights
OR
reducedby2,270k9(5,0001b),
(2) The associated
fan air modulation
valveis open,
and takeoff and landing performancelimited
by3,180k9(7,0001b).
weightsarereduced
NOTE l: Securingthe PRSOVcloseddisablesthe forwardcargoair conditioning.
The
NOTE 2: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.
HMG is not requiredfor non-ETOPS.
PLACARD
- L(R) PRSOVINOP CLOSED
Pneumatic
controlpanelasappropriate
OPERATIONS
{OI
NOTE:At approximately17,000feet APU may be used to operateone pack to supplypneumatic
powerpressurization.
Averagefuel consumptionfor APU operationis 90 kg (200 lbs) per
nour.
Airplanetakeotfand landingweightpenaltiesare requiredby thefan air valvedeactivation.
1. Turnoff packon affectedside
2. The centerisolationvalvemustbe closedwhen usingAPU air duringtakeoffand landingand
ooenedwhenAPUis shutdown.
Page36-1
REV17 MAR10/2007.
.IIMIEW Hungarian Airlinesfi
.74.7
.?zrEtl'YZF
LIST
EQUIPMENT
MINIMUM
36, PNEUMATIC
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
3 , The affectedbleedisolationvalve must be openedenrouteto pressurizethe hydraulicreservoir
procedures
will requirethe subsequent
closingof thisvalve.
Somenon-normal
4 . lf remainingbleedsourcefails,do the following
procedure.
(O)- BothPacksinoperative
Packs,OPERATIONS
See21-51-1AirConditioning
penalties.
5. Referto item29-11-3forADPinoperative
HIGH
36.11.2ENGINE
STAGEBleed
Valves(HPSOV)
provided:
1 (M) (O) Onemaybe inoperative
a) Valveis securedclosed,
b) A minimumof 70%(55 % below10,000feet MSL)
enginein icing
on the associated
N1 is maintained
conditions,
c) The remainingoppositeengine bleed system
operatesnormally,
d) HydraulicMotorGeneratoris not required,and
engines,
e) ForCF6-80C2
1) Associatedthrust reverser is secured in the
foMardthrustoosition,and
2) Appropriate performance adjustments are
apPlied.
NOTE I : For GE, the HPSOVhasthe samepart numberasthe pressureregulatingvalveandthetwo
valvesareinterchangeable.
Seeitem 36-11-8.
NOTE 2: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.The
HMG is not requiredfor non-ETOPS.
PLACARD
- L(R) HPSOVINOP
Pneumatic
controlpanelasappropriate
(O)
OPERATIONS
tlrust reverserhasbeenlockedout.
1. On CF6-80C2enginesthe associated
A.
For airplaneperformancecalculationsthat include the effect of reversethrust, adjust
performanceto accountfor the inoperativethrust reverser.
duringapplicationof thrustreverse.
may annunciate
B. The IDLE DISAGREEadvisorymessage
to high idle to insureadequate
is
commanded
reverse
is
selected,
the
engine
When thrust
reverserdrives its respective
one
pneumaticpressureto run the reverseractuation.Since
engineto high idle andthe otherreverseris lockedout, with its respectiveenginein ground
annunciates.
idle,theIDLE DISAGREEmessage
maintain70% (55% below 10,000feet MSL - exceptas
2. If icing conditionsare encountered
requiredfor landing)Nl on affectedengineto ensurethat adequatebleedair is availablefor antiicing systems.
Page36-2
REV17 MAR'10i2007.
.I+UIEV
Hungarian AirlinesB
.ezrEttyaF
7A?
LIST
MINIMUMEQUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
3. With thehigh stagebleedvalve/HPSOVlockedclosed,it is possiblethatthe enginebleedair OFF
light andPACK OFFlight may illuminatewith the engineat idle undercertainconditions.To
extinguishthe enginebleedair OFFandPACK OFFlights:
A. Verify manifoldpressureon affectedsideis lessthan 10 psi.
B. Verifo isolationvalveon affectedsideis closed.
C. Veri! air conditioningpackon affectedsideis not selectedOFF(for -200f300,selectAUTO
or STBY).
D. Advancethe throttle off idle to approximately80% N2 to openthe PRSOVand PackFlow
ControlValve.This will extinguishtheenginebleedair OFFlight andPACK OFF light. When
poweris reducedthe enginebleedOFFlight andPACK OFFlight may illuminateagain'
4. The followingflight deckeffectsmayoccur:.
A. CF6-80C2,The engineBLEED light may illuminateand L/R ENG HPSOV messagemay
annunciate
at hiehthrustsettinss.
36-11-3 Intermediate
PressureCheck
Valves
(LowPressure)
1
openprovided:
(M) (O) One maybe inoperative
a) Associatedhigh stage bleed valve / HPSOV is
securedclosed
(55o/o
below10,000feet MSL)
b) A minimumof TOoA
N1 is maintainedon affected engine in icing
conditions,
The remaining opposite engine bleed system
operatesnormally,
MotorGeneratoris notrequired,and
d ) Hydraulic
engines.
ForCF6-80C2
1) Associatedthrust reverseris secured in the
forwardthrustposition,and
2) Appropriate performance adjustments are
applied.
NOTE: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative'
HMG is not requiredfor non-ETOPS.
PLACARD
- L(R) ENGIIPSOV INOP CLOSED
Pneumatic
controlpanelasappropriate
Page36-3
REV17 MAR10/2007.
/VAIEV
Hungarian Airlines
fi
.7Ez
.CzZEtjtYAF
LIST
EQUIPMENT
MINIMUM
36. PNEUMATIC
REPAIRINTERVAL
NUMBERREQUIREDFORDISPATCH
REMARKOR/ANDEXCEPTIONS
(O)
OPERATIONS
1. On enginesthe associated
thrustreverserhat beenlockedout.
For airplaneperformancecalculationsthat include the effect of reversethrust, adjust
performanceto accountfor the inoperativethrust reverser.
duringapplicationof thrustreverse.
mayannunciate
B. The IDLE DISAGREEadvisorymessage
to high idle to insuteadequate
When thrust reverseis selected,the engineis commanded
pneumaticpressureto run the reverseractuation.Sinceone reverserdrives its respective
engineto high idle andthe otherreverseris lockedout, with its respectiveenginein ground
idle,the IDLE DISAGREEmessage
annunciates.
A.
2. lf icing conditionsare encounteredmaintain707oN1 (557obelow 10,000feet MSL exceptas
requiredfor landing)on atfectedengineto ensurethat adequatebleedair is availablefor anti-icing
systems.
thatthe EngineBleedAir OFFlight
3. Withthe HighStageBleedvalvelockedclosed,it is possible
To extinguish
the enginebleedair
with
idle
certain
conditions.
mayilluminate the engineat
under
OFFlight:
A.
B.
c.
D.
Verifymanifoldpressureon affectedsideis lessthan 10 PSl.
Verifyisolationvalveon affectedsideis closed.
packon affectedsideis not selectedOFF(selectAUTOor STBY).
Verifyair conditioning
Advancethe throttleoff idle to approximately
80% N2 to open PRSOVand extinguishthe
enginebleedeir OFFlight.
4. The followingflight deckeffectsmayoccur:.
may
A. CF6-80C2,:The engineBLEED light may illuminateandL/R ENG HPSOVmessage
at hieh thrustsettines.
annunciate
36-11.{ APUBLEEDValve C
'1
0
provided:
(M) Maybe inoperative
and
a) Valveis closed,
b) BleedswitchremainsOFF.
NOTE:TheAPU maybe usedfor electricalpower.
PLACARD
Pneumaticcontrol nanel - APU BLEED VALVE INOP CLOSED
Page36-4
REV17 MAR10/2007.
t+U,EV
Hungarian Airlines
fi
.?aEttve.787
LIST
MINIMUM
EOUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
May be inop€rativeprovidedthe APU bleed valve
remainsclosed,exceptfor enginestart.
36.11.5 APUBLEED
CheckValve
0
36-11-6LandR Bleed
ISLNValves
1 (M) Exceptfor ETOPSoperationsbeyond120 minutes,
one maybe inoperative
Provided:
a) Valveis closedexceptfor enginestart,
b) The airplaneis not operatedin knownor forecast
and
icingconditions,
c) Bothenginebleedvalvesoperatenormally.
PLACARD
- L(R) ISLN VALVE INOP
Pneumatic
controlpanelasappropriate
36-11-7CenterBleed
lsolationValve
C
1
0
provided:
(M) (O) Maybe inoperative
a) Valveremainsclosedexceptfor enginestart,
b) The APU is used as an air sourceduringtakeoff
and landing, or ADP inoperativepenaltiesare
applied,
c) Both center electrical hydraulic pumps operate
normally,
remainsat or belowFL270,and
d) Theairolane
e) HydraulicMotorGeneratoris not required.
NOTE: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.The
HMG is not reouiredfor non-ETOPS.
PLACARD
- ALTITUDE
panelas appropriate
TO FL 270
LIMITED
On theinstrument
On the oneumaticcontrolDanelthe affectedswitch- INOP
OPERATIONS
{O)
penalties.
1. Referto item29-11-3for ADP inoperative
17,000feet,APUbleedair maybe usedas a sourcefor aftandbulk(if
2, Up to approximately
maybe impactedabovethisaltitude.
installed)cargoheat.Carriageof animalsand/orperishables
NOTE:lf APU air is to be used for startingan enginethe centerisolationvalve must be manually
openedpriorto enginestartand manuallyclosedafterthe engineis started.Accessto valveis
throughthe leftwheelwell.
Page36-5
REV17 MAR10/2007.
ttadJEV
,sarEtjve
Hungarian Airlinesfi
.787
EQUIPMENT
LIST
MINIMUM
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
1
36-118 EnginePressure
Valves
Regulating
(PRV)
C
2
(M) (O) Except for ETOPS operationsbeyond 120
minutes,one may be inoperativesecured CLOSED
provided:
a) Associatedbleedvalveswitchremainsclosed,
b) Associatedbleed isolationvalve is opened afier
takeoff,and closedbeforeapproachand landing,
c) The airplaneiE not operatedin knownor forecast
icingconditions,
d) APU is used as air source for takeoff, or ADP
penalties
areapplied,
inoperative
e) The remaining opposite engine bleed system
oPeratesnormallY,
remains
at or belowFL 350,
f) Theairplane
g) HydraulicMotorGeneratoris not required,and
h) Associatedthrustreverseris securedin the foMard
and
thrustpositron,
i) Approirriateperformanceadjustmentsare appliedf
I
for eitherof the followingconiitions:
valve
is
modulation
fan
air
1) The associated
securedin the intermediateposition,and takeoff and landing performancelimited weights
reducedbY2,270kg (5,000lbs.),or
valveis open
2) The associatedfan air modulation
and takeoff and landing performancelimited
weightsarereducedby3,180kg (7,000lbs).
1 (M) (O) Except for ETOPS operationsbeyond 120
OPENprovided:
minutes,
onemaybe inoperative
a) Associated high stage bleed valve is secured
ctose0,
D ) Associatedbleed isolationvalve is opened after
takeoff,and closedbeforeapproachand landing,
c) Asrociatedpressureregulatingvalvewill open fully
pneumatically
d ) APU is used as air source for takeoff, or ADP
penalti€sare applied,
inoperative
AssociatedEngineBleedSwitchremainsOFF,
0 Airplaneremainsat or belowFL350,
s) A minimumof 70oA(55o below10,000feetinMSL)
engine icing
on the associated
Nl is maintained
conditions,
MotorGeneratoris not required,
h ) Hydraulic
i) Associatedthrustreverseris securedin the foMard
thrustposition,
Page36€
REV17 MAR10/2007.
:|MIEV
,aarEf'ytt
Hungarian Airlines'fr
.78?
LIST
MINIMUM
EQUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
j)
Bleed system on remainingopposite engine
operatesnormallyand
k) Appropriateperformanceadiustmentsare applied
for eitherof the followingconditions:
1) The associatedfan air modulationvalve is
secured in the intermediateposition, with
limitedweights
takeoffand landingperformance
by2,270k9(5,000lb),or
reduced
valveis open
2) The associatedfan air modulation
and takeoff and landingperformancelimited
weightsarereducedby3,180kg (7,000lbs).
NOTE 1: The PRV hasthe samepartnumberasthe enginehigh stagevalveandthetwo valvesare
interchangeable.
Seeitem 36-11-2.
NOTE 2: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.The
HMG is not requiredfor non-ETOPS.
PLACARD
- ALTITUDE
panelas appropriate
TO FL 350
LIMITED
On the instrument
(OI
OPERATIONS
1).PRVCLOSED
A. Performance
and limit weightadjustments:
full openor
penaltiesarerequiredwhenfan air modulationvalveis deactivated
l) Performance
position.Reduceperformance
limitedweightsasshownin item36-12-2'
in intermediate
2) On CF6-80C2enginesthe associated
thrustreverserhasbeenlockedout.
a). For airplaneperformancecalculationsthat includethe effect of reversethrust,adjust
performanceto accountfor the inoperativethrust reverser.
b). The IDLE DISAGREEadvisorymessagemay annunciateduring applicationof thrust
to high idle to insure
the engineis commanded
reverse.Whenthrustreverseis selected,
pneumaticpressureto run the reverseractuation.Sinceone reverserdrivesits
adequate
respectiveengineto high idle and the otherreverseris lockedout, with its resp€ctive
annunciates.
enginein groundidle,the IDLE DISAGREEmessage
penalties.
3) APU bleedair canbe usedto avoidADP performance
for APU operationis 200 lbs (90 Kg) perhour'
a). For -200l-300,averagefuel consumption
penaltiespet item 29-11-3
4) If APU bleedair is not available,applyADP performance
B. Selectassociated
L/R ENG bleedair switchOFF.
Page36-7
REV17 MAR10/2007.
Hungarian Airlinesfi
:tMlEV
.78.7
.Az7Ett'UaF
LIST
MINIMUM
EOUIPMENT
36.PNEUMATIC
REPAIRINTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
A/C packswitchto OFF.
C. Selectassociated
the hydraulicreservoir.
D. Associated
bleedisolationvalvemustbe openedenrouteto pressurize
Openthe affectedbleedisolationvalveaftertakeoffandcloseit prior to approach.Somenonnormalprocedures
will requirethe subsequent
closingofthis valvewhile enroute.
E. SelectAPU ON andAPU BleedAir VALVE on for takeoff,ifpossible.F. After gearup and
flap retraction,theAPU BleedAir VALVE andAPU canbe selectedOFF.
G. Remainclearof icing conditions.
H. Limit altitudeto FL350or below.
2), PRV OPEN
A. Performance
andlimit weightadjustments:
-2001300:
penaltiesarerequiredwhenfan air modulationvalveis deactivated
l)
Performance
position.Reduceperfomancelimitedweightsasshownin item
full openor in intermediate
36-12-2.
2) The associated
thrustreverserhasbeenlockedout.
that includethe effectofreversethrust,adjust
a). For airplaneperformance
calculations
performance
thrustreverser.
to accountfot the inoperative
b. The IDLE DISAGREEadvisorymessagemay annunciateduring applicationof thrust
to high idle to insure
the engineis commanded
reverse.Whenthrustreverseis selected,
reverserdrivesits
one
pneumatic
pressure
actuation.
Since
run
the
reverser
adequate
to
with
its respective
respectiveengineto high idle and the otherreverseris lockedout,
annunciaies.
enginein groundidle,theIDLE DISAGREEmessage
penalties.
3) APU bleedair canbe usedto avoidADP performance
-200l-300,
for APU operationis 200 lbs (90 Kg) perhour.
a).For
averagefuel consumption
penaltiesper item 29-11-3
4) If APU bleedair is not available,applyADP performance
B . Selectassociated
L/R ENG bleedair switchOFF.
A/C packswitchto OFF.
C . Selectassociated
D , The centerisolationvalvemustbe closedwhenusingAPU air duringtakeoffandlandingand
openwhenAPU is shutdown.
E. The affectedbleed isolation valve must be openedenrouteto pressurizethe hydraulic
reservoir.Openthe aflectedbleedisolationvalveaftertakeoffandcloseit prior to approach.
closingofthis valve.
will requirethe subsequent
Somenon-normalprocedures
F. Limit altitudeto FL350or below.
Page36-8
REV17 MAR10/2007.
I!'AIEV
Hungarian Airlinesd
^?zrEtlvaF
.7A7
LIST
EQUIPMENT
MINIMUM
36. PNEUMATIC
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXGEPTIONS
G. If icing conditionsare encountered
maintain70To(55o/obelow 10,000feet MSL exceptas
bleedair is availablefor
requiredfor landing)N1 on affectedengineto ensurethat adequate
anti-icingsystems.
non-normal
associated
H. In the eventof oppositesidebleedsystemfailure,afteraccomplishing
checklists,accomplishthe followingsteps:
select:
l) To providefor continuedpressurization
ENGINEBLEEDswitchfor PRV failedopenside..........................................ON
.. AUTO
PACKCONTROLselector
for PRVfailedopenside..........................'.
valve,
Wing Anti-ice
preclude
isolation
opening
the
2) If the non-normalchecklistdoesnot
capabilityis availableby selecting:
..............ON
ISOLATIONswitchfor opposite
side...................
36-12-1 Pre-coolers
1 (M) (O) Except for ETOPS operationsbeyond 120
minutes,the aircrafrmay be dispatchedwith damageto
one precoolerand associatedducting between the
Pressure RegulatingValve (PRV) and Pressure
provided:
Regulating
andShutoffValve(PRSOV)
a) The associatedPRVis securedclosed,
b) The associatedPRSOVis securedclosed,
c) Airplaneis not operatedin knownor forecasticing
conditions,
d) Associatedbleed isolationvalve is opened after
takeoffand closedbeforeapproachand landing,
e) The remaining opposite engine bleed system
operatesnormally,
remainsat or belowFL 350,
f) Theairplane
is
as air source for takeoff, or ADP
APU
used
s)
penaltiesare applied,
inoperative
n) HydraulicMotorGeneratoris not required,and
i) Associatedthrustreverseris securedin the foMard
and
thrustposition,
j) Appropriateperformanceadjustmentsare applied
for eitherofthe followingconditions:
1) The associatedfan air modulationvalve is
securedin the intermediateposition,and tekeoff and landing performancelimited weights
reducedby 2,270kg (5,000lbs),or
valveis open
2) The associatedfan air modulation
and takeoff and landing performancelimited
weightsarereducedby 3,180kg (7,000lbs).
Page36-9
REV17 MAR10/2007
tlMlEW
Hungarian eirlinesA
.AZTEttUZt
.7Ez
LIST
EQUIPMENT
MINIMUM
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE 1: Securingthe PRSOVcloseddisablesthe forrvardcargoair conditioning.
NOTE 2: The HMC is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative.The
HMG is not reouiredfor non-ETOPS.
PLACARD
- ALTITUDE
panelas appropriate
TO FL 350
LIMITED
On theinstrument
(OI
OPERATIONS
1. Performancepenaltiesare requiredby the fan air valve deactivation.Reduceperformance
(O) procedure.
limitedweightsasshownin Item 36-12-2Operations
2. On CF6-80C2enginesthe associated
thrustreverserhasbeenlockedout.
that includethe effectofreversethrust,adjust
A. For airplaneperformance
calculations
performance
thrustreverser.
to accountfor the inoperative
B. The IDLE DISAGREEadvisorymessagemay annunciateduring applicationof thrust
to high idle to insure
reverse.Whenthrustreverseis selected,the engineis commanded
adequatepneumaticpressurcto run the reverseractuation.Sinceone reverserdrivesits
respectiveengineto high idle and the other reverseris lockedout, with its respective
annunciates.
enginein groundidle,the IDLE DISAGREEmessage
3. Remainclearof icins conditions.
36-12-2 FanAir (Precooler) C
ControlSvstems
(M) (O) Except for ETOPS operationsbeyond 120
provided:
minutes,maybe inoperative
a) The associatedfan air modulationvalveis secured
position,
and
in an intermediate
b) Takeoff and landingperformancelimitedweights
by2,268kg (5,000lbs).
are reduced
maybe
(M)(O)Exceptfor ETOPSbeyond120minutes,
provided:
inoperative
a) Associatedfan air modulationvalve is securedfull
open,
b) Takeoff and landing performancelimitedweights
arereducedby3,176kg (7,000lbs),and
c) The airplaneis not operatedin knownor forecast
icingconditions.
PLACARD
- FAMV INOP
OverheadBleedAir Controlpanelasappropriate
Page36-10
REV17 MAR10/2007.
Hungarian AirlinesB
.:tMlEW
,TarEttve
.787
LIST
MINIMUMEQUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS
{OI
L
Reduceperformance
limitedweightsasfollows:
Model / Engine
-200& -300cF6-80c2
FAMV Position
Intermediate
Full Open
Takeofl Landing & Enroute
Climb
2.268ke (5,000lb)
3.176ke (7,000lb)
valvein the intemediateposition,
A. Fuelburnwill increaseapproximately
0.6%per inoperative
position.
and1.2%perinoperative
full
valvein the open
speeds
listedabovearebasedon singleengineoperating
B. Theen-route
climbweightpenalties
that approximatemaximumlift-to-dragratio speed.To accountfor the differencein level otf
altitudewhenoperatingat otherspeeds,multiplythe enrouteclimbweightpenaltylistedaboveby
DIVERSION
SPEEDEFFECTS
the appropriate
factorlistedon page3-01-0.0in the EN-ROUTE
paragrapn.
On engine,
is degraded.
Winganti-ice
capability
2. Airplane
is notto be operated
in icingconditions.
thenacelleanti-ice
is degraded.
capability
36-21-1 BleedAir DUCT
PRESSIndication
Systems
36-21-2 EngineBleedAir
OFFLights
PLACARD
Affectedlight- LIGHTINOP
36-22-1 BLEEDLights
provided:
(M)(O)Onemaybe inoperative
a) Associated high stage bleed valve/HPSOVis
securedclosed,
b) A minimumof 70%(55 % below10,000feet MSL)
enginein icing
on the associated
Nl is maintained
conditions,
c) The remaining opposite engine bleed system
operatesnormally,
Page36-11
REV17 MAR10/2007.
tlAlEV
,?aTEtjyE
Hungarian Airlinesfi
.78.7
LIST
MINIMUM
EQUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
d) HydraulicMotorGeneratoris not required,and
engines.
e) ForCF6-80C2
1) Associatedthrust reverseris secured in the
foMardthrustpoisition,and
2) Appropriate performance adjustments are
aPPlied.
NOTE: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative'Thel
HMG is not requiredfor non-ETOPS.
I
PLACARD
Affectedlight- LIGHTINOP
(OI
OPERATIONS
1. On enginesthe associated
thrustreverserhas beenlockedout.
A.
For airplaneperformancecalculationsthat include the effect of reversethrust, adjust
performance
thrustreverser.
to accountfor the inoperative
duringapplicationof thmst reverse.
may annunciate
B. The IDLE DISAGREEadvisorymessage
When thrustreverseis selected,the engineis commandedto high idle to insureadequate
pneumaticpressureto run the reverseractuation.Sinceone reverserdrives its respective
engineto high idle and the otherreverseris lockedout, with its respectiveenginein ground
idle,the IDLE DISAGREEmessage
annunciates.
for landing) Nl on
2. Maintain
a minimumof 70 o/ol55Vobelow10,000feetMSLexceptas required
affected
enginein icingconditions.
thatthe EngineBleedAir OFF
3. Withthe HighStageBleedvalve/HPSOV
lockedclosed,it is possible
theenginebleed
To
lightmayilluminate
withthe engineat idleundercertainconditions. extinguish
airOFFlight:
A.
B.
C.
D.
Verifymanifoldpressureon affectedside is lessthan 10 PSl.
Verifyisolationvalveon affectedsideis closed.
packon affectedsideis notselectedOFF(selectAUTOor STBY).
Verifyair conditioning
807oN2 to open the PRSOVand eack FlowI
Advancethe throftleoff idle to approximately
ControlValve,Thiswillextinguish
the enginebleedair OFF lightand packOFFlight.WhenI
again.
poweris reduced
OFF
lightandpackOFFlightmayilluminate
theenginebleed
Page36-12
REV17 MAR10i2007.
I?MIEV
,aarEttve
Hungarian Airlinesfi
.787
LIST
MINIMUMEQUIPMENT
36. PNEUMATIC
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
36-22€ OVHTLights
C
2
1
provided:
(M) (O) One maybe inoperative
a) Associated high stage bleed valve is secured
closed,
b) A minimumof 70%(55% below10,000FeetMSL)
enginein icing
on the associated
N1 is maintained
conditions,
c) The remaining opposite engine bleed system
operatesnormally,
d) HydraulicMotorGeneratoris not required,and
engines:
e) ForCF6-80C2
1) Associatedthrust reverseris secured in the
forwardthrustPosition,and
2) Appropriate performance adjustments are
applied.
NOTE: The HMG is requiredfor ETOPSroutesif an IDG or APU generatoris inoperative'Thel
HMG is not requiredfot non-ETOPS.
I
PLACARD
Affected
light- LIGHTINOP
OPERATIONS
{OI
A. On CF6-80C2enginesthe associatedthrustreverserhasbeenlockedout
l) For airplane performancecalculationsthat include the effect of reversethrust, adjust
performance
thrustreverser.
to accountfor the inoperative
duringapplicationof thrustreverse.
may annunciate
2) The IDLE DISAGREEadvisorymessage
When thrust reverseis selected,the engineis commandedto high idle to insureadequate
pneumaticpressureto run the reverseractuation.Since one reverserdrives its respective
engineto high idle and the otherreverseris lockedout, with its respectiveenginein ground
idle,the IDLE DISAGREEmessage
annunciates.
N1 on
for landing)'
B. Maintain
a minimumot 70%(55o below10,00feetMSLexceptas required
when
in
icing
conditions.
affectedengine
lockedclosed,it is possiblethatthe enginebleedair
C. Withthe highstagebleedvalve/HPSOV
To
withtheengineat idleundercertainconditions.
OFFlightandpackOFFlightmayilluminate
extinguish
theenginebleedair OFFandpackOFFlights:
'l)
2\
3)
4)
Verifymanifoldpressureon affectedsideis lessthan 10 psi.
Verifyisolationvalveon affectedsideis closed.
packon affectedsideis notselectedOFF(selectAUTOor STBY).
Verifyair conditioning
I
N2 to openthe PRSOVand PackFlow
80o/o
Advancethe throtlleoff idleto approximately
I
theenginebleedairOFFlightandpackOFF lightWhen I
ControlValve.Thiswillextinguish
again.
poweris reduced
theenginebleedOFFlightandpackOFFlightmayilluminate
Page36-13
REV17 MAR10/2007.
tlMlEV
.azEtlvzF
Hungarian Airlinesh
.78.7
EQUIPMENT
LIST
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
36-224 Land R Bleed
ISLNValveLights
C
2
1 (O) One may be inoperativeprovidedassociatedduct
pressureindicatoroperatesnormally.
PLACARD
Atfectedlight- LIGHTINOP
OPERATIONS
{O)
lf properoperationof an lsolationValve is in question,refer to the ECS synopticpage on EICAS
andiorDuctPressureindications.
36-22-5C BleedISLN
VALVELight
PLACARD
As appropriate
36-22-6APUBleedISLN
VALVELight
PLACARD
As appropriate
Page36-14
REV17 MAY30/2007.
Hungarian Airlinesfi
ttMlEV
.78.?zrEtjyaF
EQUIPMENT
LIST
MINIMUM
38. WATER/WASTE
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
38-10-1 PotableWater
System
C
2
C
2
provided:
maybe inoperative
1 (M) Individualcomponents
are deactivated
or isolated,
a) Associatedcomponents
ano
b) Associatedsystemcomponentsare verifiednot to
haveleaks.
NOTE:Any portionof systemwhichoperatesnormally
maybe used.
provided:
0 (M) Maybe inoperative
a) Systemts drained,and
to ensurethat systemis
are established
b) Procedures
notserviced.
PLACARD
- INOP- DO NOT USE
For deactivated
or isolatedcomponents,
asappropriate
For inoperativepotablewater system,Aft PotableWaterServicePanel- POTABLE WATER SYS
INOP. DO NOT FILL
38-30-1 LavatorySystems
767-200 C
767-300 C
7
6
5
5
767-200
767-300 c
6
5
provided:
(M)Individual
maybe inoperative
components
isolated,
or
are
deactivated
a) Associatedcomponents
ano
b) Associatedsystemcomponentsare verifiednot to
haveleaks.
NOTE:Any portionof systemwhichoperatesnormally
mavbe used.
(M) Associatedlavatorysystem(s)may be inoperative
Drovided:
-Associatedcomponentsare deactivatedor isolatedto
preventleaks,
-Associatedlavatorydoo(s) is secured closed and
.INOPERATIVE
- DO NOTENTER".
placarded
NOTE: These provisionsare not intendedto prohibit
by crewmembers.
inspections
PLACARD
- DO NOTENTER
Placardatfectedlavatorydoor- INOPERATIVE
38-32-1 Tank Precharge
ControlSvstem
0
(M) May be inoperative provided the applicable
prechargecontrolvalveis securedin the open position.
Page38-1
REV17 MAR10/2007.
t?adlEW Hungarian Airlinesfi
.azEtjvaF
.747
LIST
MINIMUMEQUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
49-l'f-l AuxiliaryPower
Unit
C
1) Pneumatic
function C
1
1
0
46 ns11sc":--l
May be inoperativeprovidedprocedures
its use.
0
(M) Exceptfor ETOPSoperations
beyond120minutes,
provided:
maybe inoperative
operatenormally,and
a) Both enginedrivengenerators
b) Hydraulic Motor Generator(HMG) is verified to
ooeratenormallv
0
do not reQuire
May be inoperativeprovidedprocedures
I
itsuse.
I
NOTE l: The APU, andAPU generator,
maybe requiredfor ETOPSdispatch.For moreinformation
generator
available,regardingETOPS,seeMEL 24-00-2.
on relief withoutAPU
NOTE 2: APU may be removedper AMM 49-11-02.Whenremovingthe APU for dispatch,ensure
that (1) the equipmentremovedis weighedand(2) that the weightand balanceis updated.
With APU removed,the APU FAULT light may remain illuminated,and the EICAS
messages
APU BLD VAL, APU FUEL VAL, andAPU GEN OFFmay displayafterengine
start.
NOTE 3: The pneumaticfunctionof the APU is controlledby the APU BleedValve MEL item 36I l-4. If the pneumaticfunctionis not working,the APU BleedValve must be closedvra
proceduredescribedin 36-11-4.
NOTE 4: Referto item OPERATIONSNOTE 24-00-2for a batterystartprocedureif a groundair
cart is not available.
PLACARD
As appropriate
49-15-1 APUAir Intake
DoorActuation
System
1) DoorClosed
2) DoorFullyOpen
(-200/-300)
(M) May be inoperativesecuredclosedprovidedAPU
inoperative.
is considered
(M) (O) May be inoperativefully openprovidedAFM
areapplied.
performance
decrements
Page49-1
REV17 MAR10/2007.
tlailEV
Hungarian AirlinesB
zaTEt/vzF
.78?
LIST
EQUIPMENT
MINIMUM
49. AIRBORNEAUXILIARYPOWERUNIT
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
3) DoorPartially
Open C
(-200/-300)
1
0
(O) May be inoperativepartiallyopenprovided:
decrements
areapplied,and
a) AFM performance
inoperative.
b) APU is considered
NOTE 1: TheAPU, andAPU generator,
maybe requiredfor ETOPSdispatch.
NOTE 2: A Door Partially Open may sausereverserotationof the APU with lessthan normal
bearinglubrication.Therefore,it may be desirableto limit the time in this configuralion.
Reverserotationis not presentwith the doorin the fully openor closedposition.
EICAS STATUSMESSAGES
APU DOOR
PLACARD
APU MasterSwitch- INLET DOORINOP(OPEN/CLOSED)
(O)
OPERATIONS
1. (2001300)DoorFully Open:
A. APU maybe usedon the groundandin flight.
B. Increaseplannedfuel bum by 0.7%.
C. Airplaneswith CF6-80C2,engineshavezero (takeoff,enrouteclimb, approachclimb and
landingclimb)performance
decrements.
D. Buffetingmayoccurwhendooris in the openposition.
2. (200f300) Door PartiallyOpen:
A. Do not useAPU. B. Increaseplannedfuel bum by 0.7o%.
C. Airplaneswith CF6-80C2,engineshavezero(takeoff,enrouteclimb,approachclimb and
landingclimb)performance
decrements.
D. Buffetingmayoccurwhendooris in the partiallyopenposition.
49-61-1APUExternal
ControlSvstem
and APU used,provideda qualified
May be inoperative
operatorremainsin the vicinityof the flightdeckAPU
conrol.
(M) May be inoperative
and APU used,providedan
and
systemis installed
fireextinguishing
APUautomatic
normally,
verifiedto operate
Page 49-2
REV17 MAR10/2007.
r*'lAlEV
Hungarian Airlines4
.7a.7
.?zrEtjyzt
LIST
EQUIPMENT
MINIMUM
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
49-70-1 APU FAULTLight
C
1
0
C
1
0
PLACARD
Affected
light- LIGHTINOP
49-70-2 APU RUNLight
(O) May be inoperativeprovidedanotheracceptable
is available
andused.
meansto verityAPUcondition
PLACARD
Affectedlight- LIGHTINOP
(OI
OPERATIONS
APUStartuo
Monitor
APURPMand EGTon EICAS,loadAPUwhenAPURPMis 95%or greater.
APUShutdown
1. PositionAPUVALVEswitchto OFF.Checkto seethatAPUVALVELightdoesnot illuminate
2. Wait120secondsforAPUcooldown.
3. TurnAPU selectorswitchto OFF.
to indicate
APUfuelvalveis
illuminates
4. Wait20 seconds,
observeAPU FAULTlightmomentarily
in transitto closed.
49-71.1 APUEGT
Indication
C
1
O
49-72-1 APUHourmeter
System
C
1
0
(M) May be inoperativeprovidedalternateprocedures
andused.
areestablished
D
0
May be inoperativeprovidedproceduresdo not require
|ts use.
49-73.1 APURPM
lndication
D
0
49-94-1APUOILQTY
Indication
C
May be inoperativeprovided APU is considered
inoperative.
D
(M) May be inoperativeprovidedoil quantityis verified
bv alternatemeans.
EICAS STATUSMESSAGf,S
APU OIL QTY
Page49-3
REV17 MAR10/2007.
I+UIEV
Hungarian Airlines
fi
.?zEttuzt
.7A,-
LIST
MINIMUM
EQUIPMENT
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
C
52-11-{ MainEntry/
ServiceDoor
EMERGENoY
oNLY
ArmedIndicators
-
0
provideda procedureis usedto
(M) May be inoperative
mechanismis in the "SLIDE
mode
select
verifythat the
and in the "SLIDE
ARMED"mode beforedeDarture
opening.
DISARM'modebeforea non-emergency
OPERATIONS
NOTE
Slidearming/disarming
can be verifiedby checkingboththe positionof slidearmingleverand visual
indicationof girt bar lockdown.Door must be armed prior to departurefrom the blocks and not
disarmeduntilblockarrival.
52-11-2 MainEntry/Service
DoorArmingLever
HingedCovers
0
52-11-3 EntryDoorPower
Assist
Opening
0
or missing.
Maybe damaged
52-114 MainEntry/
Service
Doors/Slides/
Exits
Emergency
1) 767-200)
or slide missing
(M) (O) One may be inoperative
provided:
arefullyoperational,
a) All othermainentrydoors,/exits
b) Atfecteddooris not usedfor passengerloading,
c) A conspicuousbarrierstrap or rope and a placard
stetingthat the door is inoperativeshall be placed
door,
acrossthe inooerative
d) Emergencyexit sign and floor proximitylights
associated with the inoperativeexit must be
coveredto obscurethe signsand lights,
e) Passengersmustbe briefednot to usethe affected
door,
0 All passengerseatshalfwayto the nextexit in each
directionfrom the inoperativedoor, across the
entirewidthof the airplane,shallbe blockedoff with
conspicuoustapes or ropesthat contrastwith the
interiorpriorto loadingpassengers.Onlythe seats
in these areas shall be blocked;main passenger
Page52-1
REV17MAR1Ol2007
.t?UaEV Hungarian Airlinesfi
.7Az
,AZTEtttYZt
EQUIPMENT
MINIMUM
LIST
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
g)
h)
i)
j)
k)
aisles,cross aisles,and exits areas must not be
forwarddoor/slide,the
blocked.(For an inoperative
blockedseatingareashall extendfrom the foMard
cabin en, rearwardto a line halfwaybetweenthe
inoperativefoMard door and the next set of doors
aft of the inoperativeone. For an inoperativerear
door/slide,the blockedseatingarea shall extend
foMardfrom the aft cabinto a linehalfwaybetween
the Inoperativedoor and the next set of doors
one).
foMardof the inoperative
shallbe placedin
signsand placards
Conspicuous
appropriatelocationsindicatingtheseseatsare not
to be occupiedby passengers,
Seatedcapacitymust not exceedratedcapacityof
pairof exits,
remaining
For extended range/overwater operations,
occupancy shall not exceed the normal rated
capacityof the slide/raftsor the remainingslide/rafts
or the rated overloadcapacityof the slides/ratfs
remainingafter loss of one additionalslide/raftof
greatestcapacity,whicheveris least,
Blockedseatinglayoutsand evacuationprocedures
must be developedand approved by the FAA
certificate holding office for inclusion in the
manual.and
oDerator's
Repairsaremadewithinoneflightday.
NOTE1: Weightand balancemanifestmustbe revised
as necessaryto ensure proper loading limits are
observed.
may be stationedin vicinity
NOTE2: Cabinattendants
of eachdoorwithinblockedarea.
Page 52-2
REV17 MAR10/2007
:tUlEV
Hungarian airlines,fi
.aatEtlvzF
.7A.7
EQUIPMENT
LIST
MINIMUM
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
2\ 767-3OO
A
6
5
(M) (O) One may be inoperativeor slide missing
provided:
l) All othermainentrydooryexitsarefullyoperational,
m) Affecteddooris not usedfor passengerloading,
n) A conspicuousbarrierstrap or rope and a placard
statingthat the door is inoperativeshall be placed
door,
acrossthe inoperative
o) Emergencyexit sign and floor proximity lights
associated with the inoperativeexit must be
coveredto obscurethe signsand lights,
p) Passengers
mustbe briefednot to usethe affected
door,
q) All passengerseatshalfwayto the nextexit in each
direction from the inoperativedoor, across the
entirewidthof the airplane,shallbe blockedoff with
conspicuoustapet or ropesthat contrastwith the
Onlythe seats
interiorpriorto loadingpassengers.
in these areas shall be blockedimain passenger
aisles, cross aisles,and exits areas must not be
foMard door/slide,the
blocked.(For an inoperative
blockedseatingareeshall extendfrom the foMard
cabin en, rearwardto a line halflr/aybetweenthe
inoperativefoMard door and the next set of doors
aft of the inoperativeone. For an inoperativerear
door/slide,the blockedseatingarea shall extend
forwardfromthe aft cabinto a linehalfwaybetween
the inoDerativedoor and the next set of doors
one).
foMardof the inoperative
shallbe placedin
signsand placards
Conspicuous
appropriatelocationsindicatingtheseseatsare not
to be occupiedby passengers,
s) Seatedcapacitymust not exceedratedcapacityof
pairof exits,
remaining
r) For extended range/overwater operations,
occupancy shall not exceed the normal rated
capacityof the slide/raftsor the remainingslide/rafts
or the rated overloadcapacityof the slidevratfs
remainingafter loss of one additionalslide/raftof
greatestcapacity,whicheveris least,
u) Blockedseatinglayoutsand evacuationprocedures
must be developedand approved by the FAA
Page52-3
REV,17MAR10/2007
t?AlEW Hungarian Airlines4
.?87
,a27Et/v2F
LIST
EQUIPMENT
MINIMUM
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
certificate holding office for inclusion in thel
manual,
and
operator's
I
v) Repairsaremadewithinoneflightday,
I
NOTE1: Weightand balancemanifestmustbe revised
as necessaryto ensure proper loading limits are
observed.
NOTE2: Cabinattendantsmay be stationedin vicinityI
of eachdoorwithinblockedarea.
I
(O)
OPERATIONS
mustbe briefedpriorto takeoffand landingregardingexitthat
Flightcrewmembersand passengers
cannotbe usedfor emergencyevacuation.
PLACARD
Affecteddoor- INOP
5230-1 LowerCargoDoors
1) CargoDoor
LifULatch
Mechanisms
(Standard
DoorAft)
C
2
1
Eithermanualor electricmode on each door may be
inooerative.
C
2
0
(M) Manualand electricmodes may be inoperative
providedthe associateddoor is verified closed and
lockedbeforeeachdeparture.
2) CargoDoorHinge
PowerUnitsand
ManualHinge
DriveSystems
(Standard
DoorAft)
C
-
0
3) CargoDoorHook- C
LatchSystem
Electrical
Function
(LargeDoor- Fwd)
-
0
provided:
(M) Maybe inoperative
a) Manualfunctionoperatesnormally,
b) Thereis no damageto thehooklatchmechanism,
c) Thereis no damageto the latchlockmechanism,
d) Door is closed and locked using an accepted
and
manualprocedure,
maintenance
e) All latch cams are visuallyconfirmedto be in the
closedpositionbeforeeachdeparture.
Page524
REV17 MAR10/2007
t+U,EV Hungarian Airlines
fi
.?zEtjve.787
LIST
EQUIPMENT
MINIMUM
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
4) CargoDoorLift
C
System
(LargeDoor- Fwd)
0
52-30-3 CargoDoorControl
PanelIndicating
Systems
1) DoorOpenLight
(Std.DoorAft)
May be inoperativeprovidedthe door closed light
operatesnormally.
provided:
(M) Maybe inoperative
for associateddoor is
System
a) Door Indication
verifiedto operatenormally,and
b) Dooris visuallyverifiedclosed,latchedand locked
beforeeachdeDarture.
(M) May be inoperativeprovidedthe door is visually
verified closed, letched and locked before each
deoarture.
2) DoorCloseLight
(Std.DoorAft)
3) DoorOpenand
DoorCloseLights
(LargeDoorFwd)
52-34-1 CargoDoorStop
FittingBearing
Plates(4ft Cargo
Door)
(M) May be inoperativeprovidedthe door is verified
closed,latchedand lockedbeforeeachdeparture.
-
C
One on the foMard and aft side of each cargo door
framemaybe missing.
MAINTENANCE
NOTE:
Item52-34-1dispatchdeviationallowsfor two missingbearingplatesper cargodoor (oneon
the forwardframe,and oneon the aft frame).
52€5-1 BulkCargoDoor
Balance
Mechanism
52-50-1 Flight CrewRest
Door
C
1
0
(M) May be inoperativeprovideda safety hold open
deviceis usedwhendooris in ooenposition.
0
(M) May be inoperativeprovided:
a) Door is removed,and
b) Crew restareais not usedfor requiredcrewmember
rest.
Page52-5
REV17 MAR10/2007
Hungarian Airlinesfi
t!'tAlEV
.?E?
,a27Et/u2F
LIST
EQUIPMENT
MINIMUM
52. DOORS
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARXOR/ANDEXCEPTIONS
52-51-3 BoeingEnhanced
FlightDeck
SecurityDoor
26
NOTE:JAR-OPS
1,1255TGLLEAFLET
(MXO)May be inoperativefor a maximumof 4 flights
provided:
and
(a)Automaticlockingsystemis deactivated,
and
(b)Alternateprocedures
established
are
thedoor,using
usedfor lockingandunlocking
restraintsystems.
deadboltsor supplementary
1)Automatic
LockingSystem
Note:Thesedispatchconditionsonlyapplyto
to andfromcountrieswhich
operations
requiresecureddoors.
B
provided:
(OXM)Maybe inoperative
and
(a) Automaticlockingsystemis deactivated,
no otherlockingsystemis used,and
and
(b)Alternateprocedures
are established
usedfor accessto the flightdeck.
2) LockControl
Selector/ Switch
1 Anysystemin excessof one maybe inoperative.
3) LOCK/ DENY
Function
provided:
(O)(M)Maybe inoperative
(a) Flightdeckaccessdevice[keypador
pushbuttonl
is deactivated,
(b) Automaticlockingsystemis verifiedto
and
operatenormally,
and
(c)Alternateprocedures
areestablished
usedto lockthe door,and for accessto the
flightdeck.
4) UNLOCK
Function
provided:
(O)(M)Maybe inoperative
(a)Automaticlockingsystemis verifiedto
operatenormally,and
and
(b)Alternateprocedures
areestablished
usedto lockthe door.
Page52-6
REV17 MAR10/2007
;!'AIEV
Hungarian Airlines
fi
.AZE'jYZF
.78,7
LIST
MINIMUM
EQUIPMENT
52. DOORS
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
5) NORM/AUTO
Function
6) DoorRelease
Mechanism
/ Door
Strike(if installed)
-
1
D
3
provided:
(O)(M)Maybe inoperative
(a) Flightdeckaccessdevicelkeypador
pushbuttonl
is deactivated,
(b) Automaticlockingsystemis verifiedto
operatenormally,and
(c) Alternateprocedures
are established
and
usedfor accessto the flightdeck.
with
Referto the dispatchconditionsassociated
part
(1).
see
automatic
locking
system
the
Onemaybe inoperative.
7) FlightDeck
Access
DevicesIKeypad/
Pushbuttonl
provided:
(OXM)Maybe inoperative
and
(a) Flightdeckaccessdeviceis deactivated,
and
(b) Alternateprocedures
are established
usedfor accessto theflightdeck.
8) LEDson keypad
or
controlpanel
providedalternate
(O) Maybe inoperative
and usedfor accessto
areestablished
orocedures
theflightdeck
9) DoorLockFAIL/
FAULTLight
May be inoperativeprovidedthe automaticlock
controlsare verifiedto operatenormally.
10)DoorLock
AUTO
UNLK/ OPEN
Light
provided:
Maybe inoperative
(a)Automaticlockcontrolsareverifiedto operate
normally,
and
normally.
(b)Doorchimeor buzzeroperates
11) Buzzer/ Chime
provided:
(OXM)Maybe inoperative
(a) Flightdeckaccessdevice[keypador
pushbuttonl
and
is deactivated,
(b)Alternateprocedures
and
are established
usedfor accessto the flightdeck.
(O)
OPERATIONS
NOTE:lf the keypadhas beendeactivated,
makesurethe FlightDeckAccessSystemswitchis in the
OFFposition(guardextended)whenflightdeckdooris closedand the flightdecknotoccupied.
Page52-7
REV17 MAR 10/2007
I!'IALEV
.zz}Ettve
Hunga rian Airlinesfi
.787
EQUIPMENT
LIST
MINIMUM
52. DOORS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
OR/ANDEXCEPTIONS
REII,IARK
52-51,4 BoeingEnhanced C
FlightDeck
SecurityDoorDead
Bolt(FAR25.795
Compliant)
0
May be inoperativeprovidedautomaticlock controls
operatenormally.
52-71-1 DoorIndication
System
0
providedan alternatemethodto
(M) Maybe inoperative
verify that associateddoo(s) is closedand lockedis
andused.
established
C
EICAS STATUSMESSAGES
AFT CARGODOORIND
FWD CARGODR IND
MN CARGODR IND
PLACARD
Associatedlight (Pilot's OverheadPanel)- LIGHT INOP
Near EICAS DOOR INDICATION INOP
52-73-1 Entry/ServiceDoor
SlideArmed
Indicating
Light
System
Page52-8
MAR1Ol2007
REV,17
tlElEV
.e?Ettvat
Hungarian Airlines,fi
.7.e-
LIST
MINIMUM
EOUIPMENT
56.WTNDOWS
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
5611-1 Flight
Compartment
Windows
A
6
5
(M) One FWD (No. 1) windowouterglassply may be
crackedprovided:
a) Visibility through the affected windshield is
acceptable
to the captain,andvisionis not impaired
windshield,
on theremaining
areobserved,
b ) AFMwindowheatlimitations
AirsDeedis limited to 280 KIAS or less below
10,000feetMSL,and
0 ) Operationsare limited to one flight only before
reoarrsare maoe.
This itemappliesonlyto the No. 1 windowand cracksor damageto the outer(non
NOTE1:
and56-11-01,
layer-Foranyotherconditions
referto AMM56-11-00
structural)
Door
56-31-1 Entry/Service
ViewportHeated
Pane(s)
B
0
(M) May be inoperativeprovidedheated panes are
deactivated.
Page56-1
REV17.MAR10/2007
Hungarian Airlines,fi
:tHlEV
.78^g2rEtt'UaF
LIST
EQUIPMENT
MINIMUM
73 ENGINEFUELANDCONTROL
NUMBERINSTALLED
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
Engine
73-21-1Electronic
ControlSystem(EEC)
1) EECNORMMode
(CF6FADEC)
C
(O) May be inoperativeprovidedboth engines are
operatedin the alternate(ALTN)mode.
2) EECFaults
(cF6 FADEC)
A
withC1, C2 faultsprovided:
Maybe dispatched
a) Repairsere madewithinoperatingintervalfor:
cl - 300HRS.
c2 - 2000HRS,
b) The messageis recorded(at first occurrence)in
AFL and filled a DIR with appropriateintervalat
the PIMUmessages,
homebase,recording
c) At following Home Station Check inspect PIMU
history for new message(s)and check previous
to DIR-SSon board,
DlRsaccording
d) Inform Power Plant Engineeringof new Fault
Messaoe
occurrence.
EICAS STATUSMESSAGES
EEC CONFIG
L (R) ENG EEC C1
PLACARD
As appropriate
MAINTENANCE
NOTES:
Operatingintervalwith L (R) ENG EEC C1 messagedependson the EEC softwareverslon.C1 and
C2 faultsare definedby faultswhichoccuron two of last threeflight legs.lf time and manpoweris
perapplic€bleFlM.
available(notto interferewith revenueflight)performtroubleshooting
as follows:
TherearefourEECfaultlevelsannunciated,
Level
c
t\1
c2
-
EICASFaultAnnunciation
L(R)ENGCONTROL (C)
(S,M)
L(R)ENGEECC1
L(R)ENGEECC2
L(R)P|MU
(M)
(M)
lnterval
Maximum
Ooeratinq
IS NOTALLOWEDI
DISPATCH
Dispatchallowedfor 300 HRS.
(withEECsoffware8.2.Oand on)
DisDatch
allowedfor 2000HRS.
Disoatchallowedwithno limit.
Page73-1
REV17 MAR10/2007.
t+UaEV Hungarian Airlines
fi
.7e.7
.?a7Etjya
LIST
EQU]PMENT
MINIMUM
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O}
OPERATIONS
ForSubitems
1, EECNORMMode(L(R)ENGEECMODE):
- SelectbothEECModeSwitchesto Alternate(ALTN).
- ForCFo FADEC,autothroftle
maybe usedif desired.
- Useof theAssumedTemperatureReducedThrustMethodmayor maynot be allowed.Referto
page.
theAFMappendix
applicability
ForSubitems
2, EECC1 Faults(L (R)ENGEECC1):
- GE FADECmaybe dispatched
withstatusmessageL (R) ENGEECCl displayedon one or two
enganes,
- Thereis no OPERETIONS
L (R)ENDEEc
(O)procedure
for dispatch
withassociated
required
Cl message
displayed.
73-21-2 ElectronicEngine
ControlSystems
(EEc)Lights
1) EECNORM/ALTNC
Lights
2
0
(O) May be inoperativeprovided both EEC'S are
switchedto the alternate(ALTN)mode.
OPERATIONS
IOI
item73-21-1.
SeeEECALTERNATE
Modeprocedure,
73-21-3 FuelControlENG
VALVElndication
System
1) FuelControl
C
ENGVALVELights
2) FuelControl
ENGFUELVAL
Indication
System
C
2
(M) May be inoperativeprovrdedthe associatedEngine
FuelValveis verifiedto operatenormally.
2
provided:
(M)(O)Onemaybe inoperative
AssociatedEngineValveis verifiedto operatenormally,
and
AssociatedEICASmetsageis deactivated.
PLACARD
ENGVALVELight(s)- ENGVALVELIGHTINOP
Page73-2
REV17 MAR10/2007.
t!'tAlEV
Hungarian Airlines4
,aza7/uaF
.78?
LIST
EQUIPMENT
MINIMUM
NUMBERINSTALLED
REPAIR INTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
(O)
OPERATIONS
(M) procedurefor EngineFuel
1. Verifyoperationof the enginefuelvalverepeatingMAINTENANCE
shouldbe notedin airplane
valveVerification
at eachshutdownof the affectedengine.Verification
logbook,by recordingtimeelapsedfromselectionof fuelCUTOFFto initiationof engineshutdown
by rapiddecrease
in N1,N2,andEGT.
as indicated
2. Startthe affectedengineusingnormalstartprocedures.
)a-rr-rrrororechanicatc
2
1
N2 Speed
Governors
L(R) ENG O/S GOV was deletedand
NOTE: In EEC softwareupdate8.2K, statuslevel message
are
levelmessages
Maintenance
replacedwith maintenance
levelL (R) ENG EEC C2 message.
per
item
with
this
MMEL
be
dispatched
can
not dispatchcritical.Airplaneswith oldersoftware
statuslevelL(R) ENG OiS GOV message
displayedon EICAS.
f,ICAS STATUSMf,SSAGES
L (R) ENG O/S GOV
PLACARD As appropriate
ldle/
73-21-8Approach
Minimum
ldle
Systems
provided:
(M) (O) Maybe inoperative
a) Flap actuatedapproachidle is verifiedto operate
normally,
and
b) Takeoffand landingperformancelimitedweightis
reducedby 1,406kg (3,100lbs).
1) Minimum
Groundldle
2) Continuous
lgnitionActuated
Approach
ldle
c
2
(M) (O) One may be inoperativeprovidedflap actuated
flightidleis verifiedto operatenormally.
Page73-3
REV17 MAR10/2007
tu'lAlEV
Hungarian Airlines4
.ezEt'YG.TE?
LIST
MINIMUM
EQUIPMENT
REPAIR INTERVAL
FORDISPATCH
NUMBERREOUIRED
REMARKOR/ANDEXCEPTIONS
EICAS STATUSMf,SSAGES
IDLEDISAGREE
PLACARD As appropriate
(O)
OPERATIONS
CF6FADECEngine
lf the continuousignition actuated idle system is inoperative,utilize operatinginstructionsof
HGA-4.
ODerations
ManualBulletin
To the
Flightshouldbe conductedto avoidthunderstorm
activityby over flightor circumnavigation.
maximumextentpossible,heavyrain or hailshouldalso be avoided.Weatherradar,pilotreportsand
flight crew observationsmay be used by the flight crew to determinewhen heavy rain or hail is
accomplishthe following
or anticipated,
anticipated.
Shouldflightin heavyrainor hailbe encountered
procedure:
CONT
ENGINESTARTSELECTORS
lf TAT is 10Cor below:
ON
ANTI-ICE
SWITCHES
(Maintains
a minimum
thrustsettingof flightidle.)
lf TAT is above10C:
DISENGAGE
AUTOTHROTTLE
(Preventsautothrottle
reductionbelowdesiredsettingduringdescent
duringtakeoff,climbandcruise.)
Autothrottles
mayremainengaged
SET
THRUSTLEVERS
of 50%N1 at or above10,000ft. 45%N'l below10,000ft exceptfor landing.
Seta minimum
a noticeabledrop
NOTE:In heavyprecipitation
engineparameterfluctuationmay occur,particularly,
uponleavingthe areaof heavy
in EGT. Engineparameterswill returnto normalimmediately
precipitation.
73-31-1 FuelFlow
lndications
C
2
1
provided:
(M) (O) Onemaybe inoperative
operatenormally,
a) AssociatedN1 and N2 indications
and
operatesnormally,
b) Maintankfuelquantityindicator
and
c) For ETOPSoperationleftand rightmaintank
are disconnected.
densitometers
withSimmonds
densitometers
On airolanes
PN S345N001-032
Page73-4
REV17 MAY30/2007.
:*AIEV
Hungarian Airlinesfi
.?zEttve.7e7
LIST
EQUIPMENT
MINIMUM
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE1: Thefollowingcombinations
of inoperative
equipmentare notallowed:
(28-41-1)
Indication
FuelFlowIndications
and FuelTankQuantity
(28-41-2)
Channels
FuelFlowIndications
and FuelQtyProcessor
aredependent
on fuelflow.
NOTE2: FMCCALCULATED
fuelquantities
NOTE3: Ailerontrim indicationon the controlwheelcan be usedto determineif a fuel imbalance
conditionexists.At cruiseairspeeds,an imbalanceof 1,800kg (4,000pounds)will require
to holdthewingslevel.
approximately
oneunitof ailerondisplacement
NOTE4: In caseof en-routefailureof FQIS,the flightcrewmustkeepa fuel log for the remainderofl
I
NOTEbelowfor samplefuellog.
the flight.Referto OPERATIONS
flight
the FMC may determine
inoperative,
NOTE5: Following
a flightwith a FuelFlowIndication
groundspeedto set at
duringhighspeedtaxi.Thiswillcausethe IRUresidual
completion
21 knotsor greater.The Faultlsolationmanualuse21 knotsas the thresholdto identifya
Manualmayprecludereplacement.
faultylRU.Testingthe IRU perthe Maintenance
to the partnumberslistedin the MELapplies
The
requirement
to
disconnect
densitometers
NOTE 6:
part
numbers.
with other
This doesnot applyto densitometers
NOTE
OPERATIONS
failure
Bothenginesoperating;
FOISinflight
SampleFuelLog:Condition:
TIME
1200uT
1300uT
1400uT
EICASFUELFLOW
5000
4900
TOTALFUELBURN
(bothenqines)
10000
9800
TOTALFUELREMAINING
109000
99000
89200
1 . Startingtimefor the fuellog is the timeat the lastknownwaypoint,foundvia FMC.
displayor EICAS
EICASFUELFLOWis in lb/hr(orkg/hr)as shownon EICASsecondary
compactdispleys.This is the fuelflowindicatedfromthe operativefuelflowsensor'
Page73-5
REV17 MAR10/2007.
Hungarian Airlines,fi
;*EIEV
.787
.gzrEttyaF
LIST
MINIMUM
EOUIPMENT
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
by2. Assumefuelflowon eachengineis
3. TOTALFUELBURNis EICASFUELFLOWmultiplied
thesame.
4. TOTALREMAINING
FUELstartsat the lastknownrecordedtotalfuelremainingdatapoint,found
progresses,
is startfuelminusTOTALFUELBURN.
via FMC.As time
TOTALFUELREMINING
The startingdatapointfor thisfuel log is recordedby the FMCat the lastwaypointpriorto FQIS
failure.Thisis foundas follows:
page:
1, POSREPORT
A. Line'1displays:
1)
LastWaypoint
zt
Time
Altitude
B. Line5 displays:
displayed
on line1.
at the lastwaypoint
1)
POSFUEL.Thisis theTotalFuelRemaining
Page73-6
REV17 MAR10/2007.
:VU,EV Hungarian Airlines,fi
7E.SZEttvzP
LIST
MINIMUM
EOUIPMENT
74.TGNtTtON
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
74-00-1 lgnitionSystems
A
4
3
provided:
(O) Onemaybe inoperative
selectorremainsin BOTHposition,
a) lgnition
b) Engineanti-icesystemsoperate normallyon the
associated
engine,and
c) Repairis madewithinoneflightday.
c
4
2
(O) Exceptfor ETOPSoperations,one per enginemay
provided:
be inoperative
and
selectorremainsin BOTHposition,
a) Ignition
b) Engineanti-icesystemsoperate normallyon the
engine(s).
associated
EICAS STATUSMf,SSAGES
L (R) ENG IGNITOR I
L (R) ENG IGNITOR 2
PLACARD As appropriate
OPERATIONS
{OI
Ground:Selectoperative
ignitor(1 or 2) or selectBOTHto startengine.
AfterenginestartselectBOTH.
in the BOTHposition.
Inflight: Maintain
lgnitron
Selector
Page74-1
REV17 MAR10/2007.
t+U,EV
Hungarian Airlines
fi
,?z7Etre.787
EQUIPMENT
LIST
MINIMUM
75, BLEEDAIR
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
75-21-1 IDGAir/OilCooler C
Valves
2
0
provided:
(M) (O) Maybe inoperative
open,and
a) Valve(s)is deactivated
b) For each inoperativevalve, performancelimited
weightsare reducedby 905 kg (2,000lbs).
EICAS STATUSMESSAGES
L (R) IDG VALVE
PLACARD As appropriate
(O}
OPERATIONS
cF6-80C2:
limit weightsasfollows:.
A. For eachinoperativevalve,reduceperformance
Model / Engine
Takeoff. EnrouteClimb and Landing
-200& -300/All
905ke (2000lb)
B. The enrouteclimb weightpenaltieslistedaboveare basedon singleengineoperatingspeeds
that approximatemaximumlift{o-drag ratio speed.To accountfor the differencein level off
multiply the enrouteclimb weightpenaltylistedabove
altitudewhenoperatingat otherspeeds,
page
by the appropriatefactor listed on
3-01-0.1in the ENROUTE DIVERSION SPEED
EFFECTSparagraph.
0.25Yofor onevalveinoperativeand0.504for two valves
C. Fuelburnwill increaseapproximately
inooerative.
75-23-1 CoreComoartment C
Cooling
Valve
2
0
provided
vatve
associateO
(M) (o) May be inoperative
remarns
open.
I
PLACARD
L (R) CORECOMPARTMENTCLNG VLV INOP
I
(O)
OPER,ATIONS
tot two valves
for one valveinoperativeopen and O.4Vo
Fuefburnwill increaseapproximately
O.2o/o
inoperative
open.
Page75-1
REV17 MAR10i2007.
Hungarian Airlines
fi
tt'AIEW
.78'7
.AaTEttYE
LIST
EQUIPMENT
MINIMUM
75.BLEEDAIR
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
75-24-l TurbineCase
CoolingSystems
(cF6 FADEC)
0
(M) May be inoperativeprovidedassociatedturbine
casecoolingvalveremainsclosed.
fuelburnpenalties:
airplane
NOTE:Inoperative
TCCsystemswillresultin thefollowing
NUMBER
of TCCSYSTEMS
INOP
ENGINETYPE
CF6FADEC
75-24-2 TurbineCoolingAir
System
EleventhStage
CoolingValves
(ESCV)(CF6
FADEC)
a
C
2
0
FUELBURN
ESTIMATED
PENAL]'T
1 . 0%
2.0 o/o
(M) May be inoperativeprovidedassociatedturbine
coolingvalvesremainopen.
will resultin the followingairplanefuel
NOTE 2: For CF6,inoperativeTurbineCoolingAir Systems
burnpenalties:
EECSOFWARE
AIR
OFCOOLING
NUMBER
INOP
SYSTEMS
8.2Jor Earlier
1
2
8.2K-8.2M
8.2Nor Later
1
2
notinstalled)
N/A (ESCV'S
ESTIMATEDFUELBURN
PENALTY
o.4yo
0.8o/o
0.2%o
0.4%
N/A
EICAS STATUSMESSAGES
L (R) ENG ESCV(CF6FADECENGINES)
PLACARD As appropriate
Page75-2
REV17 MAR10/2007.
;+U,EV Hungarian Airlinesfi
.?zEt'ye.7A7
LIST
MINIMUM
EQUIPMENT
77.ENGINEINDICATING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
77-00-1TargetParameter
lndications
0
(O) May be inoperetiveprovidedan alternatemeansof
andused.
desiredvaluesis available
achieving
(O)
OPERATIONS
Observethat desiredvaluesere achieved.Only itemsindicatedby arrowsmay be inoperative(may
notappearon display).
Autothrottle
maystilloperate,butare set at maximumthruston takeotfand climb.
NOTE:For Nl referencereadout,see MELitem22-30-1for possiblerelief.
TAT + l2c
Page77-1
REV17 MAR10/2007.
Hungarian Airlinesfi
rfrllEV
-7e?
.ZaTEZ/YE
LIST
EQUIPMENT
MINIMUM
77. ENGINEINDICATING
NUMBERINSTALLED
REPAIRINTERVAL
FOROISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
77-12-2 N2 Tachometer
Systems(EICAS)
B
2
providedonlyl
(M) One N2 indicationmaybe inoperative
the indicationfunctionis inoperative,
I
provided:
1 One maybe inoperative
I
operates
normally,
a) EICASEGTindication
I
indications
forl
b) Nl and N2 (EICASand STANDBY)
bothenginesoperatenormally.
I
77-21-1 EGTIndications
(Standby
Engine
Indicator)
Indicating c
77-31-1Vibration
Systems
1
2
4
Page77-?
REV17 MAR10/2007.
rtMlEW Hungarian Airlines
fi
.7aF7
.?z7EttvzF
LIST
EQUIPMENT
MINIMUM
78, EXHAUST
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
78-31-1 ThrustReversers
C
2
provided:
1 (M) (O) Onemaybe inoperative
reverseris securedin the foMardthrust
a) Inoperative
oosition.
and
performance
adjustments
are applied.
b) Appropriate
brakingmay
NOTE:Duringlandingroll-out,differential
control.
be reouiredto maintaindirectional
action to
NOTE: The following flight deck effectsare the result of maintenance
certaincircuitbreakersat the endoftheir task:
REV ISLN light illuminatedon ground(inhibitedin air)
(inhibitedin air)
L(R) REV ISLN VAL advisorylevelEICASmessage
L(R) REV ISLN VAL statuslevelEICASmessage
*U-l
Ort*O
EICAS STATUSMESSAGES
L ENG REV POS
R ENG REV POS
L REV ISLN VAL
RREV ISLNVAL
PLACARD
- L or R REVERSERINOP
As appropriate
OPERATIONS (O)
1. For airplaneperformance
calculationsthat includethe effectof reversethrust,adjustperformance
to accountfor the inoperativethrust reverser.
an IDLE DISAGREE
2. Airplaneswith CF6-80C2engines(bothPMC and FADEC)may experience
advisorymessage
arnunciationduringapplicationof thrustreverse.Whenthrustreverseis selected,
the engineis commandedto high idle to insureadequatepneumaticpressureto run the reverser
actuation.Sinceonereverserddvesits respectiveengineto high idle andthe otherreverseris locked
annunciates.
enginein groundidle,the IDLE DISAGREEmessage
out,with its respective
Page78-1
REV17 MAR10/2007.
rtMlEW Hungarian*irlines4
.7A.7
,?z7EttuaF
LIST
MINIMUM
EQUIPMENT
78. EXHAUST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
0 (M) (o) May be inoperativeprovidedthe reverser
vaNeano reverserunlockindicationsoperate
isolation
normally.
78-34-1 REVISLNValve
Light
PLACARD
Affectedlight- LIGHTINOP
(O)
OPERATIONS
Withoutthe REVISLNlightto warnthatoneor bothisolationvalvesare in thewrong(openor closed)
position,flightcrewshould:
1. In flight,assumethat reversersmaybe armed:do not movereverseleverc.
2. Be awarethata subsequent
systemfailurecouldrendera reverserinoperative.
78-34-2 EngineReverse
LeverInterlock
(cF6 FADEC)
C
1 (O) one may be inoperativeextendedor retracted
provided appropriateperformanceadiustmentsare
aoolied.
NOTE: Associatedreverserthrustis limitedto reverse
retracted.
idlewheninoperative
I,ICAS STATUSMf,SSAGES
L REV INTERLOCK
RREV INTERLOCK
PLACARD
As appropriate -
(R) REVERSE THRUST
L
EXTENDEDiRETRACTED
LEVER
INTERLOCK
INOP
(O)
OPERATIONS
Inoperative
extended
When selectingreversethrust,pull both reverseleversup to the normalinterlockpositionand apply
reversethrustas requiredwhenthe operativeinterlockreleases.
Page78-2
REV17 MAR10/2007.
t+UaEV
Hungarian Airlinesfi
.ea}EttvaF
.747
EQUIPMENT
LIST
MINIMUM
78. EXHAUST
REPAIRINTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
NOTE:lf the interlockis inoperativeextended,therewill be no physicalstop for that reversethrust
leverwhenit is pulledup to the interlockposition.The EECwill still protectthe engineby not
lettingreversethrust increaseabove idle until the thrust reversersleevesare sufficiently
deployed.
Inooerative
retracted
Whenselectingreversethrust,pullbothreverseleversup to the normalinterlockposition.Usenormal
thrust reversingtechniqueon the operativesystemand if it appearsthat the rudderauthorityis
becoming
limitedduringdeceleration,
returnleverto reverseidledetent.
NOTE:lf the intedockis inoperativeretracted(lnterlockposition),it will not be physicallypossibleto
movethat reversethrustleverbeyondreverseidle,evenwhenthe reversersleevesare fully
deployed.
For airplaneperformance
calculations
that includethe effectofreversethrust,adjustperfomanceto
accountfor lhe inoperativethrustreverser.
78-34-3 ThrustReverserAir
System
ThrustReverser
C
PRSOV
2
provided:
1 (M)(O)Onemaybe inoperative
Associatedthrust reversedis securedin the foMard
and
thrustoosition.
performance
are applied.
Appropriate
adjustments
PLACARD
- L (R) REVERSERINOP
As appropriate
OPERATIONS(O)
1. For airplaneperformance
calculationsthat includethe effectof reversethrust,adjustperformance
to accountfor the inoperativethrust reverser.
an IDLE DISAGREE
2. Airplaneswith CF6-80C2engines(both PMC and FADEC) mayexperience
advisorymessage
annunciationduringapplicationof thrustreverse.Whenthrustreverseis selected,
the engineis commandedto high idle to insureadequatepneumaticpressureto run the reverser
actuation.Sinceonereverserdrivesits respectiveengineto high idle andthe otler reverseris locked
annunciates.
out, with its respectiveenginein groundidle,theIDLE DISAGREEmessage
Page78-3
REV17 MAR10/2007.
:tAlEV
EZEtFtyaF
Hungarian Airlinesfi
.78,7
LIST
EQUIPMENT
MINIMUM
78. EXHAUST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
78-36-1 REVUnlock
lndications
C
2
provided:
1 (M) (O) Onemaybe inoperative
a) No thrust reverser damage exists which would
adverselyaffectairplaneoperation,and
b) Thrust reverser for the associated engine is
deactivatedand locked in the stowed (forward
thrust)position.
performance
adiustments
are applied.
c) Appropriate
PLACARD
- L (R) REV IJNLOCKINDICATION INOP
As appropriate
- L (R) REVERSERINOP
As appropriate
OPERATIONS(O)
1. For airplaneperformance
calculationsthat includethe effectofreversethrust,adjustperformance
to accountfor the inoperativethrustreverser.
an IDLE DISAGREE
2. Airplaneswith CF6-80C2engines(bothPMC and FADEC)may experience
reverseis selected,
reverse.
When
thrust
advisorymessage
annunciationduringapplicationof thrust
pressure
to run the reverser
the engineis commandedto high idle to insureadequatepneumatic
actuation.Sinceonereverserdrivesits respectiveengineto high idle andthe otherreverseris locked
annunciates.
out,with its respectiveenginein groundidle,the IDLE DISAGREEmessage
78-36-2 FullREVPosition
Indications
C
2
0
May be inoperativeprovidedthe associatedreverser
unlockindicationoperatesnormally.
PLACARD
- L (R) FULL REV INDICATIONINOP
As appropriate
78-36-3 ReverserPosition
SensingSystems
(CF6FADEC)
1
provided:
(M) (O)One maybe inoperative
a) Associatedthrustreverseris securedin the foMard
and
thrustposition,
performance
are applied.
adjustments
Appropriate
b)
EICAS STATUSMESSAGES
L ENG REV POS
RENGRXV POS
Page784
REV17 MAR10/2007.
.tlElEW
.?ZE]IIVZF
Hungarian Airlinesfi
.7e'7
EQUIPMENT
LIST
MINIMUM
78. EXHAUST
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
PLACARD
- L (R) REVERSERINOP
As appropriate
OPERATIONS (O)
1. For airplane perlormancecalculationsthat include the effect of reversethrust, adjust performalce
to accountfor the inoperativethrust reverser.
2. Airplanes with CF6-80C2 engines(both PMC and FADEC) may experiencean IDLE DISAGREE
advisory messageannunciationduring application of thrust reverse.When thrust reverseis selected,
the engineis commandedto high idle to insure adequatepneumaticpressureto run the reverser
actuation.Since one reverserdrives its respectiveengineto high idle and the other reverseris locked
out, with its respectiveengine in ground idle, the IDLE DISAGREE messageannunciates.
3. During landing rollout, differential braking may be required.
Page78-5
REV17 MAR10/2007.
:!'WIEV Hungarian Airlinesfi
.78'7
.AzrEtjVZF
LIST
EQUIPMENT
MINIMUM
79.ENGINEOIL
REPAIRINTERVAL
FORDISPATGH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
1 (M) Except for ETOPS, one may be inoperative
orovided:
a) The oil tank is filled to recommendedcapacity
beforeeachdeoarture,
b) There is no evidence of above normal oil
or leakage,
and
consumption
ENGOILPRESS,OILTEMPindications
c) Associated
andlowENGOILPRESSlightoperatenormally.
79-31-1 oll QTY
Indications
PLACARD
- L (R) OIL QTY INDICATIONINOP
As appropriate
79-33-1 LowENGOIL
PRESSLight
Systems
C
2
1 (M) One may be inoperativeprovidedassociatedOIL
operatenormally.
PRESS.TEMP.andQTYindications
NOTE: The EngineLow Oil PressureSwitchtriggersthe L/R ENG OIL PRESSlight and L/R ENG
The low ENG OIL PRESSindicationsystemincludesthe light,
OIL PRESSeicasmessage.
message,
andswitch.
PLACARD
Atfectedlight- LIGHTINOP
79-34-2 ENG OIL TEMP
SensingElements
C
2
2
(O) One sensingelement on each engine may be
inoperativeprovided both Engine Oil Temperature
indicationsareavailablefrom oneEICAScomputer.
PLACARD
As appropriate- L and/orR ENG OIL TEMP SENSINGELEMENT INOP
OPERATIONS(O)
Position the EICAS computerselectoron the forward electronicspanel to AUTO, L, or R as
at the sametime.
necessary
to displaybothengineoil temperatures
Page79-1
REV17 MAR10/2007.
tt'lAlEW
Hungarian anrines4
.aa7Etlve
.78.7
LIST
MINIMUMEQUIPMENT
79.ENGINEOIL
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
79-35-1 Oil FilterBypass
WarningSystem
B
2
0
provided:
(M) Maybe inoperetive
a) lt is verifiedthat the malfunctionis in the alerting
sysem,ano
b) The mainoil screenis checkedfor the presenceof
beforeeachdeparture.
contiaminants
L(R) OIL FILTER
NOTE: The pressuredifferentialswitchwhich activatesEICASadvisorymessage
I
is associated
with the scavenge
oil filter.
I
EICAS STATUSMESSAGES
L OIL FILTER
R OIL FILTER
PLACARD
- L or R OIL FILTERBYPASSALERTINGSYSTEMINOP
As appropriate
Page79-2
REV17 MAR10i2007.
Hungarian Airlines
:tUlEV
fi
7E?
,az7EtttVZF
MINIMUM
EOUIPMENT
LIST
80. STARTING
REPAIRINTERVAL
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
provided:
1 (M) One maybe inoperative
a) Startvalveis verifiedclosed,and
b) Enginestart selectorswitch is returnedto AUTO
afterenginestart.
80-00.1 EngineStart
VALVELights
PLACARD
Affectedlight- LIGHTINOP
80-00-2 EngineSiart
Valves
C
2
1
provided:
(M) (O)One maybe inoperative
a) The associatedstartVALVElightoperatesnormally,
ano
are used.
b) Manualoverndestartprocedures
PLACARD
panel)- STARTVALVE INOP
Associated
startselector(overhead
(O)
OPERATIONS
MANUAL
OVERRIDE
START
Performnormalenginestartprocedureexcept:
'1. Announce
"OPENSTARTVALVE".Position
to GND.
startselector
"CLOSESTARTVALVE." Veriry thatthe enginestartselectorreturnsto
2. At 50%N2 announce
panelmomentarilyilluminates,then
AUTO, andthatthe startVALVE light on the overhead
extinguishes.
AIR START
start(see
lf en in flightrestartbecomesnecessary,
ensurethatairspeedis sufficientfor a windmilling
FAAApprovedAirplaneFlightManualspeedrequirements).
80-11-2 StarterSwitch
Holding/Cutout
Systems
C
2
0
(O) May be inoperativeprovidedalternateprocedures
andused.
areestablished
PLACARD
Associated
ENG STARTselectoron P5 oanel- HOLD and/orAUTO CUTOUTINOP
Page80-1
REV17 MAR10/2007
z!fllEV
Hungarian Airlinesfi
.787
.aaTEtjvzF
LIST
MINIMUM
EQUIPMENT
80. STARTING
REPAIRINTERVAL
NUMBERINSTALLED
FORDISPATCH
NUMBERREQUIRED
REMARKOR/ANDEXCEPTIONS
OPERATIONS
{O):
Startthe associatedengine(s)using normal enginestart procedureswith the flight crew manually
holdingand/orreleasingtheENG STARTselector.
1. Positionthe ENG STARTselectorto the GND positionandhold if required.
2. PositiontheENG STARTselectorto theAUTO positionat 50%N2
CAUTION: DELAYING ROTATION OF TI{E ENG START SELECTORTO TI{E AUTO
POSITIONCAN CAUSESTARTEROVERSPEEDAND DAMAGE.
3. Verifi that the start VALVE light on the overheadpanel momentarilyilluminates,then
extinsuishes.
Pege80-2
REV17 MAR10/2007