Extra 300LT Manuel utilisateur
CHAPTER 1
PAGE 2
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
Table of Contents
Chapter Title
01-00-00 GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
01-00-01 Related Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
01-00-02 TradeMarks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
01-10-00 SAFETY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
CHAPTER 1
PAGE 4
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
GENERAL
•Weightand Balance Data Sheetand associated papers
•Equipmentlist
Engine: LycomingAEIO-580-B1A
incl.: Christen Inverted Oil System
•Operatonand Installation Manual AEIO-580
(P/N:60297-32)
•Maintenanceand OverhaulMan. AEIO-580
(P/N:LMO-AEIO-580)
•Service Letters, Bulletins and Instructions INDEX
•Service Letters, Bulletins and Instructions
Manufacturer: LYCOMINGENGINES
652 Oliver Street,
Williamsport,PA17701, USA
Propeller: MTV-9-B-C/C 198-25 (3-blade)
•Operation-and Installation Manual E-124
•OverhaulManual and Parts List E-220
•Service Bulletins
Manufacturer: MT-PropellerEntwicklungGmbH,
AirportStraubing,94348Atting,
Germany
Governor: P-880-5 and P-880-41
A-210988 (Woodward)
•Operation-and Installation Manual E-1048
Manufacturer: MT-PropellerEntwicklungGmbH,
AirportStraubing,94348Atting,
Germany
Magneto: SLICK No.6350 and 6393
•4300/6300Ser.MagnetoMaintenanceand OverhaulManual
(L-1363F)
CHAPTER 1
PAGE 5
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
•Service Bulletins (refer to Lycoming Service Letters, Bul-
letinsand Instructions INDEX)
Manufacturer: ChampionAerospaceLLC
1230 Old Norris Road
Liberty,South Carolina,USA29657
Magneto Start Booster: SlickSTART SS1001
•Operation,Maintenance and
Troubleshooting Manual L-1492
•Service Bulletins
Manufacturer: UNISONINDUSTRIES
530BlackhawkPartAvenue
Rockford,IL61104,USA
Cleveland Wheels & Brakes
•MaintenanceManualAWBCMM0001
•Technician’sServiceGuideAWBTSG0001
•Illustrated Parts List
•Service Bulletins
Manufacturer: ParkerHannifinCorporation
1160 Center Road
Avon,Ohio44011,USA
Hooker Harness
•General Restraint System Installation Guidelines
Manufacturer: HOOKERHARNESS
324 East Stephenson Street
Freeport, Illinois 61032, USA
GENERAL
CHAPTER 1
PAGE 6
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
ArtexME406 ELT
•Description,Operation, Installation and Maintenance
Manual ME406 and ME406HM ELT(P/N: 570-1600)
Manufacturer: ArtexAircraftSupplies
P.O. Box 1270
Canby,Oregon97013
Aspen EFD1000/500 System
•Installation Manual #900-00003-001(Rev. G)
•ICADocument #900-00012-001(Rev. D)
Manufacturer: AspenAvionicsInc.
5001IndianSchoolRd.NE
Albuquerque,NM87110
Electronics International MVP-50P
•Installation Instructions II 0425051 (Rev. I)
•Operationg Instructions OI 1002051 (Rev. D)
Manufacturer: ElectronicsInternationalInc.
63296 Powell Butte Hwy
Bend, OR 97701
Kannad406AFELT
•Installationand OperationManual 406AF-COMPACT
ELT (P/N: DOC08038E Rev. 04)
•InitialInstallation Manual406AF-INTEGRA ELT(P/N:
DOC09081C Rev. 02)
•OperationManual 406AF-INTEGRA ELT(P/N:
DOC09078C Rev. 02)
Manufacturer: KannadAviation(McMurdoGroup)
OroliaSAS
Z.I. des 5 Chemins BP 23
56520 Guidel (F)
CHAPTER 1
PAGE 7
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
OtherVendorEquipment
(Vendor publication should be obtained directly from the
vendor.)
•Operation-and Installation Manuals
•Service Bulletins
01-00-02 TradeMarks
Even when the brand names used in this manual are not
marked as registered trade-marks, this does not mean, that
these names are free in the sense of trademark legislation.
CHAPTER 1
PAGE 8
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
01-10-00 SAFETY
To keep the security risks during the execution of the
inspectionandmaintenanceworkaslowaspossible,observe
the following points:
•Inspectionand maintenance work has to becarried out only
byqualified and authorized personnel.
•The execution has to be in accordance with the respective
national safety requirements.
•Beforebeginning anywork, this maintenancemanual has to
beread and understood. In caseof doubt or lackof informa-
tion the manufacturer has to be contacted for advice.
•The safety notes given in this manual are to be observed
unconditionally.
Refer to Chapter 02-10-06 for information concerning
safety notes.
CHAPTER 5
PAGE 2
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
Table of Contents
Chapter/Figure Title
05-00-00 GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
05-10-00 TIMELIMITCOMPONENTS . . . . . . . . . . . . . . . . . . 4
05-10-01 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
05-10-02 OverhaulSchedule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
05-10-03 RecommendedReplacement Times. . . . . . . . . . . . . . . . 5
05-10-04 Time Between Inspection. . . . . . . . . . . . . . . . . . . . . . . . 6
05-20-00 SCHEDULEDMAINTENANCECHECKS . . . . . . . . 7
05-20-01 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
05-20-02 25Hour Inspection - Engine . . . . . . . . . . . . . . . . . . . . . 7
05-20-03 25 Hour Inspection -Aircraft . . . . . . . . . . . . . . . . . . . . 7
Figure 1 Drain and Vent Holes . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Figure 2 Lubrication Chart 25 hours . . . . . . . . . . . . . . . . . . . . . 9
Figure 3 Lubrication Chart 50 hours . . . . . . . . . . . . . . . . . . . . 10
Figure 4 Lubrication Chart 100 hours . . . . . . . . . . . . . . . . . . . 11
05-20-04 MaintenanceChecks Schedule . . . . . . . . . . . . . . . . . . 12
05-20-05 Significant ItemsInspection . . . . . . . . . . . . . . . . . . . . 28
05-50-00 UNSCHEDULEDMAINTENANCECHECKS. . . . . 37
05-50-01 Violent Stopping of the Engine (Propeller Strike) . . . . 37
05-50-02 HardLanding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37
05-50-03 EngineFire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
05-50-04 LightningStrike . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40
05-50-05 Flightline Inspections . . . . . . . . . . . . . . . . . . . . . . . . . 40
CHAPTER 5
PAGE 5
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
TIMELIMITCOMPONENTS
05-10-03 Recommended Replacement Times
Itisrecommendedtoreplacetheitemsshowninthefollow-
ing schedule at the times indicated. The times may be
modified by the respective national authorities.
* on the recommendation
of the manufacturer
**** if not stated otherwise
** recommended replacement
every 5 years to avoid
unscheduled maintenance
Item Replace
Battery Concorde on condition
on condition **
Batteries of the Artex ELT
Batteries of Garmin GNx 4x0W/
530W and GTN 6xx/7xx
Internal batteries of
Aspen EFD1000/500 3 years or 2200 hours
or on condition *
5 years *
Wheels (Cleveland, Parker)
First aid pack
on condition
as stated on the pack
Tires on condition
Brake hoses (PTFE-type)
Wingtip position/strobe light
on condition
If any one LED fails,
the unit must be
repaired or replaced
Fuel, oil & sensing hoses
(PTFE Type MIL-DTL-25579) on condition,
but in engine comp. at
the latest together with
engine removal
Seat belts (Hooker) rework*** or replace
a period of 6 years
use, service life limit
of national aviation
authority must be
considered
after
in
Brake and brake assembly
(Cleveland, Parker) on condition
Rudder control cable on condition
Fairleads on condition
Shock mounts
(Lord Kinematics, Barry
Controls)
on condition,
but at the latest at each
engine overhaul
Bolts and Nuts on condition ****
Batteries of the Kannad ELT 6 years *
*** reworking only by
authorized services
CHAPTER 5
PAGE 12
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
05-20-04 Maintenance Checks Schedule
Themaintenancechecksdescribedinthischapterincludeall
the scheduled checks which must be performed. Use the
followingscheduleandthelubricationcharts(figures2-4).
Operational Checks
O O 1 Start engine (in accordance with the Pilot`s Operating Handbook)
O O 2 Checkthefuelquantityindication.
O O 3 Check oil pressure and temperature.
O O 4 Checkgeneratoroutput.
O O 5 Check magneto RPM-drop at 1800 RPM. (Allowed drop is
175 RPM and no greater diff. between L + R than 50 RPM)
O O 6 Check ignition OFF function at 1000 RPM for a short
moment.
O O 7 Check response of the engine by power setting changes.
O O 8 Check the propeller response at 1800 RPM when changing
pitch.
O O 9 Check idle rpm is between 650 and 750.
O O 10 Checkthefuel flowand manifoldpressure indicaton.
O O 11 ChecktheEGTandCHTindicaton.
O O 12 CheckmixerfunctionperCHT/EGTindication.
O O 13 Check mixture at 1200 rpm.
O O 14 Check the function of the fuel selector valve.
O O 15 Check the radio and the other electronic equipment.
O O 16 Shutdownengineusingmixturelever.Checkthealternator
warninglightandammeter.
Inspector:
Mechanic:
Date:
SerialNo.: Inspections
as specified
each 50 hours
each 100 hours
SCHEDULEDMAINTENANCECHECKS
CHAPTER 5
PAGE 14
PAGEDATE:15.October2014
MAINTENANCEMANUALEXTRA300LT
TEMPORARYREVISION
N° 0D702-TR-08-20141015
Inspector:
Mechanic:
Date:
SerialNo.: Inspections
as specified
each 50 hours
each 100 hours
Engine compartment
(Refer to latest edition ofTextron Lycoming Operator´s and
MaintenanceManualandSB's, SlickMagnetoMaintenance
andOverhaulManualandSB's.
Ground magneto primary circuit before
working on engine
O O 1 Removeengine cowlingas per chapter 71.
O O 2 Inspect cowling and air inlet screen for damage, cracks,
distortion, overheated areas and loose or missing blind nuts
and secure attachment of oil level access plate.
O O 3 Inspectlandinglight fordirt.
O O 4 After this inspection clean cowling.
5,6 Deleted.
O1O2O 7 Drainoil sump in accordance with Chapter 12-10-04 “En-
gineOilReplenishing”
O1O O 8 Clean oil suction screen at oil change, check suction screen
for metal particles, shavings, or flakes. Consider Lyc. SB
N° 480 latest issue.
O1O O 9 Clean oil pressure screen at oil change, check pressure
screen for metal particles, shavings, or flakes. Consider
Lyc. SB N° 480 latest issue.
O 10 Inspect oil temperature sensor unit for leaks and security.
O O 11 Inspect flexible oil lines, oil return lines and fittings for
leaks,security,chafing,dents,andcracks(ref:FAAAC
43.13-1A). Replace flexible oil lines at engine TBO per
Lyc. SB 240.
O 12 Cleanandinspectoilradiatorandattachment.
O313 Removeandflushoilradiator.
O O 14 InspectChristen Inverted Oil Systemfor general condition,
leaks,securemounting andtight connections.
SCHEDULEDMAINTENANCECHECKS
Maintenance Checks Schedule
DANGE R
1 each 25 hours
2 a spectrographic oil analysis is recommended at every 50 hours oil change.
3 each 500 hours
Autres manuels pour 300LT
3
Table des matières
Autres manuels Extra Aéronef
Extra
Extra 200 Manuel utilisateur
Extra
Extra 300S Guide de configuration rapide
Extra
Extra 300LT Guide de configuration rapide
Extra
Extra 300L Guide de configuration rapide
Extra
Extra 300/SC Manuel utilisateur
Extra
Extra 200 Guide de configuration rapide
Extra
Extra 300LT Manuel utilisateur
Extra
Extra 330lx Guide de configuration rapide
Extra
Extra 300L Guide de configuration rapide
Extra
Extra 300LX Manuel utilisateur
