`1|o"o

- Department
Republic
of Indonesia
of Communication
Directorate
General
of Air Communications
rhisAirworHn-s
Di*cri*,oo,n*""jnoi1H3iT:*:f"ffiU'od':f"?"*Yf" "o.* pa,r
3e.ADs
afect
aviarion
safety and
Jegdalions
are
which roquiro imanodiateatbntion. Pad 39 of CASF is ame.d€d by adding the lollowing new AD. No porson
may op€rab a product to wlich an AD apdi6s oxcept in accordanco with ths r€quirefipnts ot tlat AD.
NOTE : A terry fight pemit to fy hs aircrafr to a location wher€ the roquiremen6 ol tris directivo can be actornDlished. mav be
granted by applicalion to DGAC. Report and inquiiing conc€rning this AD shoutd bo addrGsed to tfre DGAC. Albrnative me'ansof
complisnc€ with ffs dir€clive may b€ us€d only if app.o/od by f|g Diroctor G€n6ral.
DAC FORM39-02
NUMBER: 06-04-01
I
DATE OF ISSUE: t2 Aoril2006
APPLICABILITY:
TheNewPiperAircraft,lnc.modelpA_2gandpA-32aircraft.
REFERENCE:
E A S AA D N o . 2 0 0 5 - 0 0 3 5 .
SUBJECT/DESCRIPTION:
- Inspection- Dueto crackingon the oleotorquelink
Main undercarriage
attachlugs.
COMPLIANCE:
Requiredprior to the accumulation
of2000 flight hoursor aircraftin excessof2,000 FH, complianceis
requiredofthe next 100hrs.inspectionor annualinspection,
whichevercomefirst.
ACCOMPLISHMENT:
- Repeatinspectionat intervarnot exceeding100FH. Inspectthe castMLc cyrindertorquerink
attachlugsfor crackasspecifiedin SB. r 13l. - If cracksarefound,the MLG oieohousin!must
be
replacedbeforefurther flight.
EFFECTM DATET22 ADdjZ006
NOTE:
'1|o"o alfof DirectorGeneralof Air Communications
a
Capt,CHRISTIANBISARA
Directorof AirworthinessCertification
AIRWORTHINESS
DIRECTIVE
ADNo:2005-0035
lssued:22December
2005
No person may operate an aircraflto which an AirworthinessDirectiveapplies, except in accordancewith
the
requirementsof that AiMorthinessDirectiveunlessotherwiseagreedwith the Authority of the State of Registry.
TypeApprovalHolder'sName
TheNewPiperAircraft.Inc.
Type/Modeldesignation:
PA-28and PA-32
FAATCDS2A13
7
DesignAD: None
Supercedure:
ATA 32
Manufacturer:
Applicability:
r
Reason:
Supersedes
CM UKAAD 002-06-99
Structure- Main undercarriage- lnspection
PiperAircraftCorporation
and The Newpiper Aircraft.lnc.
Cherokee
Cruiser2B-2OOO1throu9h
28-7725290
I PA-28-140
PA-28-150
Cherokee
28-1
through
2g-4377
and
28-1760A
I
PA-28-15 1Warrior28-741 5001through2A-771S31|
4
PA-28-160
Cherokee
28-1 through28-4377and 28-1760A
PA-28-1
61 Warriortt 28-77I 6001through2816109
PA-28-161
Warrior
lll 2816110
Onty
PA-28-16'1
Cadet2841001through284.1365
PA-28-180
Cherokee
28-3through28-720S31
8
PA-28-180
Archer28-E13,2A-7305001
through28-7505259
PA-28-235
Cherokeepathfinder28-.10001
through28-Z71OOB1
and 2A-E1j
PA-32-260
CherokeeSix 260 32-1through32-7800008
The abovereferenced
cAA uK Mo waslaEealnlesponffi
an incidentin 1995
andrecurring
failures
of the mainlandinggearlegcastings,(partNo.65319-02,
_03
or -04),dueto crackingon the oreotorquerinkaitachrugs.ihe potentiar
for simirar
eventsexistsin.theEuropeanfleet. These failurescari remain undetecteduntilthe
aircrafttouchesthe groundduringranding,readingto colapse of the associated
main.landinggear,consequential
airframedamageand loss of control.These
eventscarrya riskof seriousinjuryand potentialfor loss of life.
since publication
of the cAA AAD piper has producedserviceBufletinNo 1131
datedAugust18, 2003 to addressthis unsafecondition.piper SB 113.tseeks
Inspections
of theoteotugsas definedin the UK AAD piper 0b2-06_99
(butat 100
hourlyintervals).
ThisEASAAD adoptsthe 100hour inspectionintervarin linewith
thePiperSBandtheapplicability
of the piperSB,whichvariesfromthe CAAAD.
EffectiveDate:
30 December
2005
Avis d'6missiond'une Directivede Navigabilit6(AD)-par
I'EASA,EuropeanAviationSafetyAgency
I
I I'autorit6primaired'un mat6riel6tranger
Lesexamensou modifications
d6critsou rappel6sci-dessous
sontimperatifs.
La nonapplication
des
exigences
dansla Directive
contenues
de Navigabilite
citeecFdessous
entrainel'inaptitude
au volde
l'aeronefconcerne
(Envoi02/2005du 18janvier2006)
Directivede Navigabilit6de l'EASAde r6f6rence2005-0035
THE NEWPIPERAIRGRAFT
INC.
Avions PA-28et PA-32
- Inspection
Atlerrisseurs
du traind'atterrissage
Notapour les exploitantset organismesd'entretien d'a6ronefsinscrits au registre franqais:
Si l'ADiointeinvitea un contactvers l'autorit6primairede I'AD,contacterle bureauconcernede la DGAC/DCS.
Si pourI'execution
d'unetachedonn6e,l'AD jointese refdrea une qualilication
de personnel
r6pondant
d une
reglementation
nationale,il est possible de faire intervenir,pour cette teche, du personnelde qualification
dquivalente
accept6e
dansI'UnionEuroD6enne.
Si IADjointese refdred unedonneede navigabilit6
pourle maintiende la navigabilit6
ou uneinstruction
(Manuel
de Vol,Manuelde Maintenance,
...)qui n'estpas celleapprouvee
ou pascelleen vigueuren Frinceou si IAD
jointepr6senteune difJicult6
d'application
li6e a sa specificit6
nationale,exposerle probldmeauprdsdu
d6partemenl
technique
du GSAC(parcourriela "[email protected]"
ou par fax au o1 46 90 4g 4g) ou aupresdu
bureau
concerne
de la DGAC/DCS.
La recopiede cetteAD peut avoir d6grad6la definitiondu documentpr6sent6.En cas de difficultdd lire certains
6l6ments
de cetteAD,se reporter
a I'ADoriginalemisea disposition
parI'autorite
primaire
de I'AD.
. cetteADestexigible
au titredu rdglement
Europeenfi0212o03
ou de la Decision
n'212003de I'EASA.
Gompliance:
00 flighthours.For aircraftin excessof
at the next 100 hrs inspection.
or annual
previously
accomplished
in whichcase
main landinggear cytindertorque link attachtuOs(piper part
!ltsp99!the cast
-03or -04)for cracks.Usinga 10xpowermagnifying-glass,
No.65319-02,
inspect
the top and bottomradiiat the torquelinkattachlugs where it connectsto the strut
housing.lf no cracksare foundby this method,use dye penetrantinspectionto
checkfor cracksaccordingto PiperServiceBulletinNo..1131
or using the dye
penetrantprocessthat can be found in the pA-29-1gl airDlanemaintenance
manual,Chapter20, Section20-10-00.
lf cracksare found,the mainlandinggear
oleohousingmustbe replacedbeforefurtherflight.
Repeatinspectionat intervalsnotexceeding100flight hours.
Replacementof the cast housingwith a forgedcylinderpart No. 65490terminates
theneedfor repeatinspections.
r
Ref. Publications: ServiceBulletin1131,avaitable
fromThe NewpiperAircraft,lnc.2926 piperDrive,
VeroBeach,Florida32960.
This AD was previouslypuOn
Remarks:
receivedare addressedin the CommentResponseDocumenton pAD 05-O1g
published
on theEASAwebsite.
Enquiries
regarding
this AD shouldbe addressed
to Mr. M. Capaccio,AD Focal
Point,Certification
Directorate,
[email protected]
For_questions
concerning
thetechnical
contents
of thisAD's requirement(s),
contact
The NewPiperAircraft,Inc.at theaddressgivenabove.
-