Historique des pièce à durée de vie limitée
Contents
1. TSR TSI CSR CSI REMOVED PART DATA ceo os TSR TSI OSIY D RE Tl C 2 EL qu 22 LO 2 5 A 227 OF CSR CSI EI LO LOG PAGE AMLO 93547 WO YAE DISZ Repair Station V2JRO78L Avantair Receiving Inspection Checklist be completed by authorized personnel only S Date Inspector Name Css Facility Conflrm the packaging af the part identifies the supplier distributor and 15 free from alteration or damage NS Packaging slip identifies vendor and type name of parts enclosed qud Parts adequatley packaged to prevent damage during shipping Verify actual part and accompanying documentation reflect the same information Kai Part numbers match 52 Serial numbers match Verlfy Authorized Release Certificate is properly filled out and appropriatly signed as well 25 traceable to an FAA approved source AN Life limit times and or cycles identifled on Tag Form IF APPLICABLE NA Verlfy that the life limit or inspection Interval has not expired IF APPLICABLE Perfarm visual Inspection of the part looking for obvious defects damage etc Wi Verify any markings data plates not been tampered with or altered 7 ER Verify that any documents referenced or the Authorized Release Certificate Inclu2. d z o N __ __ ow RER i 7 4 gt F v NM S w 5 2 I 12 x i 2 K i i 5 o H u i H NN gt I 85 gt 2 gt P 2 ki H 5 2 5 pt d SE a x 5 NT Y P x a 3 i i Y LV FU Fr 5 e l i
3. ASSY 91 94 _ Aircraft No 02 assy E e p Signature 2 Cert amp ces y ML LC e eee ees M e EE EE EE EE EE pp Work Order Ra aa DISTRIBUTION REQUIREMENTS ns E FE E Remains with A C Flight Log AML or Spare Part When robbed part has been replaced White return WHITE copy and all associated paperwork to Maintenance Records Copy 1 _ MA ___ 2 Dat Station PIE bfo _ Mechani Sign n frein GOTVa ft 77 Work Ord r RROIQS oss e 2 Attach to Robbed Part as proof of Yellow serviceability and retained in aircraft work package Copy 3 Serves as unserviceable parts tag and Pink Must be attached to unserviceable part Revision Date April 8 2009 Form AA 86 600 Revision 19Vd 90 1 5 AJ ITI lt m Og 79 P A O gt f gt NOILISOd 56 AN JAUNLYIONANON 2 m o 70 m j mas gt Approving National Aviation 3 Form Tracking Number Authortylccuntr A AUTHORIZED RELEASE CE
4. 24 0078 BOOM DE CNDTIE Alrrnpie erm ENGINE SERVICE AND MAINTENANCE RECORD TIME RUN TIME SINCE OVERHAUL INSTALLATIONS INSPECTIO DATE r NS REPAIRS ADJ NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLE Ch MATMENTS MODIFICATIONS sms ENTRIES DRAW DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE BROUGHT xU u FORWARD 1 amu 22 anti 2 Engine Logbook WO 2602 N156SL 11 02 2009 _ ______ i N156SL Piaggio 180 Avanti S N 1115 2 Engine Hours 4355 8 Gompiied with tne Foliowing Items Pratt E Whitney PT6A 66 S N PCE RK 0125 2 000 Compliec with Applicable Portions P amp W Periodi Inzpeaci Guide Engine 2 AW PAW MM 72 00 70 6 001 Complied with 720007 Air Filter Inspection En ine 7 6 004 Complied with 790009 Engine Magnetic Chip Detector Inspection Engine 2 6 002 with 720011 Power Turbine Blade Inspection Engine 2 L 6 003 Complied with 790005 Engine Oil Filter Inspection Engine 2 mm OO t RE dns The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is
5. F 52 E a a o O bb A Defective Part PN 69 C gt 03 ke n Defective Part SIN BADE MEN Authorizing Dut i URN r s an EE ieren s m GE s e Ra CSN 4j 5 5 een Please Print Discrepancy S WS SEA LEak en Eu Requested By CY Work Order 8 OoOoOoOoO2OZ O OoOO Please Print ROBBED FROM 4 ROBBED FOR AND INSTALLED ON d t 1 DAS ASSY Name id ___ Accomplish visual check of part for damage Work Order K 2125 _ Part f 20 or ASSY SIN or Part FT ASSY SIN _ _ Aircraft No 102 2 Jani asy oOo Station X SE OM Date 2 0 20 ET Mechanic Signature MT Ce Work Order me e a DISTRIBUTION REQUIREMENTS Remains with A C Flight Log AML or Spare Part When robbed part has been replaced White return WHITE and all associated paperwork to Maintenance Records Copy 1 Copy2 Attach to Robbed Part as proof of Yellow serviceability and retained in aircraft work package Copy 3 Serves as unserviceable parts tag and Pink Must be attached to unserviceable part Revision Date April 8 2009 Form AA 86 600 Revision 1 19Vd 901 OM 952 29 amp 7 V 99Z C 9 1840f ZA uoneis
6. indiqu es la case 12 non approved design data specified in block 12 in block 12 has 13e Date dd mmm yyyy 14d Nom Name _ 14e Date dd mmm yyyy D Ramsay 15 APR 2010 S O N A S O N A _ FORM ONE 2009 12 PAWC 5720 2009 12 Le monteur doit contre v rifier l admissibilit avec les donn es approuv es Installer must cross chack eligibility with approved data RESPONSABILIT S DU MONTEUR INSTALLER RESPONSIBILITIES 1 Le pr sent bon de sortie ne constitue pas une autorisation de montage 1 This certificate does not constitute authority to install 2 Le monteur qui travaille conform ment la r glementation d un pays autre que celul sp cifi la case 1 doit s assurer que la r glementation en question reconnait la certification du pays ainsi sp cifi 2 Installers working irr accordance with the national regulations of a country other than that specified in block 1 must ensure that their regulations recognize certifications from country specified 3 Les d clarations des cases 13a et 14a ne constituent pas une certification du montage Dans tous les cas le dossier technique de l a ronef doit inclure une certification de montage d livr e conform ment la r glementation nationale qui s applique avant que l a ronef puisse voler 3 Statements in block 13a and 14a do not constitute installatio n certification In cases the technical record for the aircraft
7. M 5 UNE ME ee A BR vg TSN 5245 2 DATE 2 14 09 Pratt amp Whitne AC CSN 3862 PT6A 66 SERIAL RK0125 ENG TSN 40732 TSO 0 0 Installed ERIAL 1083 N147SL OSITION 2 ENG CSN 3059 CSO 0 Authorized Signature CRS Number V2JR078L LI lien 3 1 ee CARRIED FORWARD TOTAL THIS a MAXIMUM HOURS BETWEEN OVERHAULS HOURS P TOTAL FROM PREVIOUS SUMMARY 4 ES eg TOTAL SINCE MFG LICENCE NUMBER ENGINE SERVICE AND MAINTENANCE RECORD ae o Ge E TIME SINCE OVERHAUL R Ee i ENTRIES DRAW A 0 5 1 D A DATE 1 NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE T m AN ME COLUMNS BROUGHT FORWARD N147SL Piaggio P 180 S N 1083 e Hours 5334 5 a 2 Englne Hours 4162 5 dic 2 Engine Cyc Lndgs 3109 Complied with the Following Items Pratt amp Whitney PT6A 66 S N PCE RK 0125 12 000 Complied with 720005 Comply with Applicable Portions P amp W Periodic Inspect Guide Engine 2 72 00 00 14 000 Complied with 720007 Air Filter Inspection Engine 2 72 00 00
8. We S wl wm BEN BN e IAM z b A D 28 E TT i h JE _ ry IS E e g F E 585 4 9 Hue o 5 2 2 5 90616 89 8 puesnoq 2 5 py 8 y lt 1 D a PI pe PI a 5 SINYBUBI 6667106 oqumN VOIKO 222 enjeusts lt lt a ui e lt Zu ux 4 5 o T oT gt 6 e i 4404 40f 2214428 10 poaoaddo si SUONDINSIM 943 SAMa 20utuagumut D Sr 2JUVPL0990 Ut pajadsut pup poamdoa spa 1u2u0diuo2 40 241 3 S pos Suiddius y au pue Surddtys 104 H auidus se auu ay sqjuseuoduo2 palinbai y 00 00 SOU SIE amp 7 0183 14 au eui GZTONH 39d N S HIN 91 a 5 oq 8 INON Sup unj 0 anq H A 0950 w 282 DNIMOTIO AHL G3HSETdIWOOO V 4512 Ter 324 Lau EX cz 109hI HOd N
9. CR nda 4 Cla P BROUGHT FORWARD Registre de maintenance Pratt amp Whitney Canada 5212 Gre pv Une spe t de Unbed Torhnclag es 4A United Technelenies Compan 7007 chemin de la Savane Maintenance Log St Hubert Qu bec Centre de service r vision St Saint Hubert 7 Canada J3Y 3X7 PWC 6481 2004 05 Fabricant Manufacturer de s rie Serial No PS RK0125 Mod le Model PT6A 66 D signation Description PRATT AND WHITNEY TURBOPROP POWER CANADA SECTION MODULE Bon de vente Sales Order TSN CSN SSN FSN 159367 4303 1 3228 N A Travail effectu Work Performed TSO Ce sso FSO ______ ______ 229 9 169 REPAIRED OVERHAUL MANUAL REV 26 PT6A 66 MAINTENANCE MANUAL REV 35 SPECIFICATION NO G PT6 ALL REV 1 4 _ AND DAA APPROVED THIS POWER SECTION MODULE HAS BEEN INSPECTED REPAIRED TESTED AND PROCESSED IN AW PT6A 66 0 SN 1 AD S WERE VERIFIED NO AD S APPLY TO THIS MODULE E NC 2 WITH GAS GENERATOR MODULE S N PCE RK0125 S O 159367 3 TEST RUN PERFORMED AND FOUND SATISFACTORY L MOORE 62 1 ei 31 JULY 2009 P amp WC SVCE CENTRE e Date V rificateur autoris Authorized Inspector T C AMO No 20 00 j E EN B xv TOTAL pase aa a TOTAL FR
10. eS ban Pt E CC OD x Certification apr s maintenance en vertu du RAC 571 Car 571 Maintenance release Autre r glementation sp cifi la case 13 Other regulations specified in block 13 F s curit conception approv es et qu ils peuvent tre utills s joe 265 donnees de 5 ela and are in condition Tor safe operation Approved desig Le pr sent bon certifie que moins d indication contraire apparaissant la case 13 le travail indiqu la case12 et d crit la case 13 t effectu conform ment au RAC 571 Certifies that except where otherwise specified in block 13 the work identified in block 12 and described in block 13 was performed in accordance with CAR 571 Des donn es de conception app En Non approved design data 15 Signature 16 R f approbation Approval Ref No 20 Autoris e Authorized Signature 21 R f d autorisation Authorization Ref No T AMO 20 00 17 Nom imprim Typed or Printed 22 Nom dactylographi ou imprim Name Typed or Printed Dale m 4 DD MMM YYY Y L MOORE 52 JUL 3 1 2009 SVCE CENTRE Le monteur doit contre v rifier l admissibilit avec les donn es approv es Installer must cross check eligibility with approved data 1 Le pr sent document n autorise aucunement le montage de la pi ce 1 T
11. forg Forging Matl Serial Service Overhaul DISC TURBINE Num ro du mat riel Material Number 3037313 Manuel R vision Manual amp Revision SB14002 REV 19 N de s rie du mat riel Material Serial No 001 Timbre du v rificateur Inspection Stamp 1039 4 073 2 Donn es sur le moteur module Engine Module Data Donn es sur mat riel Material Data Temps depuis 2 amp Installation d entretien d neuf S i IM umul cette installation Cumul jusqu pr sent nstallation d entretien de l installation du N de s rie du l enl vement i r vision bon travail et ti cd du mat riel moteur module du mat riel Accumulated This Installation Tel Accumulated T6 Date ii Enaine Module Engine Module Engine Module Eng Module SN When erial No TSN When SN When Material Installed Material Material Installed Removed 5 Maintenance Overhaul Facility Work Order A Inspection Stamp Reference Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter te Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as ap
12. d E 1 Autorite de l aviation du pays d approbation pays ENGINE SERVICE AND MAINTENANCE RECORD TTT TIME since TIME RUN INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS DATE e NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR ENTRIES DRAW DIAGONAL LINE THROUGH UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE BROUGHT E 4 e FORWARD uei gt fa S j T M j fe ps Engine Logbook WO 8350 N156SL 01 17 2010 Airframe Hours 3615 8 Airframe Landings 2702 IT E p at 2 Engine Hours 4632 9 NAM D 2 Engine Cyc Lndgs 3480 8 m M Complied withthe Foliowing items Pratt amp Whitney PT6A 86 S N PCE RK 0125 ME y 32 000 Complied with applicable portions of P amp Ewa mM W periodic inspection guide on engine 2 LAW P amp W 72 00 00 _ 38 000 Removed and replaced 2 engine P3 filter with new filter IAW PRW 73 00 00 S PN 1018 SN OFF NSN PN ON P 1018 SN ON NSN 40 000 A ENGINE PERIODIC BORESCOPE INSPECTION IAW p amp W MM 72 00 00 NO DEFECTS NOTED AT THIS E 42 000 REMOVED amp REPLACED 2 ENGINE FUEL NOZZLES WITH INSPECTED LL _ ___ 05 OPS CHECK LEAK EE D FUEL NOZZLES IAW P amp W MM
13. m lt ITI H gt gt gt ejeq uonejejsuj OVL LNANOdNOI SQHOO3MW 1 APPROVING NATIONAL AVIATION AUTHORITY COUNTR Y FAA UNITED STATES 4 Organization CONSOLIDATED SUPPLY INC AUTHORIZED RELEASE CERTIFICATE 2721 Tracking Number 8130 3 AIRWORTHINESS APPROVAL TAG f AS 631 861 SE 1 THIS UNIT OVERHAULED RERMREE FUNETRIONALLY TESTED IN ACCORDANCE WITH MANUFACTURER S MANUAL 2 DETAILS OF THE WORK ARE CONTAINED ON ATTACHED WORK ORDER 3 CERTIFIEB THAT THE WORK SPECIFIED EXCEPT OTHERWISE SPECIFIED WAS CARRIED OUT IN ACCORDANCE WITH EASA 145 AND WITH THAT WORK HE AIRCE COMPONENT 15 CONSIDERED REA EAS TO SERVICE UNDER EASA SEH TE IBER EASA 145 4348 Gr 09 4 Other Regulation Specified in Block 13 Certifies thai unless otherwise sp xified i in Black 13 the work In Diech 18 and described in Block 13 was accomplished accordance with Title 14 Code Federal Regulations Part 43 and in respect to that work the items approved for rolum io service provali ale GI 16 Date J gp Dre gt It is important to understand that the existence ot this document alone does not GEET constitute ep io install the TETTE T EE Where the user install
14. 0 come CT 31 2008 Le monteur doit v ffier l admissibilit avec las donn es approuv es Installer must eligibility with approved data 1 Le pr sent document n autorise aucunement le montage la pi ce 1 This document does constitute authority to install the part 2 Si le monteur se base sur la r glementation nationale d une autorit de navigabilit autre que celle indiqu e la case 1 il doit s assurer 2 Where the installer works in accordance with the national regulations of an Airworthiness Authority other than the Authority specified in que l autorit de navigabilit dont il rel ve accepte les produits ou les travaux de maintenance de l autorit de navigabilit indiqu e la block 1 the installer ensures that his her Airworthiness Authority accepts products or maitenance fram the Airworthiness Authority case 1 specified in block 1 3 Les nonc s des cases 14 et 18 ne sauraient constituer une certification du montage Dans tous les cas le dossier technique 3 Stataments 14 and 19 do not constitute installations certification In all cases the aircraft technical record must contain an installation l a ronef doit renfermer une certification de montage d livr e conform ment la r glementation de l Etat d immatriculation et ce avant certification Issued accordance with the national regulations of the state of registry before tne aircraft may ba flown
15. 16 000 Complied with 720011 Power Turbine Blade Inspection Engine 2 72 00 00 18 000 Complied with 790005 Engine Oil Filter Inspection Engine 2 72 00 00 20 000 Complied with 790009 Engine Magnetic Chip Detector Inspection Engine 2 72 00 00 The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Engines Propellers or Appliances stated above was repaired and inspected accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department Certificate Number V2JR078L 4311 General Howard Drive Clearwater FL 33762 Phone 727 539 0071 Fax 272 539 7007 Signed For Avantair Inc TOTAL THIS PAGE TOTAL FROM PREVIOUS F sort SINCE MFG ______ 2 Engine Logbook WO 293 N147SL 04 18 2009 Airframe Landings 3912 Ga MAXIMUM HOURS BETWEEN OVERHAULS HOURS LICENCE NUMBER MAINTENANCE RECORD ENGINE SERVICE AND 4 Si 3 3 7 ch PN A ES 1 ERES L 4 am N
16. G PTGALL REV 1 4 1 ALL AD S WERE VERIFIED NO AD S APPLY TO THIS MODULE 2 AND TESTED WITH GAS GENERATOR MODULE S N PCE RK0125 5 0 155100 C T VANE RING AREA 7 08 VANE RING AREA 24 02 CAVITY 252 3 TEST RUN PERFORMED AND FOUND SATISFACTORY October 31 2008 Date ZA BE i Ven MAXIMUM HOURS BETWEEN OVERHAULS HOURS 2 KC E 24 0078 2003 10 PAWCJR3 6932 2005 03 7602 2 19 07 2 2 z TCAC 24 0078 3 de suivie de formulaire Fom Tracking BON DE SORTIE AUTORISEE 6800797209 12522907 1 Autorit de l aviation du pays d approbation Approving national aviation authority Transport Transports 4 Nom et adresse de l organisme agr e Approved organization and Address Centre de service St Hubert 5 du bon de travallcontrat facture Service Centre St Hubert Work Order No Contract Invoice Pratt amp e E Canada 7007 de la Savane Le Ais us Ee zg HEIC nod 1 551 00 1 25 GG AUTHORIZED RELEASE CERTIFICATE TCCA 24 0078 8 s 7 Description 8 N de pi ce Part d Qt ri i 112 tat Travail Status Work em 0001 GAS GENERATOR MODULE 3036400 OVERHAULED 13 Remarques Remarks OVERHAULED IN A W PT6A 66 OVERHAUL MANUAL REV 25 AND APPROVED DATA REFER TO LOGBOOK FOR COMPLETE DETAILS CU
17. Mechanic Signature Meter 80 027 S Ad OZEL Work Order PSS Revision Date April 8 2009 Copy 1 White return WHITE and all associated Form AA 86 600 e E ENEE M E FF Authorizing Duty 5 E E Please Print RASE Requested By 4 ROBBEDFOR AND INSTALLED Accomplish visual check of part for damage Aircraft No N 1365 55 304545 01 sn me Mechanic Signature Work Order 44 7 A DISTRIBUTION REQUIREMENTS Remains with A C Flight Log AML or Spare Part When robbed part has been replaced paperwork to Maintenance Records Copy 2 Attach to Robbed Part as proof of Yellow serviceability and retained in aircraft work package Copy 3 Serves as unserviceable parts tag and Pink Must be attached to unserviceable part Revision 901 2295 209 NV 226 C 9 3 Q 18Z0Hf ZA uonejs V1VO 14Vd Q3AONW3 265 ___ 1 ejeq uo dIANNN 2 Jen rv ToN3WON OYL LN3NOdIlNO2 1 _ Authority Country 3 Form Tracking Number AUTHORIZED RELEASE CERTIFICATE FAA United States FAA Form 8130 3 AIRWORTHINESS APPROVAL TAG 65777 5 Work Order Contract Invoice Number 4 Organization Name and Address International Governor Services L
18. Typed or Printed March 26 2010 CHAD User Installer Responsibilities It is important 10 understand that the existence of this document alone does not automatically constitute authority to install the part component assembiy Where the user installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country Specified in Block 1 it is essential that the user installer ensures that his her airworthiness authority accepts parts components assemblies from the airworthiness authority of the country specified in Block 1 Statements in Block 14 and 19 do not constitute installation certification in all Cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user installer before the aircraft may be flown FAA Form 8130 3 6 01 Installer must cross check eligibility with applicable technical data D052 00 012 9005 This form 15 to only be used Avantalr Inc Avantair Receiving Inspection Checklist To be completed by authorized personnel only Date 74 7 Inspector Name FE TM Zu the packaging of the part identifles the supplier or distributor and is free from alteration or damage ackaging slip identifies vendor and type name of parts enclosed arts adequatley packaged to prevent damage during shipping erify
19. S 60219 ama 99 914 8 595 2 cj uonisog ourdug ESOT etos LEOP 891240 eo WHINY 08 PPN L SLYS pelo Je et TIME RUN ALNA MOOH 907 NVAL LdOddfiS SONVNZLNIVW LAL RE DATE BROUGHT FORWARD TOTAL SINCE MFG TOTAL FROM PREVIOUS SUMMARY LLLA UELLE TOTAL THIS PAGE gg ENGINE SERVICE AND MAINTENANCE RECORD TIME since OVERH AUL INSTALLATIONS INSPECTIONS z REPAIRS ADJUSTMENTS MODIFICATIONS NOTE USE BOTH PAGES AND AS MANY LINES 5 REQUIRED FOR COMPLETE ENTRIES DRAW DIAGONAL LINE THROUGH UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE NUMBER ns wn IY C BROUGHT FORWARD IN o ET M 2 Engine Logbook WO 1165 N147SL 06 08 2009 N147SL Piaggio 180 S N 1083 Airframe Hours 5475 1 Airframe Landings 4031 2 Engine Hours 4303 1 2 Engine Cyc Lndgs 3228 Complied with the Following Items Pratt amp Whitney PT6A 66 S N PCE RK 0125 32 000 COMPLIED WITH 2 ENGINE APPLICABLE PORTIONS OF P amp W PERIODIC INSPECTION GUIDE 150 HOUR IAW P amp W MM 72 00 00 N 32 001 Complied with 720007 Air Filter Inspection Engine 2 32 002 Complied with 720011 Power Turbine Blade Inspection Engine 2 M 32 003 Complied with 790005 En
20. SORTIE AUTORIS E TCAC 24 0078 AUTHORIZED RELEASE CERTIFICATE TCCA 24 0078 3 N de suivi du formulaire Form Tracking No 6800874660 Pratt amp Whitney Canada Corp 7007 Chemin de la Savane Pratt amp Whitney Canada St Hubert Quebec Canada J3Y 3X7 5 de travail contrat facture Work Order Contract Invoice 159367 RK0125 PS Une soci t de United Technologies A United Technologies Company 8 N la pi ce Part No Q Qt e Qty 11 N de s rie lot Serial Batch No 12 tat Travail Status Work 6 Article 7 Description Item 0001 POWER SECTION MODULE 3036900 LA ML 0001 PS RK0125 REPAIRED 13 Remarques Remarks REPAIRED IN A W 66 MAINTENANCE MANUAL REV 35 AND APPROVED DATA REFER TO LOGBOOK FOR COMPLETE DETAILS TTSN 4303 1 TTSO 229 9 TCSN 3228 TCSO 169 de s rie du dernier moteur Last Engine Serial No DNA 1 B 397 DGCA E 136 DAC 9902 01 INAC TMAV 332 EASA 145 7098 F 01100154 pr sent bon certifie que les articles indiqu s ci dessus ont t construits conform ment EK ER hat the items identified above were conformity 19 x Certification apr s maintenance en vertu du RAC 571 Car 571 Maintenance release Autre r glementation sp cifi la case 13 Other regulations specified in block 13 Des donn esage conception approv es et quie peuvent tr
21. actual part and accompanying documentation reflect the same Information Part numbers match Serial numbers match Verify Authorized Release Certificate Is properly fi filled out and appropriatly sew as well as traceable to approved source Ld Life limit times and or cycles identified on Tag Form IF APPLICABLE Verify that the life limit or inspection interval has not explred IF APPLICABLE erform visual inspection of the part looking for obvious defects damage etc erify markings data plates have not been tampered with or altered ei Verify that any documents referenced on the Authorized Release Certificate included with the Tear down report workorder etc IF APPLICABLE Conduct random sampling of standard hardware and Inspect for conformity Preserved If applicable 7 No sign of contamination Part Description Cent Part Number KIS CO 6 Kun Number gt gt T 200 Hours _ 7152 32 2 3 Cycles N PART ACCEPTED Inspector Initials PART REJECTED inspector initials REASON FOR REIECTION Inspector Signature Date signed Revlson Farm AA 86 800 Revision Date June 3 2008 Robbed Parts Form PART INFO AUTHORIZATION REQUIREMENTS Aircraft No 2079 Station _ 79 ROB Control Ae ZN 6 252 207 Defective Part
22. must contain an installation certification issued in accordance with the applicable natlonal regulations before the aircraft may be flewn P amp WC JR3 0054 E 2009 12 RECORDS COMPONENT TAG o 0 NOMENCLATURE _ X2 DATE Installation Data WA 72 0 N o e 2 2 OLI 21 N LU REMOVED PART DATA S N OFF BOLES P N OFF LOG AMLA QAZA URSS 795 Repair Station V2JRO78L This form i to be used by Avantalr Inc Avantair Receiving Inspection Checklist be completed by authorized personnel only Date S JI IO Inspector Name E je Facility j Confirm the packaging of the part identifies the supplier or distributor and is free from alteration or damage Packaging slip identifies vendor and type name of parts enclosed arts adequatley packaged to prevent damage during shipping numbers match numbers match Verify Authorized Release Certificate is properly filled out and appropriatly signed as well as traceable to an FAA approved source UP Life limit times and or cycles identified Tag Form APPLICABLE fi iferify that the life limit or inspection interval has not expired IF APPLICABLE Perform visual inspection of the part looking for obviaus defects damage etc erify any markings or data plates have not been tampered with or alte
23. pre 65 age 3 Serves unserviceable parts tag and Pink Must be attached to unserviceable part _ Work Order Enns 4455 is eM Revision Date April 8 2009 Form AA 86 600 Revision Revlson Original This form s to only be used by Avantalr Ine Farm AA 85 000 Revision Date June 3 2008 1 3 Form Tracking Number 1 Approving National Aviation Authority Country FAA UNITED STATES AUTHORIZED RELEASE CERTIFICATE C173765 Form 8130 3 AIRWORTHINESS APPROVAL TAG 4 Organization Name and Address Purolator Inc 8439 Triad Drive Greensboro 27409 9621 1207 1 Part Number 5 Work Order Contract Invoice Number 24328 9 Eligibility 10 Quantity 11 SerialBatch Number 12 Status Work N A 80 Description Element Replacement Kit 1743 645 02 Remarks MFG DATE 02 0 CURE DATE 3Q08 SHELF LIFE 10 Years Airworthiness Approval APPROVED REPLACEMENT FOR Certifies the items identified above were manufactured in conformityito Approved design data and are in a condition for safe operation Federal Regulations part 43 and i ified in Block 13 Non Approved design data specified in Bloc un Authorized Sie ture Name Typed or Printed Rich
24. que tout vol puisse avoir ligu P amp WC 6727 2004 12 21 002 2229 OM oae essnd on enb pene eu 940jeq 51 Jo eme au jo au eauepJoooe penser uoeaynieo en ja Ia el FPPP eun JauJsjueJ yop ue uiejuoa pona Uu eu seseg UE uj uoneognis eymneuoo pue sjusuisjB S snbiuuse Jolssop e sed sej no suec eBejuouu nb uoge ynie eun juajeJnes eu seses sop sgououg se E og eu Jo jonbod sjdeooe Ajuoujmv sseunjuowur Jeu ai seJnsue Jeesu e egnbipur ap emol ep no se eydaaoe eyiqeBiaeu ep anb ui peuis2eds Ajuouyrmy eq uei apo ALOUNY Wim Lt eu SJSUAA 5 5 9522 sonbipur ejes enb Siwe El ns esed as e IS Z 6002 1 190
25. remplac es Page 1 De 1 Ce moteur est muni de l quipement standard figurant sur la liste illustr es des pi ces de P amp WC sauf COMET NEW List of Parts Re placed exception mention e sur le pr sent document Palette Skid GOOD Dossier qualit Quality Record This unit is complete with standard equipment as listed the P amp WC Ilustrated Parts List except as noted Berceau Cradle GOOD Date 2009 07 31 P amp WC JR3 6934 E 6934 2004 10 herein Manchon Sleeve N de s ri 2 i RKO125 PS 06 159367 Not Ghrg N de la pi ce Designation de la pi ce Qt Part No art Description Qty WASHER SLTD PWR TURB SHAFT BEARING OPTION 3112561 01 STRAINER SCAVENGE OIL RDCN GEARBOX 3117607 01 RING RETAINING J 2009 07 31 14 16 43 R3 2009 07 31 14 16 32 PR1 400 EX35533 fopt uni queua tmp mfd57820731141643B Fin du document End of document m N de s rie du conteneur m tal Metal Container SN Client Customer Mod le de P amp WC P amp WC Model PT6A 66 Section Motrice N de s rie sur la plaque Sonideiommande 159367 Power Section signal tique Sales Order No Unit s de s rie Serialized Units N de pi ce Part Number N de s rie Serial Number TSN TSO Remarques Remarks R gulateur d h lice 5 RECEIVED R gulateur de turbine de puissance N A Power Turbine Governor R gulateur survitesse d h lice N A Propeller Overs
26. that any documents referenced anthe Authorized Release Certificate a Work Order AK QJ 5 _ included with the Tear down report workorder etc IF APPLICABLE ASSY SIN or E D p Ka Conduct random sampling of standard hardware and inspect for conformity Part Name co 6o ASSY SIN Aircraft No __ 2 202 9 Vo _ Station Pal ET OS fb Part Preserved If applicable up flo sign of contamination Part No 2 0 D y Port Description y i m 2294 3 Ser RR PCS S E Hours CZ p 7 942 SR So STE 7A Cycles eo Station VE pue _ 0 Z aa GT ITE Work Order 760 7 u 0 e 5 iN PART ACCEPTED Inspector g A PART REJECTED mspetribls _________ ET Li 5 REPLACEMENT FOR ROBBED PART DISTRIBUTION REQUIREMENTS Part Number __2270 _________ E Remains with A C Flight Log AML or Spare Serial Number 475 077 ____ Copy 1 Part When robbed part has been replaced m White retum WHITE copy and all associated TSN tso EI paperwork to Maintenance Records Inspector Signature 2 s gt Copy 2 Attach to Robbed Part as proof of ES 272 ______ Station l 2 4 Yellow serviceability and retained in aircraft MIN work package Mechanic Signature
27. 00 06 ON uonezueugn y p Jed eu 0 ans jou ssop SI L ee ep gt estioje u jueseud 1 gep peAoxddg 42802 55039 en segAhcidde Gel 87 eg el Jo pad4 wudu ng WON ZL Dg orf ON m 91 T ameus 7 peaoudde 1 CL 0522 T due wal uondeauoo seguuop sac uongjedo age 10 uonipuoo ui are pue Pran penouddy 7 LAS eouepioooe SEM g og ein 5 uondeouco Speaguuop seq ui paquasap pue SU CL peuroads oun deoxo Weu sappan 46 59 pewawojuos enee 2 EL ej 2 ZLOSED SE ui Siem pahuepi SWAY 1 1527 FSLOOLIO 1 27720 8602 97 VSV3 ZE AVWL OVNI 10 2066 DEL 3 V29d 6 d L YNA An3jou 9595 00591 6406 NSOL 00 OSIL lt 0 NSIL SI 39IAH3S LNJYYNO S IIV L3 3L3 1d NO2 10049071 OL 38434 Qa3AOddV 5
28. 2 ATH IVONVIN 10 vHHa3AO 99 V91d AVV NI syewsy senbjeue CL Ia vHsaA Ao SCLOMH Sd 0069 0 WOM SENS 233 5 looss L 1 90 iibi SVIS ON NS DEUE tum ett pm ay TREE s r Sd G LOHAH OCLSSEL pid me uas sp nel punk nt uisi at wc dn OUBAES 9 Sang XIOM 4 auis AAT ZS d d M ep np N S 12 sselppy pue awen ism 8ssalpe WON peur suodsueil odsueil 7062292 LE LC 2620088 8100 72 wO GAZINOHLNV 13ST01NY 4114065 30 sked np SJUOMY uuo SIAINS Sp Ne 8 00 Pratt amp Whitney Canada Cle Liste de v rifications du moteur s rie Pratt amp Whitney Canada Pratt amp Whitney Canada Corp PT6A Engine Check List Canada J4G 141 P amp WC 9442 2003 11 Conteneur Container moteur est muni de l quipement standard figurant sur la liste illustr es des pi ces de P amp VVC sauf LONG COUT EW exception mention e sur le pr sent document Palette Skid GOOD This unit is complete with s
29. 8 FORM ONE 1473186 4 Nom et adresse de l organisme Organization Name and Address Pratt amp Whitney Canada Cle Pratt amp Whitney Canada Corp 5 Bon de travail Contrat Facture Work Order Contractilnvoic a gt H 1000 boul Marie Victorin Pratt amp Whitney Canada Longueuil Qu bec 2326572 Une soci t United Technologies A United Technologies Company Canada JAG dai 450 677 9411 196357 11 Situation Travail Status Work 6 Article Item 7 Description B Num ro de pi ce Part No 9 t e Qty 10 Num ro de s rie de lot Seriai Batch No 000001 OIL LEVEL SENSOR IND ATOR 3045458 01 2 NEW 12 Remarques Remarks Note Les num ros de s rie figurant sur les tiquettes ou sur les pi ces servent a la fabrication et ne doivent pas tre inscrits sur le pr sent certificat Note Any serial numbers that may be present on labels or parts are for manufacturing purposes and need not be referenced on this certificate CERTIFIED Le cas ch ant la dur e de stockage est pr cis e sur l emballage de l article When applicable shelf life is indicated on the item packaging Le num ro de pi ce Identifi sur la pi ce peut inclure un suffixe alphab tique Ce suffixe alphab tique The part number marked on a part may include an aipha suffix This alpha suffix denotes the parts d note le niveau de revision de la pi ce Tous les niveaux de revision pour une pi ce donn e sont re
30. CH 790 ben The above maintenance was periormed in accordance with i ggio Pratt amp Whitney and Hartzell maintenance and e Rm MUR SE dees We Geht Propellers or Appliances stated above was repaired and inspected in ant Federal Aviation Regulations and is approved to return t wi __ III Avantair Inc s Quality Assurance Department amp 05 383 2037 La ERE L 00 2 Le 27 d Ge EE D DEEE TOTAL THIS PAGE MAXIMUM HOURS BETWEEN OVERHAULS HOURS MM MH RE H Q TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG LICENCE NUMBER ENGINE SERVICE MAINTENANCE RECORD TIME SINCE TIME RUN OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS DATE ES NOTE USE BOTH PAGES AND 5 LINES REQUIRED FOR COMPLETE EN TRIES DRAW DIAGONAL LINE THROUGH UNUSED LINES IN DATE AND TIME COLUMNS LICENCE E NUMBER BROUGHT FORWARD n das 3 Engine Logbook WO 3857 1565 1 SE Avanti V S N 1115 Airframe Hours 3759 4 Airframe Landings 2804 3 Engine Hours __ F ii 3 Engine Cyc Lndgs Complied with the Following Items Pratt amp W
31. LC 7290 West 118 Place Broomfield 80020 303 464 0043 REPAIR STATION IGOR976N remm Dees o 001 WOODWARD FUEL 9063 016 REV A CONTROL 65777 9 Eligibility 10 Quantity 11 Serial Batch Number 12 Status Work 2482012 REPAIRED REPLACED ROD GUIDE AND RECALIBRATED FUEL CONTROL PER WOODWARD MANUAL WG60089 73 20 13 REV 04 08 TSO 1322 3 13 Remarks CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12 13 WAS CARRIED OUT IN ACCORDANCE WITH EASA 145 AND WITH RESPECT TO THAT WORK THE AIRCRAFT COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA ACCEPTANCE CERTIFICATE NUMBER 145 4575 4 C rites that items identified above were mantiactured vi contomuly 19 718 14 CFR 73 9 Return to service 6 Other regulation specified in Block 13 Sean date and are condition for safe operation Certifies that unless otherwise specified Block 13 the work identified in Block 12 and described In Block 13 was accomplished in accordance with Title 14 Code of Federal Regulations part 43 and in respect to that work the items are approved for return to service 20 Authorized Signature 21 Approval Cartificate Mo e IGOR976N 23 Date m d y Non approved data specified in Block 13 m fdthortzed Signature 17 Name Typed 22
32. OM MAXIMUM HOURS BETWEEN OVERHAULS HOURS PREVIOUS SUMMARY M M a m E EE TOTAL SINCE 5 1 LICENCE NUMBER 1 Autorit de l aviation du pays d approbation pays Approving national aviation authority country 3 N de suivi du formulaire Form Tracking No 6800874662 BON DE SORTIE AUTORIS E TCAC 24 0078 AUTHORIZED RELEASE CERTIFICATE TCCA 24 0078 Transports Transport Canada Canada 4 Organisme Organization Pratt amp Whitney Canada Corp 7007 Chemin de la Savane VA Pratt amp Whitney Canada St Hubert Quebec Canada J3Y 3X7 5 Bon de travail contrat Tacture Work Order Contract Invoice 15936 RK0125 GG Une soci t de United Technologias A United Technologies Company 6 Article 7 Description B N de la pi ce Part No d 12 tat Travail Status Work tem 0001 GAS GENERATOR MODULE 13036400 REPAIRED 13 Remarques Remarks REPAIRED IN AW PT6B 66 MAINTENANCE MANUAL REV 35 AND APPROVED DATA REFER TO LOGBOOK FOR COMPLETE DETAILS TTSN 4303 1 TTSO 229 9 TCSN 3228 TCSO 169 Last Engine Serial No DNA 1 B 397 DGCA E 136 DAC 9902 01 INAC TMAV 332 EASA 145 7098 CAAC F 01100154 19 e pr sent bon certifie que les articles indiqu s ci dessus ont t construits conform ment dente
33. POWER 2 X J 2008 10 31 13 52 22 R3 31 10 2008 13 52 08 PR1 400 PW23015 opt unig queue tmp mid57821031135222B Fin du document End of document EN TRIES 2 MAINTENANCE RECORD REPAIRS ADJUSTMENTS MODIFICATIONS SIGNATURE LICENCE DRAW DIAGONAL LINE THROUGH UNUSED LINES IN DATE AND TIME COLUMNS NUMBER This Power Section module is combined with Gas Generator S N PCE 22 NG Y0 54450 Rpm at amp Shp 5 0 ITT Trim _ C TS Trim resistance Ohms 4 55 S WE ts lem 299977 29 2977 99202127 PER Registre de maintenance 2 Prati amp Whitney Canada Pratt amp Whitney Canada Une de Uniled Technlegies A Technelegss Cemwany Pratt amp Whitney Canada Corp Maintenance Log 7007 chemin de la Savane we St Hubert Qu b Centre de service r vision St Saint Hubert Service Centre St Hubert P amp WC 6481 2004 05 Fabricant Manufacturer DesignationD signation Description Mod le Model N de s rie Serial PRATT AND WHITNEY TURBOPROP POWER PT6A 66 SECTION MODULE PS RK0125 Bon de vente Sales Order TSN CSN Depart SSN 155100 4073 2 3059 Travail effectu WorkPerformed 550 OVERHAULED 0 0 N A THIS POWER SECTION MODULE HAS BEEN OVERHAULED MODIFIED TESTED AND PROCESSED IN PT8A 66 OVERHAUL MANUAL REV 25 DAA APPROVED DATA AND SPECIFICATION NO
34. RRENT SERVICE LIFE IS TTSN 4073 2 TTSO 0 0 TCSN 3059 10500 N de s rie du dernier moteur DNA 1 B 397 DGCA E 136 DAC 9902 01 INAC TMAV 332 EASA 145 7098 01100154 Last Engine Serial No 2 qua les artides indiqu s ci dassus ont t construits conform ment das that the items identified were manufactured in conformity to 19 Le pr sent bon certifie que moins d indication contraire apparaissant la case 13 le travail indiqu la 12 et d crit case 13 t effectu conform ment au 571 Certifies that except where otherwise specified in block 13 the work identified in block 12 and described in block 13 was performed in accordance with CAR 571 ee san apr s malgtenance en vertu 571 Car 571 Maintenance release conception approuv es et qu ils peuvent tre utills s en e s curit Des Haig and ar in condition f r safe operation Approved desig Des donn es de conception Moman 12019098 case 13 Non approved design data sp cifi la case 13 Other regulations specified in black 13 15 Signature 16 R f in Approval Ref No 2 21 R f d autorisation Authorization Ref No ua s AMO 20 00 17 Nom dactylograpls bu imprim Name Typed or Printed in Date 23
35. RTIFICATE FAA United States FAA Form 8130 3 AIRWORTHINESS APPROVAL TAG 66389 5 Work Order Contract Invoice Number 4 Organization Name and Address International Governor Services LLC 7290 West 118 Place Broomfield CO 80020 66389 USA 303 464 0043 REPAIR STATION IGOR976N 7 Description 9 Eligibility 10 Quantity 11 Serial Batch Number 12 Status Work WOODWARD GOVERNOR 8210 411 13751674 OVERHAULED OVERHAULED AND RECALIBRATED GOVERNOR PER WOODWARD MANUAL WG60153 61 20 36 REV 0 10 98 COMPLIED WITH WOODWARD SB 33531 33606R1 TSO 0 0 43 Remarks CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12 13 WAS CARRIED OUT IN ACCORDANCE WITH EASA 145 AND WITH RESPECT TO THAT WORK THE AIRCRAFT COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA ACCEPTANCE CERTIFICATE NUMBER EASA 145 4575 4 Genes that tema identified above were manutactured in conformity ta 18 EN 14 73 9 Return to service Other regulation specified in Block 13 Approve design data and are in a condition for safe operation Certifies that unless otherwise specified in Block 13 the work identified in Block 12 and described in Block 13 was accomplished i in accordance with Title 14 Code of Federal Regulations part 43 and in respect to that work the items are approved for return to service 20 Authorized Signature 1 Non approved dein data specified in Block 13 21 Approval Certif
36. Remarques Remarks NOTE 3 YELLOW LOGBOOKS IN A WHITE BINDER VERRE par rom attire Checked oui by ame amp stay CLIFFORD ANCTIL WA98 31 07 09 MARTIN PROVENCAL SC218 31 07 09 Sans objet NR Non re u SL Nort exp di TSN Temps depuis neuf T50 Temps depuis r visions Not Applicable Not Received Ship Less Time Since New Tine Since Overhaul d DN SUIVI au rormulaire rrackina No ExPCRGECH LLLI BL PAL EC ENGINE SERVICE AND MAINTENANCE RECORD OVERH AUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS DATE Hes NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE Zen ENTRIES DRAW A DIAGONAL LINE THROUGH UNUSED LINES IN DATE TIME COLUMNS Ss st BROUGHT Bra AC TSN 3286 0 DATE 10 15 09 Pratt amp Whitne CSN 26 _________ PT6A 66 SERIAL RK0125 ENG TSN 43031 TSO 229 9 POSITION 2 ENG CSN 3228 CSO 169 WO i 2395 1565 un J gt Fi Authorized Signature CRS Number V2JRO78L ARR EN EM Dae RM N MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG LICENCE NUMBER 3 N de suivi du formulaire Form Trackina
37. Ts ra T r Tip Chis Vasgeation a G IA DO fi Powat Blady cos Mil aV ed with the following AD ge EEE None complied with at this time P the followi Md 4 llam Installed PTG O Ring kit Frag Engine with BP 2380 Tinbine a 4 f nctiongl cheske performed with dns HO faults found p Romoved and Replaced Dip Stick PN OFF 3045451 01 SN OFF AB0364 EN ON 30454 58 01 SN ON bie e E was performer accordance with Pingpio Pratt amp Wuitnay and Hartzell maintenance d ouent Federal Avintian Beta ge ES or Appliances stated above was repaired and inspested in Ge pm _ Assurance Department pproved to return tp service Pertinent detaijs are on file with Avaninir ine s Quality SR gt 272 Gegen Nune TOTAL THIS TOTAL FROM PREVIOUS SUMMARY TOTAL SINCE MFG ce MAINTENANCE RECORD REPAIRS ADJUSTMENTS MODIFICATIONS EN TRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE MAXIMUM HOURS BETWEEN OVERHAULS HOURS Ki x b D IN LICENCE NUMBER 3 N de suivi du formulaire Form Tracking 24 0078 Deal CODTIE
38. aire Form Tracking Z4 UU 6 COIDTIE AIITARISEE H AND MAINTENANCE RECORD TIME SINCE OVER diia INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS m ih ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE _ TIME RUN pan A c n ME 1 n LE BROUGHT FORWARD Removed P SERIAL 1115 _________ AC TSN 3891 9 WO 4341 15651 NIS6SL __ A DATE 04 14 10 AC CSN 2892 PT6A 66 ERIAL 0125 ENG TSN 4909 0 180 8358 TI 5 008 O O POSITION 2 ENG CSN 3670 CSO 611 Removed in serviceable condition Authorized Nu Number V2IRG78L D H r zi E o M M HR M I p 00000 ka E d D o d E Installed m pu N1578L SERIAL 1116 AC TSN 3981 8 WO 4955 N157SL DATE 06 08 10 Pratt amp Whitney AC CSN 3015 E PT6A 66 SERIAL RK0125 ENG TSN 4909 0 TSO 835 8 ENG CSN 3670 CSO 611 POSITION 2 CARRIED FORWARD j PD _ _ _ TOTAL THIS TOTAL FROM MAXIMUM PREVIOUS SUMMARY UM HOURS BETWEEN OVERHAULS HOURS TOTAL SINCE MFG 3 N
39. appraved to return to service Pertinent details are on file with Avantair Inc s Quality Assurance Department E i r e i 575 Aviation Dr Camarillo 93010 Phone 805 383 1100 Fax 805 383 2037 LH LA 0 22 122 gt u Signed For Inc CARRIED FORWARD KC M ume EI m seen ne RE MIEDD j L TOTAL FROM PREVIOUS SUMMARY MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL SINCE MFG E 9i LICENCE NUMBER 5 N de suivi du formulaire Form Trackina No E OI FE RRE A ENGINE SERVICE AND be SEH TIME SINCE TIME RUN OVERHAUL DATE INSTALL ATIONS INSPECTIONS I 15 BROUGHT FORWARD EP s NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE e NISRSL SERIAL 1115 pe DATE 12 13 09 Pratt amp Whitre PTGA 66 f Com led wiih uh tho following Sohegnied T IS0hvI Year Engine Mounts and Vibration 0 2 i r Appi cable Portions P amp W Periodic Jnanegtinn Gui ALL 150 kr P3 Air Filter Inspecti Guide an 1 s an Keen 150 hr Engine Filter
40. ard W Home 16 Approval Authorization No DMIR511162CE 18 Date 87875 22 None pcd or Printed 23 Date m d y Mar 31 2010 s User Installer Responsibilities Approval Certificate No It is important to understand that the existence of this document alone does not automatically constitute authority to install the part component assembly Where the user installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user installer ensures that his her airworthiness authority accepts parts components assemblies from the airworthiness authority f the country specified in Blockl Statements in Blocks 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations the user installer before the aircraft may be flown Form 8130 3 6 01 Installer must cross check eligibility with applicable technical data NSN 0052 00 012 9005 RECORDS TAG NOMENCLATURE Jro GQ 0424 EE mg nl DATE Q 72 ETF NUMBER j3 755 72 C 72 5 oz S Installation Data 2 Os gt O S S F e CD e
41. cified in s assurer que l autorit de navigabilit dont il rel ve accepte les produits ou les travaux de maintenance de l autorit de navigabilit eer Me ele d ensures that his her Airworthiness Authority accepts products or maitenance from the Airworthiness Authority indiqu e la case 1 3 Les nonc s des cases 14 et 19 ne sauraient constituer une certification du montage Dans tous les cas le dossier technique 2 Statements 14 and 19 do not constitute installation certification In all cases the aircraft technical record must contain an installation l a ronef dait renfermer une certification de montage d livr e conform ment la r glementation de l tat d immatriculation et ce avant Certification issued in accordance with the national regulations of the state of registry before the aircraft may be flown que tout vol puisse avoir lieu 24 0078 2003 10 PRWCJRS3 6932 E 2005 03 Pratt amp Whitney Canada Cie Liste de v rifications du moteur s rie PT6A 2 Pratt amp Whitney Canada Pratt amp Whitney Canada Corp 22 Pratt amp Wh itney Can a fil a E E eed Li nci ts de United Technologies United Technolagies Company 1000 Marie Victorin Una soci t de United Technologies A United Technologies Company 7007 Chemin De La Savane ng Ist Longueui Qu bec St Hubert Quebec Canada J4G 1A1 Canada J3Y 3X7 P amp WC 9442 2003 11 Liste des pieces
42. de suivi du formulaire Form Trackina No TCAC 24 0078 Mh AP TIE AI EE Davs LAIT UI ALULI LILI LICET ENGINE SERVICE AND MAINTENANCE RECORD 1 Heec RE TIME SINCE TIME RUN DATE OVERHAUL INST ALL ATIONS INSPECTIONS REPAIRS USTMENTS MODIFICATIONS i se Fa NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED F OR nes ACE LETE EN TRIES DRAW A DIAGONAL LINE THROUGH UNUSED LINES IN DATE AND TIME COLUMNS E BE m pu i y a3 L H BROUGHT FORWARD C Ee Gates Dei HE c __ NE THEE Lr s n JEN Bn n L m E run Eat d rrr m TO FEL _ L 5 E om u PS n 2 Engine Logbook WO 4955 N157SL 12 Jun 2010 LICENCE NUMBER N157SL Piaggio P 180 Avanti II S N 1116 Linie 3981 8 A irframa anmrlinnme 3015 2 Engine Hours 4909 0 2 Engine Cyc Lndgs 3670 Complied with the Following Items Pratt amp Whitney PT6A 66 S N PCE RK 0125 Complied with Comply with Applicable Portions P amp W Periodic Inspect Guide Engine 2 Complied with P3 Air Filter inspection Engine 2 Complied with Power Turbine Blade Inspection Engine 2 Complied with Fue Pump Inlet Screen Ins
43. ded with the part Tear down report workorder IF APPLICABLE Conduct random sampling of standard hardware and Inspect for conformity Part Preserved If applicable No sign of contamination 5 Part Description pe he NENT 7 Part Number 43 S Serlal Number der LUE Za Hours s MEG Q3 Cycles 7 CEP DAE LE o ker PART REJECTED Inspector Initials me Re nl ETE REASON FOR w inspector Signature Date signed 6 ee d Revison Original This farm 15 to only be used by Avantalr Inc Form 86 800 Bevlslan Date June 3 2008
44. e utills s s curit Approved desig ala and are in condition for safe operation Le pr sent bon certifie que moins ame apparaissant la zase 13 le travail indiqu la case12 et TR d crit la case 13 t effectue conform ment au RAC 571 ES Des donn es de conception indiqu e Certifies that except where otherwise specified in block 13 the work identified in bock 12 and described in block 13 Non approved design data k 1 was performed in accordance with CAR 571 20 Autoris e Authorized Signature 21 R f d autorisation Authorization Ref No AMO 20 00 llla 15 Signature 16 R f approbation Approval m Naps de or Printed imprim Name Typed or Printed 18 Date 22 dactylographi amp ou impri SVCE CENTRE 6 Le monteur doit contre v rifier admissibilit avec les donn es approv es Installer must cross check eligibility with approved data 1 Le pr sent document n autorise aucunement le montage de la pi ce 1 This document does not constitute authority to install the part 2 Si le monteur se base sur la r glementation nationale d une autorit de navigabilit autre que celle indiqu e la case 1 il doit 2 Where the installer works in accordance with the national regulations of an Airworthiness Authority other than the Authority spe
45. er performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user installer ensures that his her airworthiness authority accepts parts components assembli s from Ihe airworthiness authority of the country specified in Black 1 Statements in Block 14 and 19 do not constitute installation certification in all cases aircraft maintenance must contain installation certification issued in accordance with the national regulations by the user installer before the aircraft may be flown Form 8130 3 6 01 Installer must cross chack eligibillty with applicable technical data NSN 0052 00 012 9005 Robbed Parts Form DEFECTIVE PART INFO AUTHORIZATION REQUIREMENTS Aircraft No JO Station Dai 229 Et ROB Control No FEQ A 02 56 26477 Defective Part Name v El Tv Defective Part PIN B3 gt S ES 57 ES eent EE a a e Authorizing Duty 5 Name Please Print 75 Do o en Lente V Ai Won Discrepancy SANY SCH Requested A D E eeng E Please Print ork Order p s ROBBED FOR AND INSTALLED Accomplish visual check of part for damage or ASSY 5 Part
46. gine Filter Inspection Engine 2 32 004 Complied with 790009 Engine Magnetic Chip Detector Inspection Engine 2 Maintenance Notes Complied with The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are file with Avantair Inc s Quality Assurance Department 575 Aviation Dr Camarillo CA 93010 Phone 805 383 1100 s SP Fax 805 383 2037 0 NI47SL SERIAL 1083 _ 1222 14791 8 _ DATE 62209 Pratt amp Whitne CSN 4031 ees Ee ENG TSN 4303 1 TSO 229 9 70007 CRuthorized gt gt hol em TOTAL THIS PAGE TOTAL FROM PREVIOUS SUMMARY MAXIMUM HOURS BETWEEN OVERHAULS HOURS TOTAL SINCE MFG in ly ENGINE SERVICE AND MAINTENANCE RECORD wi H e dm m M ru ME EUN TIME SINCE OVERHAUL INSTALLATIONS INSPECTIONS REPAIRS ADJUSTMENTS MODIFICATIONS ER NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE t e e ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE A 1 i
47. his document does not constitute authority to install the part 2 Si le monteur se base sur la r glementation nationale d une autorit navigabilit autre que celle indiqu e la cese 1 il doit GE e works in accordance with the national regulations of an Airworthiness Authority other than the Authority specified s assurer que l autorit de navigabilit dont il rel ve accepte les produits ou les travaux de maintenance de l autorit de navigabilit block 1 the installer ensures that his her Airworthiness Authority accepts products or maitenance from the Airworthiness Authority indiqu e la case 1 specified in block 1 3 Les nonc s des cases 14 et 19 ne sauraient constituer une certification du montage Dans tous les cas dossier technique de 2 Statements 14 and 19 do constitute installation certification In cases the aircraft technical record must contain an installation l a ronef doit renfermer une certification de montage d livr e conform ment la r gtementation de l tat d immatriculation et ce avant Certification issued in accordance with the national regulations of the state of registry before the aircraft may be flown que tout vol puisse avoir lieu 24 0078 2003 10 P amp WCJR3 6932 E 2005 03 1 Autorit de l aviation du pays d approbation pays Approving national aviation authority country Transports Transport Canada Canada 4 Organisme Organization BON DE
48. hitney PT6A 66 S N PCE RK 0125 6 000 COMPLIED WITH APPLICABLE PORTIONS OF P amp W PERIODIC INSPECTION GUIDE ON 2 ENGINE LAW P amp W MM 72 00 00 3 N de SUIVI QU TOrImureme 7 a wnn risen 6 001 with 720007 Air Filter Inspection Engine 2 6 002 Compliad with 720011 Power Turbine Blade Inspection Engine 2 6 003 Complied with 790005 Engine Filter Inspection Engine 2 6 004 Complied wiih 790008 Engine Magnetic Chip Detector inspection Engine 2 6 005 Complied with 790011 Engine Magnetic Chip Datactor Bridge Inspection Engine 2 The maintenance was performed accordance with Plagglo Pratt amp Whitney and Hartzell maintenance and component manuals The Alrcraft Alrframe Engines Propellers or Appliances stated above was repaired and inspected accordance with current Federal Aviation Regulations and is approved to return to service Pertinent detalls are on file with Avantair inc s Quality Assurance Department EL Camarillo CA 93010 Phone 805 983 1100 Fax 905 383 2047 h LL g D lt D C 2 C B e ES 4 j Signed ForAvantair Inc 74 aviation du pays d approbation pays MM D m MAXIMUM HOURS BETW TOTAL FROM DON HOURS PREVIOUS SUMMARY TOTAL SINCE MFG D 1 Autorit 10 3 N suivi du formul
49. icate No CFE me 4 Signature IGOR976N 23 Date m d y NATHAN LONG May 18 2010 User Installer Responsibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the part component assembly Where the user installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user installer ensures that his her airworthiness authority accepts parts components assemblies from the airworthiness authority of the country specified in Block 1 Statements in Block 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user installer before the aircraft may be flown FAA Form 8130 3 6 01 Installer must cross check eligibility with applicable technical data NSN 0052 00 012 9005 22222221222 Robbed Parts Form Receiving inspection Checklist l DEFECTIVE PART INFO AUTHORIZATION REQUIREMENTS completed by ourhorized personnel only Date 6 0 Aircraft No V 225 station __ Date 25 0 Inspector Name f Defective Part Name 6o V Facility i NE MM Defective PIN S 270 ROB C
50. is Installation Remarks Maintenance Overhaul Facility Work Order amp inspection Stamp Reference Engine Module When Material Installed Engine Module Engine Module Eng Module SN When erial No TEN When Material Material Installed Removed Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part re CNN g 2 Pratt amp Whitney Canada Prat amp ra Canada Corp Historique des piece a du ree de limit e Une soci t de United Technologies A United Technologies Company 1959 Marie Victorin a i ongueuil Qu bec Canada Life Limited Parts History Record 450 677 9414 Centre de revision P amp WC JR3 8904 F 2007 05 Service Center D signation de la pi ce N de bulletin de vente Part Name Sales Order No 155100 mis le A M J Issue Date Y M D 2008 10 31 Temps depuis neuf Cycles depuis neuf Time Since Cycles Since New 3 059 Code de traitement thermique Heat Code LASWY N de s rie du
51. ontrol No AE PACE T 2689 2 the packaging of the part identifies the supplier distributor and is free from alteration or damage Defective Part 5 HI SUA DE M 4 Packaging slip identifies vendor and type name of parts endosed 3 Authorizing Duty cintas denter vendor dere 570 22 576 3 Parts adequatley packaged prevent damage during shipping S 550 02 5 50 226 2 _ Manager s Name _ x 6 Gei 0 E AJ NN Verify actual part and accompanying documentation reflect the same information csN 7574 T M CSO T d Es Please Print Part numbers match Serial numbers match Discrepancy 220 2 74 LS 2 9 Verify Authorized Release Certificate is properly filled out and Work Order 2 60 7 AJ 2 SL am Requested By Please Print siened as well as traceable to FAA approved source hafif irc times and or cycles identified on Tag Form IF Verify that the fife limit or inspection interval has not expired APPLICABLE ROBBED FOR INSTALLED ON 07 visual inspection of the part locking for obvious defects damage 9 07 000 RAS mandags or data plates have not tampered With or altered ED Aircraft Ne ASSY Name tz 4620 25 Accomplish visual check of part for damage i my ronthe Authorized Release Certificate are e Se verify
52. pection Engine 2 Complied with Engine Oil Filter Inspection Engine 2 REPLACED 2 PROP GOVERNOR IAW P amp W 61 20 00 SEE 093842 P N 8210 411 S N OFF 14183431 PN ON 8210 411 SN ON 13751674 REPLACED 2 ENGINE DRIVEN FUEL PUMP IAW P amp W MM 73 10 02 SEE AML 093842 PN OFF 3040760 SN OFF 0149 825601 5 SN ON 1806 REPLACED 2 FUEL CONTROL UNIT IAW P amp W MM 73 20 00 SEE 093842 PN OFF 3120832 04 SN OFF 13991223 PN ON 8063 016 SN ON 2482012 The above maintenance was performed in accordance with Piaggio Pratt amp Whitney and Hartzell maintenance and component manuals The Aircraft Airframe Engines Propellers or Appliances stated above was repaired and inspected in accordance with current Federal Aviation Regulations and is approved to return to service Pertinent details are on file with Avantair Inc e Quality Assurance Department Certificate Number V2JRO78L 4311 General Howard Drive Clearwater FL 33762 Phone 727 539 0071 Fax 272 539 7007 TOTAL THIS E m TOTAL FROM MAXIMUM HOURS BETWEEN OVERHAULS PREVIOUS SUMMARY TOTAL SINCE HOURS Autorit de l aviation civile Pays qui approuve le bon de sortie Approving Civil Aviation Authority Country Transport Canada BON DE SORTIE AUTORIS E AUTHORIZED RELEASE CERTIF ICATE 3 de suivi du formulaire Form Tracking No 81488418 00000
53. peed Governor NEW 3023059 3072811 01 N A Limiteur de couple Torque Limiter Valve de mise en drapeau automatique Auto Feather Valve G n rateur de tachym tre N A Tach Generator Livret Section Motrice Quantit Quantity Couleur Colour Type Power Section Log Book 1 YELLOW CAN Section du g n rateur do gaz N de s rie sur la plaque Bon de commande 159367 Gas Generator Section Signal tique Sales Order Unit s n s de s rie Serialized Units N de pi ce Part Number N de s rie Serial Number TSN TSO Remarques Remarks Compensateur de temperature N A Temperature Compensator id a Seit 825601 5 5873 2 0149 TSO 441 8 AS RECEIVED R gulateur de carburant AS RECEIVED changeur thermique 5 Oil to Fuel 50 229 9 iind N A changeur thermique N A Fuel to Oil Cooler Commande de d marrage N A Starting Control R gulateur d allumage haute nergie NOT RECEIVED lanition Requlator Exciter Vanne de d charge compresseur f S cameo ete 3059835 01 AHX001911 80 229 9 Vanne de d charge compresseur N A Compressor Bleed Valve Diviseur d bit soupage de d charge CEIVED Flow Divider Dump Valve 9959524042 150 229 9 3038242 PWCO8L2678 AS RECEIVED Check Valve Livret g n rateur de gaz moteur Quantit Quantity Couleur Colour Type Gas Generator Engine Log Book 2 YELLOW CAN
54. plicable Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the engine module logbook where this part is ie 1 Ln 4 Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Pratt amp Une soci t de United Technologies A United Technologies Company 7007 Chemin De La Savana St Hubert Quebec Canada J3Y 3X7 Liste des pi ces remplac es List of Parts Replaced ossier qualit Quality Record 3 RWC JR3 6934 E 6934 2004 10 Date 31 Page Serial No Model ales Order No Customer RK0125 PS PT6A 66 155100 __ Avantair N de la pi ce Part No Designation de la pi ce Qt Non Fact art Description Qty Not Chrg NEW 3004589 RING RET 2 215 GAGE DIA 1 3023059 WASHER SLTD PWR TURB SHAFT 1 3032995 STRAINER IC 3 3039526 GASKET PROP GOV MTG 1 3039718CL09 SEAL AIR POWER TURBINE ROTOR 1 3043825 01 WIRING HARNESS T5 THERMOCOUPLE 1 3059925 01 GEAR SET PLANET FIRST STAGE REDUCTION 1 3059927 01 GEAR RING FIRST STAGE REDUCTION 3059928 01 GEAR SET SUN FIRST STAGE REDUCTION 1 3100027 01 SEAL RING NON METALLIC 1 3100027 02 SEAL RING NON METALLIC 1 3106808 01 SPACER ADJUSTING 1 3116132 01 THERMOCOUPLE IMMERSION T5 10 3117607 01 RING RETAINING 1 AK66S 60 Kit Assy 665 65 Kit Assy 1 AK66S 70 Kit Assy 1 AK66SPK Kit Assy 1 MS9193 04 NIPPLE TUBE 1 REPAIR 3108028 01 INSUL BLANKET
55. red B Y jv Verify that any documents referenced onthe Authorized Release Certificate are included with the part Tear down report workorder etc IF APPLICABLE nduct random sampling of standard hardware and inspect for conformity art Preserved if applicable No sign of contaminatlon Part Description 2 j Jen d Senso Part Number zeit 5 4s 3 rd Seriol Number OUTS Cycles PART ACCEPTED inspector initials 2 2 ef PART REJECTED inspector initials REASON FOR REJECTION j inspector Signature Date signed Ferm AA 86 800 erify actual part and accompanying documentation reflect the same information Ravison Original Revision Date June 3 2008 ter eis DEFECTIVE PART INFO Robbed Parts Form AUTHORIZATION REQUIREMENTS Aircraft No N 3651 Station HUE 4 38 10 Defective Name Jii Proco Defective Part P N 545 01 Defective Part am AS HEN Discrepancy ifj Ne indico Work Order d EEN ROBBED FROM Er P CE RKO 019 5 RTE ASSY Name Work Order 900 Part E or Part Name Oil Proba _ ASSYSIN 00 Part No 3045 45 01 _ NEM sn 5 Station HIE e Date y 99 10 2 Cert Ces 3 REPLACEMENT FOR ROBBED PART Signatur Part Number 3045 459 9 csn oO Station T amp ofra _
56. tandard equipment as listed in the P amp WC Illustrated Parts List except as noted Berceau Cradle GOOD herein Manchon Sleeve NEW N de s rie du conteneur de m tal Metal Container SN Client Customer Mod le de P amp WC Model PT6A 66 Section Motrice de s rie sur la plaque Bon de commande 159367 Power Section signal tique Sales Order No Remarques Remarks Unit s n s de s rie Serialized Units N de pi ce Part Number N de s rie Serial Number TSN TSO R gulateur d h lice R gulateur de turbine de puissance N A Power Turbine Governor R gulateur survitesse d h lice N A Propeller Overspeed Governor Limiteur de couple Torque Limiter Valve de mise en drapeau automatique N A Auto Feather Valve G n rateur de tachym tre Tach Generator Livret Section Motrice Quantit Quantity Couleur Colour Power Section Log Book 1 YELLOW CAN Section du g n rateur de gaz N de s rie sur la plaque Bon de commande 159367 Gas Generator Section Signal tique Sales Order No Unit s n s de s rie Serialized Units de pi ce Part Number N de s rie Serial Number TSN TSO Remarques Remarks D Compensateur de temperature N A Temperature Compensator Pompe carburant R gulateur carburant Fuel Control 8063 016 AS TSO 441 8 AS RECEIVED changeur thermique Oil to Heater WA21195 80 229 9 AS RECEIVED changeur
57. thermique N A Fuel to Oil Cooler N A NOT RECEIVED Commande de d marrage Starting Control R gulateur d allumage haute nergie tanition Reauiator Exciter Vanne de d charge compresseur Compressor Bleed Valve 3059835 01 001911 TS0 229 9 AS RECEIVED Vanne de d charge compresseur N A Compressor Bleed Valve Diviseur de d bit soupage de d charge Clapet antiretour NI CHE UAE 3038242 PWCO8L2678 AS RECEIVED Livret g n rateur de gaz moteur Quantit Quantity Couleur Colour Type Gas Generator Engine Log Book 2 YELLOW CAN Remarques Remarks NOTE 3 YELLOW LOGBOOKS IN WHITE BINDER VERTE par nom Checked ouf by name amp sam CLIFFORD ANCTIL 98 31 07 09 MARTIN PROVENCAL SC218 31 07 09 Sans objet NR Non regu SL Non exp di TSN Temps depuis neuf TSO Temps depuis r visions Not Applicable Not Received Ship Less Time Since New Tine Since Overhaul D d ENGINE SERVICE AND MAINTENANCE RECORD E TIME SINCE TIME RUN OUERHH INSTALL ATIONS INSPECTIONS REFAIRS ADJUSTMENTS MODIFICATIONS EN TRIES DRAW DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS DATE NOTE USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE BROUGHT Pm FORWARD Em Cem EE LX MN M m e a
58. vision level revision levels for a given part number are fully interchangeable The part s revision parfaitement interchangeables Le niveau de revision d une pi ce n est pas requis pour ce certificat is not required for this certification 7 138 Le pr sent bon de sortie certifie que les articles indiqu s ci dessus ont t construits conform ment Certifies that the items identified above were manufactured in conformity to perd 1 10 certification apr s maintenance CAR 571 10 Maintenance Release des donn es de conception approuv es ot qu ils peuvent tre utilis s en toute s curit Autre r glementation Pr sisde g la case 12 specified in block 12 approved design data and condition for safe operation Le pr sent bon de sortie certifie que sauf indication 2 ego 12 le travail indiqu case 11 et d crit case 12 t effectu conform men am ment de l aviation Certifies that unless others in block 12 the work identified in block 11 ame been performegumeerriBliance with the Canadian Aviation Regulations 19b Signature 13c Num ro de l organisme agr 14b Signature 14c Num ro de l organisme agr i f 6 G i Approved Organization Number vm KZ Approved SON Number 122 4 58 S O 13d Nom des donn es de Dn non
59. z Pratt amp Whitney Canada Prati amp Whitney Canada Corp Historique des dur e de vie limit e Une soci t de United Technologies United Technologies Company Canadi Life Limited Parts History Record dat Centre de revision P amp WC JR3 6904 2007 05 Service Center D signation de la pi ce Code de traitement thermique le A M J N de bulletin de vente Part lame SS Code 1 Issue BAS Y M D Sales Order No Service DISC TURBINE LASWY 2008 10 31 155100 Overhaul Manuel amp R vision Manual amp Revision SB14002 REV 18 N de s rie du mafl Temps depuis Cycles depuis neuf forg Forging Mat Serial Time Since New Cycles Since New Num ro du mat riel N de s rie du mat riel Material Number Material Serial No 3037312 AO01KRNT Timbre du v rificateur Inspection Stamp 1026 4 073 2 3 059 Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data Observations Installation d entretien r vision bon de travail et timbre du v rificateur R f rence Cycles depuis Temps depuis neuf neuf l installation du N de s rie du l enl vement mat riel moteur module du mat riel Temps depuis neuf l installation du mat riel Cumul jusqu pr sent Total Accumulated To Date Cumul de cette installation Accumulated Th
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