Airplane 414 N8222Q Aircraft Log Nov-23-2012
Contents
1. LA 2308 0 2 60 Yo 50 xe 16 a 4 O mem T 50 NOMENCLATURE TET ALTIMETER PRESSURE 3 7 OOO Fee TEST INDICATOR READ INGS AT 25 C poy 25 C d d i INDICATOR READ INGS AT 25 Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of RECORDING TODAY S TOTAL Technician or Repair Facility See back pages for other specific entries FLIGHT TIME IN SERVICE 21 41 Transponder tests amp Inspections as required by FAR 2 Altimete Altimeter Signature Date NU WM C Z RADIO SHOP PUN APPROVED CRS FU RS33K LAFAYETTE LOUISIANA 70509 5 82220 en ud MR e reporting equipment ond z 4 Sie System tected as required Dy FAR ot A11 ormai H FAR amp 3 Appendix Para e AA ZZ THE RADI G SHOP LAFAYETTE ENAN n Blind 550 120 SRA Lio RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of SERVICE Technician or Repair Facility See back pages for other specific entries Aircraft 2220 Cesna4ld Serial 0152 Hobbs 0258 6 Date 02 10 10 W O 1174 Installed overhauled Tac2. VS VSV 3100 L3VHOHIV 2 psepuels au lt WE bl t 9107 833 pomg lyg Aircraft Record General Information 1771 Date of Manufacture Engine s currently installed Manufacturer _ Manufacturer Propeller s currently installed Manufacturer HUB 0 Serial Blade Model Serial Blade Model Serial Serial Serial Serial Serial Serial Current Weight and Balance Information Date 2 2 2 2 certify that this aircraft weight and balance has been preformed this date as equipted New Aircraft Weight New Aircraft C G YIYS 3 Sg 9s Charles Roberts AP 488366 56 C hanbe gt AP S Haltom Qincraft Devices 5007 Hangar Denton JX 76207 940 887 1818 N 8222Q Hobbs 1029 3 Date 11 15 06 4173 5 1 Inspected aircraft 414 inspection checklist Removed right hand engine to facilitate overhaul by Custom Airmotive of Tulsa OK Reinstalled engine after overhaul Replaced engine mounts p n J9613 58 and bolts Replaced air filter p n 202831 on both engines Due replacement at Hobbs 1529 3 Installed rear striker bar p n 5012042 2 Replaced ELT battery Function tested per FAR 207 91 Due replacement December 2008 Replaced existing intercom system Replaced vacuum filter p n 09 14 3 Installed Cessna kit SK4148E for landing gear mod on both
3. for obvious damage verify part number attach appropriate documents RECEIVING INSPECTION Pending 10 Start Complete III 20 Disassemble Clean Evaluate and inspect for hidden damage Define scope of work Pending Start Complete TTT 1 amp ABOVE 30 and Above Details Start Complete Aerospace Turbine Rotables Inc 3414 W 29th St South Wichita KS 67217 US Ph 316 943 6100 Fax 316 943 2917 To Ship To PREFERRED AIRPARTS PREFERRED AIRPARTS PO BOX 12 11234 HACKETT RD 11234 HACKETT RD KIDRON OH 44636 KIDRON OH 44636 UNITED STATES UNITED STATES Need Date 10 19 201 Ref R42331 Phone 800 433 0814 Descr STROBE POWER SUPPLY Mfg HGL Code 12559 PN 30 1172 1 SN 4359 Ship Via UPS REGL Sched Date Qty 1 00 Cust PN Mfg SN 890 Ship Acct 499771 Container 40 Perform required workscope requisition parts and assemble in accordance with approved data IN PROCESS Pending Start Complete 23545 2354 Aerospace Turbine Rotables Inc 3414 W 29th St South Wichita KS 67217 us Ph 316 943 6100 Fax 316 943 2917 To PREFERRED AIRPARTS PO BOX 12 11234 HACKETT RD KIDRON OH 44636 UNITED STATES Ref R42331 Phone
4. Replaced LH main tire using 650 10 ply Air Hawk I certify that the maintenance Preventive Maintenance Inspection or Alteration was performed as described above and that I am authorized to release this aircraft for return to service Further I certify that the above work was performed in accordance with current Federal Aviation Regulations and applicable Technical Data as required by FAR Part 43 All items required to be inspected were inspecte by an authorized person that determined the work was Satisfactorily completed and no known conditio exits that would make the aircraft unairworthy and so far as the work or reference work is concerned the aircraft is approved for return to service Details of work performed on file under Work Order No 1710 Certe 1175062 AP Name Global Executive Jet Maintenance 120 Olmsted Way 5 Monterey CA 93940
5. To Ship To PREFERRED AIRPARTS PREFERRED AIRPARTS PO BOX 12 11234 HACKETT RD 11234 HACKETT RD KIDRON OH 44636 UNITED STATES KIDRON OH 44636 UNITED STATES Ref R42331 Phone 800 433 0814 Descr STROBE POWER SUPPLY Mfg HGL Need Date 10 19 201C Code 12559 PN 30 1172 1 SN 4359 Ship Via UPS REGL Sched Date Qty 1 00 Cust PN Mfg SN 890 Ship Acct 499771 Container 50 Functional Test TEST Pending Start Complete Measurements INPUT VOLTAGE 9 23555 2355C LOAD FPM 52 STROBE VOLTAGE STROBE INTENSITY 7 OSCILLOSCOPE TESTS 4 20 INSPECTOR T DATElac 1 9 2016 FINAL INSPECTION Pending 60 Inspection review of all work performed all test results content and approved data Make airworthiness determination and release product for return to service Start Complete 285 6C RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE Technician or Repair Facility See back pages for other specific entries AIRFRAME LOGBOOK ENTRY Aircraft Reg A C Make Model Date A F Hours Eng 1 Hrs Eng 2 Hrs A F Cycles Eng 1 Cycl Eng 2 Cyc Cleaned amp Serviced nose gear strut note some leakage noted
6. 44 04 0 NE 10512 CLIP K 21 03 0 NE CL052 CLIP K 21 04 0 NE ECG130 TRANSISTOR SK3027 1 08 07 1 NE MCR1906 6 SCR CS39 4D K 25 03 1 NE MR501 DIODE 1N5401 K 26 03 0 NE RC 880 SCR SK3578 11 08 TEST Functional Test Start Signature Stamp Complete SD Milli Measurement INPUT VOLTAGE 28 LOAD 3 STROBE VOLTAGE 0K STROBE INTENSITY 6 7 9 OSCILLOSCOPE TES 60 INSPECTOR FER Inspection review component Review all work performed content embodied amp data used in the MRO cycle Make airworthiness determination amp release the product for return to service if appropriate FINAL INSPECTION amp MAINTENANCE RELEASE lil Imut Signature Stamp Complete uoz 6 0 833 34600C Manuals used to service this unit e ESR MD30 1 Rev 2 Date 6 1 1979 Cc 76 08 02 R2 0 AMENDMENT 39 4540 CESSNA Rev Date 1 31 1983 30 0515 33 0009 Rev C Date 6 25 1975 1 Approving National Aviation 3 Form Tracking Number Authority Country AUTHORIZED RELEASE CERTIFICATE FAA FORM 8130 3 AIRWORTHINESS APPROVAL TAG 4 Organization Name and Address Aerospace Turbine Rotables Inc 5750 FAA UNITED STATES 3414 W 29th St South 5 Work Order Contract or Wichita KS 67217 Invoice Number us Ph 316 943 6100 Fax 316 943 2917 WO336 FAA Approval Holder NV2R045L TT Number 7
7. 800 433 0814 Descr STROBE POWER SUPPLY Ship To PREFERRED AIRPARTS 11234 HACKETT RD KIDRON OH 44636 UNITED STATES Mfg HGL Need Date 10 19 2010 Code 12559 PN 30 1172 1 SN 4359 Ship Via UPS REGL Sched Date Qty 1 00 Cust PN Mfg SN 890 Ship 499771 Container Qty CD PN Description 0 NE RC 880 SCR SK3578 177 MR501 DIODE 1N5401 17 NE MCR1906 6 SCR CS39 4D 0 NE ECG130 TRANSISTOR SK3027 NE CL052 CLIP 0 NE CL0512 CLIP 2 NE AEC1001 4 CAP 55 0339 321G2C2 1 NE 87F5048 CAP 10UT 50V 70K8846 1 65F2366 CAP 74 150D35V6 8 1 NE 61 0981 1 DECAL WARNING 0 600D126F075KDA KD4 lt 55 0276 1 TRANSISTOR 1 NE 55 0221 1 FLASHTUBE 0 NE 55 0073 5 TRIGGER COIL 477 NE 501H47W224KQ4 TRIGGER CAP 0 NE 47F149 TRIG 75 225P400V0 22 1 NE 39D228G025HP4 CAPACITOR 18F2639 A am NE 31 3791 1 SPACER 177 31 2401 1 DECAL TRIGGER PE NE 31 2106 1 INSULATOR 0 NE 31 1723 7 PLATE 17 NE 2N4893 TRANSISTOR 0 NE 2N4870 TRANSISTOR NTE6410 0 NE 2N3055 TRANSISTOR A NE 27F779 FUSE HOLDER 67K0263 0 25 0491 1 LENS 0 NE 1N645 DIODE 526 NTE116 1 NE 1N5399 RECT 512 1N5399 0 NE 1N4754A ZENER 78 1N4754A 17 1 4752 2 0 NE 1N4007 DIODE 78K2222 47 NE 173 9 320P INSULATOR 4677843 0 NE 01 80VDC CAPACITOR 1872528 Aerospace Turbine Rotables Inc 3414 W 29th St South Wichita KS 67217 US Ph 316 943 6100 Fax 316 943 2917
8. 1 WORK ORDER Metro Aircraft Instruments Inc 2135 Airport Rd Oakland County Int l Airport Waterford MI 48327 1207 248 666 3670 Customer PREFE PREFERRED AIRPARTS Cust RO 841312 Step READY FOR SHIPPING TSO 0 00 P N 512 01 TACH IND DUAL W SYNC SN 5833 Reason Rm SYNCHRONISER IS NOT WORKING PLEASE INSPECT AND QUOTE FOR OVERHAUL Date Reqrd Date Estmtd Nov 13 2009 Preliminary Inspection Date Nov 6 2009 NO EXTERNAL DAMAGE Pre Test Yes No Y 3 2009 UNIT IS OPERATIONAL EXCEPT FOR SYNCHRONISER _ Date Dec e FAA CRS NO JY2R943K WORKORDER 123174 09 Dept CUS Location BRYAN Warranty Code 00 360 Goodthru AD Mfg INST INC POINTER TRAVEL IS SLUGGISH Teardown Findings NORMAL DIRT AND WEAR SYNCHRONISER INOP DUE TO CORROSION BUT REPAIRABLE Technician ST 270 Date Dec 4 2009 Final Inspection Before Assembly Date Dec 7 2009 Corrective Action OVERHAULED OVERHAULED AND TESTED USING MANUAL 86M087 CESSNA P N C668016 0101 Date Dec Technician ST A Final Inspection Technician STEVEN THOMPSON 7 2009 Inspector GG Inspector GREGORY GARZA 2463291 Parts Detail Line Part Number Description WCD RmvCde Qty Serial Number 1 SSR 2ZZR d BEARING _ MAINTENANCE RELEASE RECORD The component identified above was OVERHAULED in accordance with the current regulations of the Federal Aviation Administration and i
9. C INGS AT 25 THE RADIO SHOP FAA APPROVED CRS FU2R833K LAFAYETTE LA ma RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE Technician or Repair Facility See back pages for other specific entries ATC Transponder tests amp Inspections as required by FAR Altimeters tested as required by FAR 91 411 91 413 IAW FAR 43 Appendix F have been performed IAW FAR 43 Appendix E Para b Transponder Model G7 X 5 2C 5 9 0 07 Pilots 5 7 EA 4 S N 9 Transponder Model Copilots 2 ZY d Y a 2 24 2 Signature amp Date ignature amp Date THE RADIO SHOP THE RADIO SHOP FAA APPROVED CRS FU2R833K N amp 222 Q FAA APPROVED CRS FU2R833K LAFAYETTE LOUISIANA 70509 LAFAYETTE LOUISIANA 70509 Automatic Pressure altitude reporting equipment and Static System tested as required by FAR 91 411 IAW FAR ATC transponder system integration test performed 43 Appendix Para a IAW FAR 43 Appendix E Par C W O No Z x P Signature amp Date Signature amp Date THE RADIO SHOP Bnd ENCODER THE RADIO SHOP y eto FAA APPROVED CRS FU2R833K FAA APPROVED CRS FU2R833K 2 __ LAFAYETTE LOUISIANA 70509 552 20 Sy SRA EE LOUISIANA 70509 A pe 2 AUTHORIZED RELEASE CERTIFICATE ority Country FORM 8130 3 AIRWORTHINESS A
10. Service Other regulation specified in Block 13 Approved 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 E described Block 13 was accomplished accordance with Title 14 Code of Federal Regulations part 43 and in respect to that work the items are approved for return to service J Non approved design data specified in Block 13 45 Authorized Signature 46 Approval Authorization No 21 Approval Certificate No NV2RO045L 17 Name Typed or Printed 22 Name Typed or Printed STEVEN L STARK User Installer Responsibilities 23 Date m d y Feb 03 2011 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 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 Statement 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 regulat
11. lt STROBE POWER SUPPLY 13 REMARKS Overhauled and certified IAW the documents listed Manual ID MD30 1 Revision 2 Revision Date 6 1 1979 Full details of work performed held on work order Manual ID 76 08 02 R2 0 AMENDMENT 39 4540 CESSNA Revision Revision Date 1 31 1983 Manual ID 30 0515 33 0009 Revision C Revision Date 6 25 1975 The work specified in Block 12 13 was performed in accordance with EASA Part 145 and with respect to the work the aircraft component is considered ready for release to service under EASA Approval Certificate EASA 145 4033 14 Certifies the items identified above were manufactured in conformity to 19 14 CFR 43 9 Return to Service Other regulation specified in Block 13 ertifies that unless otherwise specified in Block 13 the work identified in Block 12 and escribed in Block 13 was accomplished in accordance with Title 14 Code of Federal Non approved design data specified in Block 13 egulations part 43 and in respect to that work the items are approved for return to service Approved design data and are in a condition for safe operation 15 Authorized Signature 16 Approval Authorization No 40 Authorized Signature 21 Approval Certificate No NV2R045L v 17 Typed or Printed 18 Date m d y 23 Date m d y STEVEN L STAR Oct 19 2010 User Installer Re ponsibilities It is important to understand that the existence of this document alone d
12. sides Installed Vortex generator per STC SA00024SE Replaced cabin door cables and forks Replaced seal p n R581535 around baggage area on both nacelles Replaced vacuum filter socks p n B3 5 1 Replaced tail rotating beacon bulb p n 02 0350433 01 AD 76 13 07 Due ACTT 5000 0 hrs AD 90 02 13 Due ACTT 5054 0 hrs AD 00 01 16 C W para b visual inspection para c due Feb 2009 para d due Hobbs 1341 0 para e by pressure test due again Nov 2007 para g right engine C W by repair by Aerospace Welding para g left engine due at engine overhaul certify this aircraft has been inspected in accordance with an annual inspection and was determined irworthy condition RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE Technician or Repair Facility See back pages for other specific entries JCaftom Derricea 5007 Ra Kangar 8B Denton SX T6207 940 387 1818 N 8222Q Hobbs 1029 3 Date 11 15 06 Removed prop from right side and installed on left side Installed new brush blocks p n RAB40012 as needed certify this prop has n inspected in accordance with an annual inspection and was determined tobei ndition ary Haltom A amp P 22120221 Dewrices 5007 pow Ra Hangar 8B Denton FH T6207 940 987 1818 N 8222Q
13. 05 1 Approving National Aviation Authority Country FAA United States 3 Form Tracking Number 02222011 JA 1 5 Work Order Contract Invoice Number 991399 20014121 10 Quantity 11 Serial Batch Number 100 BATCH 30058754 SN 39422 BATCH 30060766 SN 39423 39473 39475 30060767 SN 39476 39522 102 00007 13 Remarks AIRWORTHINESS APPROVAL Eligibility RESISTANCE TEMPERATURE DETECTOR 14 the items identifed above were manufactured i in conformity t to PI n 197 E 14 CFR 43 9 Return to Service Other regulation specified in X A A 7 i Certifies that unless otherwise specified in Block 13 the work Block 12 Appro veg 22 ud PANES ed uS safe permtion 4 and described i Block 13 was accomplished in accordance with Title 14 Code of pproved degn Gata MOCE AI Federal Regulations part43 and in respect to that worl tfie items are approved for return to service 16 Approval Authorization No SEE 21 Approval Certificate No DMIR 832878 NE 18 Date m d y p d or Printed 23 Date m d y FEB 22 2011 User Installer Responsibilities 120 Authorized Signature 17 Nake Typed or Printed JOHN ALBRECHT It is important to understand that the existence of this document alone does not automatically constitute authority to install the part componen
14. 75 y BATCH 30060767 SN 39476 39522 13 Remarks AIRWORTHINESS APPROVAL 14 Certifies the items identified above were manufactured in conformity to x Approved design data and are in a condition for safe operation Ll Non approved design data specified in Block 13 return to service 16 Approval Authorization No 20 Authorized Signature DMIR 832878 NE 17 y ke Typed or Printed 18 Date m d y 22 or Printed 23 Date m d y JO n ALBRECHT FEB 22 2011 y User Installer Responsibilities It is important to understand that the existence of this document alone does not automatically con stitute 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 Blocks 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain 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 90
15. Hobbs 1029 3 Date 11 15 06 TSO 0 installed overhauled propeller on right hand side Overhaul due in 5 years or 1500 hrs whichever occurs first Installed new brush blocks p n RAB40012 as needed certify this prop has been inspected in accordance with an annual inspection and was determined to be in aipworthy condition 22120221 YEAR RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations 20 TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of err TIME SERVICE Technician or Repair Facility See back pages for other specific entries SCaftom Gift Devdices 5007 Ra Hangar 8B Denton TX 76207 940 387 1818 N 8222Q Hobbs 0 Date 11 28 06 4189 9 7 Replaced hours meter p n 100689 Time at removal was 1045 2 Total aircraft time 4189 9 Replaced both voitage regulators p n VSF7403A sin G092133 amp 509350 Test run aircraft Checked okay led to service for work accomplished Haltom Serrices Brepost Hanger 58 Denton 5 76207 94098728148 Hobbs 10 1 Date 12 42 06 N 8222Q new landing gear motor pin 9910002 3RX s n 3761 Checked gear electrically and Checked Installed new edis pin C 668017 0101RX s n 3476AM accomplished to service for work RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT T
16. IME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE Technician or Repair Facility See back pages for other specific entries JCaftom Devices 5007 Quport Ra Hangar Denton TX 76207 940 387 1818 N 8222Q Hobbs 25 5 Date 12 29 06 AD 04 25 16R1 visually inspected Checked okay Aircraft r tu service for work accomplished fy Haltom A amp P 22120221 2 5 08 82220 SN 0152 AFTT 4309 4 HOBBS 170 2 1 2 3 C W AD 2004 25 16 R1 by visual inspection No defects noted C W AD 2000 01 16 part b c e visual inspection No defects noted C W AD 76 02 07 alternator slip ring inspection AD does not apply to RH engine alternator by model number No defects noted on LH alternator C W AD 95 24 05 on both propellers by visual inspection No defects noted Performed ELT inspection Per 91 207 d Changed Engine oil and Filter PN 7 CH48108 1 both engines serviced with 12 qts aeroshell 100w Repacked RH brake caliper due to leakage 8 Repaired rudder trim rod 9 Replaced aircraft battery SN on GO2373146 10 anlared avxraoen lina fram hottle Vay A111 LLULL UV LLIW to bulkhead 166011 0108 Repaired battery box and painted with acid resistant paint Replaced 2 ea static wicks PN 16165 Replaced both wingtip strobe covers PN 25 0491 1 Repacked all wheel beari
17. NE ASD INSPECTED DK FER FERRY FOUGHT Gene EETERCI Sen Cur OF CSAC Ene moe PAG Description of Inspections Tests Repairs and Alterations TIME IN Entries must be endorsed with Name Rating and Certificate Number of SERVICE Technician or Repair Facility See back pages for other specific entries ACC CK MEETS Een ul Nel ROF EA HAS TO MAKAQA ASD LORS DETER ESE Fee Remtes DATED Hen e CS OG L T Ot _ S TH SDSHELDS COVER gt A lt E s Ae s REPLACED come TODAY S TOTAL FLIGHT TIME IN SERVICE Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility See back pages for other specific entries es sss 2242 ASRR C deck t Fue ub DA SEED eR 2 RUDDER Rams Bears OTH Come e Rus 2 AIRCRAFT HAS SEABED OS OAL A Co pilot c ALTIMETER SCALE ERROR F 2 NOMENCLATURE SERIAL NO ALTIMETER PRESSURE O O9O0f ee BY LL E uc INGS 25 PT FT INGS AT 25 C PT FT INGS AT 25 30 sol 477 5 7 2
18. PPROVAL TAG UNITED STATES Organization Name Adr 3 Farm Tracking Number 3407156 Cessna Aircraft Company PC4 Cesana Parts Ppa Dept 702 Wichita KS 67218 7 Description 8 Part Number BOLT FORK 5243518 3 1173586 12 Status Work d z an 2 a New 4 Cartes the items identfied above were manufactured in conformity to Approved design data sed are in a conditon far tafe operation LI Non approved design daw spacified in Block 13 5 Authorized Signature f 4 Kesh CY Sonya 17 Name Typed or Printed 3 KEITH THOMPSON ODA 001295 r MAR 07 2012 User Installer Responsibilities It is important to understand that Ihe 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 th airworthins thority of the country specified in Block 1 it is essential that the user installer ensures that his her airworthiness authority accepts parts componants assemblies from the airworthiness authority of the country specified in Block 1 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 by t
19. Y2R943K 23 Date m d y GREGORY GARZA 2463291 Dec 7 2009 User Installer Responsibilities It is important to understand that the existence of this Document alone does not automatically constitute authority to install the petia n oe 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 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 Aerospace TURBINE ROTABLES INC 3414 W 29th St South Wichita Ks 67212 US FAA Certified Repair Station No NV2R045L EASA 145 4033 Ph 316 943 6100 Fax 316 943 2917 Certificates and Stamps Technician Signature AETR Work Order Jim 01 05 2011 VVUIT W O Number WO4574 Part Number 30 1172 1 Serial No 1703 Work Type OVERHAUL Printed 1 25 2011 Page Page 3 of 3 FEA o 3 20 Page
20. e Stamp Ili r Qty CD Part Number Description Location 0 NE 01 80VDC CAPACITOR 18F2528 K 01 02 1 173 9 320 INSULATOR 46 7843 26 02 0 1 4007 DIODE 78 2222 02 04 1 1 4752 ZENER K 03 01 0 NE 1N4754A ZENER 78 1N4754A K 03 02 1 NE 1N5399 RECT 512 1N5399 K 04 01 0 NE 1N645 DIODE 526 NTE116 K 04 03 0 NE 25 0491 1 LENS 1 03 10 0 NE 27F779 FUSE HOLDER 67K0263 K 06 01 0 2 3055 TRANSISTOR K 08 06 Aerosp ace VVOTA Uruci TURBINE rs INC W O Number WO4574 Part Number 30 1172 1 Serial No 1703 Work Type OVERHAUL Printed 1 25 2011 Page Page 2 of 3 TAN 3414 W 29th St South Wichita Ks 67212 US FAA Certified Repair Station No NV2R045L EASA 145 4033 Ph 316 943 6100 Fax 316 943 2917 0 NE 2N4870 TRANSISTOR NTE6410 1 04 04 1 2N4893 TRANSISTOR K 09 01 0 NE 31 1723 7 PLATE 1 04 10 0 31 2106 1 INSULATOR K 09 07 1 31 2401 1 DECAL TRIGGER K 10 02 0 31 3791 1 SPACER K 10 04 1 NE 39D228G025HP4 CAPACITOR 18F2639 K 12 05 AN 21 20 0 NE 47F149 TRIG 75 225P400V0 22 K 14 02 1 501H47W224KQ4 TRIGGER 14 03 1 55 0073 5 TRIGGER COIL K 15 09 1 55 0221 1 FLASHTUBE K 16 01 1 55 0276 1 TRANSISTOR 863 2N3055AG K 16 02 0 600D126F075KDA CAP KD4 K 17 03 14 61 0981 1 WARNING 18 04 1 NE 65F2366 CAP 74 150D35V6 8 K 19 03 1 87F5048 CAP 10UT 50V 70K8846 K 19 08 21 AEC1001 4 55 0339 321G2C2
21. h Indicator p n 512 01 s n 5833 ops checked satisfactory work done LAW Cessna 414 maintenance manual Aircraft is approved for return to service for work performed 4 p J 2834843 Date 2 2 Noble Flight Aircraft Services LLCe118 John Glenn Dr Lafayette LA 70508 337 266 8991 gt RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations TIME IN Entries must be endorsed with Name Rating and Certificate Number of SERVICE Technician or Repair Facility See back pages for other specific entries Aeae Taio ACESA ECC GEAR ReTRACTIOS TEST OK Geni EXTENSION O Bort UAW GERE lt DEL G6 33 ex ve eo Rote HyDeRoSTATIC TESE Sue 614 The ENGINE Fire DNE A 05 C L Tt ERATIONS lt AS ce K U E I RATER Wate OG LL AD USTIN iW L lt NON e D AAC M a k A H parted accordance wW RARA wepection and was determined to b in 8D aoeweorthy con dition 208 L7 9 are SIZUCIGIA YEAR RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations 20 TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Num of DATE TIME SERVICE Technician or Repair Facility See back pages for other specific entr
22. he 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 3 Form Tracking Number paren ti vation 1 AUTHORIZED RELEASE CERTIFICATE FAA UNITED STATES FAA Form 8130 3 AIRWORTHINESS APPROVAL TAG 33826 4 Organization Name and Address CRS JY2R943K 5 Work Order Contract Invoice Number 123174 R41312 Metro Aircraft Instruments Inc 2135 Airport Rd Oakland County Int l Airport Waterford MI 48327 1207 248 666 3670 8 Part Number 9 Eligibility 10 Quantity 11 Serial Batch Number 12 Status Work TACH IND DUAL N A 5833 OVERHAULED W SYNC 13 Remarks OVERHAULED AND TESTED USING MANUAL 86M087 CESSNA P N C668016 0101 Certifies that the work specified in block 12 13 was cai component is considered ready for release to service uni ied out in accordance with EASA Part 145 and in respect to that work the er EASA Part 145 Approval Number EASA 145 5112 PUES 14 CFR 43 9 Return to Service Other regulation specified in Block 13 Certifies that unless otherwise specified in 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 21 Approval Certificate No J
23. ies 4 Apr ig NE 1482220 3116 2 997 9 Removed and replaced ELT battery Due FEB 2014 Function check ELT IAW FAR 91 2074 CW AD76 08 02R2 by installation of wing tip strobe power ft wing tip strobe Sn 4359 and RH wing tip SN i landing gear aircraft performed gear extension and retraction test in electrical and manual modes with no discrepancies C W AD 98 04 28 by insertion of AD in to limitations section of AFM C W AD 2004 21 05 100 hr 24 month pressure decay test of heater and operational test of combustion air pressure switch with no discrepancies Heater hobbs time reads 135 1 Installed engine compartment fire bottles with hydrostatic test dates of 09 2015 Change right main tire with new air hawk PN 06 07918 and Michelin tube PN 092 344 0 Serviced and lubed as per Cessna service manual inspected as per Cessna 414 100hr Annual checklist I certify that this aircraft has been inspected IAW an annual inspection and was determined to be in airworthy condition Zee us p oe BY 316005924 1 Approving National Aviation 3 Form Tracking Number Authority Country i FAA United States AUTHORIZED RELEASE CERTIFICATE 02222011 1 Form 8130 3 AIRWORTI 5 Work Order Contract Invoice Number 991399 20014121 6 7 Description 8 Part Number 9 EM 10 Quantity Serial Batch Number 102 00007 100 30058754 DETECTOR SN 39422 30060766 SN 39423 39473 394
24. ions by the user installer before the aircraft may be flown FAA Form 8130 3 8 04 Installer must cross check eligibility with applicable technical data NSN 0052 00 012 9005 yN Aerospace VVOrK P um A TURBINE ROTABLES INC W O Number WO4574 j Part Number 30 1172 1 3414 W 29th St South Serial No 1703 Wichita Ks 67212 US Work OVERHAUL FAA Certified Repair Station No NV2R045L EASA 145 4033 STU Ph 316 943 6100 Fax 316 943 2917 Printed 1 25 2041 Page Page 1 of 3 Bill To 12559 Phone 800 433 0814 Ship To PREFERRED AIRPARTS PREFERRED AIRPARTS PO BOX 12 11234 HACKETT RD 11234 HACKETT RD KIDRON OH 44636 KIDRON OH 44636 US US Part No 30 1172 1 Qty 1 Refno R42637 Need Date 2 9 2011 Cust PN Mfg HGL Ship Via UPS REGULAR Sched Date 2 9 2011 Descr STROBE POWER SUPPLY Mfg SN Ship Acct 499 771 SN 1703 Terms NET 30 Notes RECEIVING INSPECTION Perform receiving inspection examine for obvious damage verify part number and attach appropriate documents mmm PRELIMINARY INSPECTION Perforp preliminary inspection hidden damage inspection disassembly amp cleaning HIDDEN DAMAGE INSPECTION C amp TEARDOWN Bm OVER amp ABOVE ir di d Above Details ASSEMBLY amp IN PROCESS Perform required workscope requisition parts amp assemble in accordance with approved INSPECTIONS data amp quality processes it Signatur
25. ngs Replaced all bushings on main gear scissors Replaced RH landing light Replaced all vacuum air filters Replaced mag compass light Replaced o rings on both wing fuel caps Removed rudder for access to clean bird nest from inside Replaced middle upper and lower upper hinge brackets I certify this aircraft has been inspected in accordance with an annual inspection and found to be in airworthy condition for return to service Stephef ier 203840128 RECORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of Technician or Repair Facility See back pages for other specific entries TIME SERVICE 6 17 08 8222Q SN 0152 AFTT 4316 1 HOBBS 176 9 I certify these aircraft records have been duplicated to the best of my knowledge and all AD s have been complied with at this ti M SERVED gt PGD Label ED A TODAY S TOTAL Description of Inspections Tests Repairs and Alterations FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of SERVICE Technician or Repair Facility See back pages for other specific entries DALS LENEN Ge ECL COpGEBRNITCS lt p 2p RED gt TD TAKS ACCESS _ REES REPLACED gt b ORO MiNID GE
26. oes not automatically constitute authority to install the part component assembly Where the user installer work in accordance with the national regulations of an airworthiness authori y 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 Statement 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 by the user installer before the aircraft may be flown 8130 3 8 04 Installer must cross check eligibility with applicable technical data NSN 0052 00 012 9005 Aerospace Turbine Rotables Inc 3414 W 29th St South Wichita KS 67217 us Ph 316 943 6100 Fax 316 943 2917 To Ship To PREFERRED AIRPARTS PREFERRED AIRPARTS PO BOX 12 11234 HACKETT RD 11234 HACKETT RD KIDRON OH 44636 KIDRON OH 44636 UNITED STATES UNITED STATES Need Date 10 19 201C Ref R42331 Phone 800 433 0814 Descr STROBE POWER SUPPLY Mfg HGL Code 12559 PN 30 1172 1 SN 4359 Ship Via UPS REGL Sched Date Qty 1 00 Cust PN Mfg SN 890 Ship 499771 er Perform receiving
27. s APPROVED return to service Other pertinent details of the repair are on file at this repair station Approved return to Service By GREGORY GARZA 2463291 Date Dec 7 2009 ss Printed Dec 7 2009 WOPSTM 09 10 46 SHOP2 shop Labor Task Control 1 Approving National Aviation 3 Form Tracking Number AUTHORIZED RELEASE CERTIFICATE 16204 FAA UNITED STATES FAA FORM 8130 3 AIRWORTHINESS APPROVAL 4 Organization Name and Address Aerospace Turbine Rotables Inc 3414 W 29th St South 5 Work Order Contract or Wichita KS 67217 Invoice Number US Ph 316 943 6100 Fax 316 943 2917 WO4574 FAA Approval Holder NV2R045L 7 Description kalam STROBE POWER SUPPLY 1 05 OVERHAULED 13 REMARKS Overhauled and certified IAW the documents listed Manual ID 030 1 Revision 2 Revision Date 6 1 1979 Full details of work performed held work order Manual ID 7608 02 R2 0 AMENDMENT 39 4540 CESSNA Revision Revision Date 1 31 1983 Manual ID 30 0515 33 0009 Revision C Revision Date 6 25 1975 The work specified in Block 12 13 was performed in accordance with EASA Part 145 and with respect to the work the aircraft component is considered ready for release to service under EASA Approval Certificate EASA 145 4033 14 Certifies the items identified above were manufactured in conformity to 19 14 CFR 43 9 Return to
28. t 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 parts components assemblies from the airworthiness authority of the country specified in Block 1 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 by 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 REGORDING TODAY S TOTAL Description of Inspections Tests Repairs and Alterations 20 2 T TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of DATE TIME SERVICE Technician or Repair Facility See back pages for other specific entries 0 9 _ SUCS 2e PLAC cen RIGHT CA XS4 ES HOBRE SH FIDE OSI NG pos eS eT PUSHED oPeRATICUAL SATISIPACTORY lt e 7 A P i INDICATOR READ INGS AT 25 C 7 BET M NOMENCLATURE M SERIAL NO ALTIMETER PRESSURE POL Fee INDICATOR READ TEST INDICATOR READ INGS AT 25
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