Registration No-------------5ignoture

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' I. Approving Civil Aviation 2. 3. Form Tracking Number: Authority/Country:

AUTHORIZED RELEASE CERTIFICATE 15082010D

FAA/UNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

4. Organization Name and Address: 5. Work Order/Contract/Invoice Aerospace Welding Minneapolis Inc 1045 Gemini Road Eagan MN 55121 Number: 41567 PQ2712CE

6. Item: 7. Description: 8. Part Number: 9. Quantity: 10. Serial/Batch Number: 11. Status/Work: 1 NEW

Stack A38137-05 1 41567

12. Remarks:

Airworthiness Approval I

AWi 83243

Installation el igibility to be determined by the installer.

13a. Certifies the items identified above were manufactured in conformity to: __ . 14e. D 14 CFR 43.9 Return ta Serviee D Other reguletien·sfJeeifieEI in Bleelc 12 - -·-- -·

[8] Approved design data and are in a condition for safe operation. Certifies that unless etherwise s13eeifieEI in llleel, 12, the ¥,erl, identified in Bleel, n D Non-approved design data specified in Block 12.

end deserilled in Bleel, 12 was eeeem13lisheEI in eeeerdenee with Title 14, Gede ef Federel Reguletiens, 13ert 43 end in res13eet ta thetwerlc, the items ere 01313r0Yed fer return ta ser,•iee.

l~-utnonzea · n~ ~-~ 13c. Approval/Authorization No.: 141:J. Autherized Signature: 14e. A1313revel/Gertifieete Ne.:

~ /\. .) j 812237748 ,,

13d.·-N'ame (Typed or Printed): 13e. Date (dd/mmm/yyyy): 14d. Nome (Ty13ed er Printed): 14e. l)ete (dd/mmm1,,,,y,9: Timothy L Mahoney

20/Aug/2015 ..

U ser/lnstaller Responsibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the aircraft engine/propeller/article.

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 I, it is essential that the user/installer ensures that his/her airworthiness authority accepts aircraft engine(s)/propeller(s)/article(s) from the airworthiness authority of the country specified in Block I.

Statements in Blocks 13a and 14a 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 (02- 14) NSN: 0052-00-012-9005

I. Approving Civil Aviation 2. 3. Form Tracking Number: Authority/Country:

AUTHORIZED RELEASE CERTIFICATE 150909010 . FAA/UNITED STATES

· FAA Form 8130-3, AIRWORTIIINESS APPROVAL TAG 4. Organization Name and Address: 5. Work Order/Contract/Invoice Aerospace Welding Minneapolis Inc I 045 Gemini Road Eagan MN 55 I 21 Number: 42358 PQ2712CE

6. Item: 7. Descriotion: 8. Part Number: 9. Quantity: 10. Serial/Batch Number: 11. Status/Work: 1 NEW

Muffler A67517-00 1 42358

12. Remarks:

Airworthiness Approval

.,

AWi 83529

Installation eligibility to be determined by the installer.

Ba. Certifies the items identified above were manufactured in conformity to: 14a. D 14 CFR 4J.9 Return ta Serviee D Other regulation Sf1eeified in Blaek 12, -·- - -- ---- -· r2J Approved design data and are in a condition for safe operation. Certifies that unless 0ther>r11ise Sfleeified in blael, U, the •.i1•0rl, identified in Blael, 11

D Non-approved design data specified in Block 12. end deseribed in Blael, l2. was eeeamf)lished in eeeardenee with Title 14, Cade af Federal Reguletians, fl&rt 4J end in resf!eet ta that work, the items ere Bflflreved fer return ta ser~·iee.

13b. Authorized Si1mature:

~ 13c. Approval/Authorization No.: 14b. Authorized Signature: He. Aflf)ra•iel/Certifieete Na.:

K---- ::::> ' _:::::-; 812237748 --IJd~ Name (Typed or Printed): 13e. Date (dd/mmm/yyyy): 14d. Name (Tyfled er Printed): 14e. l)ete (ddlmmm/~·~·y~•): Timothy L Mahoney

09/Seo/2015

User/Installer Responsibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the aircraft engine/propeller/article.

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 I, it is essential that the user/installer ensures that his/her airworthiness authority accepts aircraft engine(s)/propeller(s)/article(s) from the airworthiness authority of the country specified in Block I.

Statements in Blocks 13a and 14a 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.

-NSN: 0052-00-012-9005

) Date

AIRCRAFT LOG

Aircraft Time Recorder Reading

Maintenance

This Date Total

·, .. · , j

. ··- -AIRBORNE AVIONICS CRS# V3QR738Y

N7008F Airframe Logbook Entry Make: Piper Model: PA-32-300 SIN 32-7740012

Tach: 4896.1

The following was performed IA W The Piper PA-32 MM and applicable PAR's unless otherwise noted.

1. Adjusted A-30 altitude encoder per ACK A-30 Altitude Encoder Installation Manual.

Verified to 20,000 ft. 2. See WO 3285e{ ~~ _

Signed '::fJ ~ Cert. No. V30R738Y Date 8 Aug., 2015

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Registration No. ___________ _

Signature Certificate No.

Aircraft Maintenance Services, Inc. 1400 Jim Hamilton Blvd, Bidg E

Columbia, SC 2920S www.amsco lumbia.com

Drained oil and replaced filter. Cut filter for inspection. Added 12 qts. Of Aeiroshell lOOWplus. customer furnished.

cleaned engine and ground run for leak c

Danny Buie A@P2834404

A&P283020-'t0-+

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N7008F PA-32-300 SN: 32-7740012

05/05/2016

AIOrDACT I,-..,-.

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AVIONICS Aircraft Maintenance Services, Inc.

1400 Jim Hamilton Blvd, Bldg E Columbia, SC 29205

www.amscolumbia.com

Removed existing KT 78 transponder, coax cable, and antenna. Removed Garmin GNS430 GPS and sent to Garmin for WAAS upgrade. Removed and replaced existing GPS antenna with a GA35 WAAS GPS antenna. Removed and replaced GPS Coax ·cable with Garmin specified length of RG400 Coax. Installed upgraded GNS430W and configured unit identical to pre-upgrade settings. Installed new Garmin GTX345 ADS-Bin-out transponder, SN: 3EG000541, Cl 105 transponder antenna, and RG400 transponder coax. Weight and balance updated and placed in aircraft records. Electrical load analysis completed and determined to be within acceptable limits. I certify that all work was done in accordance with the applicable installation manuals and current FAA regulations. This aircraft has been returned to

service with respect to the work performed on thi ate: 05/05/2016.

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TRANSPORT CANADA! FOqM 0NE ! 2016- 4288 ~ 4. Approved organization name and address

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I r N= ""'"°'· Mam,t"'""d as pee PDA 04-8. Rep,aoeme"' foe p,pec Part 67517-00 w,,aeo As Pee AWS 017 ,

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Approved design data and a re in condition for safe operation

1 Jc . Approved Organization Number 100-91

..,ells: tuu, 11111111 1, yyyy~ .. ,.... A.•- Ar ! L-.H.1 .. !~- ! Q

14b. Authorized signature

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accoraancewrm tne nauona1 regu1auons or an a,rworuuness autnorny omer man me aumonw specmea m 01ocK , , me tnsta11er must ensure tnatnismer -·· .. -.............. __ :;: .:. .... _ .. .... ,. ... ,. . ....... _ .......... ,_,, ...... -...... .. ......... ... -··· ............. .................... ... ,. ........ , .. .. .. ............. .. ' . •.. ___ ,.,._,, , ............ ...... ·- .... -- ...... -- .. ........ ... installation certification. In all cases the aircraft technical record must contain an installation certification, issued In accordance with the ni.tional regulations of the st0;tt: vi rt-gistry, Ui:ivre me 0;lr,:;rMt m0;·v Ue iivwn.

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Registration No. _________ _

·-·------···--- ···----·---·-----·---··-· ·-··-------------·-------·-··-- .... _ -·····-----·· - -· ····- -- -·-··· -----------· ·-·-- ---~----- --------....J _____ _

l / NOV 4,2016 N7008F TACH/ TT 5112.98 AIRFRAME ENTRY I j ANNUAL INSPECTION COMPLETED PER PA32 SERVICE MANUAL AND INSPECTION I CHECKLIST .. INSPECTED ALL FLIGHT CONTROLS,LUBED ALL PIVOT POINTS, RESET I STABILATOR CABLE TENSION,ELT TESTED PER FAR 91.207 (d ),CHECKED GOOD.LANDING I GEA~ INSPECTED,LUBED AND GREASED WHEEL BEARINGS, REPLACED RIGHT MAIN ! ii TIRE,INSTALLED NEW AFT MUFFLER(67517-00AWL) REPAIRED MUFFLER SHROUD AS :·. 1! NEEDED,CW AD 'S 78-23-01 FUEL DRAIN DOOR CHECK,95-26-13 AMOC OIL COOLER HOSE ,1

ii INSPECTION.ALL AD 'S COMPLIED WITH THRU BIWEEKLY 2016-22 (SEE LISTINGS) . ! ! JI CERTIFY THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL , ._,.

1

.. I INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION ON THIS DATE OF ; :: jl NOV 4 ,2016. ! ,

1

ii ~' 'I f 'Lj · l,1 I --- --- - --- ---------------JOHN A. KOENIG A&P 3565366 IA···--·· 11·/!.·~.·.'·

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--· Date

N7008f PA-32-300 SN: 32-7740012 Tach Time: 5192.2

02/23/2017

Aircraft Time

Al RC RAFT LOG

Recorder 0- - J~ - ~·

AVIONICS Aircraft Maintenance Services, Inc.

1400 Jim Hamilton Blvd, Bldg E

Columbia, SC 29205 www.amscolumbia.com

Removed existing KMA 20 audio panel and symphony 468 intercom system. Installed new Garmi, GMA350c audio panel with 6 place intercom. New stereo headset and microphone jacks ran thro the cabin. Installed new Garmin GS Electronic Flight Display IAW STC# SA01818WI. Retained bot turn coordinator and attitude indicator. Electrical load analysis within limits. Previous weight an balance totals unchanged with respect to the work performed on this date. I certify thot all wor! done in occordonce with the applicable installation monuals and current FAA regulations. This ai has been returned to service with respect to t11e w ., performed on this date: 02/23/2017.

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AVIONICS

i~ I certify that the pitot static system on this aircraft has been tested in accordance with FAR 91.411 and FAR part 43, and has been found to be satisfactory at this time. N 7oo~·J ::. S/N: ').9_-YJ"(ooi?., HM: __________ _ Aircraft Maintenance Services, Inc. FAA Repair Station #F07R634N d.'j,h~ WO: ?..1(;y

Aircraft Maintenance Services, Inc. 1400 Jim Hamilton Blvd, Bldg . E

Columbia, SC 2920S

www.am sco fumbia.com

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The following Altimeters have been tested: , .r-.

Altimeter 1: hta", Model: \P"" S/N: ~41 1<-( Date: 5-~4-;).oq Alt: 9-ol::c Altimeter 2: Model: S/N: Date: ,---..... Alt, - - - ---

Altimeter 3: Model: S/N: Date: - ·· Alt: ____ _ _

These Altimeters were tested in accordance with FAR 91.411 a,,ct FAR~ 43, Appendix E and found to be sat isfactory. Aircraft Maintenance services, Inc. FAA Repair Station #F07R634N ~ WO: ~ 7.,g-

The Following ATC TransJJonders have been tested:

Transponder 1: <for"'~"' Model: G<T)( •1/5 S/N : lt.(f)OOoJ'-{/ Date: ______ _ Transponder 2: Model: S/N: Date: _______ _

These Transponders were tested in accordance wit.h FAR 91.413 and F~ ~A_ependix F and found to be .satisfactory. Aircraft. Maintenance services, Inc. FAA Repair Station #F07R634N ~ WO: '9..f6 r

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N7008F PA-32-300 SN: 32-7740012 Tach Time: 5254 AVIONICS

I

i' 5/24/2017 Aircraft Maintenance Services, Inc. 1400 Jim Hamilton Blvd, Bldg E

Columbia, SC 29205 I\ 11

www.amscolumbia .com 'i i I 11 I Removed ADF system. Installed Electronic International MVP-SOP engine monitor system per E.1.

\

·1· Installation Instruction manual (II 0425051, Rev. I 02/05/2009). Installed EDC per instructions and Wired

1 all probes, transducers, fuel flow, and sensors per install manual. Fuel gauges calibrated and checked f

l\ function. Installed annunciator per instructions. New altitude encoder (ACK A-30) installed to replace 0

\\I faulty unit (checked pitot static system FAA Repair Station #F07R634N, W0:2768).

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Ryan Turiak yz,11 l i..JJU~ A&P365358S

etL@igistics, TECHNICAL SERVICES

Reg. #: N7008F

Acft Hrs: 5332.47

AIRFRAME ENTRY

5400 Airport Dr. I Tel: 919.840.0555 Charlotte, NC 28208 Fax: 877.520.7582

Model: PA32-300 Serial: 32-7740012

Acft Cycles: W/0:7095

X DISCllEPANCIES/MISCELLANIOUS MAINTENANCE:

RAINED OIL REMOVED AND INSPECTED OIL FfLTER NO DEFECTS NOTED. INSTALLED NEW OlL TL TER P/N CH48 l l 0-1 AND SERVICED ENGINE WITH 10 QUARTS AEROSHEELL W lOOPLUS OIL LEAK HECKS GOOD. ALL WORK DONE IN ACCORDANCE WITH PIPER PA32-300 SERVICE MANUAL PIN 53-690 SECTION 2-46 AND 2-47

he aircraft and/or component identified above was repaired and inspected in accordance with current regulations of the ederal Aviation Regulations and is approved for return to service. Pertinent details of the repair are on file at this gency under this work order.

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Date

N7008F SN: 32-7740012 Meter Time 5438.1 13 September 2017

Total To Carry Forward

Al RC RAFT LOG

Aircraft Time

This Date Total Recorder Reading

Brought Forward +

Aircraft Maintenance Services Columbia, SC 29205

Phone : (803) 708-7191 www.amscolumbia .com Email: frank@amscolumbia .com

~ ·~ ·

and Remarks

N7008F

~ ,,., -- ... ,, . ..

SN: 32-7740012 1 Meter Time 5438.1 11

13 September 2017 I , 1

Registration No. ___________ _

Aircraft Maintenance Services Columbia, SC 29205

Phone: (803) 708-7191 www.amscolumbia .com Email: frank@amsco!umbia.com

Signature Certificate No.

l' Changed Engine Oil. Removed oil filter, cut filter open for inspection. Serviced engine with AeroShell 100. Cleaned, degreased, ground run and leak checked engine, leak checked good.

Frederick Dickens~~'."...> . A&P:3643176

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Al RC RAFT LOG

DEC 28,2017 N7008F TACH/ TT 5558.7 AIRFRAME ENTRY ANNUAL INSPECTION COMPLETED PER PA32 SERVICE MANUAL AND INSPECTION CH ECKLIST.INSPECTED ALL FLIGHT CONTROLS,LUBED ALL PIVOT POINTS,ELT BATTERl l:s REPLACED( DUE DEC 19)TESTED PER FAR 91.207 {d ),CHECKED GOOD.LANDING GEAR INSPECTED,LUBED AND GREASED WHEEL BEARINGS,REPLACED LEFT BRAKE PADS AN D 0-RINGS,INSTALLED NEW CENTER MUFFLER(67517-00AWL) REPAIRED MUFFLER

i SHROUD AS NEEDED,CW AD'S 78-23-01 FUEL DRAIN DOOR CHECK(DUE EACH 100),AD l : 17-14-04 NA DUE TO TYPED HOSES,17-16-01 AK-450 ELT TEST(DUE YEARLY).ALL AD'S ·:' COMPLIED WITH THRU BIWEEKLY 2017-26(SEE LISTINGS) .! CERTIFY THIS AIRCRAFT HAS·

BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS l DETERMINED TO BE IN AIRWORTHY CONDITION ON THIS DATE OF DEC 28,2017. I ...,

: I ·n,J;C IF=-.-. =--- -~-~~=OHN A. KOENl:. :P~565366 IA·-···_--__

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