ENGINE L O G

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P u b l i c a t i o n E L B - O I

S e r v i c e I n f o r m a t i o n Consult the Continental Motors web site at continentalmotors.aero for engine related news or announcements. Continental Motors Internet Service contains useful information for Continental Motors engine owners, including electronic versions of the most current engine Instructions for Continued Airworthiness and service bulletins that may be pertinent to your engine model.

If internet access is not available, contact our Customer Service Department at: 1-888-826-5465 Toll free in the United States or 1-251438-8299 International ,

E n g i n e R e t u r n s Return engines for core credit with this log book to: Continental Motors, Inc. 2039 Broad Street Mobile, AL 36615 USA

Return engines for overhaul with this log book to: Mattituck Services 410 Airway Drive Mattituck, NY 11952 USA

U S E O N L Y F U E L C O N F O R M I N G T O A S T M D 9 1 0

U S E O F A U T O M O T I V E F U E L I S P R O H I B I T E D

C o n t i n e n t a l M o t o r s ^ I n c . Production Certificate 508

Printed: 8/27/2013 Test Date: 8/26/2013

This engine model TSI0550C14B, serial number 1008922 was rebuilt by Continental Motors in accordance with approved <li'vi<rn H»ti tn\ imnlicti Mr rcflirirements of Part 21 nf #1m» — • » — i ' i — — • 1 — — - - — Federal Aviation Regulation. The approved design data for this engine incorporates all changes required by applicable Airworthiness Directives and Continental Motors Service Bulletins.

'/tow/

Total Time

Date

Hours Min

Time Since Last Overhaul

Hours Min

Engine Service and Maintenance Record Record maintenance actions including engine part removal and installation and compliance with inspections, Airworthiness Directives, Sneriai insnections. Modifications and Service Bulletins

Sky Way Aircraft Inc. Piper PA46-310P N9127Z S/N 4608059 Hobs 3742.7 Hobbs (0) 09-23-2013 TCM TSI0-550C14B S/N 1008922 (0) time rebuilt engine New Hobbs (0)

• Performed Annual inspection and found to be in an airworthy condition • Serviced with 8qts.20WS0XC Phillips (M). Added 2qts after run in • Installed this Engine in Piper PA46-310P S/N 4608059 • Installed Overhauled Alternator #2 P/N E3FF10300BA S/N H-M100609 • Bleed blasted all alum. Baffles, primed and painted. Installed rubber

baffles on alum, baffles and installed on engine • Made new engine mount stainless steel exhaust shields. Installed new

P/N 84104-017 Canopy shield over exhaust cross over pipe rear of engine

• Reinstalled propeller with new o ring gasket • Installed new engine Lord mounts P/N J9613-55

John P Dennis A&P1693927IA

4. Organization/Name and Address

Aero Accessories, Inc. • 1240 Springwood Avenue • Gibsonville, NC 27249 USA FAA-PMA (PQ1206CE)

proving National A v i a T i o n I ' . T , T U n D i 7 c n n c i C A O C a - » C D T I C i r A T E C 3 ' FoitaJracking Number: Approving Authority/Country:

FAA/'Jnited States AUTHORIZED RELEASE CERTIFICATE

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

Description

Dry Air Pump

Part Number Eligibility

N/A

10. Quantity

AA 5. Work Order/Contract/Invoice Number:

Mud Serial/Batch Number Status/Work

Overhauled

13. Remaps Overhauled & Tested in accordance with FAA approved data fT^^^'^^t 14. Certifies the items identified above were manufactured in conformity to:

• Approved design data and are in a condrtion for safe operation.

• Non-approval design data specified in Block 13.

15. Authorized Signature 16. Approval/Authorization No.

17. Name (Typed or Printed): 18 Date (M / D / Y)

9 IS 14 CFR 43.9 Return To Service • Other Regulation Specified in Block 13

CerlilkM i w . n w , otriwww sceolw) ' i DUCK 13, U «ort kMnflliad to Ho« 12 mc tocOM H owe* 13 M l accom-pliiromiccnrMnw»rt>TVoe 14 Code ol <iMeral Regiikrtoni part *3 ana H- m « K mat arork me lama w awrovad (Of rlfcm K Mnaoa

22. Name (Typed or Printed)

21. ApprovaVCertrlicate No

YV4R688M «e (M /D /Y l

1 9 TOO* User/Installer Responsibilities

11 a irxwtam 10 unOenjtarc lliet We BkWenca C* 1M Oocumenl More COM rot aulonatcalV :oroMuta autront, te ratal flie wVronronent/aaaernoi, i n a j oserfinslaflef work n accoroarce wkh tne naiona; reguawis ot an Airwonniress A jhorky d*fe~t rnan Ine Ajn.cThin«_ Aulhcray of me courrry MoaH80 in Beck 11 a essenlal thai toe wer'irBtaw ars.res H MM » » » - n a i - Ajrk-y accam oa r. ocmconenwassentikas Iron ine Ajrwrrhkwss Ajtlxrty ok lh» courrtry aoediea r. Ckock i

FAA form 8130-3 (06-01) <ibility with applicable data.

S E R V I C E A B L E

This unit ts a stock corCit has been disassembled, cleaned, inspected and has been Overhauled in accordance with Manufacturer's Specifications.... Parts installed are new Date Part Number /Hh2.C vV--y-Serial Number fap5l J _____ A&P Number A&P Nairn Signature

Carton # 0000124616 Order # 87888

PO # ENG0033902 C o n t i n e n t a l M o t o r s , I n c . Date Printed 9/4/2013 3:28:12PM

139 Broad Street EPN # 355417 «iobile # AL 36615 S h i p V j a e | | 0 W Roadway Corp. (Truck)

Gate D1 Shipping Information Customer # 85101

A c c o u n t * E n g i n e S # Description

Ship to: SKYWAY AIRCRAFT , Bill to: AIR POWER, INC 341 8TH AVE SE HANGAR 3C 4900 SOUTH COLLINS ST PETERSBURG, FL 33701 ARLINGTON, TX 76018 US

Item # Description QTY N/R TSIO550C14 ENGINE - REBUILT 1 R

Serial/Lot Number(s) 1008922

It is hereby certified that all materials or parts on this shipment are in conformance with the requirements, specifications, and/or drawings listed for the above engine model/part number.

September 04, 2013 Michael E. Ward Date

Director, Compliance

Thank you for purchasing Genuine Continental Engines and Parts! Go Continental! Page 1 of 1

A i r c r a f t E n g i n e T e s t V e r i f i c a t i o n

This document verifies that the engine model listed below has satisfactorily completed all testing listed below in accordance with CM standard engine testing specifications as approved by the FAA.

Engine Model R-TS^TOSSbCfH/?

Engine Serial Number / f l Q <_? 9 2 ' 2 .

T e s t i n g C o m p l e t e d

Standard Acceptance Test:

Date of Completion 8J2g/20 \3 Test Operator

Form No 98344 C o n t i n e n t a l M o t o r s , I nc .

1. Approving National Aviation

Authority/Country:

FAA/United States

AUTHORIZED RELEASE CERTIFICATE

FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG

. Form Tracking Number

286885

4 Organization Name and Address:

Continental Motors, 2039 Broad Street, Mobile, Alabama 36615

PC #508 5, Work Order/Contract/Invoice Number:

"355417 ' 0000124616

6. Item: 7. Description: 8. Pari Number: 9. Eligibility: ' 10. Quantity: 11. Serial/Batch Number: 12. Status/Work:

1 ENGINE - REBUILT TSIO550C14 N/A 1 See Block 13 See Box 13

13. Remarks:

Rebuilt to original PAH's specifications in accordance with 14 CFR §43.3(j). Total Time: 0 Preservation: This Engine was treated 08/27/13 for one hundred eighty days corrosion protection.

Senal/Baich Nunibei(s)

Serial 1008922

Description ENGINE - REBUILT

14. Certifies the items identified above were manufactured in conformity to:

j Approved design data and are in condition for safe operation.

| Non-approved design data specified in Block 13.

'9 ~J 14 CFR 1 1 9 icI 1" taMM X 1 Hlici regulation specified in Block 13

Certifies thai unless otheiwiseil ilieil in Block 1 V the woik identified in Block 12 and described in Block 13 was

accomplished in ;K C niilatii I- v\h 1 illr 1 1 ( ode ol 1 iilci.il Kcj'iilalinii s pait 43 and in respect to that work, the items aie

approved tor reliim In service

1 5 Autiiorized Signature: 16. Approval'Authorization No.: 20. Authorized Signature , / /} 21. Approval/Certificate No.:

PC #508 17. Name (Typed or Printed): 18Date(m/d/y): 22. Name (Typed 01 I'nnU'd)

Daniel L. Nicholas

23. Date (m/d/y):

Sep/04/2013

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 user/installer before aircraft may be flown.

FAA Form 8130-3 (6-01) * Installer must cross check eligibility with applicable technical data NSN-0052-00-012-9005

Customer Copy

C o n t i n e n t a l M o t o r s , I n c .

Engine Component Information Sheet Pr in t ed : 8/27/2013

S e r i a l : 1008922 Assembled: 8/24/2013 Spec: TSI0550C14B Shipped: New/Rebuilt: REBUILT • Packed: 8/27/2013

Customer Name: Shipping Address:

C o m p o n e n t S e r i a l N u m b e r C o m p o n e n t S e r i a l N u m b e r

CAMSHAFT 165620 L. TURBO H-QEL00168 CRANKSHAFT N01IA079 R. TURBO H-QEL00170 CRANKCASE R13GA217 OVERBOOST N/A CONNROD AE13FA416 CONTROLLER H-QCD00128 CONNROD

C r^KTNTD CSV\

AE13FA407 WASTEGATE H-QCD00202

A h l o r A 4 U o CYLINDER - 1 AC13DB648 CONNROD AE13FA415 CYLINDER - 2 AC13GA319 CONNROD AE13FA414 CYLINDER - 3 AC13DB682 CONNROD AE13FA408 CYLINDER - 4 AC13GA253 L MAGNETO D13HA084R CYLINDER - 5 AC13GA254 R MAGNETO D13HA069R CYLINDER - 6 AC13GA241 CARBURETOR N/A CYL FLOW CODE N/A FUEL PUMP B13HA093R NOZZLE - 1 1515 MANIFOLD VALVE C13HA040R NOZZLE - 2 2531 METERING UNIT A13HA050R NOZZLE - 3 3531 STARTER H-U-221304 NOZZLE - 4 4531 ALTERNATOR 013GA026R NOZZLE - 5 5520 ALTERNATOR 2 N/A NOZZLE - 6 6526 DRIVE GEAR N/A OIL COOLER F13-10919-40 DRIVEN GEAR N/A PISTON WEIGHT N/A

F o r m Q A - 8 5 A ( M A R 2 0 1 2 } /JCm

Pack Inspection Stamp \ J 3 ^ A l l o f t h e i n f o r m a t i o n p r o v i d e d h e r e i n i s s u b j e c t t o v e r i f i c a t i o n by t h e u s e r . C o n t i n e n t a l M otors, I n c . makes no r e p r e s e n t a t i o n o r w a r r a n t y c o n c e r n i n g t h e a c c u r a c y o r completeness o f

th e i n f o r m a t i o n and assumes no r e s p o n s i b i l i t y w i t h r e s p e c t t h e r e t o .

I. Approving National Aviation Authority/Country:

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

3. Form Tracking Number:

H-M100609

4. Organization Name and Address:

HARTZELL ENGINE TECHNOLOGIES, 2900 SELMA HWY., MONTGOMERY, AL. 36108 (1HZR769B) 5. Work Order/Contract/Invoice Number: W/0: M054430

6. Item: Description: 8. Part Number: 9. Eligibility: 10. Quantity: 11. Serial/Batch Number: 12. Status/Work:

ALTERNATOR N/A E3FF10300BA MOD/NO

END ***********'****H*********************tt**********

H-M100609 OVERHAULED

13. Remarks: COpy OF WORK ORDER AVAILABLE ON REQUEST FROM HARTZELL ENGINE TECHNOLOGIES

CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12/13 WAS CARRIED OUT IN ACCORDANCE

WITH EASA PART 145 AND WITH RESPECT TO THAT WORK THE AIRCRAFT COMPONENT IS

CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA APPROVAL CERTIFICATE NUMBER

EASA.145.4418 AND BY THE FAA AIR AGENCY CERTIFICATE NUMBER 1HZR769B. APPROVED FOR EXPORT

THE ORIG. EQUIP. MFG. DATA APPEARS ON THE DATA PLATE IN THE LINES IDENTIFIED AS MOD/NO & ORIG. MFG.

COMPLIES WITH PPS-9001 LATEST REVISION.

OVERHAUL PER CESSNA MANUAL #D5107-1-13, REV. 1

04489

19. G*! 14 CFR 43.9 Return to Service Other regulation specified in Block 13

Certifies that unless olhcr wise s|M'cificd in lllock 13, (lie work identified in Block 12 and described in Block 13 was accomplished in accordance with Til It- 14, Code of Federal Regulations, part 43 and in rcs|>ccl to thai work, the items are approved for return to service.

^Certifies the items identified above were manufactured in conformity to:

• Tipproved design data and are in a condition for safe opera};

• Non-approveadesign data specified in Block 13,

User/Installer Responsibi 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 'XXIi

OS

A V) 111 I ('( )!)!•• (IT1

T. Approving National Aviation Authority/Country:

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

3. Form Tracking Number:

41823 4. Organization Name and Address:

THE AVIATION GROUP, INC. 211 PROSPECT PARK, PEACHTREE CITY, GA 30269 (VGOR728L) 5. Work Order/Contract/Invoice Number: 41823

6. Item: Description: 8. Part Number: 9. Eligibility: 10. Quantity: 11. Serial/Batch Number: 12. StatusAVork:

1 ACTUATOR 11-20 N/A 1 1107MA REPAIRED

13. Remarks: THE ABOVE APPLIANCE WAS REPAIRED AND , INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE. Manual: 761-783 Revision#:CR980701 Revision Date: 07/01/1998 (Full details held on W.O. 41823 .) Comments:

CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12/13 WAS CARRIED OUT IN ACCORDANCE WITH EASA PART-145, AND IN RESPECT TO THAT WORK THE COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA PART-145 APPROVAL NUMBER: EASA. 145. 4208. (*rNSTALLER MUST CROSS CHECK ELIGIBILITY WITH APPLICABLE TECHNICAL DATA.)

LIFE LIMIT PARTS MUST BE ACCOMPANIED BY MAINTENANCE HISTORY INCLUDING T OTAL TIME/TOTAL CYCLES:

"XLTertifies the items identified above were manufactured in conformity to:

1 1 Apph»*j^d design data and are in a condition for safe operation,^^^

[""I Non-approvea"S«s<isn data specified in Block 13.

19. $

C a F

] 14 CFR 43.9 Return to Service [>3 Other regulation specified in Block 13

ertifies that unless otherwise specified in block 13, the work identified in Block 12 id described in Block 13 was accomplished in accordance with Title 14, Code of :deral Regulations, part 43 and in respect to that work, the items are approved for turn to service.

15. Authorized Signature: ^^^^ 16. Approval/Authorization No.: 20. Authorized Signature: 21. Approval/Certificate No.:

VGOR728L * 17. Name (Typed^Trinted):

^^^^ %

18. Date (tnToTy): 22. Nai ne (Typed or Printed):

Richard H. Hewitt

23. Date (mmm/dd/yyyy):

JUL/22/2013

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).

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.

FAA Form 8130-3 (6-01) *Insta11er must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005