Engine Service and Maintenance Record Installations, Inspections, Airworthiness Directives, Special Inspections, Modifications and Service Bulletins

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Total Time Time Since Hrs. Min. Hrs. Min. IO-550N 691933 Performed engine 100 Hour Inspection law TCM ICA inspection document. Drained oil; took sample.

Performed ground run and leak check. Performed compression check; results as follows. Calibrated orifice 64/80, #1 76/80, #2 74/80, #376/80, #4 74/80, #5 76/80, #674/80.

1 Total Time Time Since Hrs. Min. Hrs. Min. IO-550N Performed engine 100 Hour Inspection law TCM ICA inspection document. Drained oil; took sample. Opened and inspected oil filter; no abnormal particulates noted. Installed new oil filter, pin CH , and serviced with 8 qts Phillips 20W50 Type M mineral oil. Performed ground run and leak check. Performed compression check; results as follows. Calibrated orifice 64/80, #1 76/80, #2 74/80, #376/80, #4 74/80, #5 76/80, #674/80. Cleaned, gapped, tested, inspected, and reinstalled all sparkplugs using new gaskets, pin M-674. Cleaned, inspected, and reinstalled fuel injection nozzles using all new o-rings (pin ), rubber washers (pin ), and copper crush washers (pin X1473). Next fuel injection nozzle service due hours TIS. Removed defective #1 alternator, pin (Kelly pin ES-10024) sin ; installed new #1 alternator, pin (Kelly pin ES-10024) sin I certify that the work described above was performed satisfactorily and in accordance with approvedlacceptable data and that this article is a roved for retum to service with re ard to work erformed. Signature: Jeffrey Shawn Crean, A&P RDU SR (TT) Preformed Cirrus Maintenance 100hr inspection law TCM MM, Chapter 5 inspection checklist. Compression test results: 1)74/802)75/80 3)75/804)78/805)75/806)78/80. Master orifice:62psi. Drained oil, sample taken, removed and inspected oil filter, no defects noted. Installed new filter, torqued and safetied. Serviced oil system with 8qts Phillips 20W50 XlC oil. Cleaned and regapped all spark plugs, ; checked mag timing and leads. Inspected all baffling, plumbing, wiring and component security. Checked cylinder and fuel nozzle condition. Lubed en ine controls. Grd run, fuel s stem checked er TCM SID 97-3E, found within limits, 0 s and leak check ood. erformed only and was found airworthy and is a roved for return to service. Pertinent details of this re air are on file at this facilit. Signature: <5l11 xi

Total Time Hrs. Min. odifications anclsenlice Sltlletins ~C L R R U S Hobbs Time RDU- 4252 7/15/2009 SR22 182.9 145.6 Engine: SIN: 1.

Drained oil and removed filter, inspected filter for contamination, No contamination noted, Installed, torqued and safetied new filter PIN: CH481 08-1. Serviced engine with 8 qts.

performed inspection check of exhaust system, inspected breather tube, inspected engine compartment for loose hardware, inspected cylinder drains for clogs and restrictions.

Bolt replaced on right side exhaust header PIN: AN4C32 b. Cleaned oil pressure sensor. **************** End ******************* Sartal No. RDU004516 9-10-09 Cirrus SR22 TCM, 10-550-N48, SIN 691933.

Compression test results: 1)78/80 2)76/80 3)76/80 4)76/80 5)76/80 6)78/80. Master orifice:68psi. Drained oil, sample taken, removed and inspected oil filter with no defects noted.

2 Total Time Hrs. Min. odifications anclsenlice Sltlletins ~C L R R U S Hobbs Time RDU /15/2009 SR Engine: SIN: 1. Performed Cirrus Maintenance Program 50 hour in service inspection. 2. Drained oil and removed filter, inspected filter for contamination, No contamination noted, Installed, torqued and safetied new filter PIN: CH Serviced engine with 8 qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis. 3. Inspected oil lines and fittings, spark plug cable ends, air intake ducts, filter, air flapper valve for general condition. performed inspection check of exhaust system, inspected breather tube, inspected engine compartment for loose hardware, inspected cylinder drains for clogs and restrictions. Visually inspected magnetos. 4. Performed ground runl operational check. With no leaks or defects noted. 5. The following descrepancies were addressed on this inspection: a. Bolt replaced on right side exhaust header PIN: AN4C32 b. Cleaned oil pressure sensor. **************** End ******************* Sartal No. RDU Cirrus SR22 TCM, N48, SIN Preformed Cirrus Maintenance Program Annual inspection. Complied with TCM SB SID97-2, Top Care Health Checklist, next due 9/2010. Compression test results: 1)78/80 2)76/80 3)76/80 4)76/80 5)76/80 6)78/80. Master orifice:68psi. Drained oil, sample taken, removed and inspected oil filter with no defects noted. Installed new filter, torqued and safetied. Serviced oil system with 8qts Phillips 20W50 XlC oil.cleaned and regapped all spark plugs, checked mag timil)g and leads. lnspscted all baffling, plumbing, wiring and component security. Checked cylinder and fuel nozzle condition. Lubed engine controls. Replaced induction air filter assembly PIN BA 111. Inspected exhaust system, removed and pressure tested heat exchanger, no defects noted, reassembled and secured. Replaced #1 and #4 exhaust risers, P/N and P/N due to securement hole elongation, assembled with new AN4C-35 bolts and keyed. Torqued per TCM overhaul manual specs. Replaced #1 EGT sensor due to broken clamp. Grd run, fuel system checked per TCM SB SID 97-3E, found within limits, ops and leak check good. I certify this Engine has been inspected law a 100hr/Annual inspection using Cirrus SR22 MM, Chapter 5-20 and TCM MM ICA, Chapter 5 inspection checklist as revised and was determined to be in airworthy condition and approved for return to service. (Ref. WO#RDU for further details). Next 50hr inspection due at FH performed onl and was found airworth and is a roved for return to service. Pertinent details of this re air are on file at this Iacili A&P IA RDU- 5060' 11/27/2009 N602UK SR Engine: SIN: 1. Performed Cirrus Maintenance Program 50 hour in service inspection I. 2. Drained oil and removed filter, inspected filter for contamination, No contamination noted, Installed, torqued and safetied filter PIN: CH Serviced engine with 8 qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis. 3. Inspected oil lines and fittings, spark plug cable ends, air intake ducts, filter, air flapper valve for general condition.perfonned inspection check of exhaust system, inspected breather tube, inspected engine compartment for loose hardware, inspected cylinder drains for clogs and restrictions. Visually inspected magnetos. 4. Performed ground runl operational check. With no leaks or defects noted. 5. The following descrepancies were addressed on this inspection: #1 Alternator replaced due to oil leakage from internal seal, replaced per AMM with new unit from Teledyne Continental ta. '" CE# under W/O: Off Unit: PIN: ES10024 SIN: On Unit: PIN: ES10024 SIN: J **************** End ****""**************

----~...= ~~~~ lnstajlations, Inspections, Airworthiness Directives, Special Inspections, 12635-001.

9 b~ ~ C I R R U S Serial No: Hobbs Time FH/TI SR22 331.9 262.3?:5~=:E~':JI :..is:!.!::;;;.;er.

)76/802)74/803)77 180 4)77 180 5)73 180 6)74/80. Master orifice:62 psi.

_Serviced engine with 7 qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis. - spark plugs. Checked mag.

3 ----~...= ~~~~ lnstajlations, Inspections, Airworthiness Directives, Special Inspections, Ground ran ops and leak checks ok. b~ ~ C I II R U S Hobbs Time Fli ht Hobbs b~ ~ C I R R U S Serial No: Hobbs Time FH/TI SR ?:5~=:E~':JI :..is:!.!::;;;.;er.larx:e Program 100 hour inspection law TCM ICA, Chapter 5 inspection checklist. )76/802)74/803) ) ) )74/80. Master orifice:62 psi. """3;;;oIreCl ii:dlr, inspected filter for contamination, No contamination noted, Installed, torqued and safetied new _Serviced engine with 7 qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis. - spark plugs. Checked mag. timing. Inspected all baffling, plumbing, wiring and component security. nozzle condition. Lubed engine controls. AD and SB researched. ~~:r: '"!-'no operational check, fuel system checked per TCM SID 97-3E, found within limits, ops and leak check Ed above was repaired and inspected in accordance with current FAA Regulations and for the work airworth a pproved for r turn to service. Pertinent details of this repair are on file at this facility. Warren Bourne A& P Jon A. Delamarter, A&P

Corrected magneto to engine timing on both mags. Cleaned, inspected, and reinstalled fuel injection nozzles using all new seals (pin 640612, 630979-9, X1473).

4 Brought Forward Total Time Time Since I----,----+~~:...r_.:..:..;.:;..::;.;...; Hrs. Min. Hrs. Min. Completed Cirrus MX Program 200 Hour Interval Items. Complied with TCM 100 Hour Inspection law MM Chapter 5. Installed new air filter element, pin BA24. Serviced gascolator using new o-ring (pin MS ) and new stat-o-seal (pin NAS B). Corrected magneto to engine timing on both mags. Cleaned, inspected, and reinstalled fuel injection nozzles using all new seals (pin , , X1473). Periormed engine compression check; results as follows: MO- 48/80, 1-73/80, 2-66/80, 3-71/80, 4-74/80,5-73/80, Cleaned, inspected, gapped, tested, rotated, and reinstalled sparkpluqs using new gaskets (pin M674). Drained engine oil; took sample. Opened and inspected oil filter; no abnormal particulates noted. Installed new oil filter, pin CH , and serviced with 8 ts Philli s 20W50 XlC oil. Periormed round run and leak check. I certify that the work described above was periormed satisfactorily and in accordance with approvedlacceptable data and that this article is a roved for return to service with re ard to work eriormed. Signature: Jon A. Delamarter, A&P SR22 TCM, IO-550-N48, SIN Preformed Cirrus Maintenance Program Annual inspection. Compression test results: 1)74/802)74/80 3)74/804)74/805)75/806)76/80. Master orifice:48psi. Drained oil, sample taken, removed and inspected oil filter with no defects noted. Installed new filter, torqued and safetied. Serviced oil system with 8qts Phillips 20W50 XlC oil. Cleaned and regapped all spark plugs, checked mag timing, retimed left mag and checked all ignition leads. Inspected all baffling, plumbing, wiring and component security. Checked cylinder and fuel nozzle condition. Lubed engine controls. Replaced induction air filter element PIN BA24. Inspected exhaust system, removed and replaced muffler pin with an overhauled unit certified by Aerospace Welding Minneapolis, Inc., FAA CRS # UWDR792L on 9/8/10 under WO # and heat exchanger pin with an overhauled unit certified by Aerospace Welding Minneapolis, Inc. FAA CRS # UWDR792L on 9/21/10 under WO # , secured per Chapter Grd run, fuel system checked per TCM SB SID 97-3E, found within limits, ops and leak check good. I certify this Engine has been inspected law a 100hriAnnuai inspection using Cirrus SR22 MM, Chapter 5-20 and TCM MM ICA, Chapter 5 inspection checklist as revised and was determined to be in airworthy condition and a roved for return to service. Ref. WO#RDU for further details. Next 50hr ins ection due at FH eriormed onl and was found airworth and is a roved for return to service. Pertinent details of this re air are on file at this facilit. RDU N 602UK Cirrus SR Engine: SIN: Performed 50 hr inspection per AMM 5-20 checklist.. 2. Drained oil and removed filter, inspected filter for contamination, No contamination noted, Installed, torque~ and safetied new filter PIN: CH Serviced engine with 8qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis Inspected oil lines and fittings, spark plug cable ends, air intak~ ducts, filter, air flapper valve for general condition.performed inspection check of exhaust system, inspected breather tube, Inspected engine compartment for loose hardware, Inspected cylinder drains for clogs and restrictions. Visually inspected magnetos.. 4. Performed ground runl operational check. With no leaks or defects noted. 4

5 Total Time Time Since Hrs. Min. Hrs. Min. Work Order No. Fli ht hobbs RDU UK CIRRUS Starter adapter slipping: Removed number one battery, heater duct, fuel lines, and throttle linkage to gain access. Removed starter and starter ad~~ter. Installed overhauled starter a~apter with new gasket and secured ground strap. Installed starter with new.o-ring and secured wlnng. Reinstalled fuel lines, throttle linkage and rekeyed, secured heater hose and clamps, and reinstalled number one battery. Ground ran, 0 s and leak checks ok. erformed onl and was found airworth and is a roved for return to service. Pertinent details of this re air are on file at this facilit Performed 100 Hr Inspection law TCM Maintenance Manual X3063"4. Drained oil; took sample. Opened and inspected oil filter; no abnormal particulates noted. Installed new oil filter, pin CH , and serviced with 8 qts Phillips 20W50 XlC oil. Performed ground run C\l)dleak check; no leaks noted. Performed engine compression check; results as follows: MO- 26/80, 1-68/80, 2-64/80, 3-71/80, 4-63/80, 5-66/80, 6-68/80. Cleaned, inspected, gapped, tested, rotated, and reinstalled sparkpluqs using new gaskets (pin M674). Corrected timing of both magnetos to 22 BTDC. Adiusted idle mixture and RPM. I certify that the work described above was performed satisfactorily aricj"in accordance with approvedlacceptable data and that this article is a roved for return to service with re ard to work erformed. 1K Jon A. Delamarter, A&P Hobbs Time RDU SR (TT) TCM, IO-550-N48, SIN Compression test results: 1)70/802)68/803)74/804)70/805)76/806)72/80. Master orifice:38psi. Drained I oil, sample taken, removed and inspected oil filter with no defects noted. Installed new filter, torqued and safetied. Serviced oil system with 7qts Phillips 20W50 XlC oil. Cleaned and regapped all spark plugs, checked mag timing (Mag 500hr inspection due), owner elected not to comply with at this time and checked all ignition leads. Fuel nozzle cleaning next due FH Inspected all baffling, plumbing, wiring and component security. Checked cylinder and fuel nozzle condition. Lubed engine controls. Replaced induction air filter assembly PIN BA 111, ': Cirrus PIN Inspected exhaust system, no defects noted. Grd run, fuel system checked per TCM SB SID 97-3E, found within limits, adjusted idle speed, ops and leak check good. I certify this Engine has been inspected law a 100hr/Annuai inspection using Cirrus SR22 MM, Chapter 5-20 inspection checklist as revised and was determined to be in airworthy condition and approved for return to service. (Ref. WO#RDU for further details). Next 50hr ins ection due at FH563.0 performed only and was found airworthy and is ap roved for return to service. Pertinent details of this re air are on file at this facilit. Signature: 5

Brou~ Total Time Time Since Hrs. Min. Hrs. Min. Engine Logbook Entry Engine Service and Maintenance Rec~rd Paragon Aircraft Service, Inc.

2 6990 ~ [Changed oil and filter cut open old filter, no metal found. Oil sample taken. Borescoped cylinders no defects noted. Serviced with 8 quarts 15W50 Aeroshell.

I certify that this engine has been inspected in accordance with an Annual Inspection and determined to be in an airworthy condition.

Signature: Steven VanderValk A&P 2919106 IA Engine Logbook Entry.Ii).ate Make/Model Serial# Total Time 8/8/2012 10-550-N48 691933 556.

on @ Flight time 1056.6. Run and leak check satisfactory.

6 Brou~ Total Time Time Since Hrs. Min. Hrs. Min. Engine Logbook Entry Engine Service and Maintenance Rec~rd Paragon Aircraft Service, Inc. 19 Wright Way, Fairfield, NJ Phone: (973) Fax (973) Make/Model Serial# Total Time w.o. 2/14/2012 Cirrus SR ~ [Changed oil and filter cut open old filter, no metal found. Oil sample taken. Borescoped cylinders no defects noted. Serviced with 8 quarts 15W50 Aeroshell. Spark plugs cleaned and gapped, magneto timing checked. #172/80, #272/80, #3 74/80, #4 74/80, #5 72/80, #6 72/80. Checked fuel flows per TCM SID 97-3C. Engine washed and run-up checked OK. I certify that this engine has been inspected in accordance with an Annual Inspection and determined to be in an airworthy condition. I certify that the work described above was performed in accordance with approved/acceptable data and is approved for return to service with regard to work performed. Signature: Steven VanderValk A&P IA Engine Logbook Entry.Ii).ate Make/Model Serial# Total Time 8/8/ N Removed Magnetos P/N SIN D08HA024 and D08HA246 and sent to G&N Aircraft for 500hr inspection see attached tags. Installed Inspected magnetos timed to engine. Next due for Flight time Run and leak check satisfactory. I certify that the work described above was performed satisfactorily and In accordance with approved/acceptable data and IS approved for return to service with regard to work performed. Signature: John L Longaker A&P Engine Logbook Entry Paragon Aircraft Service, Inc. 19 Wright Way, Fairfield, NJ Phone: (973) Fax (973) N' Number Make/Model Seriill# Flight Total Time W. O. 5/2/2013 N602UK TCMII0550N Changed oil and filter cut open old filter, no metal found. Borescoped cylinders checked OK. Serviced with 7 quarts Phillips 20W50. Spark plugs replaced with new URHB32E, magneto timing checked. #1 70/80, #2 72/80, #3 72/80, #4 70/80, #5 72/80, #6 70/80. Checked fuel flows per TCM SID 97-3C. Engine washed and run-up checked OK. I certify that this engine has been inspected in accordance with an Annual Inspection and determined to be in an airworthy condition. I certify that the work described above was performed in accordance with approved/acceptable data and is approved for return to service with regard to work performed.. Signature: Steven VanderValk A&P IA 6

CIRRUS AIRPLANE MAINTENANCE MANUAL

CIRRUS AIRPLANE MAINTENANCE MANUAL POWER PLANT 1. GENERAL This chapter describes maintenance practices for the airplane systems which provide the means to induce and convert fuel-air mixture into power such as the engine, baffling, cowling,