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. Opened and inspected oil filter; no abnormal particulates noted. Installed new oil filter, pin CH48108-1, 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 630979-9), rubber washers (pin 640612), and copper crush washers (pin X1473). Next fuel injection nozzle service due 332.2 hours TIS. Removed defective #1 alternator, pin 656802 (Kelly pin ES-10024) sin 1081327; installed new #1 alternator, pin 656802 (Kelly pin ES-10024) sin 1102201. 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 3230521 RDU003618 SR22 89.7(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. 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: CH481 08-1. 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. RDU004516 9-10-09 Cirrus SR22 TCM, 10-550-N48, SIN 691933. 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 15080-001 and P/N 15073-001due to securement hole elongation, assembled with new AN4C-35 bolts and keyed. Torqued per TCM 10-550 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#RDU004527 for further details). Next 50hr inspection due at FH218.6. 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&P246826452IA RDU- 5060' 11/27/2009 N602UK SR22 279.7 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: CH48108-1. 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 24-30 with new unit from Teledyne Continental ta. '" CE#-832441 under W/O: 109997 Off Unit: PIN: ES10024 SIN: 1102201 On Unit: PIN: ES10024 SIN: J081813 **************** End ****""**************
----~...= ~~~~ lnstajlations, Inspections, Airworthiness Directives, Special Inspections, 12635-001. Ground ran ops and leak checks ok. b~ ~ C I II R U S Hobbs Time Fli ht Hobbs 304.8 240.9 b~ ~ C I R R U S Serial No: Hobbs Time FH/TI SR22 331.9 262.3?:5~=:E~':JI :..is:!.!::;;;.;er.larx:e Program 100 hour inspection law TCM ICA, Chapter 5 inspection checklist. )76/802)74/803)77 180 4)77 180 5)73 180 6)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 3236539 Jon A. Delamarter, A&P 3035359 3
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 MS29513-137) and new stat-o-seal (pin NAS 1523-8B). Corrected magneto to engine timing on both mags. Cleaned, inspected, and reinstalled fuel injection nozzles using all new seals (pin 640612, 630979-9, 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, 6-72180. 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 CH48108-1, 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 3035359 9-29-10 SR22 TCM, IO-550-N48, SIN 691933. 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 14836-001 with an overhauled unit certified by Aerospace Welding Minneapolis, Inc., FAA CRS # UWDR792L on 9/8/10 under WO # 135498 and heat exchanger pin 21892-001 with an overhauled unit certified by Aerospace Welding Minneapolis, Inc. FAA CRS # UWDR792L on 9/21/10 under WO # 135875, secured per Chapter 78-20. 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#RDU007001 for further details. Next 50hr ins ection due at FH446.3. 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-7888 1-18-11 N 602UK Cirrus SR22 553.2 Engine: SIN: 691933 1. 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: CH48108-1. Serviced engine with 8qts. Oil, type: Phillips 20W50 XC, Oil sample taken for analysis... 3. 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
Total Time Time Since Hrs. Min. Hrs. Min. Work Order No. Fli ht hobbs RDU 8193 2-25-11 602UK CIRRUS 563.5 451.2 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. 691933 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 CH481 08-1, 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 3035359 Hobbs Time RDU009869 9-21-11 SR22 638.3 513.0(TT) TCM, IO-550-N48, SIN 691933. 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 653.7. 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 50207-001. 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#RDU009930 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. 19 Wright Way, Fairfield, NJ 07004 Phone: (973)575-0364 Fax (973)244-1884 Make/Model Serial# Total Time w.o. 2/14/2012 Cirrus SR22 534.2 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. 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 2919106 IA Engine Logbook Entry.Ii).ate Make/Model Serial# Total Time 8/8/2012 10-550-N48 691933 556.6 7228 Removed Magnetos P/N1 0-500556-1 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 inspecti.on @ Flight time 1056.6. 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 3532411 Engine Logbook Entry Paragon Aircraft Service, Inc. 19 Wright Way, Fairfield, NJ 07004 Phone: (973)575-0364 Fax (973)244-1884 N' Number Make/Model Seriill# Flight Total Time W. O. 5/2/2013 N602UK TCMII0550N48 691933 572.3 713.6 572.3 7487 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 2919106 IA 6