Technical History for Cessna 414A SN 414A0317

Manufacturer: Cessna Total Time 5673.4 Prepared by: Shoreline Aviation, Inc., Marshfield, MA Model: 414A Ser. # 414A-0317 Item Part PART Part Serial D U E Installed # No. Description Number Hours Cycle Date HoursCycl Date Hours Cycle Date 1 TSIO 520-NB Engine, Left 514067 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 2 TSIO-520-NB Engine, Right 519264 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 3 PHC-C3YF-2UFPropeller, Left EB7625B 7226.9 5/31/2025 2400.0 72 months 4826.9 5/23/2019 4 PHC-C3YF-2UFPropeller, Right EB7629B 7226.9 5/21/2025 2400.0 72 months 4826.9 5/23/2019 5 DCFS290D9/T3Prop. Gov., Left 950126 7452.5 3/31/2028 2000.0 60 months 5452.5 3/14/2023 6 DCFS290D9/T3Prop Gov., Right 990118 7452.5 3/31/2028 2000.0 60 months 5452.5 3/14/2023 7 ES6320 L eng, L magneto K-K07006 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 8 ES6320 L eng, R magneto K-K07007 7052.5 3/31/2035 1600.0 144 mionths 5452.5 3/14/2023 9 ES6320 R eng, L magneto K-K07008 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 10 ES6320 R eng, R magneto K-K07009 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 11 RAP442CW Vac. Pump, Left D10833 6052.5 600.0 5452.5 3/14/2023 12 AA442CW Vac. Pump, Right D10647 6052.5 600.0 5452.5 3/14/2023 13 ALV-9610 Alternator, Left H-W091335 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 14 ALV-9610 Alternator, Right H-W091336 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 15 466412-5 Turbo, Left H-ZIL00019 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 16 466412-5 Turbo, Right H-ZIL00018 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 17 470836-9020 Turbo control, left BK0199 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 18 470836-9020 Turbo control, Right ELR0103 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 19 470908-9012 Wastegate, Left OKR0112 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 20 470908-9012 Wastegate, Right EK016184 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 21 1020-1 MAP popoff, Left CG0156 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 22 1020-2 MAP popoff, Right H-YIO00132 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 23 646210-11A4 Fuel pump, Left B00EA404R 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 24 646210-11A5 Fuel pump, Right D029922BR 7153.5 3/31/2035 1600.0 144 months 5553.5 11/14/2023 25 1697-2 Throttle body, Left N/A 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 26 1697.2 Throttle body, Right N/A 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 27 640718-2A4 Fuel Spider, Right B139506CR 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 28 640718-2A4 Fuel Spider, Left C189513CR 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 29 642100-5/6 Fuel Press Reg.-LH 225009 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 30 642100-5/6 Fuel Press Reg.-RH 497080 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 31 8000440 Oil Cooler, Left 1672104 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 32 8000440 Oil Cooler, Right 4082828 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 33 1638-4 Intercooler, Left 1753759 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 34 1638-4 Intercooler, Right 1753758 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 35 24199LAA Hyd. Pump, RH 338 7052.5 1600.0 144 months 5452.5 3/14/2023 36 24199LAA Hyd. Pump, LH 1717 7052.5 1600.0 144 months 5452.5 3/14/2023 37 642085A4 Str. Adapter, LH 227090 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 38 642085A4 Str. Adapter, RH 228090 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 39 646275-1 Starter, Left T-149957 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 40 646275-1 Starter, Right H050037 7052.5 3/31/2035 1600.0 144 months 5452.5 3/14/2023 Service Life N414MP COMPONENT TIMES ...,.......,""'l;n,................... . .---. ------ ... ---to-- --.............. . ..---1------ -- •••••••••••• AD NOTES COMPLIANCE RECORD Airframe - Cessna - 414A s/n: 414A-0317 Appliance - Air Filter - Paper Induction Appliance - Heaters - Kelly Aerospace Power Systems Appliance - Safety Belts - AM Safe Appliance - Transponder - GARMIN GTX 330 s/n: 84108536 AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA per serial #. 72-03-07 Landing gear failure Ed Novak A+P 2832024 IA X DNA per serial #. 76-13-07 Fork bolts X Ed Novak A+P 2832024 IA DNA per serial #. 76-16-07 Engine attachment tangs X Ed Novak A+P 2832024 IA DNA per serial #. 78-11-05 Autopilot actuator Ed Novak A+P 2832024 IA X DNA per serial #. 78-13-05 Improperly installed seats Ed Novak A+P 2832024 IA X DNA per serial #. 80-13-14 Fuel flow transducer Ed Novak A+P 2832024 IA X DNA - windshields are not original factory installation. 84-03-04 Windshield instln. insp. Ed Novak A+P 2832024 IA X Installed SK421-121 per MEB84-10. 84-20-02 Nose landing gear 11/1/84 - 760.0 Ed Novak See log entry X Superseded by 97-26-16. 85-13-03 R2 Engine mount beams X Ed Novak A+P 2832024 IA Installed SAD531-037 fuel filler restrictors. 87-21-02 R1 Fuel filler openings 6/16/89 - 1271.0 Ed Novak See log entry X Both MLG strut bearings replaced with new 5141109-1 units. 90-02-13 Main landing gear 5/13/98 - 3902.1 X Ed Novak See log entry. Superseded by 95-09-13. 93-05-03 Fuel float valve X Ed Novak A+P 2832024 IA Performed fuel inlet float valve test per MEB93-10R1. 95-09-13 Fuel float valve 9/13/21 - 5233.6 X 5833.6 Ed Novak See log entry DNA - affected component not installed. 97-01-13 Fuel, oil, or hydraulic hose Ed Novak A+P 2832024 IA X Installed kit # SK414-19B. 97-26-16 Engine mount beams 9/9/85 - 853.0 X Ed Novak See log entry Inserted copy of AD into AFM. 98-04-28 Severe Icing Conditions 7/22/13 - 208.6 Ed Novak See Log Entry X DNA per date of mfg. 98-24-14 Exhaust leaks caused by nonwelded exhaust system components Ed Novak A+P 2832024 IA X 1 09/13/2024 3 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. Para. B next due 5700.9 Para. C due 03/25 Para. D due 5952.5 Para. E due 03/25 or 6097.8 Para. F - DNA all clamps are one piece design. Para. G due 03/35 or 7972.5 2000-01-16 Detect and correct cracks and corrosion in the exhaust system 8/1/24 - 5650.9 X 5700.9 (para B) Ed Novak A+P 2832024 IA Superseded by PL2005-05-52. PL2005-05-51 Detect and correct cracking in the wing spars before the cracks grow to failure X Ed Novak A+P 2832024 IA Superseded by 2005-12-13. PL2005-05-52 Detect and correct cracking in the wing spars before the cracks grow to failure X Ed Novak A+P 2832024 IA Due at 15,000 hrs. ACTT. 2005-12-13 Prevent wing spar cap failure caused by undetected fatigue cracks X Ed Novak A+P 2832024 IA Switch p/n 110-240 installed. 2005-20-25 Prevent failure of the avionics bus circuit breaker switch Ed Novak See log entry X DNA - affected STC is not installed. 2012-23-01 To prevent failure of the flap system Ed Novak A+P 2832024 IA X Due at 15,000 hrs. 2015-07-03 Engine Mount Beams X Ed Novak A+P 2832024 IA Superseded by 2016-17-08. 2016-07-24 Elevator Trim Tab Assembly Parts Attachment Hardware Security X Ed Novak A+P 2832024 IA Inspected hardware repetitively per AD instructions and noted no defects. 2016-17-08 Elevator Trim Tab Assembly Parts Attachment Hardware Security 8/1/24 - 5650.9 (ACTT) X 8/25 or 5760.9 (ACTT) Ed Novak A+P 2832024 IA DNA until SK402-47 is installed. 2017-10-09 Engine Nacelle Fittings Integrity X Ed Novak A+P 2832024 IA Superseded by revision R1 2018-03-03 Lower Forward Carry Through Spar Cap Integrity X Ed Novak A+P 2832024 IA Due at 15000 ACTT. 2018-03-03 R1 Lower Forward Carry Through Spar Cap Integrity X 15000 Ed Novak A+P 2832024 IA DNA - the installed turbo tailpipe clamps are not segmented vee/spot welded type. 2023-09-09 Failures of Spot-Welded, Multi-Segment V-Band Couplings X Ed Novak A+P 2832024 IA New paper induction air filters installed. 84-26-02 Paper induction air filters 12/2/22 - 5452.5 X 5952.5 Ed Novak See log entry Superseded by 96-20-07. 82-07-03 Janitrol combustion heaters X Ed Novak A+P 2832024 IA Superseded by 2004-21-05. 96-20-07 Janitrol combustion heaters X Ed Novak A+P 2832024 IA Superseded by 2001-17-13. 2001-08-01 Prevent fuel leakage in airplanes Ed Novak A+P 2832024 IA X Superseded by 2004-25-16. 2001-17-13 Potential for fuel leakage in aircraft X Ed Novak A+P 2832024 IA Completed pressure decay test and airflow switch test to the cabin heater. 2004-21-05 Prevent combustion by-products (carbon-monoxide exhaust) and fuel leakage from the combustion heaters 3/1/24 - HH 630.5 X 03/26 or HH 730.5 Ed Novak A+P 2832024 IA Superseded by R1. 2004-25-16 Prevent failure of the fuel regulator shutoff valve X Ed Novak A+P 2832024 IA 2 09/13/2024 3 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. Duplicate. 2004-25-16 R1 Prevent failure of the fuel regulator shutoff valve X Ed Novak A+P 2832024 IA Check heater fuel regulator/shutoff valve for proper operation. 2004-25-16R1 Prevent failure of the fuel regulator shutoff valve 08/01/24 - 5650.9 X 08/25 or 5750.9 Ed Novak See log entry DNA per part #. 87-17-06 AM Safe restraint system Ed Novak A+P 2832024 IA X Superseded by 2005-01-19. 2004-10-15 Prevent interrogating aircraft from possibly receiving inaccurate replies Ed Novak A+P 2832024 IA X DNA per software version installed. 2005-01-19 Prevent interrogating aircraft from possibly receiving inaccurate replies Ed Novak A+P 2832024 IA X 3 09/13/2024 3 Page of N414MP N414MP PERFORMANCE CHARTS WEIGHT & BALANCE \ • \ ,. ' . . • I . . . . . : • • • • 1 . Aircraft Registration ________ Engine Position _ h L....-...- ~ _,__ 9 _ -\- _____ Engine Serial No. _5_ 1_4_o_" _7_____ ENGIN E MAINTE NAN CE RECORDS Log No. _ _ _ _ Aircraft Registration No. _ ________ Model __ --r_~~J O~ -_ S_"J.._O_ -o _ f!J______ _ Serial No . .5 /t..Jo~7 Date installed on aircraft _________ Time Between Overhauls (TBO,__ _ __ Hours If used on multi-engine aircraft: 0 Right ~ Left Waco Regional Airport 7505 Karl May Drive • P.O. Box 5219 • Waco, Texas 76708 Phone: (254) 752-8381 Fax: 254-752-3307 www.ramaircraft.com "LOGBOOK FORMAT REPRINTED WITH THE PERMISSION OF AEROTECH PUBLICATIONS, INC., THE AD LOG(™) SYSTEM, COPYRIGHT 1979." Page No..___ DATE TOTAL TIME IN SERVICE Total Date Time In Service 09/28/2022 5832.6 TOTAL TIME SINCE OVERHAUL Total Time Since overhaul 0.0 TACH OR RECORDING METER TIME Recording Meter llme DESCRIPTION OF WORK PERFORMED- SIGNATURE & CERTIFICATION NO. OF PERSON PERFORMING WORK TOTALS brought forward from previous page RAM Aircraft, Limiled Partnership• Waco Regional Airport CONTINENTAL TSIO-520-NB Series VII 414A Left Engine S/N 514067 Above referenced engine overhauled to new parts limits per FAR 43.2(a)(1){2) to conform w/CMI SM X-30574 and Continental M-0. Standard Practice Maintenance Manual. Applicable AD's and Service Bulletins ciw at this time. All gears cleaned, polished when requi re d. inspected, magnetic particle inspected, and no cracks found. Finish and dimensional limits within RAM Gear Inspection Specification No. 1818, Rev. P dated 07/19/2017. Above referenced engine modified to TSIO-520-NB 335 HP per STC SE09104SC-D (includes STC SE4327SW-D). Installed new RAM camshaft pin 1058-20, s/n XI 21078 per S TC SE09104SC-D. Installed new lifters p/n SA628488 (int), pin SA646277 (exh}. AD 10-11-04 n/a to lifter p/n installed. AD 97-26-17 c/w per installation of overhauled VAR cranks haft p/n 642396, s/n F462 per TCM CS B96-8. CNV ultrasonic inspection per MSB96-10B, due at next overhaul or when crankshaft removed. AD 99-19- 01 n/a per crankshaft date of manufacture 1/A/W TCM MSB99-3C. AD 2000-23-21 NIA to crankshaft serial number/date of manufacture 1/A/W TCM Mandatory Service Bulletin MSB00-5O. Engine assembled with new RAM crankcase pin 2922-1, s/n 21 K0397. Installed new Superior steel cylinders. Installed overhauled oil cooler p/n 654580, sin 1672104. C/W AD 89-24-01 R1 per installation of starter adapter pin 642085A4 with current scavenge pump gears. AD 2012-10-13 AND MSB11-4B Starter Adapter inspection NIA per p/n installed or manufacture date. Installed new RAM/FAA/PMA fuel nozzles p/n 2562-14D. TCM Service Bulletin SB06-1A NIA per installation of RAM fuel nozzles. lnsta.lled modified connecting rods pin 1162 per STC SE4327SW-D as FAA/PMA approved replacement. Engine accessories exchanged for overhauled or new units with exception of prop governor, alternator, vacuum pump, hydraulic pump and tach generat or wh ich were not i ns~alled per this work order. New Kelly pressurized magnetos p/n ES6320 installed per STC SE4651SW-D and pressurized. MSB94- 8O on magneto timing procedu re c/w per timing to STC degree requirements with TDC locator and protractor with pointer. Engine modified to TSIO-520- NB per Continental Service Bulletin M75-6 Rev 1. P/N 652130 & 652131 rocker arms installed. Installed RAM/FAA/PMA oil cooler baffle pin 1253-1, rocker arm cover gaskets pi n 1387-1 ,spring loaded induction clamps p/n 1170-2 and double clamp pin 1170-5. Category 1 thru 3 CMI Service Bulletin Compliance Listing in RAM Manual. Engine ground run on test stand per RAM specifications for 120 minutes. Engine run - in with Aeroshell 100 Mineral oil. See RAM Recommended Oil Graci e Maintenance Tip MT-1 for recommended oils. Engine approved for return to service for the work performed. Engine preserved per Continental M-0. Standard Practice Maintenance Manual temp. storage up to 90 days. Pertinent details on file under Project No 10271 . • RAM Aircraft, Limited fuership, P.O. Box 5219, Waco Texas 76708 CRS VA1R551K SUB-TOTALS this page TOTALS-Carry forward to next page 3114/2023 N414MP A~Shoreline ..ti.VIATION Shoreline Aviation, Inc. - ----------Marshffeld Munjcipal Airport GeorQ<i! Harlow Field (GHG) _. 93 Old Colony Lan& • _.. Mari:.hlield. MA 02050 Engine 1 Logbook Cessna 414A, serial # 414A-0317 Hobbs Hours: 1629.9 :: Aircraft TT: 5452.5 ;: #1 Engine TT: 4692.5 :: #1 Engine TSMOH: o.o 1) This engine install7d onto_the right side of Cessna 414A, N414MP, serial# 414A-0317 using all new engine mounts per Ram and Cessna 414A mamtenance manual 1nstruct1ons. · 2) All accessories and oil and fuel h~ses were provided by_RAM an~ installed except for vac. pump, tach gen, hydraulic pumps, prop, prop gov and aJtern~t~r. Prop gov was 0/H an~ reinstalled from_ the prel.'.1ous engine. A new vacuum pump was installed. A new alternator was installed reusin !he e~isting altemato~ dnve coupling from the_Prev1ous eng!ne. Tach gen was reinstalled from the previous engine in "as removed" condit1on. 9 Land!ng gear_hydr_aulic pump was replaced with an 0/H unit Propeller was reinstalled from the previous engine in "as removed" condition after flushing the 011 cylinder. 3/ Engine was serviced with 12 qts. of Phillips Type M 20w-50 mineral oil and pre-oiled per RAM instructions. Engine was also turned by hand n011 pressure was read on the cockpit gage. un 1 4) Set idle speed, idle mixture, low ~nmetered fuel pump pres.sure, high unmetered fuel pump pressure & maximum MAP at full power. 5) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. Thhe above work ~as completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for t e work accomplished. Shoreline Aviation, Inc. 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 5/10/2023 N414MP Edward J_ Novak Jr. A+P 2832024 IA Shoreline Aviation, Inc. ,) Marshfield Munic;ipaf Airport George Harlow Field (GH G) 93 Old Colony Len@ • ~ Marakfield. MA 02060 Cessna 414A, serial# 414A-0317 Engine 1 Logbook Hobbs Hours: 1658.2 :: Aircraft TT: 5480.8 .. #1 Engine TSMOH: 28.3 :: #1Propeller SMOH: 653.9 :: #2 Propeller SMOH: 653.9 :: #2 Engine TSMOH: 28.3 :: Heater Hobbs: 612.5 Completed Operation #3 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) Cyl. Comp. Checked per TCM SB 03-03 - all cyls. checked above minimum (42). 1) 70/80 2) 72/80 3) 72/80 4} 68180 5} 72/80 6) 74/80. 2) C/W the follwing TCM repetitive SB's: M90-17 {C/C lnsp), S895-2 {Control Linkage lnsp), S895-7 (Fuel Manifold valve cover insp), S696-12 {cyl lnsp.), SB9S.7C (Torque Values), MSB94-8D (Mag Timing), S1D97-3G (Fuel System), SB09-14 (C/S Rust} and SB17-01A {flanged nut insp.), S620- 01 (fuel screen} and noted no defects. 3} #1 lower spark p!ug replaced with a new unit (part# URHB32E}. 4) Drained oil, added 11 qts. of Phillips Victory 100W (SAE-50) oil. Installed and saftied a new M48108-2 oil filter. Cut open filter and found no abnormal contaminants. 5) Ground runup and systems functional checks completed with satisfactory results and no fuel I certify that this Engine has been inspected in accordance with an Operation #3 inspecU and :,;:~=p- be in an airworthy condition. 612912023 N414MP Hobbs Hours: 1686.9 :: Aircraft TT: 5509.5 TSMOH: 57.0 :: Heater Hobbs: 613.8 Signed_-',S!t._..:+-1~--11--- --------- ---- A.Shoreline fiVIATION Shorelln& Aviation, Inc. • •➔ Matshllokl Municipal Airpert Geo,ge Harlow Flefd (GHG) 93 Old Colony Lane ~ Mal'lthfie!d. MA02050 Cessna 414A, serial# 414A-0317 •• #1 Engine TSMOH: 57.0 :: #1Propeller SMOH: 682.6 Engine 1 Logbook :: #2 Propeller SMOH: 682.6 :: #2 Engine Completed 50 hr. Special inspection items as follows: Drained oil, added 11 qts. of Phillips Victory SAE50 oil. Installed and saftied a new AA48108- 2 oil filter. Cut open filter and found no abnormal contaminants. Runup and leak check OK. The above work was completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work accomplished. • Signed atw-t"'-JJJ/,1~ ~ Edward J. Novak Jr. A4>2a32024 IA TOTAlS-Carry forward to next page A.:'horeline fiVIATION _____Sho _ re_ Hn_e_A_~Ja_ ti_o_n_,'_,"c+. •➔ Man;hllold Municipal A;rp0n G90f9f/ Hlll1ow Field (GHG) _. $3 Old ColonylaM __.. Melllhfiekt MA 02050 10/25/2023 N414MP Cessna 414A, serial# 414A--0317 Engine 1 Logbook Hobbs Hours: 1724.6 :: Aircraft TT: 5547.2 ;: #1 Engine TSMOH: 94.7 :: #1 Propeller SMOH: 720.3 :: #2 Propeller SMOH: 720.3 :: #2 Engine TSMOH: 94.7 :: Heater Hobbs: 613.8 Completed Operation #1 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) •CyL Comp. Checked per TCM SB 03-03 1) 72/80 2) 72/80 3) 62/80 4) 72180 5) 68/80 6) 70/80. 2) CN'J the follwing TCM repetitive SB's: M90-17 {CIC lnsp}, SB95-2 (Control Linkage lnsp), SB95-7 {Fuel Manifold valve cover insp), S696-12 (cyl lnsp.), S896-7C (Torque Values), MSB94-8D (Mag Timing), S1D97-3G (Fuel System), S809-14 {C/S Rusi) and SB17-01A (flanged nut insp.), S820- 01 (fuel screen) and noted no defects. 3) Completed 50 hr. special inspection as follows: Drained oil, added 11 qts. of Phillips X/C 20W-50 o!I. Installed and saftied a new M48108-2 oil filter. Cut open filter and found no abnormal contaminants. 4) Installed one new URHB32E for the RH magneto, #3 cylinder (lower spark plug). 5) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. I certify that this Engine has been inspected in accordance with an Operation #1 i;;e~lo~:ite:tn~fn airworthy condition. Edw~. Novak Jr. A+P 2832024 IA t----- --·-···--------- At,horeline rtVIATION ____ _s_h_o_re_11n_e_ A_v_1a_ti_o_n,_1n-->t'c. ,) Marshfield Municipal Airport Gl>Otge Harlo,o, Field (GHG) 93 Old Colony Lane ~ Marst>fiald. MA 02050 3/1/2024 N414MP Cessna 414A, serial# 414A--0317 Engine 1 Logbook Hobbs Hours: 1775.2 :: Aircraft TT: 5597.8 :: #1 Engine TSMOH: 145.3 :; #1 Propeller SMOH: 770.9 :: #2 Propeller SMOH: ._.__ 770.9 :: #2 Engine TSMOH: 145.3 :: Heater Hobbs: 630.5 Completed Operation #2 inpseclion items per the Cessna 414A Maintenance manual progressive care inspection fonn. 1----- 1) Drained oil, added 11 qts. of Phillips XJC 20w-50 oil. Installed and saflied a new AA48108-2 oil filler. Cut open filter and found no abnormal contaminants. 2) Adjusted the idle mixture setting 1/2 tum towards rich. . ---- 3) Ground runup and systems functional checks completed with satisfactory results and no fuel or 011 leaks noted. The above work was completed in accordance with current regulations of the Federal Aviation Administration nd is approved for t----- return to service for the work accomplished. /; / . / 8/1/2024 N414MP Hobbs Hours: 1828.3 :: Aircraft TT: 5650.9 TSMOH: 198.4 :: Heater Hobbs: 632.7 Signed ~(,,,-f...lHVv\.#1_ Edward J. Novak Jr. A+P 2832024 IA Shoreline AVIATION Shoreline Aviation, In~. • .,, Marshfield Munlelpal Airport George Harlow Field (GHG) 93 Old Colony Lan" ~ Mar!!h~eld. MA!)2()5() Cessna 414A, serial # 414A..{1317 Engine 1 Logbook :: #1 Engine TSMOH: 19S.4 :: #1Prope!ler SMOH: 824.0 :: #2 Propeller SMOH: 824.0 :: #2 Engine Completed Operation #3 & #4 inspection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) Cyl. Comp. Checked per TCM SB 03-03 1) 70/80 2) 72/80 3) 70/80 4) 65/80 5) 70/80 6) 68/80. 2) C/W the follwing TCM repetitive SB's: S895-2 (Control Linkage lnsp), SB95-7 (Fuel Manifold valve cover insp), 5B96-12 (cyl lnsp.), SB96·7C (Torque Values), MS894-8D {Mag Timing), S1D97-3G (Fuel System), 5B09-14 (CIS Rust) and SB17-01A (flanged nut insp.), S620-01 (fuel screen) and noted no defects. 3) Completed 50 hr. special inspection as follows: Drained oil, added 11 qts. of Phillips XJC 20W-50 oil. Installed and saftied a new AA48108-2 oil filter. Cut open filter and found no abnormal contaminants. 4) Installed 10 new URHB32E spark plugs (all but '116 upper & #3 lower). 5) Adjusted the idle mixture 1/2 turn CW to richen the idle mixture. 6) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. I certify that this Engine has been inspected in accordance with an Operallon #3 & #4 inspectio ermined to Signed '1- AD NOTES COMPLIANCE RECORD Engine - Continental Motors - TSIO-520-NB s/n: 514067 Propeller - Hartzell - ( )HC-( )( )Y( ) m/n: PHC-C3YF-2UF s/n: EB7625B Appliance - Connecting Rods - Engine Components Incorporated (ECi) Appliance - Governors - McCauley Appliance - Magnetos - Slick Appliance - Cylinder assembly - Superior Air Parts AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA - affected component not installed. 2006-10-21 CORRECTION - To prevent fatigue failure of the connecting rod and a possible uncommanded shutdown of the engine. Ed Novak A+P 2832024 IA X DNA per part #. 75-12-07 McCauley governors Ed Novak A+P 2832024 IA X DNA to LH gov. per Bruce at New England Prop. because they don't use these McCauley bearings. 2020-19-06 Idler Gear Bearing Unapproved Variant Ed Novak A+P 2832024 IA X DNA per part serial #. 74-18-05 Slick magnetos X Ed Novak A+P 2832024 IA DNA per part serial #. 80-06-05 Slick magnetos Ed Novak A+P 2832024 IA X DNA per part serial #. 81-16-05 Slick magnetos Ed Novak A+P 2832024 IA X DNA per engine model #. 99-04-04 Magneto impulse coupling X Ed Novak A+P 2832024 IA DNA per engine model #. 2011-26-07 To prevent engine failure due to migration of the magneto impulse coupling stop pin X Ed Novak A+P 2832024 IA DNA per engine model #. 97-01-04 Cylinder assemblies X Ed Novak A+P 2832024 IA Superseded by R1 2007-04-19 To prevent cylinder separation that can lead to engine failure X Ed Novak A+P 2832024 IA DNA per cylinder part #'s. 2007-04-19R1 To prevent cylinder separation that can lead to engine failure X Ed Novak A+P 2832024 IA DNA per engine model #. 78-06-01 R2 Flexible intake elbow X Ed Novak A+P 2832024 IA C/W by RAM during engine O/H. 79-05-09 Oil pressure relief valve 3/14/23 - 0 SMOH Ed Novak A+P 2832024 IA X DNA - affected component not installed. 80-01-04 Cylinder holddown flanges Ed Novak A+P 2832024 IA X DNA per date of installation. 81-24-06 Fuel pump X Ed Novak A+P 2832024 IA 1 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA per engine S/N. 82-09-01 Fuel pressure regulator leaks Ed Novak A+P 2832024 IA X DNA - affected component not installed. 86-13-04 R3 Cylinder assemblies X Ed Novak A+P 2832024 IA Superseded by 97-26-17. 87-23-08 Crankshaft fatigue cracks X Ed Novak A+P 2832024 IA DNA - affected component not installed. 88-03-06 Oil filter Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 89-24-01 R1 Scavenge oil pump gears 3/14/23 - 0 TSMOH Ed Novak A+P 2832024 IA X DNA - affected component not installed. 91-19-03 Champion oil filter Ed Novak A+P 2832024 IA X DNA per engine model #. 93-08-17 Incorrect oil pick-up tube Ed Novak A+P 2832024 IA X DNA - affected component not installed. 93-10-02 Cylinder valve retainer Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 93-16-15 Fuel pumps 3/14/23 - 0 TSMOH Ed Novak A+P 2832024 IA X Superseded by 95-21-15. 94-14-12 Low octane detonation Ed Novak A+P 2832024 IA X DNA per date of installation. 95-21-15 Engine teardown and analytical inspect. Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 97-26-17 CORRECTION - Crankshaft fatigue cracks 3/14/23 - 0 TSMOH X Next O/H or crankshaft removal Ed Novak A+P 2832024 IA DNA - affected component not installed. PL98-01-08 Exhaust roller rocker arms Ed Novak A+P 2832024 IA X Superseded by 99-19-01. PL99-09-17 Crankshaft failure Ed Novak A+P 2832024 IA X DNA per date of installation. 99-19-01 Crankshaft failure Ed Novak A+P 2832024 IA X Superseded by 2000-23-21. PL2000-08-51 Crankshaft connecting rod journal fracture X Ed Novak A+P 2832024 IA DNA per date of mfg. 2000-23-21 Fracture of the crankshaft connecting rod journal Ed Novak A+P 2832024 IA X DNA per date of mfg. 2004-08-10 Prevent loss of engine power Ed Novak A+P 2832024 IA X Superseded by 2014-05-29. 2009-16-03 To prevent the separation of the cylinder head X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2009-19-07 Correction - To prevent loss of engine power due to cracks in the cylinder head, possible engine failure, and fire in the engine compartment X Ed Novak A+P 2832024 IA Superseded by 2009-24-52. 2009-24-51 To address rapid wear on the face of hydraulic lifters X Ed Novak A+P 2832024 IA 2 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. Superseded by 2010-11-04. 2009-24-52 To address rapid wear on the face of hydraulic lifters X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2010-11-04 To prevent excessive hydraulic lifter wear X Ed Novak A+P 2832024 IA Superseded by 2012-10-13. 2011-25-51 To address fractures in starter adapter shaft gears Ed Novak A+P 2832024 IA X DNA - affected component not installed. 2012-03-06 To prevent an in-flight shutdown due to a failed fuel servo diaphragm X Ed Novak A+P 2832024 IA DNA per part #. 2012-10-13 To prevent starter adapter gear shaft failure X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2014-05-29 Superior Air Parts Investment Cast Cylinder Assemblies X Ed Novak A+P 2832024 IA DNA - all cyls are above serial # 61176 2016-16-12 ECI Class 71 or Class 76 Cylinder Assembly Failures Ed Novak A+P 2832024 IA X Superseded by 2023-17-04. 2022-04-04 STC Stratus Oil Filter Adapter Fiber Gasket Oil Loss Ed Novak A+P 2832024 IA X N/A - affected item not installed. 2022-16-03 S-1200 Series Magnetos Roller Bearings Improper Lubricatio Ed Novak A+P 2832024 IA X DNA per cylinder serial #'s. 2023-02-12 Intake Valve Failures Ed Novak A+P 2832024 IA X Superseded by 2023-05-16. 2023-04-08 Crankshaft Assembly Counterweight Retaining Rings in the Counterweight Groove Ed Novak A+P 2832024 IA X DNA - engine serial number. DNA - engine not assembled at TCM factory. 2023-05-16 Improper Installation of Counterweight Retaining Rings Ed Novak A+P 2832024 IA X N/A - affected STC not installed. 2023-17-04 STC F&M or Stratus Oil Filter Adapter Fiber Gasket Oil Loss Ed Novak A+P 2832024 IA X Superseded by 2002-09-08. 77-12-06 R2 Prop blade X Ed Novak A+P 2832024 IA DNA - propeller not returned to service by BASCO. 2001-07-03 CORRECTION - Prevent propeller failure of the propellers returned to service by BASCO Ed Novak A+P 2832024 IA X DNA per date of mfg. 2001-23-08 Prevent failure of the propeller hub resulting from cracks X Ed Novak A+P 2832024 IA Superseded by 2007-26-09. 2002-09-08 Prevent failure of the propeller blade from fatigue cracks Ed Novak A+P 2832024 IA X DNA per date of mfg. 2003-01-03 Prevent in-flight propeller blade separation Ed Novak A+P 2832024 IA X DNA per model #. 2003-03-20 Prevent fatigue failure of the original propeller hub and blades Ed Novak A+P 2832024 IA X DNA - propeller is O.E.M. 2003-13-17 Maintenance by T&W Propellers Inc. Ed Novak A+P 2832024 IA X DNA - propeller is O.E.M. 2005-14-11 Maintenance by Southern California Propeller Service Ed Novak A+P 2832024 IA X Superseded by 2009-22-03. 2006-18-15 To prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control X Ed Novak A+P 2832024 IA 3 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA - propeller is O.E.M. 2006-24-07 To detect unsafe conditions that could result in a propeller blade separating from the hub and loss of control of the airplane Ed Novak A+P 2832024 IA X DNA per date of mfg. 2007-26-09 To prevent failure of the propeller blade from fatigue cracks in the blade shank radius Ed Novak A+P 2832024 IA X DNA - propeller is NOT LH rotating. 2008-13-28 To prevent failure of the propeller hub X Ed Novak A+P 2832024 IA DNA per part serial #. 2009-22-03 To prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control X Ed Novak A+P 2832024 IA 4 09/13/2024 4 Page of N414MP N414MP LH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 514067 Item Bulletin Bulletin Bulletin Date # No. Description Date Completed Remarks 1 M67-12 Overboost - Engine 5/31/1967 Due if MAP goes 6" over redline 2 M70-11 Slick SB # 1-70 6/22/1970 DNA - Magneto M/N 3 M71-14 Slick SB # 1-71 6/21/1971 DNA - Magneto M/N 4 M71-21 Turbo Shaft Insp. 11/22/1971 Information Only 5 M72-17R1 Max Allowable Piston/Rod Weight Difference 10/5/1973 Information Only 6 M74-18 Slick S.B. 1-74 9/16/1974 DNA - Magneto M/N 7 M75-6R1 Model Conversion 6/4/1975 Information Only 8 M75-30 Prestolite Alternators 12/19/1975 DNA - not installed 9 M76-4 Crankcase Oil Seal Installation 3/12/1976 3/14/23 - 5425.5 Due at C/S oil seal change 10 M76-5R1 Remote Mounted Oil Coolers 5/25/1976 DNA - No Remote Oil Cooler 11 M77-3 Fuel Alternate Grades 1/11/1977 Infomation Only 12 M77-9 Thru Bolt Change 3/16/1977 DNA - already incorporated 13 M78-6 R+R of Rosan Exh. Studs 3/3/1978 Due during Exh. Stud R+R 14 M78-5R3 Flexible Elbow p/n 635930 10/23/1978 DNA - Engine M/N 15 M78-16 #2 Cyl. Intake Elbow p/n 629138 11/29/1978 DNA - Engine M/N 16 M80-10 R+R of Some 642232 Elbows 3/28/1980 C/W by RAM during O/H 17 M81-16 AiResearch S.L. TP61-0043-2 7/27/1981 DNA - RAM O/H Turbo 18 M81-19 Availability of New Flex Elbows 8/5/1981 DNA - RAM Elbows Installed 19 M81-25 Exhaust Flange to Cyl. Installation 11/30/1981 Superseded by SB14-8 20 M83-5 Slick S.B. 3-82 3/7/1983 DNA - Magneto M/N 21 M83-6 Slick S.B. 2-82 3/7/1983 DNA - Magneto M/N 22 M81-4R1 Airesearch S.L. TP61-0046 4/29/1983 3/14/23 - 5425.5 DNA per Date of O/H 23 M81-15R1 Prestolite Alternators 6/16/1983 DNA - not installed 24 M84-5 Gear Driven Alter. Insp. 2/13/1984 Due @ any alternator malfunction 25 M84-8 Mag Timing Indicator Plate 6/19/1984 DNA - No Timing Plate Installed 26 M84-13 Slick S.B. 1-84 10/27/1984 DNA - Magneto M/N 27 M85-9R1 Piston to Cyl. Dome Clearance 8/6/1985 DNA - ECI Cyls. Installed 28 M85-10 Cyl. Hold Down Nuts 7/18/1985 3/14/23 - 5425.5 C/W by RAM During O/H 29 M86-4 Fuel Pumps 1/9/1986 Due if fuel pump press. Wanders 30 M86-13R1 Cam Plug Insp. 10/17/1986 DNA per Date of O/H 31 M86-14 Camshaft 629726 Rework 10/1/1986 DNA - RAM Cam Installed 32 M87-15 Alternator Ground Strap 7/13/1987 3/14/23 - 5425.5 Due at eng. or alter. Replacement 33 M87-16 Slick S.B. SB1-86A 8/14/1987 DNA - Magneto M/N 3 M87-23 C/S Counterweights ID @ O/H 11/24/1987 3/14/23 - 5425.5 C/W by RAM During O/H 4 M88-4 TCM Oil Filters AD 88-03-06 1/15/1988 DNA - Not Installed 35 M88-9 Lightning Strikes 8/24/1988 Due at any lightning strike 36 M88-10 Contaminated Fuels 8/24/1988 Due when wrong fuel is used 37 M89-7 R1 Eng. Ops. After O/H or Cyl. R+R 8/4/1989 3/14/23 - 5425.5 C/W by RAM During O/H 38 M89-9 Excessive Crankcase Pressures 4/21/1989 Information Only 39 M89-18 EGT Recommendations 8/10/1989 EGT Information 40 M90-6 Scavenge Pump Gears 2/26/1990 3/14/23 - 5425.5 C/W by RAM during O/H 41 M90-13 Exh. Valve Stem Corr./Erosion 7/16/1990 Due at any access to exh. Valves 42 M90-16 7th Stud Improvement 8/22/1990 3/14/23 - 5425.5 C/W by RAM during O/H 43 M90-17 C/C Insp. Criteria 8/23/1990 DNA - RAM C/C Due at each 100 hr. Insp. 44 M91-4 Piston to Ring Application 2/11/1991 3/14/23 - 5425.5 Due at any piston ring change 45 M91-7 Cyl. Barrel Ultrasonic Insp. 3/20/1991 DNA - affected Cyls. NOT Installed 46 M91-6 Cyl. Barrel Insp. 3/20/1991 DNA - affected Cyls. NOT Installed 47 M91-9 Cam & Lifter Lube During Build 8/9/1991 3/14/23 - 5425.5 C/W by RAM during O/H 48 M92-6 Rockershaft Retention Improvement 2/28/1992 3/14/23 - 5425.5 C/W by RAM during O/H 49 M92-7 Deck Studs 5/26/1992 3/14/23 - 5425.5 C/W by RAM during O/H 50 M92-9 Flanged Thru-Bolt p/n 652541 5/29/1992 3/14/23 - 5425.5 C/W by RAM during O/H 51 M92-12 Alternator Thru-Bolt Insp. 8/27/1992 DNA per Alter. S/N 52 M92-14 Modine Oil Coolers 9/9/1992 DNA per Oil Cooler P/N 53 M93-4 C/S Counterweights 2/12/1993 3/14/23 - 5425.5 C/W by RAM during O/H 54 M93-8 Rocker Arm to Rotocoil Clearance 2/19/1993 3/14/23 - 5425.5 C/W by RAM during O/H 55 M93-5 Chamfer of Oil Feed Holes 2/19/1993 3/14/23 - 5425.5 C/W by RAM during O/H 56 M93-10 TCM Ign. SB No. 639 3/1/1993 DNA - No Impulse Couplings 57 MSB93-12 Valve Retainer Key Insp. AD 93-10-02 5/12/1993 DNA - Eng. S/N 58 CSB94-1 TCM Ign. SB No. 641 AD94-06-09 2/1/1994 DNA - Slick Mags Installed 59 SB94-2 Oil Filter adapter Mounting Stud 2/10/1994 3/14/23 - 5425.5 C/W by RAM during O/H 60 SB94-11 Oil Pump Gasket 11/14/1994 3/14/23 - 5425.5 C/W by RAM during O/H 61 CSB94-15 C/C Stud Insp. 12/2/1994 DNA - Eng. S/N 62 SB95-2 Insp.& Maint. Of Eng. Con. & Linkage 4/21/1995 8/1/24 - 5650.9 Due at ea. 100 hr. Or linkage work 63 MSB95-6 Fuel Pump Drive Coupling 10/19/1995 3/14/23 - 5425.5 C/W by RAM during O/H 64 SB95-7 Manifold valve Cover Insp. 12/8/1995 8/1/24 - 5650.9 Due ea. 100 hr. Or FF fluctuation 65 SB96-3B C/S Gear Bolt Insp. 3/14/23 - 5425.5 C/W by RAM during O/H 66 MSB96-10A C/S Ultrasonic Insp. AD 97-26-17 10/14/2008 3/14/23 - 5425.5 C/W by RAM during O/H N414MP LH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 514067 67 M90-14 Champion Action Alert 90-1 8/7/1990 DNA - effected part not installed 68 SB96-12 Continued A.W. Instr. For TCM Cyls. 9/10/1996 DNA - ECI Cyls. Installed 69 SB96-3B C/S Gear Bolt Insp. 10/14/1996 DNA per Date of Mfg. 70 CSB97-10A Piston Pin Plug Wear AD 97-21-02 7/15/1997 DNA - Eng. S/N 71 SB97-11 Single Piece Rocker Bushing 8/10/1997 DNA - RAM Engines 72 SB97-15 TCM Ign. SB 660 12/5/1997 DNA - No Affected switch installed 73 CSB98-1B Intake & Exh. Valve insp. 6/1/1998 DNA per Date of Mfg. 74 MSB99-3C C/S Inspection AD 99-09-17 7/27/1999 DNA per Date of Mfg. & C/S S/N 75 SB99-8 Fuel Injection System Preservation 11/18/1999 DNA - RAM O/H 76 SB00-4A Australian Avgas Contamination 3/7/2000 DNA - Eng. Not operated in Australia 77 SB00-10 Fuel Pump Seal 649198 12/19/2000 3/14/23 - 5425.5 C/W by RAM During O/H 78 CSB01-01 Fuel Pump Insp. And Seal Leak Test 4/25/2001 DNA per Date of Mfg. 78a SIL00-7B Oil Gage Rod Application 6/19/2017 Due when oil gage rod (dipstick) is replaced 79 MSB00-5D Crankshaft Inspection AD 00-23-21 10/17/2001 DNA - Eng. S/N 80 CSB02-8 Ignition CSB 664 9/6/2002 DNA per Magnetos S/N's 81 SB01-3A TCM Gear Driven Alternators 12/10/2002 3/14/23 - 5425.5 Due @ next Alter. O/H or R+R 82 CSB02-2C Str. Adapter Shaft Seal Insp. 12/11/2002 3/14/23 - 5425.5 C/W by RAM During O/H 83 SB03-3 Cyl. Comp. Check procedures 3/28/2003 8/1/24 - 5650.9 Due at each 100 hr. or annual insp. 84 CSB04-5A Ign. S.B. 665A 8/30/2004 DNA - Slick Mags Installed 85 SB04-11 Valve Guide Install & Reaming Procedures 11/2/2004 DNA - ECI Cyls. Installed 86 SB04-10 Piston Position Marking 10/26/2004 3/14/23 - 5425.5 Due @ ea. Piston R+R 87 SB00-3A C/S, Rod & Counterweight Repair Info. 10/29/2004 3/14/23 - 5425.5 C/W by RAM During O/H 88 SB05-2 Overspeed Limitations 1/31/2005 Due @ any C/S Overspeed 89 SB96-7D Torque Limits 8/11/2015 8/1/24 - 5650.9 Due during all Maintenance 90 CSB05-8D Improved Cam Gear p/n 656818 8/22/2018 3/14/23 - 5425.5 C/W by RAM During O/H 91 SB05-9 Slick S.B. SB1-88B 10/20/2005 DNA to this A/C Model 92 SB06-1A TCM Fuel Nozzle Insp. & R+R 4/28/2006 DNA - RAM Nozzles are Installed 93 CSB07-01A Piston Pin Bushing Insp. 9/2/2020 3/14/23 - 5425.5 Due @ any Cyl. R+R 94 MSB94-8D Mag to Eng. Timing 2/17/2010 8/1/24 - 5650.9 Due at each 100 hr. or mag work 95 SB07-8 Recommended RPM & MAP Settings 11/2/2007 3/14/23 - 5425.5 Information & Recommendations 96 SB08-3A Thr. & Mix. Control Arms 7/30/2010 3/14/23 - 5425.5 Due whenever bronze arm is R+R 97 SB08-4 Fuel Injection System Contamination 3/25/2008 3/14/23 - 5425.5 Due @ any Fuel System Component R+R 98 SID97-3G Fuel System Adjustment Procedures 10/21/2015 8/1/24 - 5650.9 Due @ O/H, ea. 100 hrs., etc. 99 SB08-8B Slick S.B. SB2-08 4/10/2009 DNA - Magneto S/N's 100 SB96-11B Prop. Strikes & Hyd. Locks 7/10/2008 Due at any prop. Strike or hyd. Lock 101 SB97-6B Mandatory Repl. Parts 11/18/2009 3/14/23 - 5425.5 Due at O/H & all eng. maintenance 102 MSB96-10B C/S Ultrasonic Insp. AD 97-26-17 8/10/2015 3/14/23 - 5425.5 C/W by RAM During O/H 103 CSB08-9A Slick S.B. SB03-8A 10/14/2008 DNA - Magneto S/N's 104 SB08-13 Induction Hose Clamp Installation 10/14/2008 3/14/23 - 5425.5 Due @ ea. Induction Hose Clamp R+R 105 SIL98-9E Recommended TBO 8/21/2015 3/14/23 - 5425.5 Due at 7025.2 hrs or 03/31/2035 106 SIL 99-1 Eng. preservation for active/stored aircraft 3/25/1999 Due if A/C is inactive for > 30 days 107 MSB09-1B Cylinder Replacement 8/18/2009 DNA - no affected cyls. Installed 108 SB08-12 Crankshaft Gear Supersedure 9/9/2008 Due @ next access or TBO 109 CSB10-2 Kelly T-Wheel Replacement 1/22/2010 DNA per Turbo Serial #'s 110 MSB09-8A TCM Hydraulic Lifters 12/14/2009 DNA per date of O/H 111 SB09-14 C/S Corrosion Treatment 10/16/2009 Due if rust is noted on C/S 112 CSB09-11A Minimum Cruise RPM Limits 11/12/2014 12/1/13 - 4054.7 Owner Advised 113 SB09-7 Push Rod Seal Leakage 7/16/2009 DNA per date of O/H 114 SB09-14 C/S Rust Treatment 10/16/2009 8/1/24 - 5650.9 Due ea. 100 hr. 115 CSB 668 Ign. Harness Attach Plate 5/18/2010 One time insp. completed OK 116 SIL04-12A TCM Authorized Adjustments 5/18/2010 Due as needed - see bulletin 117 MSB10-3 Kelly SB 039A AD 2010-07-0 5/18/2010 DNA per Turbo s/n 118 SID10-4 Volcanic Ash Contamination 7/21/2010 DNA-no ash contamination occurred 119 SB11-3 Alter. Drive Coupling Installation 3/18/2011 3/14/23 - 5425.5 Due @ ea. Access to coupling 120 CSB08-3C Remove Bronze Levers from Service 7/7/2013 Found PCW 121 SID97-4F Cyl. Bore & Piston Fit Specs. 8/13/2014 DNA - ECI Cyls. Installed 122 SB13-4C Aneroid Equipped Fuel Pumps 11/7/2016 DNA per pump s/n's installed 123 MSB13-7 H.E.T. Bulletin 048, rev. 1 1/15/2014 DNA per eng. m/n 124 SIL 13-2A Alternator ICA's 1/15/2014 3/14/23 - 5425.5 Due during Alternator Maintenance 125 SID 05-1A Insp. Guidelines for Cams & Lifters 5/2/2014 3/14/23 - 5425.5 Due & access to Cam and/or Lifters 126 MSB14-3 H.E.T. Bulletin # 057 5/5/2014 DNA per Turbo s/n's 127 SB14-5 H.E.T. Bulletin # 059 6/19/2014 DNA per Alter. s/n 128 SIL99-2C Authorized Sealants, Lubes & Adjesives 9/16/2014 8/1/24 - 5650.9 Due during all Maintenance 129 SB14-8 Exh. Flange Installation 2/3/2015 3/14/23 - 5425.5 Due during any exhaust installation 130 SB15-4 Slick SB1-15 8/19/2015 DNA per both magneto s/n's 131 SB15-5 Slick SL 74-20-001 (RPM drops) 10/6/2015 Due if timing drifts more the 4 degrees 132 SB15-6C NiC3 Cylinders 9/27/2019 Applies if these cylinders are installed-none are 133 SIL16-2 Standard Practices Manual 4/15/2016 8/1/24 - 5650.9 Due during all Maintenance 134 SB16-6 Engine Kickback Damage 10/19/2016 Due when kickback occurs 135 SB16-7 H.E.T. Bulletin $ 067 2/3/2017 DNA per eng. m/n N414MP LH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 514067 136 SB16-8 Turbo Exh. Transition 2/3/2017 DNA per Eng. m/n 137 SB16-9 H,E.T. Bulletin # 066 2/3/2017 DNA per Alter. p/n 138 SB17-01A Flanged Nut (652541) Insp & Corr. Prev. 10/20/2017 DNA - affected part # not installed 139 SB 670 TCM Magnetos Maint. 7/14/2017 DNA - Slick Mags Installed 140 SIL17-02 Turbo Check Valve Filter Insp. & Cleaning 7/12/2017 DNA per Eng. M/N 141 SIL17-03 Oil Filter Anti-stick Gasket 7/27/2017 Info. Only 142 SB17-04 TCM SB 670 - R+R of Dist. Block 7/17/2017 DNA - Slick Mags Installed 143 SB17-05 TCM SB 643C - Insp. Intervals 9/29/2017 DNA - Slick Mags Installed 144 SB17-06 Conn. Rod Bolt Insp. 10/20/2017 3/14/23 - 5425.5 Due at Connecting Rod Bolt Install 145 SIL 17-07 Discontinued Alternator 11/14/2017 Info. Only 146 SB18-04A R+R of Flanged Nut 12/18/2018 DNA per Date 147 SIL 18-02 Service Documents 2/15/2018 Info. Only 148 SIL19-04 Oil Brand Selection 10/11/2019 Info. Only 149 SB19-05 Valve Guide Application 10/24/2019 3/14/23 - 5425.5 Due @ O/H or Cyl. Repair 150 CSB19-06 Hartzell Alert SB 081A (Alter. Hub Nut) COMPLET 11/19/2019 9/13/21 - 5233.6 See SB for affected Units 151 SB19-07 C/S End Play 12/10/2019 DNA per Eng. S/N 152 SIL19-10 Oil Filter Removal 12/16/2019 Info. Only 153 SB20-01 Fuel Screen Maint. 2/20/2020 8/1/24 - 5650.9 Due ea. 100 hr./Annual 154 SB20-03 Eng. Pres. During COVID 4/13/2020 Info. Only 155 SIL20-05 Energizer Starter ICA's 9/28/2020 Info. Only 156 SB673C 1200 series Mag Bearings 5/24/2022 DNA - slick Mags are installed 157 MSB23-01A C/S Counterweights 2/16/2023 DNA per Eng. S/N 158 SB23-03 Hartzell SB 096 (Alternator) 5/24/2023 DNA per Alter. S/N . --~~--·_:· .·~__:,_~---, •11••·· .,., Aircraft Registration ________ Engine Posi~~on ---..aR _,_~--- ~*----- Engine Serial No. ___ .5..._ /9 .......'2. ......C,_'-I______ ENGINE MAINTENANCE RECORDS Log No. ____ Aircraft Registration No. _________ Engine Manufacturer ~\·,~+o-.1 Model 'f"SlO - 5~0 ·NB Serial No. 5 19 "-'2'-1 Date installed on aircraft _________ Time Between Overhauls (TBO) J&:,00 Hours If used on multi-engine aircraft: ~ Right 0 Left Waco Regional Airport 7505 Karl May Drive• P.O. Box 5219. • Waco, Texas 76708 Phone: (254) 752-8381 Fax: 254-752-3307 www.ramaircraft.com VLOGBOOK FORMAT REPRINT ED WITH TH E PERMISSION OF AEROTECH PUBLICATIONS, INC., THE AD LOG (™) SYSTEM, COPYRIGHT 1979." Page No..___ DATE TOTAL TIME IN SERVICE Total Date Time In Service 10/05/2022 4692.5 TOTAL TIME SINCE OVERHAUL Total Time Since Overhaul 0.0 TACH OR RECORDING M ETER TIME Tach or Recording Meter Time DESCRIPTION OF WORK PERFORMED- SIGNATU RE & CERTIFICATION NO. OF PERSON PERFORMING WORK TOTALS brought forwa rd from previous page RAM Aircraft, limited Partnership • Waco Regional Airport TCM TSIO-520-NB Series VII Ri ght En gine SIN 519264 Above referenced engine overhauled to new parts limits per FAR 43.2(a)(1 )(2) to conform w/CM SM X-30574A and Continental M-0, Standard Practice Maintenance Manua l. Applicable AD's and Service Bulletins CM/ at this time. All gears cleaned, polished when required, inspected, magnafluxed, and no cracks found. Finish and dimensional limits within RAM Gear Inspection Specification No. 1818, Rev. P dated 07/1912017. Above referenced engine modified to TSIO-520-NB 335 HP per STC SE09104SC-D (includes STC SE4327SW-D). Installed new RAM camshaft p/n 1058-20, s/n Xl21076 per STC SE09104SC-D. Installed new lifters p/n SA628488 (int), pin SA646277 (exh). AD 10-11-04 n/a to lifter p/n installed. AD 97-26- 17 c/w per installation of overhauled VAR -crankshaft pin 649898, s/n N05KA278 per CAT CSB96-8. CM/ ultrasonic inspection per MS896- 1 OB, due at next overhaul or when crankshaft removed. AD 99-19-01 n/a per crankshaft date of manufacture I/N\N TCM MSB99-3C. AD 2000,-23-21 N/A to crankshaft serial number/date of manufacture IIN\N TCM Mandatory Service Bulletin MSB00-5D. Engine assembled with new RAM crankcase pin 2922- 1, sin 21J0361 . Installed new Superior steel cylinders. Installed overhauled oil cooler pi n 8000440, sin 4082828. CM/ AD 89-24-01 R1 per installa tion of starter adapter pin 642085A4 with current scavenge pump gear s. AD 2012-10- 13 and MSB11-4B starter adapter inspection n/a per pin installed or manufacture date. Installed new RAMIFAA/PMA fuel nozzles pin 2562-140. TCM Service Bulletin SB06-1A NIA per installation of RAM fuel nozzles. Installed modified connecting rods p/n 1162 per STC SE4327SW-D as FAA/PMA approved replacement. Engi ne accessories exchanged for overhauled or new units with exception of the prop governor, alternator, vacuum pump, hydraulic pump and tach generator which were not installed per this work order. New Kelly pressurized magnetos pin ES6320 installed per STC SE4651 SW-O and pressurized. MSB94-8D on magneto timing procedure c/w per timing to STC degree requirements with TDC locator and protractor with pointer. PIN 652130 & 652131 rock er arms installed. Installed RAM/FAA/PMA oil cooler baffle pin 1253-1 , rocker box cover gaskets p/n 1387- 1, spring loaded induction clamps p/n 1170-2 and double clamps pin 1170-5. Category 1 thru 3 CMI Service Bulletin Compliance Listing in RAM Manual. Engine ground run on test stand per RAM specifications for 120 minutes. Engine run-in with Aeroshell 100 mineral oi l. See RAM Recommended Oil Grade Maintenance Tip MT-1 for recommended oils. Engine approved for .return to service for the work performed. Engine preserved per Continental M-0, Standard Practice Maintenance Maunal temp. storage up to 90 days. Pertinent details on file under Project No 10271. RAM Aircraft, Limited Partnership, P.O. Box 5219,Waco, Texas 76708 CRS VA1R551K SUB-TOTALS this page TOTALS-Carry for wa rd to ne xt page A.Shoreline r1VIATION Shoreline Aviation, Inc. -r---------+•➔ Mall!hlleld MumcipaI Ai,p0rt George Harlow Flekl (GHG) ---- 98 Old Colony Lane ._. Me~h"eld. MA 02050 12114/2022 N414MP Cessna 414A, serial# 414A-0317 Hobbs Hours: 1629.9 :: Aircraft TT: 5452.5 :: #2 Engine TT: 4692.5 :: #2 Engine TSMOH : 0.0 Engine 2 Logbook 1) This engine installed onto the right side of Cessna 414A, N414P, serlal #414A-0317 using all new engine mounts per Ram and Cessna 414A maintenance manual instructions. 2) All accessories and oil and fuel hoses were provided by RAM and installed except for vac. pump, tach gen, hydraulic pumps, prop, prop gov and alternator. Prop gov was O/H and reinstalled from the previous engine. A new vacuum pump was Installed. A new alternator was installed reusing the existing alternator drive coupling from the previous engine. Tach gen was reinstalled from the previous engine in "as removed" condition. Air conditioning hydraulic pump was reinstalled in "as removed" condition from the p revious engine. Landing gear hydraulic pump was replaced with an O/H unit. Propeller was reinstalled from the previous engine in "as removedff condition after flushing the oil cylinder. f 3) Engine was serviced with 12 qts. of Phillips Type M 20w-50 mineral oil and pre-oiled per RAM instructions. Engine was also turned by hand until oil pressure was read on the cockpit gage. 4) Ground run up revealed that the propeller blades would NOT go back to low pitch after the blades were moved toward the feather position. Prop. blades wou ld go to feather on engine shutdown. 5) Installed a known good prop governor from the other engine on this aircraft for troubleshooting puiposes and the same problem occured. 6) Completed leak down test of the oil transfer coJJar per Continental/RAM instructions and found the gage 113ading to be 0/80. 7) Removed the alternator and removed the RH side of the prop governor oil transfer collar. Found the transfer collar inner surfaces that ride on the crankshaft to be scored and grooved. 8) Removed engine and returned to RAM tor repair. T he above work was completed in accordance with current regulations of the Federal Aviation Administration and is NOT approved for return to sarvice for the work accomplished . Shoreline Aviation , Inc. 93 Old Colony Lane Marshfield , MA 02050 781-837-8521 Date 02-20-23 Total Time In Service 4692.S Total nme Since overhaul 0.0 Recordi ng Meter 'Time 1629.9 RAM Aircraft, limited Partnership• Waco Re gional Airport CONTINENTAL TSI0-520-NB RIGHT ENGINE SIN 519264 The above referenced engine was disassembled for maintenance. The engine was cleaned, inspected and reassembled to service limits per CMI Standard Practice Maintenance Man ual M-0 and CMI Overhaul Manual X-30574. Reused crankcase, camshaft and lifters. Installed overhauled crankshaft SIN C449711 N, and new main and rod bearings. CNV MSB96-10B ultrasonic inspection. Disassembled and cleaned cylinders. Re installed cy linder assembl ies. MSB22-01 NIA per S/N's. In stalled overhauled oil coo ler SIN E98-3059-912. Installed accessories in their re spective positions with existing time in service with the exception of the vacu um pump, prop governor, tach generator, alternator, and hydrau li c pump which were not installed per th is work order. Cleaned and flushed li fte rs, starter adapter and oil pump. Serviced engine wi th Aeroshell 100 oil. Run in test cell for 1 hour. Engine is approved for return to servi ce for work performed. Engine preserved per CMI M-0 Standard Practice Maintenance Man ual temp. sto rage up to 90 days. Pertin en t details on flle under Project No. 10536. ~ N ~RAM Aircraft, Limited Partnership,.O.Box 5219, Waco Texas. 76708 CRS VA1R551K TOTALS -Carry forward to next page Page No.. DAT l l A,Shoreline rtVIATION Shoreline Aviation, Inc. ,), Marshfield Municipal Ai(J)<ll'I Q~ Harlow Field (GHG) 93 Old COiony Lane ~ Msno.hfiekl. MA 02050 3/1412023 N414MP Cessna 414A, serial# 414A-0317 Hobbs Hours: 1629.9 :: Aircraft TT: 5452.5 :: #2 Engine TT: 4692.5 :: #2 Engine TSMOH : 0.0 Engine 2 Logbook 1) This engine reinstalled onto the right side of Cessna 414A, N414P, serial #414A-0317 after repairs by RAM as shown on the previous page. 2) Engine was serviced with 12 qts. of Phillips Type M 20w-50 mineral oil and pre-oiled per RAM instructions. Engine was also turned by hand until oil pressure was read on the cockpit gage. , 3) Set idle speed, idle mixture, low unmetered fuel pump pressure, high unmetered fuel pump pressure & maximum MAP at full power. 4) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. The above work was completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work accomplished. Shoreline Aviation, Inc . 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 Edward J. Novak Jr. A+P 2832024 IA ------,-.....---------r--- -....--- - - - ------------ ShoreliM AvlaHon, In c. ---- - - ---- +Marsnffeld Municipal Airport George Harlow F"'ld (GHG) 93 Old Colony Lanr, .::::::;:,r Mn rshffekl. MA 02050 5/10/2023 N414MP Cessna414A, serial#414A-0317 Hobbs Hours; 1658.2 :: Aircraft TT: 5480,8 :: #1 Engine TSMOH : 28.3 :: #1Propeller SMOH: 653.9 TSMOH: 28.3 :: Heater Hobbs: 612.5 Engine 2 Logbook :: #2 Propeller SMOH: 653.9 :: #2 Engine Completed Operation #3 inpsection items per the Cessna 414A Maintenance manual progressive care Inspection fonn. 1} Cyl. Comp. Checked per TCM SB 03-03 - all cyls. checked above minimum (42). 1) 64/80 2) 72/80 3) 70/80 4) 66/80 5) 66/80 6) 68/80 2) CrN the follwing TCM repetitive SB's: MS0-17 (CIC lnsp), S895-2 (Control Unkage lnsp), S895-7 (Fuel Manifold valve cover insp), SB96-12 (cyl lnsp.}, S896-7C (Torque Values), MSB94-8D (Mag Timing), SID97-3G (Fuel System}, S809-14 (C/S Rust) and S817-01A (flanged nut insp.), S820- 01 (fuel screen) and noted no defects. 3) Drained oil, added 10 qts. of Phillips Victory 100W (SAE-50) oil. Installed and saftied a new AA48108-2 oil filter. Cut open filter and found no abnonnal contaminants. 4) Ground runup and systems functional checks completed with satisfactory results and no fue I certify that this Engine has been inspected in accordance with an Operation #3 ins in an airworthy condition. Signe,v-'~ ~..:....,.._..."'---+----'------------ Shoreline .Aviation, Inc. Marshfield Municipal Alrp0rt G&orge HarloY, Field (GHG) 93 Cid Colony Lane ._w M:.rahfield. MA 02050 6/29/2023 N414MP Cessna 414A;sorlal # 414A-0317 Engine 2 Logbook Hobbs Hours: 1686.9 :: Aircraft TT: 5509.5 :: #1 Engine TSMOH: 57.0 :: #1Propelfer SMOH 682.6 :: #2 Propeller SMOH: 682.6 :'. #2 Engi ne TSMOH: 57.0 :: Healer Hobbs: 613.8 1) Completed 50 hr. Special inspection items as follows: Drained oil, added 11 qts. of Phillips Victory SAE50 oil. Installed and saftied a new AA48108-2 oil filter. Cut open filter and found no abnormal contaminants. Runup and leak check OK. 2) Installed new RH832E spark plug at the upper #6 cylinder location, The above work was completed in accordance with current regulations of the Federal Aviation Administration the work accomplished, ~.kzc. • Signed.___ __·_~+--'-- -~~-------- for return to service for Edward J. Novak Jr. A+P 2832024 IA TOTALS - Carry forward to next page 2' Shoreline Aviation, Inc. ) Marshfield Municipal Airport 0~ Hat!ow Field (GHG) __. 93 Old Co!Ql\y l.a/l9 ._. Marshfield. MA 02050 10/25/2023 N414MP Hobbs Hours: 1724.6 :: Aircraft TT: 5547.2 TSMOH: 94.7 :: Heater Hobbs: 613.8 Cessna 414A, serial# 414A-0317 #1 Engine TSMOH: 94.7 :: #1Propeller SMOH: 720.3 •• Engine 2 Logbook #2 Propeller SMOH: 720.3 :: #2 Engine Completed Operation #1 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) Cyl. Comp. Checked per TCM SB 03-03 1) 70/80 2) 70/80 3) 70/80 4) 66/80 5) 68/80 6) 68/80. 2) CNJ the follwing TCM repetitive SB's: M90-17 (CIC lnsp), S895-2 (Control Linkage lnsp), S895-7 (Fuel Manifold valve cover insp), SB96-12 (cyl lnsp.), SB96-7C (Torque Values), MSB94-8D (Mag Timing), SlD97-3G (Fuel System), $B09-14 (C/S Rust) and SB17-01A (flanged nut insp.), S820- 01 (fuel screen) and noted no defects. 3) Completed 50 hr. special inspection as follows: Drained oil, added 11 qts. of Phillips X/C 20w-50 oil. Installed and saftied a new M48108-2 oil filter. Cut open filter and found no abnormal contaminants. 4) Installed one new URHB32E for the LH magneto, #4 cylinder (upper spark plug), 5) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. I certify that this Engine has been inspected in accordance with an Operation #1 inspection nd was te ined to S~ned,...!:~&::.!:!Qj~..!/1--C.~=-..:.:...n.=-- ------- 11/14/2023 N414MP Engine 2 Logbook Hobbs Hours: 1730.9 :: Aircraft TT: 5553.5 :: #1 Engine TSMOH: 101.0 :: #2 Engine TSMOH: 101.0 Installed an overhauled fuel pump (part# 646210-11A5, serial# D029922BR) from Ram Aircraft as shown on the attached 8130- 3 form. Adjusted this pump as needed per TCM SID 97-3G and RAM ICA instructions. Functional and leak checks were normal. The above work was completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work accomplished. o .-f-.. Signed /,; vy,ah( ~~ r /Jj7?(,, 7 Donald Harring7+P 1939767 Shoreline AVIATION ----------➔ Shonillne Aviation, Inc.· Marsh!iltld Muoicipal Airport Geor;J6 Harlow Fle!d {GHGJ 93 Oki Colony Lane • w Marshfield. MA 02050 3/1/2024 N414MP Cessna 414A, serial #414A-0317 Hobbs Hours: 1775.2 :: Aircraft TT: 5597.B :: #1 Engine TSMOH: 145.3 :: #1Propeller SMOH: 770.9 .. 770.9 :: #2 Engine TSMOH: 145.3 :: Heater Hobbs: 630.5 Engine 2 Logbook #2 Propeller SMOH: Completed Operation #2 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) Drained oil, added 11 qls. of Phillips X/C 20w-50 oil. Installed and saftied a new AA48108-2 oil filter. Cul open filter and found no abnormal contaminants. 2) Repaired one broken terminal end for an outboard prop. Deicer boot heating element. Function check prop heat OK. 3) Ground runup and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. I certify that this Engine has been inspected in accordance with an Operation #2 inspection and was detennined to be in an airworthy condition. Signed ~Jt 'l4.tJ. /y Edward J. Novak Jr/ A+P 2832024 IA SUB-TOTALS this page TOTALS-Carry forward to next page Page No•. DAl I 81112024 N414MP A,Shoreline ..l"l.VIATION Shoreline Aviation, Inc. ) Marshllek/ Munrcipal AitpO!'I Geot!)ft Harlow Field (GHGl 93 Old C<JOff'J Lane MA<shftald. MA 02050 Cessna 414A, serial # 414A-0317 k Engine 2 Logboo Hobbs Hours: 1828.3 :: Aircraft TT: 5650.9 :: #1 Engine TSMOH: 198.4 :: #1 Propeller SMOH: 824.0 :: #2 Propeller SMOH: 824.0 :: #2 Engine TSMOH: 198.4 :: Heater Hobbs: 632.7 Completed Operation #3 & #4 inspection items per the Cessna 414A Maintenance manual progressive care inspection fonn. 1) Cyl. Comp. Checked per TCM SB 03-03 1) 60/80 2} 68/80 3) 58/80 4) 68/80 5) 60/80 6) 62/80. 2) CIW the follwing TCM repetitive SB's: S895-2 {Control Linkage lnsp), S895-7 (Fuel Manifold valve cover insp), SB96- 12 (cyl lnsp.), SB96-7C (Torque Values), MSB94-8D {Mag Timing), S1D97-3G (Fuel System), S809- 14 (C/S Rust) and SB17-01A (flanged nut insp.), S820-01 (fuel screen) and noted no defects. 3) Completed 50 hr. special inspection as follows: Drained oil, added 11 qts. of Phillips X/C 20w-50 oil. Installed and saftied a new AA48f108-2 oil filter. Cut open filter and found no abnonnal contaminants. 4) Installed 10 new URHB32E spark plugs (all but #2 & #4 upper). 5) LH header pipe assembly replaced with a new unit from Aerospace Welding (part# A9910295-13). 6) Ground run up and systems functional checks completed with satisfactory results and no fuel or oil leaks noted. I certify that this Engine has been inspected In accordance with an Operation #3 & #4 insp•~~:1ho and wa1~/effeM in;;J to iffin n airworthy condition. . Signed . ''.!..'"'' · Edward~- Novak Jr. A~P 2832024 IA SUB •TOTAlS this page TOTAlS-Carry forward to next page AD NOTES COMPLIANCE RECORD Engine - Continental Motors - TSIO-520-NB s/n: 519264 Propeller - Hartzell - ( )HC-( )( )Y( ) m/n: PHC-C3YF-2UF s/n: EB7629B Appliance - Connecting Rods - Engine Components Incorporated (ECi) Appliance - Governors - McCauley Appliance - Magnetos - Slick Appliance - Cylinder assembly - Superior Air Parts AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA - affected component not installed. 2006-10-21 CORRECTION - To prevent fatigue failure of the connecting rod and a possible uncommanded shutdown of the engine. Ed Novak A+P 2832024 IA X DNA per part #. 75-12-07 McCauley governors Ed Novak A+P 2832024 IA X DNA per date of governor O/H. 2020-19-06 Idler Gear Bearing Unapproved Variant Ed Novak A+P 2832024 IA X DNA per part serial #. 74-18-05 Slick magnetos X Ed Novak A+P 2832024 IA DNA per part serial #. 80-06-05 Slick magnetos Ed Novak A+P 2832024 IA X DNA per part serial #. 81-16-05 Slick magnetos Ed Novak A+P 2832024 IA X DNA per engine model #. 99-04-04 Magneto impulse coupling X Ed Novak A+P 2832024 IA DNA per engine model #. 2011-26-07 To prevent engine failure due to migration of the magneto impulse coupling stop pin X Ed Novak A+P 2832024 IA DNA per eng. Model #. 97-01-04 Cylinder assemblies X Ed Novak A+P 2832024 IA Superseded by R1. 2007-04-19 To prevent cylinder separation that can lead to engine failure X Ed Novak A+P 2832024 IA DNA per cylinder part #'s & s/n's. 2007-04-19R1 To prevent cylinder separation that can lead to engine failure X Ed Novak A+P 2832024 IA DNA per engine model #. 78-06-01 R2 Flexible intake elbow X Ed Novak A+P 2832024 IA C/W by RAM during engine O/H. 79-05-09 Oil pressure relief valve 3/14/23 - 0 SMOH Ed Novak A+P 2832024 IA X DNA - affected component not installed. 80-01-04 Cylinder holddown flanges Ed Novak A+P 2832024 IA X DNA per date of installation. 81-24-06 Fuel pump X Ed Novak A+P 2832024 IA 1 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA per engine S/N. 82-09-01 Fuel pressure regulator leaks Ed Novak A+P 2832024 IA X DNA - affected component not installed. 86-13-04 R3 Cylinder assemblies X Ed Novak A+P 2832024 IA Superseded by 97-26-17. 87-23-08 Crankshaft fatigue cracks X Ed Novak A+P 2832024 IA DNA - affected component not installed. 88-03-06 Oil filter Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 89-24-01 R1 Scavenge oil pump gears 3/14/23 - 0 TSMOH Ed Novak A+P 2832024 IA X DNA - affected component not installed. 91-19-03 Champion oil filter Ed Novak A+P 2832024 IA X DNA per engine model #. 93-08-17 Incorrect oil pick-up tube Ed Novak A+P 2832024 IA X DNA - affected component not installed. 93-10-02 Cylinder valve retainer Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 93-16-15 Fuel pumps 3/14/23 - 0 TSMOH Ed Novak A+P 2832024 IA X Superseded by 95-21-15. 94-14-12 Low octane detonation Ed Novak A+P 2832024 IA X DNA per date of installation. 95-21-15 Engine teardown and analytical inspect. Ed Novak A+P 2832024 IA X C/W by RAM during engine O/H. 97-26-17 CORRECTION - Crankshaft fatigue cracks 3/14/23 - 0 TSMOH X Next O/H or crankshaft removal Ed Novak A+P 2832024 IA DNA - affected component not installed. PL98-01-08 Exhaust roller rocker arms Ed Novak A+P 2832024 IA X Superseded by 99-19-01. PL99-09-17 Crankshaft failure Ed Novak A+P 2832024 IA X DNA per date of installation. 99-19-01 Crankshaft failure Ed Novak A+P 2832024 IA X Superseded by 2000-23-21. PL2000-08-51 Crankshaft connecting rod journal fracture X Ed Novak A+P 2832024 IA DNA per date of mfg. 2000-23-21 Fracture of the crankshaft connecting rod journal Ed Novak A+P 2832024 IA X DNA per date of mfg. 2004-08-10 Prevent loss of engine power Ed Novak A+P 2832024 IA X Superseded by 2014-05-29. 2009-16-03 To prevent the separation of the cylinder head X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2009-19-07 Correction - To prevent loss of engine power due to cracks in the cylinder head, possible engine failure, and fire in the engine compartment X Ed Novak A+P 2832024 IA Superseded by 2009-24-52. 2009-24-51 To address rapid wear on the face of hydraulic lifters X Ed Novak A+P 2832024 IA 2 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. Superseded by 2010-11-04. 2009-24-52 To address rapid wear on the face of hydraulic lifters X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2010-11-04 To prevent excessive hydraulic lifter wear X Ed Novak A+P 2832024 IA Superseded by 2012-10-13. 2011-25-51 To address fractures in starter adapter shaft gears Ed Novak A+P 2832024 IA X DNA - affected component not installed. 2012-03-06 To prevent an in-flight shutdown due to a failed fuel servo diaphragm X Ed Novak A+P 2832024 IA DNA per part #. 2012-10-13 To prevent starter adapter gear shaft failure X Ed Novak A+P 2832024 IA DNA - affected component not installed. 2014-05-29 Superior Air Parts Investment Cast Cylinder Assemblies X Ed Novak A+P 2832024 IA Superseded by 2023-17-04. 2022-04-04 STC Stratus Oil Filter Adapter Fiber Gasket Oil Loss Ed Novak A+P 2832024 IA X N/A - affected item not installed. 2022-16-03 S-1200 Series Magnetos Roller Bearings Improper Lubricatio Ed Novak A+P 2832024 IA X DNA per cylinder s/n's. 2023-02-12 Intake Valve Failures Ed Novak A+P 2832024 IA X Superseded by 2023-05-16. 2023-04-08 Crankshaft Assembly Counterweight Retaining Rings in the Counterweight Groove Ed Novak A+P 2832024 IA X DNA - engine serial number. DNA - engine not assembled at TCM factory. 2023-05-16 Improper Installation of Counterweight Retaining Rings Ed Novak A+P 2832024 IA X N/A - affected STC not installed. 2023-17-04 STC F&M or Stratus Oil Filter Adapter Fiber Gasket Oil Loss Ed Novak A+P 2832024 IA X Superseded by 2002-09-08. 77-12-06 R2 Prop blade X Ed Novak A+P 2832024 IA DNA - propeller not returned to service by BASCO. 2001-07-03 CORRECTION - Prevent propeller failure of the propellers returned to service by BASCO Ed Novak A+P 2832024 IA X DNA per date of mfg. 2001-23-08 Prevent failure of the propeller hub resulting from cracks X Ed Novak A+P 2832024 IA Superseded by 2007-26-09. 2002-09-08 Prevent failure of the propeller blade from fatigue cracks Ed Novak A+P 2832024 IA X DNA per date of mfg. 2003-01-03 Prevent in-flight propeller blade separation Ed Novak A+P 2832024 IA X DNA per model #. 2003-03-20 Prevent fatigue failure of the original propeller hub and blades Ed Novak A+P 2832024 IA X DNA - propeller is O.E.M. 2003-13-17 Maintenance by T&W Propellers Inc. Ed Novak A+P 2832024 IA X DNA - propeller is O.E.M. 2005-14-11 Maintenance by Southern California Propeller Service Ed Novak A+P 2832024 IA X Superseded by 2009-22-03. 2006-18-15 To prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control X Ed Novak A+P 2832024 IA 3 09/13/2024 4 Page of N414MP AD# Applicable S.B. # & Subject Method of Compliance Recurring One Time Next Comp. @ Hrs/Date Authorized Signature & Number Date & Hours @ Comp. DNA - propeller is O.E.M. 2006-24-07 To detect unsafe conditions that could result in a propeller blade separating from the hub and loss of control of the airplane Ed Novak A+P 2832024 IA X DNA per date of mfg. 2007-26-09 To prevent failure of the propeller blade from fatigue cracks in the blade shank radius Ed Novak A+P 2832024 IA X DNA - propeller is NOT LH rotating. 2008-13-28 To prevent failure of the propeller hub X Ed Novak A+P 2832024 IA DNA per part serial #. 2009-22-03 To prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control X Ed Novak A+P 2832024 IA 4 09/13/2024 4 Page of N414MP N414MP RH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 519264 Item Bulletin Bulletin Bulletin Date # No. Description Date Completed Remarks 1 M67-12 Overboost - Engine 5/31/1967 Due if MAP goes 6" over redline 2 M70-11 Slick SB # 1-70 6/22/1970 DNA - Magneto M/N 3 M71-14 Slick SB # 1-71 6/21/1971 DNA - Magneto M/N 4 M71-21 Turbo Shaft Insp. 11/22/1971 Information Only 5 M72-17R1 Max Allowable Piston/Rod Weight Difference 10/5/1973 Information Only 6 M74-18 Slick S.B. 1-74 9/16/1974 DNA - Magneto M/N 7 M75-6R1 Model Conversion 6/4/1975 Information Only 8 M75-30 Prestolite Alternators 12/19/1975 DNA - not installed 9 M76-4 Crankcase Oil Seal Installation 3/12/1976 3/14/23 - 5425.5 Due at C/S oil seal change 10 M76-5R1 Remote Mounted Oil Coolers 5/25/1976 DNA - No Remote Oil Cooler 11 M77-3 Fuel Alternate Grades 1/11/1977 Infomation Only 12 M77-9 Thru Bolt Change 3/16/1977 DNA - already incorporated 13 M78-6 R+R of Rosan Exh. Studs 3/3/1978 Due during Exh. Stud R+R 14 M78-5R3 Flexible Elbow p/n 635930 10/23/1978 DNA - Engine M/N 15 M78-16 #2 Cyl. Intake Elbow p/n 629138 11/29/1978 DNA - Engine M/N 16 M80-10 R+R of Some 642232 Elbows 3/28/1980 C/W by RAM during O/H 17 M81-16 AiResearch S.L. TP61-0043-2 7/27/1981 DNA - RAM O/H Turbo 18 M81-19 Availability of New Flex Elbows 8/5/1981 DNA - RAM Elbows Installed 19 M81-25 Exhaust Flange to Cyl. Installation 11/30/1981 3/14/23 - 5425.5 Superseded by SB14-8 20 M83-5 Slick S.B. 3-82 3/7/1983 DNA - Magneto M/N 21 M83-6 Slick S.B. 2-82 3/7/1983 DNA - Magneto M/N 22 M81-4R1 Airesearch S.L. TP61-0046 4/29/1983 DNA per Date of O/H 23 M81-15R1 Prestolite Alternators 6/16/1983 DNA - not installed 24 M84-5 Gear Driven Alter. Insp. 2/13/1984 Due @ any alternator malfunction 25 M84-8 Mag Timing Indicator Plate 6/19/1984 DNA - No Timing Plate Installed 26 M84-13 Slick S.B. 1-84 10/27/1984 DNA - Magneto M/N 27 M85-9R1 Piston to Cyl. Dome Clearance 8/6/1985 DNA - ECI Cyls. Installed 28 M85-10 Cyl. Hold Down Nuts 7/18/1985 3/14/23 - 5425.5 C/W by RAM During O/H 29 M86-4 Fuel Pumps 1/9/1986 Due if fuel pump press. Wanders 30 M86-13R1 Cam Plug Insp. 10/17/1986 DNA per Date of O/H 31 M86-14 Camshaft 629726 Rework 10/1/1986 DNA - RAM Cam Installed 32 M87-15 Alternator Ground Strap 7/13/1987 3/14/23 - 5425.5 Due at eng. or alter. Replacement 33 M87-16 Slick S.B. SB1-86A 8/14/1987 DNA - Magneto M/N 3 M87-23 C/S Counterweights ID @ O/H 11/24/1987 3/14/23 - 5425.5 C/W by RAM During O/H 4 M88-4 TCM Oil Filters AD 88-03-06 1/15/1988 DNA - Not Installed 35 M88-9 Lightning Strikes 8/24/1988 Due at any lightning strike 36 M88-10 Contaminated Fuels 8/24/1988 Due when wrong fuel is used 37 M89-7 R1 Eng. Ops. After O/H or Cyl. R+R 8/4/1989 3/14/23 - 5425.5 C/W by RAM During O/H 38 M89-9 Excessive Crankcase Pressures 4/21/1989 Information Only 39 M89-18 EGT Recommendations 8/10/1989 EGT Information 40 M90-6 Scavenge Pump Gears 2/26/1990 3/14/23 - 5425.5 C/W by RAM during O/H 41 M90-13 Exh. Valve Stem Corr./Erosion 7/16/1990 Due at any access to exh. Valves 42 M90-16 7th Stud Improvement 8/22/1990 3/14/23 - 5425.5 C/W by RAM during O/H 43 M90-17 C/C Insp. Criteria 8/23/1990 N/A RAM C/C Due at each 100 hr. Insp. 44 M91-4 Piston to Ring Application 2/11/1991 3/14/23 - 5425.5 Due at any piston ring change 45 M91-7 Cyl. Barrel Ultrasonic Insp. 3/20/1991 DNA - affected Cyls. NOT Installed 46 M91-6 Cyl. Barrel Insp. 3/20/1991 DNA - affected Cyls. NOT Installed 47 M91-9 Cam & Lifter Lube During Build 8/9/1991 3/14/23 - 5425.5 C/W by RAM during O/H 48 M92-6 Rockershaft Retention Improvement 2/28/1992 3/14/23 - 5425.5 C/W by RAM during O/H 49 M92-7 Deck Studs 5/26/1992 3/14/23 - 5425.5 C/W by RAM during O/H 50 M92-9 Flanged Thru-Bolt p/n 652541 5/29/1992 3/14/23 - 5425.5 C/W by RAM during O/H 51 M92-12 Alternator Thru-Bolt Insp. 8/27/1992 DNA per Alter. S/N 52 M92-14 Modine Oil Coolers 9/9/1992 DNA per Oil Cooler P/N 53 M93-4 C/S Counterweights 2/12/1993 3/14/23 - 5425.5 7/22/13 - 4054.7 54 M93-8 Rocker Arm to Rotocoil Clearance 2/19/1993 3/14/23 - 5425.5 C/W by RAM during O/H 55 M93-5 Chamfer of Oil Feed Holes 2/19/1993 12/2/22 - 5452.5 C/W by RAM during O/H 56 M93-10 TCM Ign. SB No. 639 3/1/1993 DNA - No Impulse Couplings 57 MSB93-12 Valve Retainer Key Insp. AD 93-10-02 5/12/1993 DNA - Eng. S/N 58 CSB94-1 TCM Ign. SB No. 641 AD94-06-09 2/1/1994 DNA - Slick Mags Installed 59 SB94-2 Oil Filter adapter Mounting Stud 2/10/1994 3/14/23 - 5425.5 C/W by RAM during O/H 60 SB94-11 Oil Pump Gasket 11/14/1994 3/14/23 - 5425.5 C/W by RAM during O/H 61 CSB94-15 C/C Stud Insp. 12/2/1994 DNA - Eng. S/N 62 SB95-2 Insp.& Maint. Of Eng. Con. & Linkage 4/21/1995 8/1/24 - 5650.9 Due at ea. 100 hr. Or linkage work 63 MSB95-6 Fuel Pump Drive Coupling 10/19/1995 3/14/23 - 5425.5 C/W by RAM during O/H 64 SB95-7 Manifold valve Cover Insp. 12/8/1995 8/1/24 - 5650.9 Due ea. 100 hr. Or FF fluctuation N414MP RH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 519264 65 SB96-3B C/S Gear Bolt Insp. 3/14/23 - 5425.5 C/W by RAM during O/H 66 MSB96-10A C/S Ultrasonic Insp. AD 97-26-17 10/14/2008 3/14/23 - 5425.5 C/W by RAM during O/H 67 M90-14 Champion Action Alert 90-1 8/7/1990 DNA - effected part not installed 68 SB96-12 Continued A.W. Instr. For TCM Cyls. 9/10/1996 DNA - ECI Cyls. Installed 69 SB96-3B C/S Gear Bolt Insp. 10/14/1996 DNA per Date of Mfg. 70 CSB97-10A Piston Pin Plug Wear AD 97-21-02 7/15/1997 DNA - Eng. S/N 71 SB97-11 Single Piece Rocker Bushing 8/10/1997 DNA - RAM Engines 72 SB97-15 TCM Ign. SB 660 12/5/1997 DNA - No Affected switch installed 73 CSB98-1B Intake & Exh. Valve insp. 6/1/1998 DNA per Date of Mfg. 74 MSB99-3C C/S Inspection AD 99-09-17 7/27/1999 DNA per Date of Mfg. & C/S S/N 75 SB99-8 Fuel Injection System Preservation 11/18/1999 DNA - RAM O/H 76 SB00-4A Australian Avgas Contamination 3/7/2000 DNA - Eng. Not operated in Australia 77 SB00-10 Fuel Pump Seal 649198 12/19/2000 3/14/23 - 5425.5 C/W by RAM During O/H 78 CSB01-01 Fuel Pump Insp. And Seal Leak Test 4/25/2001 DNA per Date of Mfg. 78a SIL00-7B Oil Gage Rod Application 6/19/2017 Due when oil gage rod (dipstick) is replaced 79 MSB00-5D Crankshaft Inspection AD 00-23-21 10/17/2001 DNA - Eng. S/N 80 CSB02-8 Ignition CSB 664 9/6/2002 DNA per Magnetos S/N's 81 SB01-3A TCM Gear Driven Alternators 12/10/2002 3/14/23 - 5425.5 Due @ next Alter. O/H or R+R 82 CSB02-2C Str. Adapter Shaft Seal Insp. 12/11/2002 3/14/23 - 5425.5 C/W by RAM During O/H 83 SB03-3 Cyl. Comp. Check procedures 3/28/2003 8/1/24 - 5650.9 Due at each 100 hr. or annual insp. 84 CSB04-5A Ign. S.B. 665A 8/30/2004 DNA - Slick Mags Installed 85 SB04-11 Valve Guide Install & Reaming Procedures 11/2/2004 DNA - ECI Cyls. Installed 86 SB04-10 Piston Position Marking 10/26/2004 3/14/23 - 5425.5 Due @ ea. Piston R+R 87 SB00-3A C/S, Rod & Counterweight Repair Info. 10/29/2004 3/14/23 - 5425.5 C/W by RAM During O/H 88 SB05-2 Overspeed Limitations 1/31/2005 Due @ any C/S Overspeed 89 SB96-7D Torque Limits 8/11/2015 8/1/24 - 5650.9 Due during all Maintenance 90 CSB05-8D Improved Cam Gear p/n 656818 8/22/2018 3/14/23 - 5425.5 C/W by RAM During O/H 91 SB05-9 Slick S.B. SB1-88B 10/20/2005 DNA to this A/C Model 92 SB06-1A TCM Fuel Nozzle Insp. & R+R 4/28/2006 DNA - RAM Nozzles are Installed 93 CSB07-01A Piston Pin Bushing Insp. 9/2/2020 3/14/23 - 5425.5 Due @ any Cyl. R+R 94 MSB94-8D Mag to Eng. Timing 2/17/2010 8/1/24 - 5650.9 Due at each 100 hr. or mag work 95 SB07-8 Recommended RPM & MAP Settings 11/2/2007 2/20/09 - 4176.0 Information & Recommendations 96 SB08-3A Thr. & Mix. Control Arms 7/30/2010 Due whenever bronze arm is R+R 97 SB08-4 Fuel Injection System Contamination 3/25/2008 3/14/23 - 5425.5 Due @ any Fuel System Component R+R 98 SID97-3G Fuel System Adjustment Procedures 10/21/2015 8/1/24 - 5650.9 Due @ O/H, ea. 100 hrs., etc. 99 SB08-8B Slick S.B. SB2-08 4/10/2009 DNA - Magneto S/N's 100 SB96-11B Prop. Strikes & Hyd. Locks 7/10/2008 Due at any prop. Strike or hyd. Lock 101 SB97-6B Mandatory Repl. Parts 11/18/2009 3/14/23 - 5425.5 Due at O/H & all eng. maintenance 102 MSB96-10B C/S Ultrasonic Insp. AD 97-26-17 8/10/2015 3/14/23 - 5425.5 C/W by RAM During Metal Contam. Repair 103 CSB08-9A Slick S.B. SB03-8A 10/14/2008 DNA - Magneto S/N's 104 SB08-13 Induction Hose Clamp Installation 10/14/2008 3/14/23 - 5425.5 Due @ ea. Induction Hose Clamp R+R 105 SIL98-9E Recommended TBO 8/21/2015 3/14/23 - 5425.5 Due at 7025.2 hrs or 03/31/35 106 SIL 99-1 Eng. preservation for active/stored aircraft 3/25/1999 Due if A/C is inactive for > 30 days 107 MSB09-1B Cylinder Replacement 8/18/2009 DNA - no affected cyls. Installed 108 SB08-12 Crankshaft Gear Supersedure 9/9/2008 Due @ next access or TBO 109 CSB10-2 Kelly T-Wheel Replacement 1/22/2010 DNA per Turbo Serial #'s 110 MSB09-8A TCM Hydraulic Lifters 12/14/2009 DNA per date of O/H 111 SB09-14 C/S Corrosion Treatment 10/16/2009 8/1/24 - 5650.9 Due if rust is noted on C/S 112 CSB09-11A Minimum Cruise RPM Limits 11/12/2014 12/1/13 - 4054.7 Owner Advised 113 SB09-7 Push Rod Seal Leakage 7/16/2009 DNA per date of O/H 114 SB09-14 C/S Rust Treatment 10/16/2009 8/1/24 - 5650.9 Due ea. 100 hr. 115 CSB 668 Ign. Harness Attach Plate 5/18/2010 One time insp. completed OK 116 SIL04-12A TCM Authorized Adjustments 5/18/2010 Due as needed - see bulletin 117 MSB10-3 Kelly SB 039A AD 2010-07-08 5/18/2010 3/14/23 - 5425.5 118 SID10-4 Volcanic Ash Contamination 7/21/2010 DNA-no ash contamination occurred 119 SB11-3 Alter. Drive Coupling Installation 3/18/2011 3/14/23 - 5425.5 Due @ ea. Access to coupling 120 CSB08-3C Remove Bronze Levers from Service 7/7/2013 Found PCW 121 SID97-4F Cyl. Bore & Piston Fit Specs. 8/13/2014 DNA - ECI Cyls. Installed 122 SB13-4C Aneroid Equipped Fuel Pumps 11/7/2016 DNA per pump s/n's installed 123 MSB13-7 H.E.T. Bulletin 048, rev. 1 1/15/2014 DNA per eng. m/n 124 SIL 13-2A Alternator ICA's 1/15/2014 3/14/23 - 5425.5 Due during Alternator Maintenance 125 SID 05-1A Insp. Guidelines for Cams & Lifters 5/2/2014 Due & access to Cam and/or Lifters 126 MSB14-3 H.E.T. Bulletin # 057 5/5/2014 DNA per Turbo s/n's 127 SB14-5 H.E.T. Bulletin # 059 6/19/2014 DNE per Alter. s/n 128 SIL99-2C Authorized Sealants, Lubes & Adhesives 9/16/2014 8/1/24 - 5650.9 Due during all Maintenance 129 SB14-8 Exhaust Flange to Cyl. Installation 2/6/2015 3/14/23 - 5425.5 Due at any Exhaust Installation 130 SB15-4 Slick SB1-15 8/19/2015 DNA per both magneto s/n's 131 SB15-5 Slick SL 74-20-001 (RPM drops) 10/6/2015 Due if timing drifts more the 4 degrees N414MP RH Eng. SB's Date: 8/1/24 Hobbs: 1828.3 ACTT: 5650.9 TSMOH: 198.4 Eng. M/N: TSIO-520-NB Serial #: 519264 132 SB15-6B NiC3 Cylinders 8/9/2018 Applies if these cylinders are installed - none are 133 SIL16-2 Standard Practices Manual 4/15/2016 8/1/24 - 5650.9 Due during all Maintenance 134 SB16-7 H.E.T. Bulletin $ 067 2/3/2017 DNA per eng. m/n 135 SB16-6 Engine Kickback Damage 10/19/2016 Due when kickback occurs 136 SB16-8 Turbo Exh. Transition 2/3/2017 DNA per Eng. m/n 137 SB16-9 H,E.T. Bulletin # 066 2/3/2017 DNA per Alter. p/n 138 SB17-01A Flanged Nut (652541) Insp & Corr. Prev. 10/20/2017 DNA Due to nut installed at O/H 139 SB 670 TCM Magnetos Maint. 7/14/2017 DNA - Slick Mags Installed 140 SIL17-02 Turbo Check Valve Filter Insp. & Cleaning 7/12/2017 DNA per Eng. M/N 141 SIL17-03 Oil Filter Anti-stick Gasket 7/27/2017 Info. Only 142 SB17-04 TCM SB 670 - R+R of Dist. Block 7/17/2017 DNA - Slick Mags Installed 143 SB17-05 TCM SB 643C - Insp. Intervals 9/29/2017 DNA - Slick Mags Installed 144 SB17-06 Conn. Rod Bolt Insp. 10/20/2017 3/14/23 - 5425.5 Due at Connecting Rod Bolt Install 145 SIL 17-07 Discontinued Alternator 11/14/2017 Info. Only 146 SB18-04A R+R of Flanged Nut 12/18/2018 DNA per Date 147 SIL 18-02 Service Documents Applicability 2/15/2018 Info. Only 148 SIL19-04 Oil Brand Selection 10/11/2019 Info. Only 149 SB19-05 Valve Guide Application 10/24/2019 3/14/23 - 5425.5 Due @ O/H or Cyl. Repair 150 CSB19-06 Hartzell Alert SB 081A (Alter. Hub Nut) COMPLET 11/19/2019 9/13/21 - 5233.6 See SB for affected Units 151 SB19-07 C/S End Play 12/10/2019 DNA per Eng. S/N 152 SIL19-10 Oil Filter Removal 12/16/2019 Info. Only 153 SB20-01 Fuel Screen Maint. 2/20/2020 8/1/24 - 5650.9 Due ea. 100 hr./Annual 154 SB20-03 Eng. Pres. During COVID 4/13/2020 Info. Only 155 SIL20-05 Energizer Starter ICA's 9/28/2020 Info. Only 156 SB673C 1200 series Mag Bearings 5/24/2022 DNA - slick Mags are installed 157 MSB23-01A C/S Counterweights 2/16/2023 DNA per Eng. S/N 158 SB23-03 Hartzell SB 096 (Alternator) 5/24/2023 DNA per Alter. S/N AIRCRAFT PROPELLER MAINTENANCE RECORDS .Aircraft Reglstratio.n .~H~ 'U.....,fff\...._ 1' __ Propeller Position ~L~&.t-......... -t _ ___ Propeffer S8rlal Na. ·......,;;;EJ ...... 1,.;;.a;;c..u...,.s__ HARTZELL PROPELLER INC Item Number: C3F00270 INSPECTION Model Number PHC-C3YF-2UF/FC7693DFB Ass'y Ser No. I IHydr Unit No. ! Bulkhead No. [ Valve No. EB7625B NA NA NA Blade 1: L26571 IBlade 2: L26572 !Blade 3:L26573 !Blade 4: Clamp 1: !Clamp 2: !Clamp 3: !Clamp 4: Reverse I Start Lock Low Pitch !High Pitch !Feather Position GrienL Qty;AI NA NA 13.0 18.0 81.1 1 L 1 Ref Radius (inches) for angles: 30 Comments: Deice Kit: 5E2748-1 Included but not inst. Packing if/ly( ~~ Date: Certified B - / _.,,A 8--2-1--/ (__ Inspected By: John Martin Date: 8121/2012 Work Order#: M605350 •• ~. -~· ". ···-~-...-......... !Blade 5: !Blade 6: j Clamp 5: I St S crw A-2424-1 0 0 0 The approved design data for this propeller incoporates all changes required by applicable Airworthiness Directives. Washer 1 ) 254/752-8381 AIRCRAFT PROPELLER MAI NTENAN CE RECORDS Log No. __ Aircraft Registration No. ....!'J_ 4_lY_M_P______ Propeller Man ufact u rer __._'4....:.A""""r_-t-'-z.=-1!.. =-.L\ _,__\______ Hub Model ·\)\-\C- C. 3'/F-JlJF'iF'C7G,<l3DF8 • Blade Design No. ____________ _ Hub Serial No. ____.,i;'"""B.._7L,~!!<,.l=5""----""'B'------------ Blade Serial No's. 1. L .aG,57 1 2. '- a<. 57a 3. L ~ ~5 7 3 4. ------------- ----- Pitch Range: High 16. 0 Feather - -= 8 ,.;:_1;;_; · \.___ _ _ Low - --''---=3'-.0 -=----- - Reverse ---'N-'-+/-'-A-=------- Governor Manufacturer _ __________ Model No. _ ______ ____ _____ Serial No. ________ _____ __ _ -Date installed on aircraft _ _________ Time Between Overhauls (TBO) __ ___ Hours If used on multi-engine aircraft: ~Lett D Right □ Front □ Rear (All applicable information must be filled in) Waco Regional Airport• P.O. Box 5219 • Waco, Texas 76708 FAX 254-752-3307 1-800-445-9713 "LOGBOOK FORMAT REPRINTED WITH THE PERMISSION OF AEROTECH PUBLICATIONS, INC. THE ADLOG /TM\ SYSTEM, COPYRIGHT 1979." Page No. ____ DA S & S AVIATION CO (L) MODEL; PHC-C3YF-2UF CHEROKEE COUNTY AIRPORT AIC REG: N414MP 1800AIRPORT DRIVE AIC SIN: 414A-0317 BALL GROUND, GA. PROP SIN; EB7625B DATE: TACH: TOTAL: 07-22-2013 0208.6 0000.0 THIS PROPELLER INSTALLED IN LEFT POSITION OF N414lvll'. TRACK CIJECKED. RETURNED TO SERVICE. SIGNED: ~~~~ CERT#: 3479116A&PIA / I I I I - ---- -- Marshfield Municipal Airpon Geot,Je I larlcw Fl~.!d (GHG) IIS Old Coklny u,r,~ Morshfiel<I. MA 02050 12/1/2013 N414MP Cessna 414A, serial# 414A.0317 Hobbs Hours: 232.1 :: Aircraft TT; 4054. 7 :: #1 Propeller TT: 23.5 Completed annual inspection per FAR 43, appendix D using the manufacturers maint manual {part# 115N) as a guide. Propeller 1 Logbook I certify that this Propeller has been inspected in accordance with an annual inspection and was determined to be in an airworthy condition. Shoreline Aviation. !nc. 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 A.~hureline ..n.VIATION /; /u It! ~ ~ -?l A ~ --:1,,(\ Signed,__;;~c....o..... , _;_" -=-\, - ~--++----'fl '--(A _ v_ ,_' _ ..,,____ _ Shorelii,e Avlatlon, Irie. Mai,;hlield M,.,.,icipal Airport GeM9" Ha.~°" Fleld (GHQ) 93 Old Colony La.1e Marstmeld. MA 02050. Edward . Novak J r. A+P 2832024 IA 1/23/2015 N414MP Cessna 414A, serial# 414A..0317 Propeller 1 Logbook Hobbs Hours: 373.1 :: Aircraft TT: 4195.7 :: #1 Engine TT: 3326.1 :: #1 Engine SMOH: 165.1 :: #1 Propeller TT: 165.1 :: #2 Propeller TT: 165.1 #2 Engine TT: 2622.6 :: #2 Engine SMOH: 165.1 Completed Operations #3 & #4 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. I certify that this Propeller has been inspected in accordance with Operations #3 & #4 of the Cessna Progressive Care inpsection program and was determined to be in an airworthy condition Shoreline Aviation, Inc. 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 SUB-TOTALS this page TOTALS-Carry forward to next page p l,lar611fleld Mooic.,al Ar,port George Ha~oc, fl ~ d (GHG) &3 Old Co!onv L.an9 Ma,,,l\fiBld. MA 02050 7/212016 N414MP Cessna 414A,. seri111#414A-0317 Propeller 1 Logbook Hobbs Hours: 422.1 :: Aircraft TT: 4244.7 :: #1 Engine TT: 3377.3 :: #1 Engine SMOH: 216.3 :: #1 Propeller TT: 216.3 :: #2 Propeller TT: 216.3 :: #2 Engine TT: 2673.8 :: #2 Engine SMOH; 216.3 Completed Inspection Operation 1 in accordance with Cessna Model 414A Maintenance Manual (50 hour inspection items) I certify that this PropeUer has been inspected in accordance With a operation #1 inspection and was determined to be in an airworthy condition. Shoreline Aviation, Inc. 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 .- . . Sheehan A+P 3439269 IA Shoreline AVIATI ON -- -- - Shorullne Avlatioo, In c. -.--- - ---~~ M;.r&hHeld Mwi icipaJ Ai<?orl George Harlow Field (GHG) ·93 Oki Col~l'ly Lana Marshfield. MA 02050 8/27/2016 N414MP Cessna 414A, serial# 414A-0317 Propeller 1 Logbook Hobbs Hours; 472.6 :: Aircraft TT: 4295.2 :: #1 Engine TT: 3427.8 ;; #1 Engine SMOH: 266.8 :: #1 Propeller TT: 266.8 ;: #2 Propeller TT: 266.8 ;: #2. Engine SMOH: 266.8 :: Heater Hobbs: 419.0 - Completed Operation #2 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. The above work was completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work accomplished. Shoreline Aviation, Inc. 93 Old Colony Lane Marshfield, MA 02050 781-637-8521 Shorelim1 AVlatioil, Ille. +M"1$1111ekl Mu~;.;ipal Ai!TJQ'I Geo,ge ~ ow Fie!<! {GHG) 93 Old C<llony Lall!! Marshlialcl. MA 02050 2111/2016 N414MP Cessna 414-A. serial# 414-A-0317 Engine 1 Logbook Hobbs Hours: 504.5 :: Aircraft TT: 4327.1 :: #1 Engine TT: 3459.7 :: ft! Engine SMOH: 298.7 :: #1 Propeller TT: 298.7 :: #2 Propeller TT: 298.7 :: #2 Engine TT: 2756.2 :: #2 Engine SMOH: 298.7 Completed Operation #s 3 & 4 inpsection items per the Cessna 414A Maintenance manual progressive care inspection form. 1) Drained oil, added 11 qts, fr Phillips X/C 20w-50 oil. Installed and saftied a new AA48108-2 oil filter. 11'1$pected drained oil and oil lllterelement and noted no abnormal contaminants. 2) Cy!. Comp. Checked per TCM SB 03-03 as follows: 1) 70/80 2) 66/80 3) 64/80 4) 68/80 5) 65/80 6) 72/80. . . 3) CNV the follwing TCM repetitive SB's: M00-17 (C/C lnsp), 8B95-2 (Control linkage lnsp), 5B95-7 (Fuel Manifold valve cover 1nsp), S896-12 (cyf lnsp.), SB96-7C (Torque Values), MSB94-8D (Mag Timing), S1D97-3F (Fuel System) & S809-7 (C/S Rust) and noted no defects. 4) Ground runup and functional checks satisfactory with no fuel or oil leaks noted. I certify that this Engine has been inspected in accordance with Operation 3 & 4 of the Cessna Progressive Care inspection program and was determined to be in an airworthy condition. Shoreline Aviation, Inc, 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 s,,~,\J~JonE.Sheehan A+P 3439269 IA TOTALS-Carry forward to next page Shoreline Aviation, Inc. • ➔ Malshfleld Municil>aJ Airport GeQl'lje Harlow Field (G HG) 93 Old Cotony Lane M.Brshfielt!. MA 02050 2/11/2018 N414MP Cessna 414A, serial# 414A-0317 Propeller 1 Logbook HobbsHours:504.5 :: AlrcraftTT: 4327.1 :: #1 EnglneTT:3459.7 :: #1 EngineSMOH: 298.7 :: #1 PropellerTT:298.7 :: #2PropellerTT:298.7 :: #2 Engine TT: 2756.2 :: #2 Engine SMOH: 298.7 Completed Operation #'s 3 & 4 inpsection items per the Cessna 414A Main1enance manual progressive care inspection form. I certify that this Propeller has been inspected in accordance with Operation 3 & 4 of the Cessna Progressive Care inspect ion program and was determined to be in an airworthy condition. Shoreline Aviation, Inc. 93 Old Colony lane Marshfield, MA 02050 781-837.8521 ~,~~~E.Shtthan A+P 3439269 IA J 6/17/2016 N414MP ,\.,Shoreline rtVIATION Shoreline Aviation, Inc. ~ + -w----- Marshfie ld Municipal Aitporl George Harl ow Field (GHG) 93 Old Golo;,y Lane Marshfield. MA 02050 Cessna 414A, Serial Number 414A0317 Propeller 1 Logbook Hobbs Hours: 554.4 :: Aircraft TT: 4376.7 :: #1 Engine TT: 3509.3 :: #1 Engine SMOH: 348.3 :: #1 Propeller TT: 348.3 :: #2 Engine TT: 2805.8 :: #2 Engine SMOH: 348.3 :: #2 Propeiier TT: 348.3 Completed Operation 1 inspection items per the Cessna 414A Maintenance manualprogressive care inspection form. I certify t hat this Propener has been inspected in accordance with Operation 1 ot the Cessna Progressfv~~ i nspection program and was determined to be in airworthy condition. . ~ ~%-- Signed--==--== ~2 •• Ryan E ((e + 3825647 9/23/2016 N414MP Cessna 414A, serial# 414A-0317 Propeller 1 Logbook Hobb~.Hours:_~5.3 _,: .Aircraft TT: _44~ .9. :: #1 _Engine TT: 3600.5 :: #1 _Engine TSMOH: 439.5 :: #1 Propeller TT: 439.5 :: #2 Propeller TT: 439.5 :: #2 Engine TT: 2897.0 ;: #2 Engine TSMOH: 439.5 :: Heater Hobbs: 436.3 Completed Operation #3 inpsection items per the Cessna 414A Maintenance manual progressive care inspection fonn. Ground runup and functional checks were satisfactory with no grease or oil leaks noted, I certify that this Propeller has been Inspected in accordance with an Operation #3 inspection a in an aiiworthy condition. Signed?"'-::::,X::.--~ c::..,:=~'--- - - - ------ - SUB-TOTALS this page TOTALS-Carry forward to next page Page No. __ _ DATE .t!'boreline rtVIATION --- ----- Shonillne Aviation, Inc. Mai,;hficid Municipal A irr,ort George Har1ow Field (GHG) 93 Old Cok)ny lane M~rshfield. MA 0201;0 218/2017 N414MP Cessna 414A, serial# 414A-0317 Propeller 1 Logbook Hobbs Hours: 675.6 :: Aircraft TT: 4498.2 :: #1 Engine TT: 3630.8 :: #1 Engine TSMOH: 469.8 :: #1 Propeller TT: 469.8 :: #2 Propeller TT: 469.8 :: #2 Engine TT: 2927.3 :: #2 Engine TSMOH: 469.8 :: Heater Hobbs: 442.7 Reset propeller accum ulalor pressure to 41 psi fron, 30 psi with nitrogen. The above work was completed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service for the work accomplished. Shoreline Aviation, Inc. 93 Old Colony Lane Marshfield, MA 02050 781-837-8521 A!'horeline rtVIATION --- -- ---- Shoreline Aviation, IFie. ---+Marshlield Municipal Airport George Harlow Field (GHG) 93 Oto Colony Lane M>l'8111isld. ;.r;A 020/iO WOAK 5125/2017 N414MP Cessna 414A, serial# 414A-0317 Propeller 1 Logbook Hobbs Hours: 725.7 :: Aircraft TT: 4548.3 •• #1 Engine TT: 3683.2 :: #1 Engine TSMOH: 522.2 :: #1 Propeller TT: 522-2 :: #2 Propeller TT: 522.2 :: #2 Engine TT: 2979.7 :: #2 Engine TSMOH: 522.2 Completed Operation #1 inspection items per the Cessna 414A Maintenance manual progressive care inspection form. I certify that this Propeller has been inspected in accordance with an Operation #1 inspedion andiwas dete~ Signed .._,_ ✓, 4 .--.. /r in an airworthy condition. __:.:......---~-~---". ·" Laurence F. Mulloy A+P 23507120 -- --- --- Shoreline, Aviation, Inc. Marshll<lld Municip<>I Airp0rt George Harlow Fi eld (GHG.l 93 Old Colony La ne Ma rshfi0ld. MA 021)50 9/1/2017 N414MP Cessna 414A, serial# 414A-0317 Hobps Hours: 818. 0 :: Aircraft TT: 4640.6 #1 Engine TT: 3775.8 : #1 Engine TSMOH: 6