<p> ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S ------75-06-01 ENGINE OIL FILTER 03/10/75 N/A BY DOM X ------RUDDER NOSE GEAR ------A&P 75-16-02 II 400002 - 7520022 07/29/75 N/A BY S/N X ------(SB 446) - 2658075281A ------75-26-18 --- LDG SELEC CABLE ------R/B AD 96-24-13 ------SEE AD - 7400002 – ELEV. TRIM TAB SYSTEM ------A&P 76-03-01 II 02/09/76 N/A BY S/N X ------76220012 (SB 481A & 477A) - 2658075281A 7400002 - 7620002, LOOSE BOLTS ------A&P 76-04-11 II 7620004, 7620005, 03/05/76 N/A BY S/N X ------(SL 643 AND SB 487) - 2658075281A 7620007 ------76-10-06 ---- FLAPS ------R/B AD 82-27-13 R2 ------SEE AD - ELEVATOR STRUCTURE ------A&P 76-18-06 II 7400001 - 7620039 09/10/76 N/A BY S/N X ------(SB 504) - 2658075281A ELECTRICAL SHORT ------77-08-02 II 7400002 - 7720008 11/15/77 N/A BY S/N X ------EA4R147M (SB 526A) - I 7804001 – 7804006 M.L.G. ROD END BEARINGS 11/29/78 C/W BY INSPECTION PER SB 78-02-01 05/09/79 X ------EA4R147M II 7400002 - 7820077 (SB 570A) 445.0 570A. 06/05/78 FLAP SYSTEM OPERATION INSTALLED REV #4 INTO 78-08-12 ALL ALL CATEGORIES 04/26/78 HOBBS X ------EA4R147M POH REVISION POH 320.0 ------78-12-06 ALL 7620012 & UP NOSE GEAR INSPECTION 05/09/79 N/A BY S/N X ------EA4R147M - 12/24/92 C/W BY INSTALLING NEW CLEVELAND MLG WHEEL 78-13-06 ALL ALL S/N S 06/29/78 HOBBS BRAKE DISC/INSPECTION X ------EA4R147M ASSY. P/N 551775 32.48.0 NO LONGER APPLIES I, LANDING GEAR HOSES 11/03/99 REPLACED ALL HOSES PER 78-25-03 ALL S/N S 10/27/78 X ------II (SB 629) 4394.9 SB 629</p><p>1 REVISED 03/28/08 D:\Docs\2017-12- 16\02a499ae1e7f5a8d14aae9aafb402914.doc ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S 01/30/80 I 7804001 - 7904031 ELEVATOR TRAVEL C/W BY INSPECTION PER SB 79-12-02 07/02/79 HOBBS X ------EA4R147M 7400002 - 7920060 (SB 649) 649 II 551.0 05/31/79 I 7804001 - 7904033 CONTROL COLUMN ROLL C/W BY INSPECTION PER SB 79-14-02 05/03/79 HOBBS X ------EA4R147M 7400002 - 7920060 PINS (SB 651) 651 II 502.0 ALL S/N S ------N/A EQUIPMENT NOT 79-18-05 REPLACE ELT BATTERY 02/28/80 X ------S/S AD 79-05-02 - INSTALLED 01/30/80 I 7804001 – 7904016 ELECTROLUMINESCENT C/W BY RELOCATING 79-19-09 09/25/79 HOBBS X ------EA4R147M PANEL (SB 640) INVERTER PER SB 640 II 7400002 - 7920036 551.0 7904001 - 7904044 I 7920001 ------80-01-08 OIL COOLER HOSES 08/13/79 N/A BY S/N X ------EA4R147M II 7920068, 7920070 - - 7920080 7804001 - 7904036, ELEVATOR BUTT RIBS I ------80-02-15 7904038 – 7904044 KIT 766-219 01/29/80 R/B AD 2001-06-01 X ------EA4R147M II - 7400002 - 7920075 (SB 658) 02/10/94 C/W BY COUPLING FUEL PUMP COUPLING 80-08-12 ENGINE 04/18/80 HOBBS REPLACEMENT LT/RT NO X ------EA4R147M (SB 1316, 3139, 12025) 3483.3 LONGER APPLICABLE. 7804001 - 7904053, ------80-11-06 I DATA PLATE 05/28/80 N/A BY S/N X ------EA4R147M 7904056, 7904057 - 01/25/85 7400002 - 7620057, C/W BY INSTALLING 80-14-08 II AFM REVISION 07/07/80 HOBBS X ------EA4R147M 7720001 – 7920004 REVISION INTO POH 604.0 I 8104001 - 8104012 VOLTAGE REG MOD PIPER ------80-25-05 11/26/80 N/A BY S/N X ------EA4R147M II 8120001 - 8120010 LTR 31-26 - I GEAR DOOR HINGES ------80-26-05 SEE AD 12/19/80 R/B AD 2000-25-01 X ------II (SB 682) - 81-01-01 I 8104007 - 8104013 DEICE RELAY PIPER LTR 12/24/80 ------N/A BY S/N X ------EA4R147M 8120008 - 8120010 </p><p>2 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S II AND 8120013 #31-28 - M4D AUTOPILOT BENDIX N/A EQUIPMENT NOT GW1R181K 81-01-06 APPLIANCE 01/12/81 12/12/03 X ------(SB M4D060) INSTALLED WO 5866 I 7804001 - 8104001 FLAP TRACK REINFORCMNT P/C/W BY INSTALLATION 81-23-06 11/16/81 03/15/84 X ------II 7400002 - 8020086 (SB 647A) KIT 763-986 OF KIT 763-986 ------SEE AD JANITROL HEATER ------R/B AD 96-20-07 ------82-07-03 - I, EMERGENCY EXIT ------82-11-04 II, SEE AD 06/03/82 N/A BY S/N X ------EA4R147M (SB 733) - IIXL JET ELECTRONICS POWER N/A EQUIPMENT NOT GW1R181K 82-21-04 APPLIANCE 10/21/82 12/12/03 X ------SUPPLY INSTALLED WO 5866 7804001 - 7804011 FLAPS S/S 82-08-06 AND I 03/28/08 C/W BY INSPECTION EACH 100 82-27-13 R2 7400002 - 7820092, 76-10-06 (SL 958 & 959, 08/18/83 X HRS. OF GW1R181K WO 7317 II EXCEPT 78200067 SB 739, 741 & 494B) 5867.8 OPERATION 7/13/05 N/A MCCAULEY PROP GW1R181K 83-08-01 R2 ALL ALL S/N S HARTZELL PROP BOLTS 04/28/83 X ------5390.0 INSTALLED WO 6426 FUSE BLKHD CRACKS ------84-08-06 ---- SEE AD 05/09/84 R/B AD 96-10-13 ------KIT 764-983 - 7804001 - 8304003, I 1104004 - 1104006 11/27/85 C/W BY INSPECTION AND LANDING GEAR 85-08-05 7400002 - 8120104 05/20/85 HOBBS PIN REPLACEMENT PER SB X ------EA4R147M II S/B 779B IIXL 8166001 - 8166071, 1386.1 779A. 8166073, 8166076 GW1R181K 86-05-02 APPLIANCE UNITED INSTRUMENTS 05/28/86 12/12/03 N/A BY S/N X ------WO 5866</p><p>HYDRAULIC HOSES ------86-17-07 ---- SEE AD ------R/B AD 96-21-04 ------SB 822 ------88-05-05 --- L.G. SIDE BRACE ------R/B AD 96-10-14 ------SEE AD -</p><p>3 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S 07/21/95 AILERON BALANCE CABLE C/W BY MARKETING 92-27-05 ALL ALL S/N S 01/29/93 HOBBS X ------EA4R147M PAINT CABLES PER INSTRUCTIONS 981.8 N/A EQUIPMENT NOT GW1R181K 93-12-04 APPLIANCE PRECISE FLIGHT PULSELITE 07/26/93 12/12/03 X ------INSTALLED WO 5866 93-24-02 R1 02/15/94 ROD END REPLACED X ------EA4R147M 11/14/95 C/W BY ALL PA-31, 31P, ELEVATOR CONTROL 11/03/99 ALL INSPECTION AND PA31T SERIES SYSTEMS 4394.9 HARDWARE CHECKED 11/3/99 MLG ACT. REINFORCE ------93-25-08 ---- SEE AD BRACKET ------R/B AD 96-21-11 ------SB 923</p><p>GW1R181K 94-06-04 APPLIANCE EROS OXYGEN MASK 05/23/94 12/12/03 N/A BY S/N X ------WO 5866</p><p>PAC. SCI. LAP BELT ASSY N/A EQUIPMENT NOT GW1R181K 94-21-06 APPLIANCE 11/25/94 12/12/03 X ------SB 1108460-25-01 INSTALLED WO 5866</p><p>FUSE BLKHD CRACKS 02/16/86 C/W BY INSTALLING KIT 96-10-13 ALL SEE AD (SB 773A) S/S 84-08-06 06/27/96 HOBBS 764-983 PER SB 773A NO X ------EA4R147M (KIT 764-983) 1429.1 LONGER APPLICABLE 96-10-14 7804001 - 8304003, MAX 1200 HR. 06/27/96 X ------EA4R147M I C/W BY INSTALLING 1104004 - 1104017 FROM 06/27/96 11/24/87 IA BRACES P/N 85166-02-03 7400002 - 8120104 L.G. SIDE BRACE HOBBS PER SB 845A NO LONGER II 8166001 - 8166076, (SB 845A) 1785.0 APPLICABLE IIXL 1166001 – 1166008 SUPERCEDES AD 88-05-05</p><p>HARTZELL PROP BLADE ASB ------96-15-04 PROPELLER 07/29/96 N/A BY MFG X ------NO. HC-ASB-61-220 -</p><p>4 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S ------96-18-14 ALL ALL S/N S HARTZELL PROP HUBS 10/16/96 N/A MCCAULEY INSTALLED X ------C/W BY REPLACEMENT OF HEATER FUEL PUMP WITH EACH 100 ALL JANITROL HEATER 12/12/03 96-20-07 EXC ALL S/N S 11/14/96 OVERHAULED S/N 191198. X HRS. OF S/S 82-07-03 & 80-09-10 5091.9 XL GWR1R81K WO 5866 OPS R/B AD 2004-21-05 7804001 - 8304003 1104004 - 1104017 C/W BY INSPECTION AND I 03/25/94 7400002 - 7400009 INSTALL OF NEW HINGES 96-21-03 II AILERON HINGES (SB 967) 12/10/96 HOBBS X ------EA4R147M 7520001 - 8120104 PER SB 967 NO LONGER 3502.7 IIXL 8166001 - 8166076 APPLICABLE 1166001 – 1166008 I 7804001 - 8304003 1104004 - 1104017 HYDRAULIC HOSES 11/07/90 C/W BY INSPECTION PER SB 96-21-04 IA 7400002 - 8120104 SUPERCEDES AD 86-17-07 12/10/96 HOBBS X ------EA4R147M 822 II 8166001 - 8166076 (SB 822) 2593.9 IIXL 1166001 – 1166008 I 7804001 – 8304003 1104004 - 1104017 MLG ACT. REINFORCE BRK 11/07/09H C/W BY INSTALLING NEW 96-21-11 7400001 - 8120104 (SB 923) 12/16/96 OBBS BRACKETS P/N 73786-02 X ------EA4R147M II 8166001 - 8166076 SUPERCEDES AD 93-25-08 2593.9 PER SB 923 IIXL 1166001 – 1166008 LDG SELEC. CABLE ------96-24-13 II 7400002-7620013 SUPERCEDES AD 75-26-18 01/17/97 N/A BY S/N X ------EA4R147M - (SB 488) BRAKE HOSE INSP./REPL. ------97-02-01 IIXL 8166001 - 8166062 02/14/97 N/A BY MODEL X ------EA4R147M CLEVELAND (SB 7034) - PT6 BLEED VALVES (SB ------N/A BY APPLICATION 97-04-12 ALL ALL S/N S 14251 R1, 13287 R1, 12134, 03/14/97 X ------EA4R147M - LT/RT 4204, 3344 R1, 1538 R3)</p><p>5 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S N/A EQUIPMENT NOT GW1R181K 97-16-10 APPLIANCE RAPCO IN-LINE FILTERS 09/18/97 12/12/03 X ------INSTALLED WO 5866 I, 06/26/98 C/W BY INSTALLING INFO 97-26-12 II, ALL S/N S AFM REV. POWER LEVERS 01/28/98 HOBBS X ------EA4R147M INTO POH IIXL 4260.7 ALLIED SIGNAL KT76A ATC GW1R181K 98-14-03 APPLIANCE TRANSPONDERS, 08/16/98 12/12/03 C/W BY INSPECTION X ------WO 5866 P/N 066-1062-00/10/02 BFG SKYWATCH SKY497 N/A EQUIPMENT NOT GW1R181K 98-25-02 ALL APPLIANCE 12/22/98 12/12/03 X ------TOP MOUNTED ANTENNA INSTALLED WO 5866</p><p>GW1R181K 98-25-10 R1 ALL ALL S/N S SEAT RESTRAINT SYSTEM 01/14/00 12/12/03 N/A BY TYPE INSTALLED X ------WO 5866 I, 07/14/99 SEVERE ICING AFM REV C/W BY INSERTING INFO 99-14-01 II, ALL S/N S 08/17/99 HOBBS X ------EA4R147M SUPERCEDES AD 98-04-27 INTO POH IIXL 4394.9 07/28/00 PNEUMATIC WING AND TAIL C/W BY INSERTING INFO 2000-06-06 ALL ALL S/N S 05/05/00 HOBBS X ------EA4R147M DEICING BOOTS MTO POH 4494.6 7804001 – 8104073, 8104101, 8304001 – I MLG INBOARD DOOR HINGE C/W BY DYE PENETRATE 8304003, 1104004 – 04/20/01 IA ASSEMBLIES INSPECTION INSPECTION NO CRACKS NEXT DUE 2000-25-01 1104017 01/19/01 HOBBS X SUPERCEDES AD 80-26-05 NOTED AT THIS TIME DUE 6591.8 HRS II 7400002 – 8120104 4591.8 SB 682 IN 2000 HRS IIXL 8166001 – 8166076, 1166001 - 1166008 ELEVATOR BUTT RIB MOD AND TRIM TAB SYSTEM S/S, KIT 766-219 03/13/92 C/W BY INSTALLING KIT 2001-06-01 ALL ALL S/N’S 05/08/01 HOBBS 766-219 PER SB 897B SB X ------EA4R147M AD 70-26-06, AD 76-03-01 2889.0 477A= N/A BY S/N AND AD 80-02-15 (SB 477A AND SB 897B)</p><p>6 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S I, JANAERO HEATER FUEL ------2001-08-01 IA, SEE AD 05/10/01 R/B AD 2001-17-13 X ------PRESSURE REGULATOR - II C/W BY VISUAL JANAERO HEATER FUEL INSPECTION PRESSURE PRESSURE REGULATOR 10/25/01 CHECK AND MARKING 2001-17-13 ALL APPLIANCE 09/11/01 HOBBS X ------EA4R147M SB A-107 INSPECTION REQUIRED 4694.4 S/S AD 2001-08-01 ONLY UPON REPLACEMENT R/B AD 2004-25-16 R1 GARMIN GNS 430 GW1R181K 2001-23-17 ALL APPLIANCE 12/28/01 12/12/03 N/A S/N X ------SB 9905 REV A WO 5866 COLLINS TRANSPONDER N/A EQUIPMENT NOT GW1R181K 2002-06-05 ALL APPLIANCE 04/26/02 12/12/03 X ------P/N 522-2703-XXX INSTALLED WO 5866 COLLINS MODE S N/A EQUIPMENT NOT GW1R181K 2002-06-06 ALL APPLIANCE TRANSPONDER SB 34-3435 05/03/02 12/12/03 X ------INSTALLED WO 5866 P/N 622-9352-004 C/ LT BY VISUAL INSPECTION NO DEFECTS 06/09/03 EXHAUST CASE FLANGE NOTED AT THIS TIME NO LT HOBBS FUTHER ACTION REQUIRED INSPECTION 4990.4 ETT PT6A TURBOPROP UNTIL O/H DUE AT 2002-23-13 ALL SB 72-1610 R2 (PT6A21-135) 12/31/02 4547.2 RT X EA4R147M O/H ENGINES HOBBS C/ RT BY VISUAL SB 72-12173 R2 (PT6A11- INSPECTION NO DEFECTS 112) 4990.4 ETT 4735.8 NOTED AT THIS TIME NO FUTHER ACTION REQUIRED UNTIL O/H N/A EQUIPMENT NOT GOODRICH TAWS 8000 3/17/05 GW1R181K 2003-13-08 ALL SEE AD 06/18/03 INSTALLED X ------GOODRICH SM #134 5288.1 WO 6309 R/B AD 2004-08-15 2003-24-07 ALL AIRFRAME RUDDER TORQUE TUBE 2/9/04 08/08/07 C/W BY INSPECTION X INITIAL 150 ASSEMBLY SB 1105A 5776.2 GW1R181K WO 7132 HR OF (KIT 767-348) EFFECTIVE DATE THEN</p><p>7 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S</p><p>ANNUAL</p><p>KIDDE HAND HELD FIRE 10/27/04 N/A EQUIPMENT NOT GW1R181K 2003-26-14 ALL ALL S/N 02/20/04 X ------EXTINGUISHER 5193.4 INSTALLED WO 6115 GOODRICH TAWS 8000 10/27/04 N/A EQUIPMENT NOT GW1R181K 2004-08-15 ALL ALL (GOODRICH ALERT SB 06/07/04 X ------5193.4 INSTALLED A117) S/S (AD 2003-13-08) WO 6115 GARMIN GTX 330 XPNDR C/W BY INSTALLATION OF (GARMIN SB 0304B, SB 10/27/04 GW1R181K 2004-10-15 ALL ALL 11/03 SWV 3.06 UPGRADE X ------0310, SB 0401, SB 0409, SB 5193.4 WO 6115 0422, SB 0426) R/B AD 2005-01-19 JANITROL HEATER 08/08/07 C/W BY INSPECTION EVERY 100 2004-21-05 M SEE AD S/S 82-07-03, 80-09-10 & 11/14/04 X HR OR 2 S/S AD 96-20-07 5776.2 WO 7132 YRS EVERY 100 2004-25-16 HEATER FUEL PRESS 03/28/08 C/W BY INSPECTION M SEE AD REGULATOR 1/15/05 X HR OR 12 R1 5867.8 GW1R181K WO 7317 S/S AD 2001-17-13 MONTH GARMIN GTX 330 XPNDR SW V3.03/3.06 OR LATER ACCEPTABLE SB 0304 R/B 3/17/05 N/A BY SOFTWARE GW1R181K 2005-01-19 M ALL 0409 SW 2/23/05 X ------5288.1 INSTALLED WO 6309 V3.0/3.01/3.02/3.04/3.05 UNACCEPTABLE S/S AD 2004-10-15 SOUTHERN PROPELLER SERVICE OVERHAUL, D/N/A SOUTHERN CALIFORNIA 12/29/05 PROPS NOT OVERHAULED GW1R181K 2005-14-11 M SEE AD PROPELLER SERVICE 08/17/05 ------5489.8 BY SOUTHERN CALIFORNIA WO 6573 OVERHAULS PROPELLER SERVICE. THIS IS TERMINATING ACTION. 2005-14-12 M HC-B3TN-2, HC- HARTZELL PROP BOLTS B- 07/29/05 12/29/05 HARTZELL PROP BOLTS B------GW1R181K B3TN-3, HC-B3TN- 3339 5489.8 3339, D/N/A AFFECTED WO 6573 5, HC-B3MN-3, HC- HARTZELL SB HC-ASB-61- LOT # NOT INSTALLED. B4TN-3, HC-B4TN- 279 R3, THIS IS TERMINATING </p><p>8 ********AIRWORTHINESS DIRECTIVE COMPLIANCE RECORDS******** AIRCRAFT REG# N115PC MAKE PIPER MODEL PA31T SERIAL NO. 31T-7820001 C</p><p>L O NEXT R AUTHORIZED AD EFFECT COMP METHOD OF N COMP. E A S/N EFFECT SUBJECT C SIGNATURE C DUE NUMBER DATE DATE COMPLIANCE E NUMBER S DATE/HR S 5, HC-B4MN, HC- B4MP-3, HC-B4MP- RAYTHEON SB 61-3737 ACTION. 5, HC-B5MP-3 D/N/A PER MFG AND P/N BFG PROP DEICER BOOT 07/06/06 GW1R181K 2005-18-20 M SEE AD 10/14/05 INSTALLED. THIS IS ------(BFG ASB-30-60-00-1) 5590.9 TERMINATING ACTION. WO 6763 D/N/A BY PROP S/N AND HARTZELL/MCCAULEY 03/14/07 GW1R181K 2006-24-07 M SEE AD 01/03/07 OVERHAUL AGENCY. THIS X ------PROP OHL’S 5696.0 IS TERMINATING ACTION. WO 6992</p><p>9</p>