Owner type
Co-owned
Serial number
31-8353006
Year built
1982
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
September 30, 1983
Certificate issued
November 13, 2023
Expires
November 30, 2030
Mode S code
A4DA7F

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.

On this page

Airworthiness directives that may apply · 106

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1969In forceSuperseded2026
ADs by the year they took effect: 125 ADs
19691
19711
19731
19741
19754
19763
19777
19784
19797
19806
19812
19832
19841
19851
19861
19871
19892
19912
19922
19932
19942
19951
19968
19974
19985
19993
20002
20012
20023
20032
20043
20054
20066
20084
20092
20102
20113
20125
20132
20152
20162
20173
20221
20231
20241
20261
See all 129 ADs

Information bulletins that may apply · 13

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations · 3

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 13

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR EPUA20190510001Door Seal · damagedPILOT REPORTS THAT THE AUTOPILOT ANNUNCIATOR LIGHTS BEGAN FLASHING, WENT OUT AND THEN THE AUTOPILOT TURNED OFF. THE DG PORTION OF THE HSI FROZE ON A HEADING OF 065 AND THEN PILOT REPORTS A SMELLED SOMETHING LIKE BURNT RUBBER OR ELECTRICAL. MAINTENANCE INSPECMay 2, 2019 · N4112K · Piper PA31350 · Passenger/Crew DoorsSDR EPUA20170221001Insert · bentDURING FLIGHT, FUEL PRESSURE ON NR 2 ENGINE TO BE UNSTABLE AND LOW. ELECTED TO SHUTDOWN ENGINE AND FEATHER PROP. MADE UNEVENTFUL LANDING. MX INSPECTED THE AIRCRAFT AND DETERMINED RT HAND OUTBOARD FUEL CAP ADAPTER INSERT ASSEMBLY WAS DEFECTIVE AND BENT WHICHFeb 18, 2017 · N4112K · Piper PA31350 · Fuel StorageSDR EPUA2011112300002Turbine Wheel · misoverhauledTURBOCHARGER FAILURE OF TURBINE WHEEL ASSY DUE TO INCORRECT ASSEMBLY OF TURBOCHARGER FROM MFG. WASHER PN 407135-0000 WAS INSTALLED ON THE WRONG SIDE OF BEARING JOURNAL 407134-0000.Nov 23, 2011 · N4112K · Piper PA31350 · Exhaust TurbochargerSDR FFS2003F00020Spool · brokenENGINE OVERSPEED DUE TO INTERNAL FAILURE OF THE PROPELLER GOVERNOR. SPOOL B-3166 SEPARATED FROM SPOOL EXTENSION A-3167, CAUSING GOVERNOR TO ACT AS IF IN AN UNDERSPEED CONDITION, SENDING BOOST OIL PRESSURE TO FORCE PROPELLER TO LOW PITCH. SEPARATION MAY HAVE Sep 12, 2003 · N4112K · Piper PA31350 · Propeller GovernorSDR FL178168Nut · looseTHE MECHANIC WAS SPINNING THE TURBOCHARGER COMPRESSOR-TURBINE SHAFT BEFORE HE PUT THE INTAKE ELBOW ON THE TURBOCHARGER. WHEN HE DISCOVERED THAT THE LOCK NUT ON THE INTAKE END OF THE SHAFT COULD BE SPUN OFF BY HAND. NO EVIDENCE OF THE INSPECTORS LOCK SEAL, ETNov 18, 2002 · N4112K · Piper PA31350 · Exhaust TurbochargerSDR FL80981Contactor · loosePILOT REPORTED INOPERATIVE RIGHT MDG ON LEFT ENGINE. UPON INSPECTION OF MAGNETO, THE CONTACT ASSEMBLY WAS FOUND TO BE THE CAUSE. THE TWO RIVETS THAT HOLD THE CAM FOLLOWER ONTO THE CONTACT ASSEMBLY WERE LOOSE. ITLOOKS LIKE THE SLOT HEADS HAVE WORN INTO THE CApr 16, 2002 · N4112K · Piper PA31350 · Magneto/DistributorSDR FFS2002F00001Support Bracket · crackedCRACK IN RADIUS OF NOSE GEAR ACTUATOR ATTACH SUPPORT BRACKET. FOUND DURING INSPECTION.Feb 8, 2002 · N4112K · Piper PA31350 · Nose/Tail Landing Gear Strut/AxleSDR FFSA200202Support Bracket · crackedCRACK IN RADIUS OF NOSE GEAR ACTUATOR ATTACH SUPPORT BRACKET, FOUND DURING INSPECTION.Feb 8, 2002 · N4112K · Piper PA31350 · Nose/Tail Landing Gear Strut/AxleSDR FL93116Shaft · stiffFLAPS WOULD NOT RETRACT AFTER LANDING. FINDINGS: THE RIGHT FLAP FLEXIBLE SHAFT ASSEMBLY TURNS VERY STIFFLY AND CONTRIBUTED TO FAILURE OF THE FLAP ACTUATOR MOTOR. THE LEFT FLEXIBLE SHAFT ASSEMBLY TURNS FREELY.(K)Nov 23, 2001 · N4112K · Piper PA31350 · Trailing Edge Flap Control SystemSDR 20001120SH036Regulator · leakingFUEL REGULATOR ON JANITROL HEATING SYSTEM (FORWARD) LEAKED AT CASE PARTING SURFACES. (X)Oct 31, 2000 · N4112K · Piper PA31350 · Heating SystemSDR 98ZZZX4559Heater · malfunctionedFUEL WAS OBSERVED RUNNING OUT OF THE FUEL REGULATOR/SHUTOFF VALVE DRAIN CAVITY ON THE FRONT HEATER DURING A ROUTINE HEAT OR MAINTENANCE CHECK. FURTHER INVESTIGATION REVEALED THE VALVE WAS LEAKING FROM THE MATING SURFACE BETWEEN THE VALVE BODY AND THE REGULATONov 20, 1998 · N4112K · Piper PA31350 · Heating SystemSDR 98ZZZX4502Regulator · leakingFUEL LEAK ON INLET SIDE OF REGULATOR BODY. SUBMITTER STATED THIS WAS ONE OF THREE REGULATORS INSTALLED IN A TWO-WEEK PERIOD THAT FAILED. MFG DATE 7-98. REMOVED 11-10-98.Nov 10, 1998 · N4112K · Piper PA31350 · Heating SystemSDR 95ZZZX685Distributor Gear · teeth missingDURING RUN-UP BEFORE FLIGHT, FOUND BAD MAG CHECK ON LT ENGINE RT MAG. REMOVED MAG FOR INSPECTION AND FOUND WHITE PLASTIC DRIVE GEAR INSIDE MAGNETO WAS MISSING NUMEROUS DRIVE TEETH, THE REST OF MAGNETO APPEARS SERVICEABLE.Jan 1, 1995 · N4112K · Piper PA31350 · Magneto/Distributor

STCs that may be installed · 300

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 300 STCs