# Service difficulty reports: Piper PA-34-220T A list on [Piper PA-34-220T](https://openairdocs.org/model/piper-pa-34-220t.md). Newest first. General aviation reporting is voluntary. Page 1 of 6 · 297 reports - [SDR 2024FA0000239](https://openairdocs.org/sdr/2024FA0000239.md): Tire · failed · Mar 15, 2024 · N8048Q · Piper PA34220T · Tire > PILOT REPORTED ON LANDING THAT HE FELT THE AIRCRAFT YAWING TO THE RIGHT AND REALIZED HE HAD A FLAT TIRE. AIRPORT USED A SET OF DOLLIES TO MOVE THE AIRCRAFT BACK TO WINGS OF HOPE RAMP AREA. BOTH MAIN TIRES AND TUBES WERE REPLACED WITH NEW. WHEEL WAS DISASSEMBLE - [SDR 2023FA0000617](https://openairdocs.org/sdr/2023FA0000617.md): Fork · cracked · Apr 25, 2023 · N9284R · Piper PA34220T · Main Landing Gear Strut/Axle/Truck > DURING ANNUAL INSPECTION, CRACKES WERE FOUND IN THE UPPER 2 BOLT HOLES OF THE FORK ON THE MLG STRUT ASSEMBLIES. LT AND RT MLG. CRACKS MAY BE STRESS PLACED ON THE LOWER FORK AT THE AXLE ATTACH POINT DURING LANDING. - [SDR 8HBR20230415051](https://openairdocs.org/sdr/8HBR20230415051.md): Bolt · mismanufactured · Apr 15, 2023 · N4324D · Piper PA34220T · Fasteners > BOLT, PIPER P/N 402-921 QUANTITY OF 8 WERE ORDERED FROM BOEING, 4 OF THE 8 DID NOT HAVE THE HOLE DRILLED THROUGH THE THREADS FOR THE COTTER PIN. PIPER TAGS ON BOLTS DATED: 01/07/2022. LINE LOT/BATCH:7365740436 ON THE INVOICE FROM BOEING. - [SDR 2022FA0000739](https://openairdocs.org/sdr/2022FA0000739.md): Magneto · failed · Dec 5, 2022 · N9284R · Piper PA34220T · Magneto/Distributor > MISFIRE FROM ENGINE IN FLIGHT, AND 200+ RPM DROP ON MAGNETO CHECK AFTER LANDING APPROXIMATELY 120 HOURS SMOH ON ENGINE, TSIO-360-RB2 CONTINENTAL. NORMAL MAGNETO DROP IS 75 RPM, SO OUTSIDE OF TOLERANCE. MAGNETOS WERE OVERHAULED BY QAA IN OKLAHOMA AT THE TIME OF - [SDR 2021FA0000101](https://openairdocs.org/sdr/2021FA0000101.md): Rod End · sheared · Apr 12, 2021 · N8350Z · Piper PA34220T · Landing Gear Door Retract Section > FAILURE OF THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY, CAUSING A NOSE LANDING GEAR COLLAPSE, AND A DUAL ENGINE PROPELLER STRIKE. THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY BENT, AND THEN SHEARED AT THE ADJUSTABLE ROD END. - [SDR IKBR2020410101](https://openairdocs.org/sdr/IKBR2020410101.md): Pitot Line · broken · Apr 9, 2020 · N9295N · Piper PA34220T · Pitot/Static System > AIRCRAFT WAS DEPARTING AFTER ANNUAL AND AIRSPEED WAS NOT SEEN AND TAKEOFF WAS ABORTED AFTER VERY HEAVY BRAKING AND RUNNING OFF THE END OF THE RUNWAY THE LEFT TIRE BLEW AND THE RIGHT PROP STRUCK THE END OF RUNWAY LIGHTS CAUSING A PROP STRIKE AND ENGINE TEAR DOW - [SDR YBBA201908280001](https://openairdocs.org/sdr/YBBA201908280001.md): Warning Light · inoperative · Aug 27, 2019 · N25460 · Piper PA34220T · Landing Gear Position and Warning > PIC REPORTS NOSE GEAR INDICATION INOP DURING GEAR DOWN CYCLE, CYCLED GEAR 3 TIMES AND CONFIRMED GEAR DOWN WITH ATC ACKNOWLEDGEMENT DURING FLY BY, AFTER CYCLING GEAR ALL THREE INDICATIONS WERE PRESENT. - [SDR CA190530009](https://openairdocs.org/sdr/CA190530009.md): Probe · malfunctioned · May 23, 2019 · Piper PA34220T · Reciprocating Engine Cylinder Section > (CAN) ON JANUARY 24, 2019 THE LEFT HAND ENGINE CHT SHOWED AN OVER TEMP INDICATION AND ACTIVATED THE MASTER CAUTION. THE CHT WAS REPLACED WITH A NEW UNIT AT 2738.8 TAT. ON MAR 19, 2019 THE R/H CHT FAILED CAUSING A MASTER CAUTION INDICATION. THE CHT PROBE WAS RE - [SDR 2018FA0000257](https://openairdocs.org/sdr/2018FA0000257.md): Pump · inoperative · Apr 19, 2018 · N948FB · Piper PA34220T · Heating System > REMOVED HEATER FUEL PUMP, P1-91E92-1, SN A97070063. PUMP INOPERATIVE. - [SDR XKBA201708180002](https://openairdocs.org/sdr/XKBA201708180002.md): Starter · inoperative · Aug 16, 2017 · N24WE · Piper PA34220T · Engine Starter > STARTER MOTOR FAILED AFTER LONG PERIOD OF CRANKING. REPLACED STARTER WITH OVERHAULED. - [SDR XKBA20170818001](https://openairdocs.org/sdr/XKBA20170818001.md): Pump · inoperative · Aug 16, 2017 · N24WE · Piper PA34220T · Fuel Boost Pump > ELECTRIC FUEL PUMP INOPERATIVE WHEN TRYING TO START THE AIRCRAFT. INSTALLED A NEW OVERHAULED PUMP. - [SDR XKBA201706280001](https://openairdocs.org/sdr/XKBA201706280001.md): Control Cable · out of adjust · Jun 28, 2017 · N24WE · Piper PA34220T · Propeller Controlling System > LEFT PROPELLER WOULDN'T FEATHER DURING TRAINING. ADJUSTED THE TRAVEL ON THE GOVERNOR CONTROL AND PROP OPERATED NORMALLY AFTER ADJUSTMENT. - [SDR 2017FA0000143](https://openairdocs.org/sdr/2017FA0000143.md): Torque Tube · out of position · Mar 24, 2017 · Piper PA34220T · Flight Control System > DURING INSPECTION OF THE AIRPLANE, AFTER REPAIR, DISCOVER THAT THE BOLT WAS DAMAGED RIGHT CHANNEL TUNNEL AGAIN. AFTER ISSUE ANALYSIS AT THE AIRPLANE, DISCOVER THAT THE TORQUE TUBE HAD AXIAL DISPLACEMENT. WHEN TORQUE TUBE IS IN RIGHT END PIER POSITION THE B - [SDR XKBA201703290001](https://openairdocs.org/sdr/XKBA201703290001.md): Skin · cracked · Mar 3, 2017 · N24WE · Piper PA34220T · Trailing Edge Flaps > FOUND SMALL CRACK IN LEFT FLAP SKIN LOWER INBOARD END. INSTALLED NEW FLAP SKIN. - [SDR 2016FA0000554](https://openairdocs.org/sdr/2016FA0000554.md): Bolt · not reported · Nov 4, 2016 · Piper PA34220T · Flight Control System > DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, INDEX NUMBER 90) DAMAGED CHANNEL-TUNEL-RIGHT, PN95599-003 (SECTION II, FUSELAGE GROUP, FIGURE NR 12, IN - [SDR 2015FA0000168](https://openairdocs.org/sdr/2015FA0000168.md): Bearing · loose · Apr 29, 2015 · N77FT · Piper PA34220T · Main Landing Gear > DURING ANNUAL INSPECTION IT WAS NOTED THAT PRESSED IN BEARING WAS LOOSE IN LOWER DRAG LINK AND ONLY THING HOLDING BEARING IN WAS THE WASHER UNDER THE BOLT HEAD - [SDR 2013FA0000094](https://openairdocs.org/sdr/2013FA0000094.md): Cap · departed · Feb 2, 2013 · N8455Z · Piper PA34220T · Wing Main, Frame Structure > FUEL CAP ON THE WING INCORRECTLY INSTALLED AFTER REFUELING, FUEL CAP EVENTUALLY DEPARTED THE ACFT INFLIGHT. CAP WAS CHECKED DURING THE PREFLIGHT, AFTER REFUELING, AND THE CAP PLACEMENT WAS CLEARLY FLUSH WITH THE WING, AND THE "HANDLE" WAS FOLDED DOWN AND FLUS - [SDR 2012FA0000717](https://openairdocs.org/sdr/2012FA0000717.md): Contactor · corroded · Oct 12, 2012 · N77FT · Piper PA34220T · Electrical Power System Wiring > AFTER ACFT WAS EXPOSED TO HEAVY RAIN. BATTERY WENT DEAD. GPU START NORMAL AND FLIGHT NORMAL. AT SHUTDOWN TURNING MASTER SWITCH OFF, DID NOT TURN POWER OFF. FOUND MASTER CONTACTOR FULL OF CORROSION. DUE TO ITS LOCATION IT IS POSSIBLE IF TIED DOWN IN A TAIL LO - [SDR 2012FA0000310](https://openairdocs.org/sdr/2012FA0000310.md): Control Cable · frayed · May 11, 2012 · N24WE · Piper PA34220T · Elevator Control System > FOUND LOWER ELEVATOR CABLE FRAYED WHERE IT RIDES ON A PHENOLIC BLOCK AT FS222.43. - [SDR CA120221012](https://openairdocs.org/sdr/CA120221012.md): Landing Gear · collapsed · Nov 25, 2011 · Piper PA34220T · Main Landing Gear > (CAN) RT LANDING GEAR SELECTED DOWN, NO INDICATION OF RT GEAR LOCKED. AIRCRAFT LANDED AND RT GEAR COLLAPSED AT SLOW SPEED. - [SDR CA110916004](https://openairdocs.org/sdr/CA110916004.md): Potentiometer · burned · Sep 15, 2011 · Piper PA34220T · Passenger Compartment Lighting > (CAN) ON CLIMB OUT CREW DETECTED A SMOKE/BURNING - SHORTLY AFTER CABIN FILLED WITH SMOKE. ACFT SHUT ELECTRIAL POWER OFF, SQUAWKED EMERGENCY ON TRANSPONDER AND LANDED WITH OUT INCIDENT. - [SDR CA110805004](https://openairdocs.org/sdr/CA110805004.md): Cable · frayed · Aug 4, 2011 · Piper PA34220T · Elevator Control System > ON INSP, FOUND A FRAYED ELEVATOR TRIM CABLE. - [SDR CA100804020](https://openairdocs.org/sdr/CA100804020.md): Selector Switch · broken · Jun 10, 2010 · Piper PA34220T · Landing Gear Retraction/Extension System > WHEN MOVING THE GEAR SELECTOR SWITCH TO THE GEAR UP POSITION FOLLOWING TAKEOFF, THE GEAR SELECTOR SWITCH PHYSICALLY BROKE OFF AT THE STEM, BETWEEN THE SWITCHES PIVOT POINT AND THE ROUND PLASTIC HANDLE, NEAR THE DETENT USED TO KEEP THE SWITCH IN THE GEAR-UP POS - [SDR 2010FA0000705](https://openairdocs.org/sdr/2010FA0000705.md): Control Cable · broken · Jun 9, 2010 · N104NW · Piper PA34220T · Elevator Control System > STABILATOR CONTROL CABLE, PN62701-129, FAILED IN FLIGHT. THE CABLE SEPARATED ON LANDING. THE PILOT WAS UNABLE TO FLARE RESULTING IN A HARD LANDING IN A NOSE LOW CONDITION. THERE WAS SUBSTANTIAL DAMAGE TO THE ACFT. THERE WAS NO CORROSION ON THE CABLE EITHER EXT - [SDR 2009FA0000463](https://openairdocs.org/sdr/2009FA0000463.md): Crankshaft · cracked · May 1, 2009 · N786MS · Piper PA34220T · Reciprocating Engine Power Section > DURING ANNUAL INSP, OIL WAS FOUND AT FRONT OF ENGINE. FURTHER INVESTIGATION REVEALED A CRACK OF THE CRANKSHAFT AT THE PROP MOUNTING FLANGE. CAUSE HAS NOT BEEN DETERMINED. (K) - [SDR 2009F00027](https://openairdocs.org/sdr/2009F00027.md): Cable · damaged · Apr 14, 2009 · N557C · Piper PA34220T · Auto Flight System > FAILURE OCCURRED WITH THE AUTOPILOT ROLL SERVO BRIDLE CABLE. THE BRIDLE CABLE APPARENTLY JUMPED AND OVERLAPPED ITSELF ON THE SERVO SPOOL, EFFECTIVELY JAMMING THE AILERON DURING CLIMB OUT IN A TURN TO THE LT. THE AP WAS NOT ENGAGED AT THE TIME AND THE PIC WAS A - [SDR 2009FA0000257](https://openairdocs.org/sdr/2009FA0000257.md): Engine · damaged · Mar 25, 2009 · N423SJ · Piper PA34220T · Engine (Turbine/Turboprop) > PILOT REPORTED THAT THE RT ENGINE LOST OIL PRESSURE AND RPMS. NO N1 INDICATION. ENGINE WAS SHUT DOWN AND ACFT RETURNED TO DEPARTURE. - [SDR 2009FA0000253](https://openairdocs.org/sdr/2009FA0000253.md): Line · chafed · Mar 19, 2009 · N104WT · Piper PA34220T · Hydraulic System, Main > WHILE COMING IN FOR A LANDING, CUSTOMER WENT TO EXTEND LANDING GEAR AND GEAR WOULD NOT EXTEND. USED EMERGENCY GEAR EXTENSION AND LANDED ACFT WITH NO INCIDENT. UPON TROUBLESHOOTING FOUND RETRACTION LINE FROM HYD POWER PACK CHAFED THROUGH. HYDRAULIC LINE WAS - [SDR 2009FA0000053](https://openairdocs.org/sdr/2009FA0000053.md): Points · loose · Jan 26, 2009 · N8456H · Piper PA34220T · Magneto/Distributor > POINTS WERE FOUND NOT MAKING CONTACT, UPON FURTHER EXAMINATION, FOUND THE STATIONARY CONTACT LOOSE IN MAG. IT SEEMED TO HAVE COME OFF THE END, THE CONTACT DISK SEPARATED FROM THE BASE. (K) - [SDR 2008FA0000004](https://openairdocs.org/sdr/2008FA0000004.md): Strut · cracked · Jan 2, 2008 · N69BP · Piper PA34220T · Main Landing Gear Strut/Axle/Truck > DURING ANNUAL INSPECTION, IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSEMBLY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION OF THE CASTING AT THE 11 O'CLOCK AND 1 O'CLOCK POSITIONS. THIS MILLED SECTION IS USED TO BOLT THE TO - [SDR 2008FA0000003](https://openairdocs.org/sdr/2008FA0000003.md): Strut · cracked · Jan 2, 2008 · N69BP · Piper PA34220T · Main Landing Gear Strut/Axle/Truck > DURING ANNUAL INSPECTION IT WAS NOTED THAT A CRACK WAS FOUND ON THE RT MAIN GEAR LOWER FORK ASSY PN 39489-003. THE CRACK IS LOCATED IN THE MILLED SECTION OF THE CASTING AT THE 11 O'CLOCK AND 1 O'CLOCK POSITIONS. THIS MILLED SECTION IS USED TO BOLT THE TORQUE - [SDR 2007FA0001074](https://openairdocs.org/sdr/2007FA0001074.md): Control System · seized · Nov 30, 2007 · N557C · Piper PA34220T · Rudder Control System > WITH FULL RT RUDDER TRIM, RT RUDDER FOR HARD CLIMBING RT TURN, RUDDER FROZE WITH FULL RT DEFLECTION. RUDDER CABLE TURNBUCKLE IN TAIL SECTION WAS (CAUGHT) UNDER BULKHEAD TOP EDGE CAUSING RUDDER TO FREEZE IN FULL RT DEFLECTION - DESPITE SIGNIFICANT LT RUDDER PR - [SDR 2007FA0000942](https://openairdocs.org/sdr/2007FA0000942.md): Landing Gear · collapsed · Sep 21, 2007 · N84643 · Piper PA34220T · Nose/Tail Landing Gear > AIRCRAFT TAXIED TO RUNWAY AFTER LOADING CARGO. AFTER NORMAL RUNUP, THE PILOT TAXIED ONTO THE RUNWAY AND STOPPED. THE PILOT ADVANCED THROTTLES AND RELEASED BRAKES, AFTER RELEASING BRAKE, THE NOSE GEAR COLLAPSED. AIRCRAFT WAS RECOVERED AND TOWED OFF RUNWAY TO - [SDR 2007FA0000729](https://openairdocs.org/sdr/2007FA0000729.md): Bushing · misinstalled · Aug 3, 2007 · N19WE · Piper PA34220T · Reciprocating Engine Power Section > DURING THE PROCESS OF INSPECTING (6 EA) CONNECTING RODS IAW SB 07-1 AND SB 00-3, IT WAS FOUND THAT ALL WRIST PIN BUSHINGS WERE INSTALLED NOT IAW THEIR POSITIONS AS REQUIRED IN THE APPLICABLE SB AS REFERENCED. SPLIT LINE OF BUSHING ON WRONG SIDE OF CENTERLINE. - [SDR 2007FA0000292](https://openairdocs.org/sdr/2007FA0000292.md): Floor Panel · debonded · Apr 2, 2007 · N682JK · Piper PA34220T · Fuselage Floor Panel > FLOORPANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED THR - [SDR 2007FA0000291](https://openairdocs.org/sdr/2007FA0000291.md): Floor Panel · debonded · Apr 2, 2007 · N682JK · Piper PA34220T · Fuselage Floor Panel > FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED T - [SDR 2007FA0000290](https://openairdocs.org/sdr/2007FA0000290.md): Floor Panel · debonded · Apr 2, 2007 · N682JK · Piper PA34220T · Fuselage Floor Panel > FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED TH - [SDR 2007FA0000289](https://openairdocs.org/sdr/2007FA0000289.md): Floor Panel · debonded · Apr 2, 2007 · N682JK · Piper PA34220T · Fuselage Floor Panel > FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED T - [SDR 2007FA0000288](https://openairdocs.org/sdr/2007FA0000288.md): Floor Panel · debonded · Apr 2, 2007 · N682JK · Piper PA34220T · Fuselage Floor Panel > FLOOR PANEL BETWEEN FORWARD AND REAR WING SPARS ON WHICH AFT FACING CENTER SEATS ARE MOUNTED IS DELAMINATING. THE FLOOR PANEL CONSISTS OF 2 SHEETS OF ALUMINUM (.040 INCH) WITH A SOUND DEADENING STIFF FOAM BETWEEN THEM. THE SEAT MOUNTING BRACKETS ARE BOLTED TH - [SDR 2007FA0000085](https://openairdocs.org/sdr/2007FA0000085.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATOR, IN IMC SIMULTANEOUSLY. COUPLING FAILURE RESULTED IN TOTAL ELECTRICAL FAILURE, RT ENGINE. - [SDR 2007FA0000077](https://openairdocs.org/sdr/2007FA0000077.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED - [SDR 2007FA0000076](https://openairdocs.org/sdr/2007FA0000076.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED - [SDR 2006FA0000571](https://openairdocs.org/sdr/2006FA0000571.md): Points · failed · May 31, 2006 · N8456H · Piper PA34220T · Ignition System > THE POINTS WHICH ONLY HAD A TOTAL OF 9.3 HR, HAD THE PLASTIC PORTION WHICH RIDES THE CAM, MELT ON THE METAL OF THE POINTS WHICH REDUCED THE GAP TO CAUSE MISFIREING. CAPACITOR CHECKED GOOD AND WAS NOT REPLACED ON THE 500 HR INSP. AFTER A NEW POINT SET WERE IN - [SDR 2006FA0000717](https://openairdocs.org/sdr/2006FA0000717.md): Rib · cracked · Mar 11, 2006 · N8164D · Piper PA34220T · Wing, Rib/Bulkhead > DURING COMPLIANCE WITH SB, LT AND RT RIBS FOUND CRACKED AS SUSPECTED. INSTALLED REPAIR KITS. LT DRAG BRACE PIVOT, PN 39479002, ALSO FOUND CORRODED AND CRACKED. THIS IS NOT PART OF SB INSPECTION. (K) - [SDR 2006FA0000372](https://openairdocs.org/sdr/2006FA0000372.md): Axle · cracked · Mar 9, 2006 · N9219X · Piper PA34220T · Main Landing Gear Strut/Axle/Truck > CRACKS IN BOTH UPPER BOLT HOLES THAT SECURE AXLE TO STRUT ASSEMBLY ON BOTH LT AND RT MLG. PROBABLE CAUSE MAYBE HARD LANDING OR FATIGUE CRACKS DO TO NORMAL USE. (K) - [SDR CA070207006](https://openairdocs.org/sdr/CA070207006.md): Trunnion · failed · Jan 20, 2006 · Piper PA34220T · Fuselage, Landing Gear Attach Fittings > (CAN) NOSE GEAR TRUNNION DAMAGED AND REPAIRED. (TC NR 20070207006) - [SDR 43881](https://openairdocs.org/sdr/43881.md): Fuel Line · chafed · Dec 13, 2005 · N1130D · Piper PA34220T · Engine Fuel Distribution > THE FUEL INJECTOR LINE FROM THE FLOW DIVIDER TO THE NR3 CYLINDER ON THE RT ENGINE WAS ROUTED UNDER A COWL LATCH FOR THE COWLING NOSE BOWL WHICH CAUSED SEVER CHAFING IN A LOCALIZED AREA. THIS WAS ORIGINAL FACTORY ROUTING. NO FAILURE OCCURRED, PART WAS REPLACE - [SDR AU510002142](https://openairdocs.org/sdr/AU510002142.md): Pump · contaminated · Dec 12, 2005 · Piper PA34220T · Engine Fuel Pump > LT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL. - [SDR AU510002141](https://openairdocs.org/sdr/AU510002141.md): Pump · contaminated · Dec 12, 2005 · Piper PA34220T · Engine Fuel Pump > RT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL. - [SDR AU510002140](https://openairdocs.org/sdr/AU510002140.md): Pump · contaminated · Dec 12, 2005 · Piper PA34220T · Engine Fuel Pump > LT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL. Next page: https://openairdocs.org/model/piper-pa-34-220t/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'PA34220T' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/piper-pa-34-220t/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.