Piper PA-28R-200

Service difficulty reports · 203

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duckdb -csv -c "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 = 'PA28R200'
  ORDER BY difficulty_date DESC"

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SDR 2024FA0000374Tube · separatedLEFT MAIN TIRE TUBE 6.00X6 AERO CLASSIC. PIPER PA28R-200 TAXIED FROM AIRCRAFT HANGAR TO HOLD SHORT RWY25 KAKR. AFTER ENGINE RUN-UP LEFT MAIN WAS FLAT. INSPECTION FOUND NO OUTER TIRE DAMAGE OR PUNCTURE MARKS. REMOVED TUBE TO DISCOVER TUBE SEPARATION 2 O'CLOCK OMay 20, 2024 · N8508C · Piper PA28R200 · Tire TubeSDR 2023FA0000561Pulley · unknownIN THE PROCESS OF REPLACING WORN PULLEYS, WE ORDERED PMA REPLACEMENT PULLEYS, PART NUMBER 41001-10 PULLEYS FROM UNIVAIR THROUGH AIRCRAFT SPRUCE. WE WERE SENT U-41001-8 PULLEYS WHICH WERE REPRESENTED AS BEING FAA/PMA REPLACEMENTS. HAVING A -8 SUPERSEDING A -1Sep 22, 2023 · N774LR · Piper PA28R200 · Flight Control SystemSDR 2022FA0000452Spar · corrodedDURING ANNUAL INSPECTION CORROSION WAS NOTED ON THE INBOARD REAR SPAR. CORROSION WAS POPPING OUT AROUND A RIB ATTACHMENT POINT. IT WAS DECIDED TO REMOVE THE SPAR IN ORDER TO ASSESS AND ADVISE THE CUSTOMER ON TREATMENT/REPAIR. WHEN THE SPAR WAS REMOVED THE IAug 17, 2022 · N55176 · Piper PA28R200 · Wing StructureSDR 2022FA0000178None · crackedWHILE PERFORMING A FUSELAGE SKIN REPAIR. THE RH WING WAS REMOVED. AN EDDY CURRENT INSPECTION WAS PERFORMED ON THE WING SPAR ATTACH FITTINGS, UPPER AND LOWER. FOUND A CRACK APPROX. 3 INCHES LONG ON THE UPPER SPAR FACE, ORIGINATING FROM THE OUTBOARD, FORWARD, SEMar 31, 2022 · N872WL · Piper PA28R200 · Wing Main, Frame StructureSDR 2021FA0000396Downlock Arm · brokenON THURSDAY, 12/09/2021, THE MAINTENANCE TEAM FOR THE AIRCRAFT OWNER/OPERATOR BECAME AWARE OF AN UNCOMMANDED NLG EXTENSION OCCURING DURING CRUISE FLIGHT THE NIGHT BEFORE. (THE PILOT PERFORMED A LOW APPROACH FOR KMKC TOWER TO INSPECT AND THEN LANDED WITHOUT INDec 8, 2021 · N44183 · Piper PA28R200 · Landing Gear SystemSDR FE4R2020110917485Mount · damagedWHILE INVESTIGATING EXCESSIVE MOVEMENT BETWEEN THE LEFT WING AND FUSELAGE, BOTH WINGS WERE REMOVED FROM FUSELAGE. THE FORWARD LEFT WING ATTACH POINT BOLT HOLES FOUND ELONGATED TO TWICE THE BOLT DIAMETER. THE ATTACH BOLT WORN TO 75% NOMINAL DIAMETER. THE AFTNov 9, 2020 · N3091T · Piper PA28R200 · Fuselage, Wing Attach FittingsSDR OF1R372KRib · crackedWHILE COMPLYING WITH PIPER SERVICE BULLETIN NR 1161B BY THE INSTALLATION OF PIPER WING RIB MODIFICATION KITS P/N 767-397 AND P/N 767-398, IT WAS FOUND THAT THE NOSE RIBS FORWARD OF THE REPAIR WERE CRACKED. NOSE RIB P/N 62021-00 ON LEFT WING AT STATION 49.25 AOct 14, 2020 · N55804 · Piper PA28R200 · Wing, Rib/BulkheadSDR 2020FA0000264Wire · chafedNOSE LANDING GEAR FAILURE ON ENGINE STARTUP. OWNER TOWED AIRCRAFT FROM HANGAR FOR A VFR FLIGHT. PREFLIGHT INSPECTION PERFORMED WITH NO ISSUES. PRESTART CHECKLIST PERFORMED. OWNER STATED THAT HE STARTED AIRCRAFT, AND WHEN BRINGING THE ENGINE MIXTURE UP FROMMay 28, 2020 · N7KL · Piper PA28R200 · Landing Gear System WiringSDR 2020FA0000152Guide · crackedTHIS MALFUNCTION LEAD TO A NOSE GEAR UP LANDING. THE NLG APPEARS TO HAVE RETRACTED IN AN OFF-CENTER POSITION. INSPECTION POST INCIDENT REVEALED A CRACKED ALIGNMENT GUIDE, WHICH IS FIXED TO THE TOP OF THE NLG STRUT. THIS PART IS RESPONSIBLE FOR ENSURING THE Jun 16, 2018 · N16566 · Piper PA28R200 · Nose/Tail Landing GearSDR 2018FA0000112Ammeter · arcedSTUDENT PILOT AND INSTRUCTOR REPORTED RADIOS QUIT AFTER A LOUD BUZZING SOUND WAS HEARD THROUGH THE HEADSETS FOR A FEW SECONDS. RADIOS STARTED FUNCTIONING NORMALLY A FEW SECONDS AFTER. BETWEEN 15 - 20 MINUTES LATER SMOKE STARTED COMING FROM BEHIND THE PANEL, OMar 20, 2018 · N56353 · Piper PA28R200 · DC Indicating SystemSDR 2018FA0000052Link Assy · crackedWHILE PERFORMING MAINTENANCE TO THE NLG ASSEMBLY, A CRACK WAS FOUND IN P/N 76426-803 BRACE & LINK ASSY APPROXIMATELY .3" FWD OF BOSS FOR THE NLG ACTUATOR ATTACHMENT. AFTER INITIAL DISCOVERY, THE PAINT IN THE AFFECTED AREA WAS REMOVED TO REVEAL THE EXTENT OF TFeb 7, 2018 · N44183 · Piper PA28R200 · Nose/Tail Landing Gear Strut/AxleSDR Q6MR201806110001Rib · crackedWHILE INVESTIGATING THE CAUSE OF A BROKEN PITOT LINE WHERE THE WING MEETS THE FUSELAGE, EXCESSIVE MOVEMENT WAS NOTICED BETWEEN THE WING AND FUSELAGE. WHEN THE WING WAS REMOVED IT WAS DISCOVERED THAT THE FORWARD WING RIB P/N 95639-002 HAD CRACKED COMPLETELY ARONov 16, 2017 · N76SA · Piper PA28R200 · Wing, Rib/BulkheadSDR 8HBR20180412011Spar · crackedCRACKS FOUND IN BOTH MAIN WING SPARS AT MLG SUPPORT BRACE TRUNNION FITTING ATTACK POINT. 1 CRACK PER WING IS APPROXIMATELY 1 INCH RUNNING BETWEEN THE NUTPLATE RIVET HOLES. 1 CRACK PER WING APPROXIMATELY 2" RUNNING LATERALLY ALONG LOWER RADIUS OF SPAR.Oct 25, 2017 · N169JP · Piper PA28R200 · Wing SparSDR 2017FA0000593Switch · inoperativeAIRCRAFT EXPERIENCED RIGHT GEAR COLLAPSE AFTER LANDING. PILOT DID NOT HAVE RIGHT GEAR DOWN INDICATION. INITIATED EMERGENCY OVERRIDE LEVER. STILL NO GREEN DOWN LOCK INDICATION ON RIGHT GEAR. DISCOVERED POSITION SWITCH WAS FAULTY ON ONE SIDE OF SWITCH, SIDE Aug 24, 2017 · N33759 · Piper PA28R200 · Landing Gear Position and WarningSDR 2016FA0000346Indicator · overheatedTHE LT FUEL QUANTITY INDICATOR OVERHEATED DURING CRUISE FLIGHT CAUSING SMOKE IN THE COCKPIT. THE UNIT WAS HOT ENOUGH TO DAMAGE THE ADJACENT FUEL PRESSURE INDICATOR.Jul 28, 2016 · N5472T · Piper PA28R200 · Fuel Quantity IndicatorSDR H5GR2016060300273Rib · crackedSIDE LOAD STRESSES ON MLG ASSEMBLIES THAT ARE TRANSMITTED THROUGH THEIR RETRACT LINK ATTACH FORGING TO THE WIN SPAR AREA ARE CAUSING FATIGUE CRACKS TO FORM IN VERTICAL FLANGES OF WS 49.25 LT AND RT AFT RIBS, AND FORWARD RIBS.May 13, 2016 · N4513T · Piper PA28R200 · Wing SparSDR H5GR2016060300272Rib · crackedSIDE LOAD STRESSES ON MLG ASSEMBLIES THAT ARE TRANSMITTED THROUGH THEIR RETRACT LINK ATTACH FORGING TO THE WING SPAR AREA ARE CAUSING FATIGUE CRACKS TO FORM IN VERTICAL FLANGES OF WS 49.25 LT AND RT AFT RIBS, AND FORWARD RIBS.May 13, 2016 · N4513T · Piper PA28R200 · Wing SparSDR 2016FA0000230Throttle Cable · brokenINSPECTED THROTTLE CABLE AND DISCOVERED THAT THE CABLE IS BROKEN INSIDE THE PROTECTED SHEATHING. THE ORIGINAL MFG PN IS 455-322. THIS THROTTLE CABLE PN IS MC455-322 WHICH IS MFG UNDER A FAA/PMA APPROVED, AFTERMARKET. THIS PART WAS INSTALLED 1/6/2004 AT TOTAL Apr 29, 2016 · N200KR · Piper PA28R200 · Power LeverSDR NKVR2016030901Mount · crackedENGINE WAS REMOVED FOR O/H, THE ENGINE MOUNT WAS INSPECTED AND REJECTED DUE TO CRACKS.Mar 7, 2016 · N56720 · Piper PA28R200 · Engine Mount SectionSDR 5HAS2015102700504Radio · failedCOM 2 RADIO FREQUENCY KNOBS FOR COM/NAV HAD PLAY INSIDE THE RADIO. THE PLAY ALLOWED THE KNOB TO FREE SPIN. THE OPERATOR COULD NOT SELECT PROPER FREQUENCY.Oct 26, 2015 · N1430X · Piper PA28R200 · VHF Communications SystemSDR 2015FA0000517Exhaust Stack · separatedEXHAUST STACK SEPARATED AT THE WELD OF THE ENGINE EXHAUST MANIFOLD MOUNT, NR 1 CYLINDER.Oct 20, 2015 · N9301N · Piper PA28R200 · Engine Collector/Tailpipe/NozzleSDR 2015FA0000453Joint · separatedTHE THROTTLE CONNECTION TO THE CARBURETOR IS CONNECTED BY A JOINT ASSEMBLY, BALL, SPRING TYPE, THE JOINT ASSY SEPARATED FROM THE "BALL" WHICH IN TURN DISCONNECTED THE THROTTLE FROM THE CARBURETOR, CREATING NO CONTROL OF THE THROTTLE ACTION.Sep 15, 2015 · N95HF · Piper PA28R200 · Fuel Control/Reciprocating EnginesSDR 2015FA0000288Stud · brokenCYLINDER BASE STUDS BROKE ON NR 3 CYLINDER. APPEARS TO HAVE STARTED FROM THE BOTTOM RIGHT PART NUMBER 76220-P01 THRU STUD BROKE AT THE CYLINDER BASE AND .500 NUT. THE REST OF THE STUDS BROKE DUE TO INCREASED LOAD FROM THE BROKEN 76220 STUD.Jun 25, 2015 · N4861T · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2015FA0000273Door · unserviceableAIRCRAFT IS OPERATED BY A PART 141 FLIGHT SCHOOL. BOTH STUDENTS & INSTRUCTORS HAD SQUAWKED DIFFICULTY CLOSING & LATCHING DOOR AND/OR WIND NOISE PAST SEAL. MAINTENANCE STAFF CHECKED DOOR & FOUND NO PROBLEMS WITH SEAL OR LATCHES, BUT NOTICED THAT THE DOOR SEEMJun 11, 2015 · N15143 · Piper PA28R200 · Passenger/Crew DoorsSDR 2015FA0000092Cylinder · separatedIN-FLIGHT . ENGINE BEGAN TO RUN VERY ROUGH. ACFT RETURNED TO AIRPORT, ENGINE WAS SHUTDOWN ON RUNWAY. INSPECTION OF ENGINE FOUND NR 1 CYLINDER SEPARATING FROM CASE, CYLINDER HOLD DOWN NUTS SHEARED OFF, ALL EXCEPT AFT LOWER HOLD DOWN NUT, AND STUD WAS BENT.Feb 28, 2015 · N8734E · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2015FA0000038Fitting · looseAIRCRAFT LOST OIL PRESSURE DURING DECENT WHICH CAUSED AN ENGINE FAILURE. THE PROP GOVENOR OIL SUPPLY LINE FITTING WAS LOOSE ALLOWING HIGH PRESSURE OIL TO ESCAPE. THIS CAUSED OIL STARVATION AND CONNECTING ROD FAILURE. THIS CAUSED ENGINE FAILURE AND AN EMERGEJan 28, 2015 · N1147X · Piper PA28R200 · Propeller GovernorSDR GO3S2014FA0000443Attach Fitting · crackedLEFT WING FORWARD SPAR ATTACH FITTING, CRACKED IN HALF. ALLOWED WING TO SHIFT FORWARD AND AFT CAUSED AFT SPAR PLATE, TO LOOSEN AND ELONGATE BOLT IN BOTH FUSELAGE AND WING FITTINGS.Jul 2, 2014 · N44740 · Piper PA28R200 · Wing, Attach FittingsSDR 2014FA0000062Landing Gear · malfunctionedFAILURE OCCURRED JUST AFTER TAKEOFF AT CRUISE ALTITUDE OF 5500 FT, AFTER A NORMAL GEAR RETRACTION ON TAKEOFF, ENROUTE. INITIAL INDICATIONS THAT A PROBLEM OCCURRED WERE THE INDICATOR "GEAR IN TRANSITION" AND RT MAIN "GREEN" WERE LIGHT. THE FLIGHT DESTINATION Nov 17, 2013 · N2696R · Piper PA28R200 · Landing Gear SystemSDR 2013FA0000476Retaining Ring · detachedRETAINING RINGDEPARTED PROPELLER BLADE, NR 1 IN FLIGHT. LANDED, REMOVED PROPELLER AND SENT FOR REPAIR AFTER 4.4 HRS SINCE O/H. BLADE NR 1 REMOVE SCRATCH MARKS SANDED AND REPAIR IAW BOM100, ALL DIMENSION CHECK FOR COMPLIANCE. PAINTED BLADE AND INSTALLED FACTAug 15, 2013 · N1043X · Piper PA28R200 · Propeller Blade SectionSDR 2013FA0000471Wire Harness · detachedDURING PRE-FLIGHT, NOTED MOVEMENT OF AILERON YOKE, FROM LT TO RT, DID NOT FUNCTION FREELY OR CORRECTLY. AT THE NEUTRAL POSITION, ROTATION OF YOKE TO THE RT WAS NOT POSSIBLE AND ACFT DEEMED UNAIRWORTHY AND GROUNDED. ELECTRICAL CONNECTOR TO THE AUTOPILOT COMAug 15, 2013 · N9301N · Piper PA28R200 · Auto Flight System WiringSDR 2013FA0000423Throttle · disconnectedLACK OF THROTTLE CONTROL ON APPROACH TO AIRPORT.Jul 27, 2013 · N5083S · Piper PA28R200 · Power LeverSDR 2012FA0000517Cowl Door · departedDURING DESCENT THROUGH 7,000 FT, TOP COWL ASSEMBLY DEPARTED THE ACFT AND STRUCK THE LEFT WINDSCREEN CAUSING A LARGE HOLE. FURTHER INSPECTION REVEALED THAT THE RIGHT SIDE BOTTOM COWL PLATE ASSY WAS ELONGATED FROM WEAR WITH THE TOP COWL ENGAGEMENT PIN, AND THE Jul 9, 2012 · N4428T · Piper PA28R200 · Engine Cowling SystemSDR 2012FA0000360Fitting · failedPILOT WAS INFORMED BY TOWER THAT THE LT GEAR WAS DOWN. PILOT PERFORMED EMERGENCY GEAR EXTENSION. LT GEAR DID NOT INDICATE A DOWN AND LOCKED POSITION. ACFT LANDED WITHOUT INCIDENT. UPON INSP THE LT GEAR FITTING BROKE AT THE ATTACH POINT OF THE ACTUATOR AND May 23, 2012 · N3066R · Piper PA28R200 · Landing Gear Retraction/Extension SystemSDR 2012FA0000171Bracket · crackedDURING AN ANNUAL INSPECTION, IT WAS NOTED THAT BOTH LT AND RT LOWER SUPPORT AILERON PULLEY BRACKETS WERE CRACKED AT THE FWD INBD RADIUS MOUNT AT EACH WING RIB. A PIECE OF 1 OF THE BRACKETS WAS DETACHED.Mar 28, 2012 · N32613 · Piper PA28R200 · Aileron Control SystemSDR 2012FA0000065O-Ring · tornA DEFECTIVE EMERGENCY LANDING GEAR EXTENSION VALVE. SPECIFICALLY THE INTERNAL O-RING SEALS WERE FOUND TORN AND DAMAGED. THIS CONDITION WAS DETERMINED TO BE CAUSING THE LANDING GEAR EMERGENCY EXTEND LEVER FROM PROPERLY FUNCTIONING, AS WELL, IT CAUSES THE LANDIJan 23, 2012 · N221SD · Piper PA28R200 · Landing Gear Retraction/Extension SystemSDR 2011FA0000687Trunnion · crackedDURING A 100 HR. INSPECTION NOTICED THAT RT MLG WAS LOOSE. FURTHER INVESTIGATION REVEALED CRACK IN RT FORWARD TRUNNION FITTING ASSY. REMOVED 4 BOLTS THAT ATTACH TRUNNION FITTING TO WING AND DISCOVERED THAT FITTING WAS COMPLETLY CRACKED AND IN 2 PIECES INSTEAOct 17, 2011 · N2611R · Piper PA28R200 · Fuselage, Landing Gear Attach FittingsSDR 2011FA0000373Filter Element · splitDURING ROUTINE INSPECTION, AIR FILTER WAS FOUND SPLIT OPEN AT THE SEAM. IT IS A CYLINDRICAL SHAPE AND IT WRAPS AROUND A METAL SCREEN. THE SPLIT AREA COMPRISED SEVERAL SQ INCHES OF UNFILTERED AIRPATH.Jun 9, 2011 · N41AT · Piper PA28R200 · Engine Air Intake SystemSDR 2010FA0000950Air Filter · debondedFOUND AIRFILTER ELEMENT TO HAVE SEPARATED AT GLUED SEAM, LEADING TO INJESTION OF UNFILTERED AIR FOR AN UNKNOWN LENGTH OF TIME.Sep 7, 2010 · N55460 · Piper PA28R200 · Engine Air Intake SystemSDR ZB0R20090002Switch · shortedFOUND ELECTRIC TRIM INOPERATIVE. TROUBLESHOT SYS AND FOUND SHORTED WIRING AT TRIM THUMB SWITCH ON CONTROL WHEEL. REPAIRED WIRING AND OPS CK OK.Nov 23, 2009 · N41331 · Piper PA28R200 · Elevator Tab Control SystemSDR 2009FA0000670Master Switch · failedELECTRICAL POWER FAILED AFTER GEAR EXTENSION. TROUBLESHOT SYS AND FOUND HIGH RESISTANCE IN MASTER SWITCH.Aug 3, 2009 · N55460 · Piper PA28R200 · Electrical Power SystemSDR 2009FA0000361Mount · corrodedENGINE MOUNT SHOWED PIN HOLES ON LOWER OUTER TUBE. REMOVED PAINT AND FOUND CORROSION. REPAIRED 13 TUBES. (K)May 1, 2009 · N5042T · Piper PA28R200 · Engine Mount SectionSDR 2009FA0000052Line · fracturedOIL LINE FRACTURED (1) INCH FROM FITTING IN FRONT OF CRANKCASE CAUSING LOSS OF OIL AND OIL PRESSURE. AS A RESULT OF MALFUNCTION, GOVERNOR HAD TO BE OVERHAULED, PROP FLUSHED AND RESEALED; ENGINE HAD TO BE REMOVED FROM SERVICE. (K)Jan 27, 2009 · N404SE · Piper PA28R200 · Reciprocating Engine Oil SystemSDR 2008FA0000658Spar · crackedLT WING SPAR CRACKED IN THE AREA OF WHERE THE PIVOT BLOCK IS INSTALLED. (K)Sep 1, 2008 · Piper PA28R200 · Wing SparSDR 2008FA0000559Drive Shaft · brokenDISTRIBUTOR (POINT CAM SHAFT BROKE FLUSH WITH UPPER MAG GEAR INNER RACE CAUSING TOTAL MAG FAILURE. PART WAS RETURNED TO OWNER. (K)Aug 10, 2008 · N2952R · Piper PA28R200 · Magneto/DistributorSDR 2007FA0001057Booster · shortedPILOT REPORTED ROUGH ENGINE; IGNITION SYSTEM TROUBLESHOOT FOUND START MAGNETO STARTER BOOSTER INTERNALLY SHORTED, GROUNDING MAGNETO P-LEAD CAUSING MAGNETO FAILURE. REMEDIED BY REMOVING START FROM AIRCRAFT AND MAGNETO OPERATING NORMALLY. (K)Nov 27, 2007 · N1473T · Piper PA28R200 · Magneto/DistributorSDR ZB0R20070006Skin · crackedDURING PROGRESSIVE INSPECTION, DISCOVERED WING WALK ON RT WING SPONGY. INSPECTION REVEALED SUBSTRATE REINFORCEMENT CRACKED IN SEVERAL LOCATIONS. REPLACED WING WALK.Nov 2, 2007 · N15143 · Piper PA28R200 · Wing, Plate/SkinSDR 2007FA0000815Rib · crackedCRACKS FOUND DURING INSPECTION, CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY. WITH NEW MFG PART 78475-004 (AN IMPROVED PART). HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THSep 20, 2007 · N2702R · Piper PA28R200 · Wing, Rib/BulkheadSDR 2007FA0000813Rib · crackedCRACKS FOUND DURING INSPECTION. CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY WITH NEW PART 78475-004 (AN IMPROVED PART). HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THE CRASep 20, 2007 · N2702R · Piper PA28R200 · Wing, Rib/BulkheadSDR ZB0R20070004Cam · wornON CLIMB-OUT, PILOT NOTICED LOW POWER. RETURNED TO AIRPORT. MAINTENANCE INSPECTION REVEALED BELOW MINIMUM VALVE TRAVELS FOR ALL INTAKE VALVES. REMOVED NR 1 CYLINDER. FOUND CAM LOBES SEVERELY WORN AND TAPPETS CORRODED AND WORN IN A CONCAVE MANNER. ENGINE REPASep 15, 2007 · N41331 · Piper PA28R200 · Reciprocating Engine Power SectionSDR 2007FA0000571Bracket · failedTHE PILOT STATED NOSE GEAR COLLAPSED ON LANDING. AFTER AIRCRAFT REMOVED FROM RUNWAY AND PUT ON JACKS. THE NOSE GEAR WOULD NOT EXTEND OR RETRACT. THE GEAR WAS EXTENDED BY EMERGENCY EXTENSION. THE NOSE GEAR ALIGNER BRACKET FELL OFF THE GEAR. AGAIN THE NOSE May 31, 2007 · N56066 · Piper PA28R200 · Nose/Tail Landing Gear
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