Service difficulty reports

1,770,704 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

Query with SQL
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'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026091719501Light · detachedSEAT 03F AISLE GUIDANCE EMERGENCY LIGHT FOUND DETATCHED. LIGHT MODULE REPLACED. FUNCTION TEST OF THE EMERGENCY LIGHTS ACCOMPLISHED. ALL OPS NOW OK. REF AMM DMC-B787-A-33-51-00-00D-320A-A.Sep 16, 2026 · N23983 · Boeing 7879 · Emergency LightingSDR CALA2026091719499Battery Pack · faultedEMERGENCY LIGHTS DOOR 1L GOES OFF LESS THAN 5 SECUNDS. NEEDS TO REPLACE POWER SUPPLY M1208. REPLACED BATTERY PACK (M1208). REPLACEMENT IAW TASK 33-51-07-022-005-001. ITEM OKAY.Sep 16, 2026 · N69063 · Boeing 767424ER · Emergency LightingSDR CALA2026091719498Battery Pack · faultedEMERGENCY TORCH AT DOOR 2 LEFT JUMPSEAT FAILS TEST L2 JUMPSEAT TORCH BATTERY REPLACED REF AMM 25-60-00-210-801-C1, NOW TESTS CORRECTL. PARTS USED: 78-2525-3-0058, QTY :1Sep 16, 2026 · N675UA · Boeing 767322 · Emergency EquipmentSDR CALA2026091719497Light · inoperativeEMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOP, SLAVED IN PROPERLY FUNCTIONING EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01-960-802, OPS CHECK GOOD. REQUIRES EXIT SIGN ASSY. INSTALLED NEW LIGHT ASSEMBLY, IAW AMM 33-51-01-960-802. UNIT OPS CHECKS GOOD, OK FOR SERVSep 16, 2026 · N26226 · Boeing 737824 · Emergency LightingSDR CALA2026091719493Unknown · odorACRID OILY ODOR IN A/C AIR FOLLOWING HYDRAULIC SERVICING W/BOTH PACKS RUNNING OFF APU BLEED. ACP TASK FIM 21-00-830 SMOKE OR FUMES IN CABIN SOURCE UNKNOWN. RAN BOTH ENGINES FOR 5 MINUTES RAN BOTH PACKS AND VERIFIED NO ODOR IN FLT DECK AND WALKED THROUGH CABINSep 16, 2026 · N17431 · Boeing 7379 · Air Distribution SystemSDR CALA2026091719492Unknown · odorWET SOCK ODOR AT T/O THRUST APPLICATION AND CLIMBOUT. NOTHING AT CRUISE OR DESCENT AND THEN AGAIN TAXIING SINGLE ENGINE WITH LT PACK OFF. PERFORMED SMOKE/ODOR CONDITIONAL INSPECTION IAW AMM 05-51-26-800-801-C1. CREW PERFORMED ENGINE RUN AND ALL CHECKED GOOD.Sep 16, 2026 · N69835 · Boeing 737924ER · Air Distribution SystemSDR CALA2026091719491Plenum · no discrepancyBIRD INGESTED INTO LEFT PACK HEAT EXCHANGER AND PLENUM/DIFFUSER ASSEMBLY. INSPECTED SURROUNDING AREA AND FOUND NO DAMAGE. CLEANED AREA AND RAN PACKS FOR AN HOUR AND NO ODOR WAS FOUND INSIDE THE CABIN. WORK PERFORMED PER AMM 12-40-04-100-801.Sep 16, 2026 · N17301 · Boeing 7378 · Cabin Cooling SystemSDR SCNA20260917403Speed Brake · faultedSPEED BRAKE DID NOT DEPLOY ON LANDING. PERFORMED FIM 27-62 804 SPEED BRAKES AUTO DEPLOY IS OPERATIVE. FAULT WAS INTERMEDIATE. ACFT OK FOR SERVICE.Sep 16, 2026 · N8059A · Boeing 73786J · Drag Control SystemSDR ABXA20260916412Smoke Goggles · deterioratedDURING INSP/MTC, FOUND FO SMOKE GOGGLES DETERIORATED. REMOVED F.O. SMOKE GOGGLES. REPLACED WITH SERV. GOGGLES IAW AMM 25-64-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.Sep 16, 2026 · N364CM · Boeing 767338 · Emergency EquipmentSDR ABXA20260916410Engine · fluctuatesDURING TAKEOFF FROM MIA, RT ENG STARTED TO ROLL BACK 2-3 PER N1. AFTER TAKEOFF FLUCUATED BETWEEN 2-3 TO 6-8%. BY 500FT IT WAS BOUNCING BETWEEN 95% & 68%. UPON THRUST REVERSER APPLICATION R ENGINE WAS 8% LOWER. CREW DECLARED EMERGENCY (EDC) AND PERFORMED AIR TUSep 16, 2026 · N745AX · Boeing 767232 · Engine (Turbine/Turboprop)SDR 2026F00209Fuel Line · kinkedFWD FUEL FLOW FLUCTUATING DURING TAKE OFF ROLL, ABORTED TAKE OFF AND RETURNED TO GATE.Sep 16, 2026 · Dhav DHC6300 · Aircraft Fuel Distribution SystemSDR YENA2026091600805Adm · faultedFLT 1196, FLL-FLL. REF ITEM 1 LG 4424380 ACCOMPLISHED STBY ACCURACY CK OF ADM #3 & STBY FOUND ADM#3 455HPA IS 21,540 FT SHOULD BE 20,000FT CAS IS 340 KTS SHOULD BE 320 KTS. ADM#3 OUT OF TOLERANCE.; VERIFIED STBY ADM 3 ACCURACT CHECKS REF AMM 34-13-00. CHCKS OKSep 16, 2026 · N652JB · Airbus A320232 · Airspeed/Mach IndicatorSDR 2A6R2026091675406Frame · crackedDAMAGE WAS DISCOVERED ON THE CABIN OVERHEAD LONGERON (PN: L533M1017282) IN THE FORM OF TWO CRACKS ON EITHER SIDE OF THE CUTOUT. THE CRACK MEASURES APPROXIMATELY 0.50” LONG (AFT) AND 1.00” LONG (FWD)Sep 16, 2026 · N110VU · Urocop EC135T2 · Fuselage Main, FrameSDR QR9R2026091600002Air Data Module · inaccurateRIGHT AIRSPEED INDICATOR INDICATED 30+ KNOTS CONSISTENTLY, ALL OTHER AIRSPEED INDICATORS INDICATED 0. MAINTENANCE ATTEMPTED TO CIRCULATE AIR THROUGH RIGHT PITOT TUBE WITH NO EFFECT. REMOVED AND REPLACED #2 ADU; OPERATIONAL CHECK SUCCESSFULLY COMPLETED.Sep 16, 2026 · Bolkms BK117C2 · Air Data ComputerSDR 2A6R2026091675405Gusset · corrodedEC135 S/N 0605 WAS FOUND TO HAVE CORROSION DAMAGE TO THE BULKHEAD, PN L533M1028221 (APPROX. FS 3150 MM)AND GUSSETS PN: L533M1028227 AND PN: L533M1028228. REPLACEMENTS WERE NOT AVAILABLE WITHIN SCHEDULED RTS AND PARTS WERE FABRICATEDSep 16, 2026 · N110VU · Urocop EC135T2 · Fuselage Main, Attach FittingsSDR 2A6R2026091675404Angle · corrodedACFT WAS FOUND TO HAVE CORROSION DAMAGE TO THE FRAME 2 ANGLE PN L533M1043427 (APPROX. FS 2675 MM). REPLACEMENT WAS NOT AVAILABLE WITHIN SCHEDULED RTS AND PART WAS FABRICATEDSep 16, 2026 · N110VU · Urocop EC135T2 · Fuselage Main, StructureSDR QR9R2026091600001Sensor · intermittentLOW ROTOR RPM LT AND AUDIO INTERMITTENTLY ACTIVE WHILE HOVER TAXIING, ALL OTHER INDICATIONS WERE NORMAL. A TESTFLIGHT EVAL FOUND UPON LANDING ON THE PAD AND REDUCING COLLECTIVE, THE ROTOR RPM AUDIO AND LIGHT ILLUMINATED WITH ROTOR RPM AT 96.8%. WHEN INCREASINGSep 16, 2026 · Bolkms BK117C2 · Main Rotor Indicating SystemSDR MASA2026091600044Battery · inoperativeAFT FA FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY OPS CHECK GOODSep 16, 2026 · N83633 · Emb ERJ170200LL · Emergency EquipmentSDR DALA2026091605177Battery Pack · inoperativeDURING SVC CHECK, FOUND EMERGENCY LIGHTS AT ROWS 28-32 INOP. REPLACED BATTERY PACK PER B737 AMM 33-51. OPS NORMAL. (LP 9443369 - AIRCRAFT WAS GROUNDED)Sep 16, 2026 · N929DZ · Boeing 737932ER · Emergency LightingSDR ABXA20260916411Warning Message · false indicationLEFT ENG FIRE LP 1 STATUS MESSAGE CAME ON AFTER SHUTDOWN. PERFORMED ENGINE FIRE DETECTION SYSTEM OPERATIONAL TEST IAW AMM 26-11-715-001. TEST SUCCESSFUL MESSAGE CLEARED NO FURTHER DEFECTS NOTED. A/C REMAINS NO ETOPS AND RETURNED TO SERVICE.Sep 16, 2026 · N677AZ · Boeing 767300 · Smoke DetectionSDR DALA2026091605174Bottle · low pressureL1 DOOR EMERGENCY DOOR OPERATING CYLINDER IN YELLOW BAND. SERVICED DOOR ASSIST BOTTLE IAW AMM 52-15. (8845769) AIRCRAFT WAS GROUNDED.Sep 16, 2026 · N409DX · Airbus A330941 · Passenger/Crew DoorsSDR JR2R20260916358Floorbeam · corrodedFLOOR BEAM FR84 HAS CORROSION BETWEEN RBL30 - RBL40 IN THE CABIN. REPAIREDSep 16, 2026 · N88327 · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR FDEA202609161354Seat Track · damagedSEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. AMM 53-10-16-06 SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080 MEL: 25-50-02-01-J LOCKED REMOVED AND PLACED IN CLOSET PER WRI 25-50/0129. C/7462504 . REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-40-21. FASep 16, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609161353Longeron · corrodedCENTRE CARGO COMPARTMENT LONGERON 51L, BS 1642, FOUND CORRODED. EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-05-2R. LONGERON REPAIR SECTION BETWEEN BS 1611 TO BS 1711, LONGERON 51L & 2 EACH EXISTING REPAIR SPLICE FITTINGS AT BS 1Sep 16, 2026 · N625FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 2026FA0000734Control Unit · faultedFLAPS FAIL CAUTION MSG. AFTER TAKEOFF RETRACTED FLAPS PER PROFILE, RECEIVED FLAP FAIL MSG. RAN QRH PROCEDURE AND RETURNED TO LAND. FLIGHT CONTROL PAGE SHOWS FLAPS 6 ON LEFT SIDE AND FLAPS 8 ON RIGHT SIDE.Sep 16, 2026 · N719AV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR DALA2026091605158Controller · faultyATB - DUE TO CAB PR EXCESS CAB ALT ECAM WARNING FOLLOWED BY CAB PR SYS 2 FAULT. #2 CPC REPLACED. (LP: 9548118, AIRCRAFT WAS GROUNDED)Sep 16, 2026 · N367NW · Airbus A320212 · Cabin Pressure ControllerSDR JR2R20260916854Stringer · corrodedSTRINGER 29R CORRODED BETWEEN FR 76 TO FR 77. REPAIREDSep 16, 2026 · N89357 · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR QMLA2026091620069Deck Plate · crackedDURING INSPECTIONS THE MGB DECK WAS FOUND TO BE CRACKED FROM THE ELECTRICAL CONNECTOR AFT TO THE FIREWALL AND FORWARD OF THE ELECTRICAL CONNECTOR APPROX. 2 INCHESSep 16, 2026 · N102HN · Urocop EC135P1 · Fuselage Main, StructureSDR SWIA2026091577839Antenna · out of limitsCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10312026COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-314 APPENDIX A AND M-93 ERJ175-53-26-03 EA ERJ411Sep 15, 2026 · N186SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026091577838Antenna · out of limitsCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10312026COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 NO CHANGE TO WEISep 15, 2026 · N186SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026091577837Antenna · out of limitsCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10312026COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 WEIGHT OF REPAISep 15, 2026 · N186SY · Emb ERJ170200LR · Standard Practices/StructuresSDR SWIA2026091577835Antenna · out of limitsCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44 C-CHECK RO 10312026COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 EA ERJ4111-44Sep 15, 2026 · N186SY · Emb ERJ170200LR · Standard Practices/StructuresSDR VNAA202610310011Screw · corrodedCORROSION ON RETEINER THROUGH ACCESS PANEL NBR:598CT INCLUDING HARDWARE (17EAS), ALSO WS= 70 TO WS=48 OF T.E AT LT WING. RETEINER THROUGH ACCESS PANEL NR 598CT WAS CLEANED AND GVI WAS PERFORMED AND CORROSION NOT WAS FOUND IAW SRM 51-41-02-001-001-A01 AND SRMSep 15, 2026 · N616NN · Cndair CL6002D24 · DoorsSDR VNAA202610230078Lug · wornIN REFERENCE TO TRFKE00BN3TP: FABRICATE OVERSIZE BUSHING (7EAS) ON HINGE 1,2,3,4 OF REAR SPART WING RIGHT. NEW OVERSIZE BUSHINGS (7 EAS) WERE FABRICATED PER REO 690-57-51-566 REV: - -Sep 15, 2026 · N555NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR IPXA2026102149392Floor Panel · damagedFLOOR PANEL 147AF HAS A PUNCTURED. FLOOR PANEL 147AF IS FABRICATED I.A.W SREO-16407-REQ001. FLOOR PANEL 147AF IS FABRICATED IAW SREO-16407-REQ001.Sep 15, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026102245620Fan Cowl · corrodedNR 1 ENG.I/B FAN COWL INNER EDGE SEAL FAN COWL HAS SURFACE CORROSIONS AND DEEP WEAR. VERIFIED REMOVAL OF RUB STRIP (INNER SEAL) ON THE #1 ENG.I/B FAN COWL IAW A300 SRM 51-40-21.Sep 15, 2026 · N146UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR SWAA2026102134422Shield · corrodedCORRODED SHIELD PLATE, BTWN BS 767 - 787, STRINGER 25R FAULT WAS RESOLVED ON ANOTHER FAULT, SEE FAULT TTG8Q01ECET5.Sep 15, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102120545Pin · deformedDEFORMED PLATING ON LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG AT RT HORIZONTAL STAB. REPLACED ONLY THE LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG IAW AMM 27-41-11-400-801, & AMM 27-41-11-400-801. FOR INSTALLATION LOWER PIN SEE TTG8R007BQES.Sep 15, 2026 · N8658A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026102174565Strap · corrodedCORRODED STRAP, BTWN BS 787 - 794.3, RBL 20, WL 156.1 IN THE AFT CARGO BAY. REPLACED THE STRAP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A0081, SHT 49, REV A.Sep 15, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101949482Bushing · crackedNR 1 ENG. INBD THRUST REVERSER, UPON THE REMOVAL PHASE, FOUND UPR-CTR-HINGE WITH (HAT) BUSHING CRACKED AT FWD-SIDE. REMOVED AND REPLACED BUSHING FROM NR 1 ENG I/B T/R CTR HINGE (PYLON SIDE) FWD SIDE IN REF SWPM 20-50-03.Sep 15, 2026 · N463UP · Boeing 75724APF · Engine Thrust ReverserSDR SIMA20260915002Sign · inoperativeEMERGENCY LIGHT EXIT IDENTIFIER LIGHT DOES NOT ILLUMINATE INSTALLED NEW EMERGENCY LIGHT POWER UNIT #1 (PN: 3400-22-10, SN: 007358), PER ERJ 175 AMM 33-50-01-400-801-A.Sep 15, 2026 · N217NN · Emb ERJ170200LR · Emergency LightingSDR REXA2026101601946Stringer Splice · corrodedAFTER REMOVAL STRINGER SPLICE, CORROSION WAS FOUND ON STRINGER 21R BTWN BS 469 - 485, REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03-201-001-A02.Sep 15, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR HNAA2026101600998Doubler · damagedHOLES ELONGATED ON 4 COCKPIT PARTITION ATTACHMENT POINT DOUBLERS BTW FR14-15. RAR DOUBLERS IAW SRM 51-40-02Sep 15, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101600994Support Angle · crackedAPU TAILCONE SUPPORT ANGLE CRACKED UDER ACCESS COVER 313AL. RAR ANGLE IAW SRM 53-32-17Sep 15, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026101493635Access Panel · delaminatedDELAMINATED ACCESS PANEL 194CR ON BODY FAIRING. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-2, REPAIR 2.Sep 15, 2026 · N8656B · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2026101311961Floorbeam · crackedCABIN FLOORBEAM AT BS 540, LBL 1 CRACKED. R & R THE FLOORBEAM IAW SRM 51-40-02.Sep 15, 2026 · N8711Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026101366719Floorbeam · crackedCABIN FLOORBEAM AT BS 540, RBL 1 CRACKED. REMOVED FLOORBEAM IAW SRM 51-40-02. INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02.Sep 15, 2026 · N8711Q · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026101234020Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.Sep 15, 2026 · N201LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026092449044Panel · damagedNR 8 SPOILER , FORWARD UPPER FIXED PANEL , PANEL RIVET HEAD SKIN DAMAGE. REMOVE THE ENLARGE HOLE MATERIALS AND CLEAN. BOND THE REPAIR PLIES AND ALUMINUM FOIL WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. I.A.W. B747-8F Sep 15, 2026 · N613UP · Boeing 7478F · SpoilersSDR AALA202610091543Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EXTERNAL SKIN LEADING EDGE SLAT 8 LOCATED 13 INCH FROM INBOARD EDGE AT RT WING L: 1. 640 INCH. PERFORMED PERMANENT REPAIR LEADING EDGE SLAT 8 LOCATED 13 INCH FROM INBOARD EDGE AT RT WING IAW B777-200 SRM 57-43-01-2R PROSep 15, 2026 · N755AN · Boeing 777223 · Leading Edge Devices