Service difficulty reports
1,771,708 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2026050476104Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGESDR SWIA2026050476103Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGESDR SWIA2026050476102Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKINSDR IPXA2026052807109Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 2360 AT S-5R. ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0025 REV.1 AND EGAT EI NO.F2026A53M-1009 REV.4.SDR IPXA2026052807087Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2360 AT S-5L. ACCOMPLISH THE REPAIR I.A.W EGAT EI NO.F2026A53M-1008 REV. 4 AND UPS EO-97410-REQ0021 REV.1.SDR IPXA2026052807089Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2360 AT S-2R. ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0024 REV.1 AND EGAT EI NO.F2026A53M-1010 REV.2.SDR SWIA2026050476100Skin · damagedCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). SEE CSDR SWIA2026050476099Skin · damagedCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44SDR SWIA2026050476098Skin · damagedCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). SEE CSDR SWIA2026050476097Skin · damagedCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-4SDR IPXA2026052607044Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2360 AT S-1L. ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0020 REV.1 AND EGAT EI NO.F2026A53M-1007 REV.2.SDR IPXA2026052207475Bracket · crackedCRACK - BRACKET, L/H WING INBD L/E CAVITY AIR DUCT SUPPORT , ILES 1030 (REPLACE). .INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO.116U0014 SH19 REV.-. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR AALA202605226404Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 ENTRY WAY LOWER SILL INNER CHORD (CREASE ANGLE) AT STA 302 AND LBL 56.. REPLACED CHORD PER AARD 10-00-05-1.SDR AALA202605227355Track · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO RIGHT HAND FRONT SPAR SLIDING SEAL TRACK AT STA 1121 AND RBL 11. REPLACED TRACK PER SRM 51-40-02.SDR IPXA2026051115829Angle · crackedCREW DOOR AFT INTERNAL SEAL, L SHAPE ANGLE IS CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-21-001.SDR IPXA2026052015262Cascade · corrodedNR 2 ENG INBD T/R UPPER CASCADE HAD SURFACE CORROSION. CASCADE VANE REMOVED AND INSTALLED ON FAULT T3F18E008U9YH LINE 1162.SDR IPXA2026051916239Bracket · crackedR/H WING FLAP MOVABLE FAIRING 635BB, AFT O/B ATTACH MOUNT BRACKET IS CRACKED. DOT 21-02. REMOVED AND REPLACED BRACKET P/N A5796554820300 BTCH:0004485243 AT R/H WING FLAP MOVABLE FAIRING 635BB AFT O/B IAW A300-600 SRM 51-40-21SDR IPXA2026051616378Panel · crackedPYLON #1, PANEL 413BL HAS CRACKS 2(EA) AT THE GRILL DOT 31-021, PANEL STORED IN THE PANEL RACK AREA. ACCOMPLISHED WELD REPAIR ON PANEL 413BL, #1 PYLON, LOUVRE IAW A300-600 SRM 54-52-51-201 AND TRAVELER #: T26/1805003.SDR HNAA2026052000422Skin · damagedCOCKPIT UNDERFLOOR HATCH 123BL HAS TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL. REPAIRED COCKPIT UNDERFLOOR HATCH 123BL TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL IAW PIEDMONT EO1-52-26-0223 AND ETD2026-145-007987.SDR IPXA2026051905095Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-12R (LEVEL1) (REPAIR). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0014 REV.1 AND EGAT EI NO.F2026A53M-1050 REV.0 AND EGAT WORK SHEET NO.60349 AND SRM 53-60-03-2R-4 REV.48.SDR IPXA2026051906531Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-9R (LEVEL1) (REPAIR). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0013 REV.1 AND EGAT EI NO.F2026A53M-1049 REV.0 AND EGAT WORK SHEET NO.60348 AND SRM 53-60-03-2R-4 REV.48. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2026051904875Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-11R (LEVEL1) (REPAIR). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0014 REV.1 AND EGAT EI NO.F2026A53M-1050 REV.0 AND EGAT WORK SHEET NO.60349 AND SRM 53-60-03-2R-4 REV.48. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2026051605100Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-19L (LEVEL1) (REPAIR). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0014 REV.1 AND EGAT EI NO.F2026A53M-1050 REV.0 AND EGAT WORK SHEET NO.60349 AND SRM 53-60-03-2R-4 REV.48. REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR IPXA2026051016492Bracket · crackedAFT CARGO FWD BULKHEAD, SIDEWALL AT FR 54 LH UPPER CORNER BRACKET CRACKED. INSTALLED NEW BRACKET (1EA) AT AFT CARGO- FR 54 I.A.W. A300-600 SRM 51-40-21.SDR IPXA2026051016514Bracket · crackedFAULT-STR-Z100, AFT CARGO FWD BULKHEAD, SIDEWALL AT FR 54 RH UPPER CORNER BRACKET CRACKED DOT 31-041. INSTALLED NEW BRACKET (1EA) AT AFT CARGO- FR 54 I.A.W. A300-600 SRM 51-40-21. REVIEWEDSDR SWAA2026051295145Lamp · inoperativeEMERGENCY EXIT LIGHT L1359 IS INOPERATIVE. RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHT L1359 IAW AMM 33-51-01-960-801.SDR SWAA2026051295146Power Supply · inoperativeEMERGENCY EXIT LIGHTS L1188 AND L1189 ARE INOPERATIVE. REMOVED AND REPLACED M1695 POWER SUPPLY AND PERFORMED GOOD FUNCTIONAL CHECK ON LIGHTS L1188 AND L1189 IAW AMM 33-51-06-960-806.;SDR SWAA2026051295147Power Supply · inoperativeEMERGENCY EXIT LIGHTS L1207 AND L1208 ARE INOPERATIVE. REMOVED AND REPLACED M1694 POWER SUPPLY AND PERFORMED GOOD FUNCTIONAL CHECK ON LIGHTS L1207 & L1208 IAW AMM 33-51-06-960-806.SDR SWAA2026051295284Bulb · inoperativeLEFT ESCAPE SLIDE AFT L732 INOPERATIVE. REPLACED LIGHT BULB L732 ON LEFT ESCAPE SLIDE AFT AND PERFORMED GOOD FUNCTIONAL TEST IAW 33-51-04-960-801.SDR IPXA2026051114526Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 5. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114600Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 12. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114640Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 RBL 23. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114729Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 5. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114784Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 12. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114767Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 23. VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026051114818Floor Support · corrodedMAIN DECK CARGO COMPART. FLOOR STRUCT. SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION, APPROX AT BS 1715 LBL 36, VERIFIED STEP 8. OK TO INSTALL ITEM LISTED IN STEP 8 IS GRANTED.SDR IPXA2026050608602Strap · corrodedAPU INLET DOOR SURROUND STRUCTURE FWD STRAP I/B END HAS CORROSION .SDR VNAA2026051117801Pcu · faultedIB SPOILERONS / IB FLT SPLRS CAUTION IN FLIGHT. REMOVED & REPLACED LH IB MULTI-FUNCTION SPOILER PCU(MPE33) IAW AMM 27-62-01-000/400-801-A02, PERFORMED BLEEDING OF HYD SYSTEM #1 IAW AMM 29-10-00-870-801-A01, LEAK TEST OF THE MULTI-FUNCTION SPOILER DONE IAWSDR DALA2026050902929Compressor · stalledON DESCENT TO ATL AROUND FL250 ENG1 BEGAN TO COMPRESSOR STALL. ECAM STALL WARNING CAME AND WENT SEVERAL TIMES. PULLED ENG1 LVR TO IDLE PER ECAM PROCEDURE. ENGINE REMAINED RUNNING INFLIGHT AND WAS ABLE TO OPERATE UP TO 40% WITHOUT STALLING. ON LANDING ROLLOUT ESDR R61A2026050400120Power Supply · no testEMERGENCY LIGHT POWER UNIT BATTERY DID NOT PASS THE FUNCTION TEST. FWD CABIN EXIT LOCATOR SIGNS TURNED OFF BEFORE 15 MINUTES ELAPSED. R&R FWD EMERGENCY LIGHT POWER UNIT 1.SDR 2DYA202605080016Oil System · leakingLEFT ENGINE INDICATING LOW OIL QUANTITY IN FLIGHT. 20 QUARTS AT TAKEOFF, 3 QUARTS AT LANDING. DIVERSION WAS REQUIRED REQUIRED FOR INDICATION. A/C DIVERTED TO TOL.4-MAY-26 LP 43645.SDR AALA202605084499Angle · brokenAIRCRAFT IN BASE MAINTENANCE: FUSELAGE LEFT HAND ECS BAY AFT END DIAGONAL ANGLE IS BROKEN AT FORWARD SIDE OF THE LEFT HAND VAPOR BARRIER. REMOVED AND REPLACED DIAGONAL ANGLE. PER SRM 51-40-02-0G.SDR DXTA2026050807948Electronic Unit · failedRETRACTED FLAPS AFTER TAKEOFF, FLAP FAIL CAS AND YELLOW FLAP 0 MFD FLAP INDICATION. CONDUCTED FLAP FAIL APPROACH QRC. FLAPS REMAINED STUCK AT 0. REMOVED FCE 2. REMOVED FCE 1, AND INSTALLED IN ORIGINAL FCE 2 POSITION. INSTALLED REPAIRED FCE 1, IAW AMM 27-03-0SDR DALA2026050802912Skin · dentedAFTER COMPLETING HFEC INSPECTION REF LOG 8624949. IT WAS DETERMINED THAT THE DENT ON NR 2 RT SLAT WAS NOT EVALUATED. EVALUATED DENT ON NR 2 RT SLAT REF A319 SRM 57-41-11-283-005, FIGURE 001 SHEET 3 FOUND TO BE OUT OF LIMITS WITH DEPT GREATER THAT 0.2 INCHES. SDR SWAA2026050795268Handle · brokenFO HANDLE ABOVE WINDSHIELD BROKEN. REMOVED AND REPLACED PILOT SEAT HANDLE PER SIP.SDR 2026FA0000334Bellows · faultedPILOT NOTICED AFTER DESCENT TO FLIGHT LEVEL 1500 FEET, LEVELING OFF AND ADDING POWER, TORQUE INDICATION DROPPED 200 AND RECOVERED ON ITS OWN WITH NO INPUT TO THE POWER LEVER. AFTER DISCUSSION WITH PRATT AND WHITTNEY, IT WAS DETERMINED THAT THE FUEL CONTROL DESDR 2026FA0000333Tire · failedFLIGHT OB 264 DIVERTED FLIGHT LPB/SRE TO SLCB DUE TO STRONG VIBRATION AT NOSE LIANDING GEAR DURING TAKEOFF. SUBSEQUENT COMMUNICATION WITH TOWER ATTEST TIRE FRAGMENTS ON THE RUNWAY. HAS BEEN INSPECTED AIRCRAFT FOR TIRE BURST DAMAGE AND WAS REPLACED NLG TIRES #SDR IPXA2026050716996Skin · damaged*** MAJOR REPAIR *** TO LINK AND ACCOMPLISH EO-97088-REQ1 (N122UP: FUSELAGE SKIN LEFT AND RIGHT SIDE EXTERNAL DOUBLER REPAIRS AT FR7 AND FR8) REVIEWEDSDR CALA2026050716048Relay · faultyGROUND HORN ALARM KEEPS GOING OFF WITH A/C POWER OFF AND GROUND POWER DISCONNECTED REFERENCE WDM 24-33-21-1, REMOVED RELAY K24019 IN P310 PANEL AND HORN STOPPED. RELAY IS DAMAGED AND SMELLS BURNT. OLD RELAY IS IN COCKPIT AND P310 PANEL IS OPENED. AIRCRAFTSDR UIEA2026050500295Signal Cond Unit · faultedHIGH SPEED RTO AT 140KTS INDICATED DUE TO ENG NR 1 NOT MAKING T/O THRUST. R & R N1 FAN SHAFT SPEED SENSOR & ENG IDLE RUN CHKD OK IAW AMM 77-12-01/401, AMM 71-00-00/501 & IPC 77-12-01-01. NEED THE ENG HIGH PWR CHK. R & R AVM SIGNAL CONDITIONER THEN OPS CHKD O