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 ASAA2026051266524Web · corrodedFWD CARGO SILL WEB CORRODED BS 440 TO 500. GROUNDED - YES. REMOVED DAMAGE ON SILL WEB BS 440 TO 500 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW SRM 51-40-02-0G & 53-30-15-1A-1.SDR ASAA2026051266522Shield · corrodedAFT CARGO FWD SHIELD CORRODED AT BS 767 - 787. GROUNDED - YES. REMOVED CORROSION SHIELD AT BS 767 - 787 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHIELD IAW SRM 51-40-02-0G-0.SDR ASAA2026051266521Shield · corrodedFWD CARGO AFT SHIELD CORRODED BS 500 - 500A. GROUNDED - YES. REMOVED CORROSION ON SHEILD BS 500 - 500A FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND INSTALLED NEW FWD CARGO AFT SHIELD IAW SRM 51-40-02-0G-0.SDR SWIA2026051276198Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581SDR SWIA2026060876197Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS SDR SWIA2026051276196Skin · 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 (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATIOSDR SWIA2026051276195Skin · 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 (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATIONSDR SWIA2026060876194Skin · 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 (DETERMINED TO BE A MAJOR REPAIR) PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TOSDR AALA202606042786Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 727H AND STA 727I AT S25L. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A.SDR R61A2026060300154Doubler · corrodedRH COCKPIT FLOOR DOUBLER BETWEEN FR 11-12 HAS SMALL AREA OF CORROSION.SDR R61A2026060300153Doubler · corrodedLT COCKPIT FLOOR DOUBLER ON I/B SIDE OF CONTROL YOKE BETWEEN FR 8-9 HAS SMALL AREA OF CORROSION.SDR SWAA2026060105688Strap · not reportedSTA 328 FRAME STRAP FROM STR 22R TO STR 20R DOES NOT MATCH WITH CONFIGURATION TASK 5311-I-17336-NG FIGURE 15. AS PER EA 26-153-01284; THE CONFIGURATION IS ACCEPTABLE.SDR IPXA2026060148785Fuel Sys · out of balance**SUPPLEMENTAL SDR** FUEL IMBALANCE. REMOVED AND REPLACED FWD AND AFT ENGINE FUEL CROSS FEED VALVE BODIES REF. UPS B757 AMM 28-22-02-004-042 AND 28-22-02-404-043. FINALIZED INSTALLATION OF THE FWD & AFT ENGINE FUEL CROSSFEED VALVE ACTUATORS, LEAK AND OPS CHECSDR AALA202605314881Door · out of adjustAIRCRAFT IN BASE MAINTENANCE: HARD TO OPERATE PASSENGER ENTRY DOOR L1 WHEN DOOR IS OPEN. MAINTENANCE PERFORMED ADJUST ON DOOR L1 IAW B777 AMM 52-11-00-820-801 ITEM G.SDR MASA20260529123Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON DOUBLER AT FR 19 LBL 14, CORROSION ON DOUBLER REMOVED BY BLEND-OUT IAW SRM 51-10-03 AND FOUND WITHIN LIMITS IAW SRM 53-10-10 AD06 REV 49.SDR MASA20260529122Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON RH DOUBLER BETWEE FR 13-14 RBL 38. RH DOUBLER BETWEEN FR 13-14 CORROSION REMOVED BY BLEND OUT IAW SRM 51-10-03 AND FOUND WITHIN LIMITS IAW SRM 53-10-10 AD 06 REV 49.SDR MASA20260529121Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT FR 17 RBL 19. FLOORBEAM UPPER FLANGE REPAIRED IAW SRM 53-00-10 REP 03 REV 49.SDR MASA20260529120Angle · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSE, FLOOR STRUCTURE, CORROSION FOUND ON SUPPORT ANGLE BRACKET AT FR 17 RBL 27. SUPPORT BRACKET AT FR 17 RBL 27 REPLACED IAW SRM 51-43-01 REV 46 DEC 03/2021 MR YQG NRC 4502607-2000-0126SDR MASA20260529119Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON LH DOUBLER AT FR 15 LBL 24. LH DOUBLER AT FR 15 LBL24 REPLACED IAW SRM 51-41-02 REV. 45 MAY 28/21
AAR YQG NRG 4502607-2000-0146SDR MASA20260529118Seat Track · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON RH I/B SEAT TRACK BETWEEN FR 12-20. RH I/B SEAT TRACK BETWEEN FR 12-20 REPLACED IAW SRM 51-41-01, 51-43-01, 51-43-02 REV 45.SDR MASA20260529117Seat Track · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON LH I/B SEAT TRACK BETWEEN FR 12-20. LH I/B SEAT TRACK BETWEEN FR 12-20 REPLACED IAW SRM 51-41-01 , 51-43-01, 51-43-02 REV 45 MAY 28/2021 AAR YQG NRC 4502607-2000-0126SDR CALA2026052916628Frame · dentedAFT CARGO COMPARTMENT L/H SIDE, FRAME AT BS 1320 AND S26L HAS 2EA DENTS. ACCOMPLISHED WORK PER UAL EC/RA:5360-02158 & VT MAE EA 757-536 0-13-A4459 REV.SDR CALA2026052916626Frame · dentedFWD CARGO BAY FRAME AT BS 800 BTW S23-24L DENTED. ACCOMPLISHED WORK PER UAL EC/RA: 5330-07769 AND VT MAE EA: 757-5 330-07769 AND VT MAE EA: 757-5330-13-A4467 REV-.SDR IPXA2026052841073Floor Panel · damagedLOADER REPORT LOWER AFT CARGO R/H SIDE NEAR DOORWAY FLOOR PANEL EDGE DAMAGE 1. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP. :CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUT OUT ( L : 3.7", W : 0.9", AT AFT EDGE, 3.5" FROM R/H EDGE ). SDR 2026FA0000462Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEW.SDR 2026FA0000461Stiffener · crackedRIGHT WING FWD LWR INBD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR AALA202605284599Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR AALA202605286649Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR SWAA2026052797685Floor Panel · crackedAFT CARGO FLOOR PANEL 140EF IS CRACKED. REMOVED AND REPLACED AFT CARGO FLOOR PNL 140EF IAW B737-800 AMM 25-52-01-201-801 AND BOEING DWG. # 453A2610 REV. D.SDR AALA202605277430Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 16 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR SWIA2026051276044Anchor Fitting · misinstalledPAX DOOR AFT ANCHOR FITTING ADJUSTMENT BOLT PREVIOUSLY INSTALLED INCORRECTLY. REPOSITIONED PAX DOOR AFT ANCHOR FITTING ADJUSTMENT BOLT IAW AMM 52-11-17-400-804-A01. OPS CHECK GOOD NO DEFECT NOTED. SEE CONTINUATION CARD FOR DETAILSCOMPLIED WITH 51-900-1002-SKSDR IPXA2026052436510Filler · corrodedFAULT - CORROSION - FILLER, AFT CGO DOOR FWD LOWER HOOK SUPPORT STRUCTURE, DOOR STA 175, BEAM NO. 10 (REPLACE) INSTALL NEW RADIUS FILLER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 140T2610 SH 1 REV: BSDR IPXA2026052037295Fairing · debonded- DISBOND - PNL , AFT WING TO BODY FAIRING L/H PNL NO : 195PL. I.A.W AMM 53-66-01-404-003 REV.148 INSTALL PNL NO.195PL.SDR IPXA2026052439460Web · corrodedCORROSION - WEB, L/H WING FIXED T/E REAR SPAR STA WS248 FUEL JETTISON TRANSFER VALVE FIXED POINT. I.A.W AMM 28-31-04-404-004 REV 148 INSTALLED THE ACTUATOR OF THE TRANSFER VALVE.SDR IPXA2026052439830Bushing · wornWORN - BUSHING, NR 2 ENG R/H CORE COWL R/H SIDE PRESSURE RELIFE DOOR UPPER AND LOWER SIDE, TOTAL: 2EA. .INSTALL NEW BUSHING I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50SDR AALA202605261293Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 294.5 AND STA 312 AT BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05-01.SDR AALA202605267008Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 270 AND STA 294.5 AT BL 0. REPLACED INTERCOSTAL PER AARD 51-00-05-01.SDR AALA202605230167Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER CREW DOOR CUT OUT LOWER FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.SDR IPXA2026052044531Floorbeam · corrodedWHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2.SDR IPXA2026051640926Plate · wornRIGHT BODY GEAR W/W INBOARD DOOR, DOOR STOP PLATE WORN 2 EA (REPLACE). INSTALL NEW PLATE I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO: 149U1608 SH 2 REV.-.SDR IPXA2026052237060Depressor · brokenFOUND M/D CGO DOOR AFT CUTOUT DISPRESSOR SEAL BROKEN (2EA). DUE TO TYPO FOUND IN CORRECTIVE ACTION 6, CORRECT REFERENCE SHOULD BE:<BR>INSTALLED THE DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV.148, TORQUED THE SCREW TO 25 IN-LB.SDR DALA2026052203122Oven · odorSHIP 3161 DISC: OVEN -INCLUDES OVEN TIMERS DAMAGED. WHEN ON AND IN USE, THE OVEN HAS A STRONG BURNT PLASTIC SMELL. THE SMELL FILLS UP THE GALLEY. I DO NOW THINK THIS OVEN SHOULD BE USED AGAIN BEFORE IT'S FIXED. C/A: DISCUSSION SMELL WITH F/A AND CAPT. RAN OVENSDR IPXA2026051947707Bracket · crackedLEFT PYLON REAR STRUT FAIRING ASSY, INNER CLIP SUPPORT (1EA) IS CRACKED. INSTALLED NEW BRACKET ON INNER CLIP SUPPORT 1 EA LT PYLON REAR STRUT FAIRING ASSY IAW SRM 51-40-02.SDR IPXA2026052137024Skin · debondedDEBONDED SKIN, RT WING OUTBD FLAP TE WEDGE. (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA ,PER 767 NDT MANUAL PART 1 51-01-01 REV:143 RESULT:NO DEFECT WAS FOUNDSDR IPXA2026052141708Sensor · out of limitsAIR TURN BACK, FWD CARGO DOOR MESSAGE ILLUMINATED IN CLIMB OUT. INSPECTED AND MEASURED SENSORS S214, S215, S893 PER AMM 52-33-00/501. FOUND SENSOR S214 OUT OF LIMITS ADJUSTED ACCORDINGLY PER REFERENCE. PERFORMED FWD CARGO DOOR OPS TEST PER AMM 52-33-00/50SDR SWIA2026051276028Skin · damagedTRANSFER FROM EAML 1887225 : DENT APPROX 4" FWD OF FR05 AND 5" BELOW STGR18L DUE TO TAT DAMAGE FROM BIRD STRIKE. (FLIGHT 5403) COMPLIED WITH ETD2026-170-008432 REV.: / DATED: MAY 13, 2026 FORWARD FUSELAGE SKIN BETWEEN FRAMES 04-05 AND STRINGERS 18L-20L - BIRSDR SWIA2026051276027Tat Probe · deformedSKIN AROUND NR 1 TAT PROBE DEFORMED DUE TO BIRD STRIKE DAMAGE. (FLIGHT 5403) UPON INSPECTION, FOUND THE DEFORMATION ON THE FWD FUSELAGE NR 1 LT TAT INTERNAL MOUNTING PLATE AND NR 1 TAT PROBE ITSELF AND NOT THE FUSELAGE SKIN AROUND THE PLATE & PROBE. PERSDR IPXA2026052036566Strut · crackedCRACKED, UPPER AND LOWER CHORD, RT WING OUTBD FXD LE CAVITY RIB, OSS 531.71. INSTALLED NEW CHORD IAW SRM 51-40-02-0G REV.55 AND DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 1, REV G.SDR IPXA2026052039321Seal · brokenBROKEN - SPRING, NR 2 PYLON AFT FAIRING PANEL NR 446CL. INSTALLED NEW SEAL IAW SRM 51-40-02-0G, REV 55 AND DWG 311T2570, SH 1, REV N.SDR IPXA2026052039547Fairing · crackedCRACKED FILLET FAIRING, NO. 2 ENG R/H T/R TRANSLATING COWL INNER SIDE BETWEEN NO. 5 AND NO. 6 BLOCKER DOOR. REMOVED DAMAGE FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55. INSTALLED NEW FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55 AND IPC 78-32-32 REV.96.