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 CALA2026031714612Web · corrodedCORROSION - AFT WET AREA WEB UPPER SURFACE AT STA 986.5 + 1 RBL 33 WITH CORROSION SPOTS. REF AAR N/R 100007269 AT AFT WET AREA WEB STA 986.5+1 & RBL 33 . REMOVED AND REPLACED WEB IN REF TO B737-700 SRM 51-40-02-0G-0 & DWG 147A5700. REMOVED AND REPLACED WEB INSDR IPXA2026031393618Strap · corrodedAPU INLET SUPPORT STRUCTURE AFT STRAP IS CORRODED ATA 53-80 INSTALLED, 1EA REPAIR STRAP, 2EA REPAIR FILLER, 1EA STRAP AND 1EA EXISTING STRAP AT APU INLET SUPPORT STRUCTURE AFT IAW 757-200PF-SRM 53-80-15-2R-1 REPAIR 1.SDR IPXA2026031499075Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1681 LBL 31 METAL PLATE PANEL SURFACE BULGING SIGN OF CORROSION. ACCOMPLISHED REPAIR PER SRM 53-60-51-2R-6 REPAIR 6.SDR IPXA2026031499159Retainer · corrodedMAIN DECK FLOOR AREA STA 1620-1640 LBL 62 ANGLE BAR SURFACE BULGING AND FASTENER HEAD FULL THROUGH SIGN OF CORROSION. INSTALLED NEW ANGLE BAR FASTENER RETAINER AT MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 IAW SRM 51-40-02-0G-0.SDR IPXA2026031499642Strap · corrodedAFT CARGO COMP LT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1560 AND 1580 IS CORRODED. 83-015. ATA 53-00 QC AUDIT C/WSDR IPXA2026031499696Strap · corrodedAFT CARGO COMP RT SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN STA 1400 AND 1420 HAS CORROSION. 83-018. INSTALLED DECOMPRESSION PANEL LANDING ON AFT CARGO COMP RH SIDE CEILING DECOMPRESSION PANEL STRAP IAW B757-200PF SRM 51-41-02-0G-0.SDR IPXA2026031499056Seat Track · corrodedMAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORROSION. INSTALLED FABRICATED FILLER AT MAIN DECK RBL45 SEAT TRACK P/N 146N5337-1SAAU IAW B757 SRM 51-40-02-0G-0 AND DWG 146N5337.SDR IPXA2026031693647Support Angle · corrodedAPU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION.SDR IPXA2026031693675Support Angle · corrodedAPU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION ATA 53-80 PRODUCTION AUDIT C/WSDR IPXA2026031493686Support Angle · corrodedAPU INLET SUPPORT STRUCTURE FWD SIDE SMALL UPPER SUPPORT ANGLE HAS CORROSION. FABRICATED LOWEER SUPPORT ANGLE APU INLET IAW DWG 148N3141/ SAMPLE, WORK ACCOMPLISHED ON TRAVELER 7003344123. LOWER SUPPORT ANGLE APU INLET WILL BE INSTALLED ON JOB CARD T3F18E008ALSDR IPXA2026031498924Support Angle · corrodedAPU INLET SUPPORT STRUCTURE LOWER SUPPORT ANGLE HAS CORROSION ATA 53-80 UPPER SUPPORT ANGLE APU INLET P/N 148N3152-1 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N.SDR ASAA2026021964814Support Angle · corrodedLAV SUPPORT ANGLE AT STA 917 LBL54 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION-ORIGINAL THICKNESS .150, REMOVED .110, REMAINING IS .040 AND REQUIRES REPLACEMENT DUE TO NO LIMITS GIVEN IN THE SRM. REMOVED AND REPLACED INTERCOSTAL P/N 147A5690U8 PO#1141724.SDR AALA202603117679Strap · missingAIRCRAFT IN BASE MAINTENANCE: OFAR FWD ESCAPE HATCH PULL STRAP MISSING. MAINTENANCE INSTALLED NEW PULL STRAP P/N BACS38A301A13N AT OFAR FWD ESCAPE HATCH IAW B787 AMM DMC B787-A-20-11-00-00A-030A-A.SDR SWAA2026031072038Megaphone · damagedAFT MEGAPHONE HANDLE FASTENER STRIPPED. TASK CARD COMPLETED, REPLACED AFT MEGAPHONE IAW AMM USE OF STANDARD INDUSTRY PRACTICES OPS CHECK GOOD.SDR SWAA2026031072301Light · damagedG1 EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED G1 EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802..SDR SWAA2026031072039Bracket · crackedPANEL 551GB INBD BRACKET CRACKED. THE BRACKET WAS REMOVED FROM PANEL 551GB IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.SDR ASAA2026021964792Transition Panel · corrodedAFT CARGO LH TRANSITION PANEL HAS CORROSION BETWEEN STATIONS 727I TO FWD BULKHEAD. GROUNDED - YES. REMOVED CORROSION BETWEEN STA. 737I - FWD BULKHEAD. ORIGINAL THICKNESS .040 MAT LOSS AT GREATEST POINTS .007, AT LOWEST POINT REMAINING THICKNESS AT .033 AREAS OSDR ASAA2026021964791Transition Panel · corrodedAFT CARGO RH TRANSITION PANEL HAS CORROSION BETWEEN STATIONS 727I TO FWD BULKHEAD. GROUNDED - YES. REMOVED CORROSION BETWEEN 727I - FWD BULKHEAD. ORIG. THICKNESS .040, MAT LOSS AT GREATEST .008, NEW THICKNESS AT LOWEST .032. AREAS OUT OF LIMITS PER B737-900 SRSDR ASAA2026021964790Transition Panel · corrodedAFT CARGO RH TRANSITION PANEL HAS CORROSION BETWEEN STATIONS 727I - 767. GROUNDED - YES. REMOVED CORROSION BETWEEN STA 727I-767 ORIG THICKNESS .040, MAT LOSS AT GREATEST .010, NEW THICKNESS AT LOWEST .030. AREAS OUT OF LIMITS PER B737-900 SRM 53-00-53-1A-1 FABSDR ASAA2026021964787Web · corrodedAFT CARGO DOOR CUTOUT SILL AREA HAS A FEW SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION . ORIGNAL THICKNESS .045 PER B737-900 SRM 53-60-15. MAT LOSS .008 AT LOWEST, NEW THICKNESS .037 AT LOWEST. AREA OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED P#146ASDR ASAA2026021964786Transition Panel · corrodedAFT CARGO LH TRANSITION PANEL HAS CORROSION BETWEEN STATIONS 727I-847. GROUNDED - YES. REMOVED CORROSION BETWEEN STA 727I-847, ORIG THICKNESS .040, MAT LOSS AT GREATEST .013, NEW THICKNESS AT LOWEST POINTS .027 MULTIPLE AREAS OUT OF LIMITS PER B737-900 SRM 53-SDR ASAA2026021964785Transition Panel · corrodedFWD CARGO LH TRANSITION PANEL HAS A PUNCTURE BETWEEN STA. 500-500A. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040. MAT LOSS 100% AT PUNCTURE FABBED AND INSTALLED REPAIR PER B737-900 SRM 53-00-53-2R-5.SDR ASAA2026021964784Web · corrodedRH WEB STA 987-1006 RBL 26-46 HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-900 SRM 51-10-02-0G-0. ORIGINAL THICKNESS .080 IAW BAC DWG #147A5116 REV- REMAINING THICKNESS IS .050 TOOL #T8224B DUE 03DEC26. .030 MAT LOSS. REMOVED AND REPLACEDSDR SWAA2026030973572Rib · wornLEFT WING UPPER FIXED TRAILING EDGE SUPPORT BEAM NEAR DEFLECTION CONTROL RIB IS WORN AT FASTENER HOLES. WEAR OUT OF LIMITS IAW SRM 57-51-02-1A-1. CUT & REMOVED THE DAMAGE IAW SRM 57-51-02-2R-1. . LOCATED AND DRILLED DOUBLER AND NEW I/B SERRATED PLATE IAW SRMSDR SWAA2026030977904Doubler · wornLEFT WING UPPER FIXED TRAILING EDGE SUPPORT BEAM, NEAR DEFLECTION CONTROL RIB, WORN AT FASTENER HOLES. WEAR OUT OF LIMITS IAW SRM 57-51-02-1A-1. CUT & REMOVED THE DAMAGE IAW SRM 57-51-02-2R-1.SDR IPXA2026022399164Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION.SDR IPXA2026022899492Floor Support · corrodedAFT CARGO COMP FLOOR SUPPORT AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. 83-010. VERIFIED REMOVAL OF FLOOR SUPPORT ON STEP 7.SDR REXA2026030900222Door Sill · corrodedCORROSION ON LOWER SILL ALSO ON SETTLEMENT AREA OF CARGO FLOOR 281JLF AT AFT BAGGAGE BAY DOOR CUT-OUT SURROUND STRUCTURE. DUE TO EXCESSIVE DAMAGE LOWER SILL OF AFT CARGO MUST BE REPLACE PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-1SDR REXA2026030900221Stringer · corrodedCORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-SDR REXA2026030900216Hinge · excess playFREE PLAY ON HINGE & WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT HINGE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS REPLACED AND WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS BLENDED OUT AND EVALUATESDR REXA2026030900214Attach Angle · crackedCRACK ON ATTACHMENT ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) WAS REPLACED PER CRJ 9SDR REXA2026030900206Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR IPXA2026022399056Seat Track · corrodedMAIN DECK FLOOR AREA STA 1661-1681 RBL 45 SEAT TRACK SPLICE PLATE HAS CORRODED. 7VERIFIED STEP 6 HAS BEEN ACCOMPLISHED.SDR AALA202603064157Garlock Seal · leakingAIRCRAFT WAS GROUNDED: APU OFF DESCENDING THROUGH 10000, FLIGHT CREW NOTED A DIRTY SOCK SMELL IN FLIGHT DECK. **ORIGINAL REPORT WAS AALA202602236304 SUBMITTED 2/23/2026 BY TUL** MAINTENANCE FOUND EVIDENCE OF COKING IN THE APU GEARBOX VENT TUBE AND REPLACED IT SDR AALA202603066304Tube · cokedAIRCRAFT WAS GROUNDED: APU OFF DESCENDING THROUGH 10000, FLIGHT CREW NOTED A DIRTY SOCK SMELL IN FLIGHT DECK. **SUPPLEMENTAL REPORT FOR AALA202602236304 SUBMITTED 2/23/2026 BY TUL: MAINTENANCE FOUND EVIDENCE OF COKING IN THE APU GEARBOX VENT TUBE AND REPLACED SDR IPXA2026022687694Spring · brokenBROKEN SPRING, NR 2 PYLON AFT FAIRING PANEL 446CL. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 94, AND DWG 311T2570, SHT 16, REV -.SDR AALA202603055393Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON AFT WET AREA FLOORBOARDS INSTALLED NEW FLOOR PANEL P/N: 151W8718-18 IAW AMM 53-01-01. SEE NR 1676SDR HNAA2026030400194Shear Tie · cracked00738 CRACK FOUND IN SHEAR TIE AT FRAME 24 BETWEEN STR 15L AND 16L. REMOVED AND INSTALLED NEW SHEAR TIE AT FR 24 BETWEEN STR 15L AND 16L. REF EMB 145 SRM 51-40-02-PR,SDR J7SA2026030200475Vhf Comm · smokeAIR TURN BACK DUE TO SMOKE IN CABIN DURING CLIMB BETWEEN 12000 AND 15000 FT. CREW NOTED THAT THE ODOR SEEMED TO BE COMING FROM BEHIND THE LT CIRCUIT BREAKER PANEL. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED THE NR 1 VHF 4000 IAW AMM 23-11-01. PERFORMEDSDR AALA202603027499Oil System · leakingAIRCRAFT WAS GROUNDED: AT FL340 GOT ECAM ADV, ENG 1 OIL QUANTITY. STARTED FLIGHT WITH 18 QT. TOOK SEVERAL MINUTES FOR OIL QUANTITY TO GO TO ZERO. ALL OTHER ENGINE PARAMETERS NORMAL. SEVERAL MINUTES AFTER QUANTITY AT ZERO, OIL PRESSURE DECREASED SLOWLY TO ZERO.SDR IPXA2026022687742Door · gougedGOUGE - PLATE, NO.2 ENG R/H T/R COWL LOWER BLOWOUT DOOR L/E. (REPLACE). INSTALL BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINEERING IPC 78-32-22 REV.94.SDR AALA202602275866Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE BETWEEN BS 500A AND 500B AT S26R. REPLACED BAFFLE PER AARD 51-00-05-1.SDR AALA202602272243Floor Support · brokenAIRCRAFT IN BASE MAINTENANCE: BROKEN FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 634 AND LBL 50. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.SDR SWAA2026022671958Battery Pack · inoperativePASSENGER OVHD EMERGENCY LIGHT INOPERATIVE AT 25DEF. REMOVED AND REPLACED M1672 BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-805-NG.SDR IPXA2026022687780Bracket · crackedFAULT - CRACK - BRACKET, NO.1 PYLON HYDRAULIC RESERVOIR VENT TUBE AT CENTER AREA. (REPLACE). FABRICATE BRACKET (P/N:313T2380-836) PER BOEING DWG NO.:313T2380 SH 105 REV."-";PL 313T2380-836 REV."A" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 14 RESDR FKEA202602260001Brake · draggingHIGH SPEED REJECTED TAKE OFF IN APF, LOSS OF DIRECTIONAL CONTROL AS AIRCRAFT ACCELERATED TO V1 DUE TO A DRAGGING LEFT MAIN MOUNT. DRAG DUE TO EITHER A HUB/BEARING FAILURE OR BRAKING SYSTEM FAILURE ALLOWING LEFT BRAKE TO STICK. THE BRAKE WAS REMOVED AND FOUNDSDR CALA2026022614113Valve · faultedMLG NOT UPLOCKED ECAM PROC DID NOT RESOLVE ISSUE. GEAR REPORTED TO HAVE RETRACTED, BUT DID NOT STAY UPLOCKED TO ALLOW GEAR DOORS TO CLOSE. PERFORMED FIM 32-31-00-810-836-A. MLG DOORS OPENED CORRECTLY BUT GEAR DID NOT PERFORM CORRECTLY. PERFORMED CHECK OF THESDR CALA2026022614104Slide · misinstalledCABIN L 2 DOOR SLIDE GIRT BAR AREA FOUND GIRT MATERIAL CLOTH PACKAGE NOT CORRECT. SLIDE CHANGED AT L2 DR.SDR 2026FA0000144Hinge · detachedAFTER LANDING AND SECURING THE AIRCRAFT, IT WAS OBSERVED THAT THE LEFT AILERON WAS HANGING DOWNWARD FROM THE WING AND WAS NO LONGER PROPERLY ATTACHED ALONG ITS NORMAL HINGE LINESDR YENA2026022500236Terminal · detachedFLT #1014 CUN-MCO. "RED EMERGENCY EXT LIGHT AT SEAT 9C INOPERATIVE. FOUND TERMINAL END DISCONNECTED FROM THE SOCKET, RECONNECTED THE TERMINAL END AND INSTALLED THE HARNESS PER AMM 31-50-00 OPS CHECK GOOD.