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 DALA2026031901907Skin · bulgedVERTICAL STABILIZER, LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 FOUND BULGE. REPAIRED VERTICAL STABILIZER LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 IAW SRM 55-30-01-2R-1 AND SRM 51-70-10-2R-4, REV 77. (LP 1501546)SDR JR2R20260319098Doubler · corrodedAFT WET AREA TEXAS GUSSET AT FR90A RBL10 IS CORRODED. REPLACEDSDR JR2R20260319100Doubler · corrodedAFT WET AREA TEXAS GUSSET AT FR90 RBL24 IS CORRODED. REPLACEDSDR IPXA2026031953595Light · inoperativeFOUND EMERGENCY LIGHT L1853, L1854, L5735 INOP (REPLACE)SDR IPXA2026031958584Indicator · inoperativeWARNING SYSTEM ARMED LIGHT WOULD NOT ACTIVATE WITH SLIDE ARMED ON L1 DOOR LIGHT ON CREW DEFERRAL REF T3F18E008H0VJ AND AUTH CODE 2872636SDR JR2R20260319099Gusset · corrodedAFT WET AREA GUSSET AT FR89 RBL10 CORRODED. REPLACEDSDR AALA202603196118Power Supply · no testAIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 13WL DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO FASDR IXXA2026031901Shaft · corrodedLEFT WING #4 FLAP SUPPORT 6-6 OUTER PIN IS CORRODED AROUND THE SPLINESSDR 2026FA0000197Compressor · damagedENGINE WAS RETURNED TO OUR REPAIR STATION FOR UNSCHEDULED REPAIR. DURING AN AIRCRAFT PRE-BUY INSPECTION BEING PERFORMED BY AN AIRCRAFT SERVICE CENTER, EVIDENCE OF FOD DAMAGE WAS FOUND IN THE COMPRESSOR SECTION OF THE ENGINE. NOTE: AIRCRAFT SELLER DID NOT REPSDR DALA2026031901893Spring · brokenR1 DOOR HANDLE RELEASE LATCH SPRING BROKEN. R & R 1R HANDLE LATCH SPRING REF B757 AMM 52-11. (8377444)SDR JR2R20260319180Support · damagedI/B SUPPORT ANGLE UNDER FLOOR GUSSET AT FR89 RBL10 HAS ELONGATED HOLE. REPAIRSDR 2026F00039Pulley Bracket · corrodedFOUND 2 AREAS OF CORROSION ON SPOILER PULLEY BRACKET ON LH WING INBD, AFT SPAR. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON LH WING SPOILER PULLEY BRACKET, INSIDE INBD FLAP WELL, AFT SPAR IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYONDSDR ABXA20260319117Warning Message · illuminatedDURING TAXI AND AFTER BOTH ENGINES START, FWD EQUIP VLV ILLUMINATED, DID ABNORMAL, DID NOT CLEAR. A/C RETURNED TO BLOCKS (BTB). AT THE GATE, AFTER APU RUNNING, IT DID CLEAR. MAINTENANCE DEFERRED PER MEL 21-58-1-1, MAINTENANCE PROCEDURES COMPLIED WITH, PLACASDR 2026F00037Stringer · corrodedFOUND SEVERAL AREAS OF CORROSION ON UPPER STRINGER INSIDE PANEL 652DB. MECHANICALLY REMOVED SEVERAL AREAS OF CORROSION ON UPPER STRINGER INSIDE PANEL 652DB, AFT AREA, FWD EDGE OF STRINGER, FROM INBD EDGE CONTINUING APPROXIMATELY 12 INCHES IN LENGTH GOING OUTBDSDR 2026F00036Spar · corrodedFOUND 2 AREAS OF CORROSION ON AFT WING SPAR, FWD SIDE IN RH MLG WHEEL WELL. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED IN RH MLG WHEEL WELL, REAR SPAR WEB NEAR RWS 17.30 IAW SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEESDR 2026F00035Skin · corrodedLEFT AND RIGHT VERTICAL STAB UPPER SKINS HAVE 2 AREAS OF CORROSION JUST BELOW TIP CAP. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB OUTER SKIN JUST BELOW TIP CAP, AFT AREA, 1 BLEND PER SIDE IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLESDR 2026F00038Skin · corrodedFOUND 1 AREA OF CORROSION ON RH WING UPPER SKIN, OUTBOARD OF #7 SPEED BRAKE IN ZONE 642. MECHANICALLY REMOVED 1 AREA OF CORROSION ON RH WING UPPER SKIN, JUST OUTBOARD OF #7 SPEED BRAKE IN ZONE 642 IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYONDSDR JR2R20260319191Shear Tie · corrodedSHEAR TIE AT FR74 IN BETWEEN STR29R - STR28R CORRODED. REPLACEDSDR 2026F00034Skin · corrodedFOUND 9 AREAS OF CORROSION OF RH WING UPPER SKIN, FWD OF AILERON IN ZONE 652. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED ON RH WING UPPER SKIN, FWD OF AILERON IN ZONE 652 ON WING SKIN TRAILING EDGE IAW CESSNA 680 SRM 51-70-02. FOUND 8 CORROSION BLENDS TSDR 2026FA0000196Tube · defectiveFIFTH OF A TOTAL OF FIVE A220 ESCAPE SLIDE ASSEMBLIES THAT WERE RECEIVED DEPLOYED, ALL OF WHICH DISPLAY THE SAME FAILURE POINT. THESE SLIDES DID NOT DEPLOY PROPERLY AS THE SUPPORT TUBE DETACHED FROM THE MAIN TUBE UPON INFLATION. THE FRANGIBLE LINKS REMAINED SDR QR9R2026031900001Display · intermittentRIGHT PFD CYCLES ON AND OFF WHILE AT GROUND IDLE AND FLIGHT. REMOVED AND REPLACED PILOT PFD IAW AMM 31-60-00, 4-1. MOC SUCCESSFULLY COMPLETED.SDR R61A2026031900063Frame · mechanic errorCONTRACT MTX MISS DRILLED HOLE IN FRAME 30 BETWEEN STR 1L AND 1R DURING WIFI MODIFICATION. FREEZE PLUG INSTALLED PER AEROMECH AMN758YX-EC01SDR JR2R20260319192Rib · corrodedAFTER REMOVAL OF LH FLAP PANEL 561ET FOUND INBD RIB CORRODED IN MULTIPLE PLACES.SDR PN1R202603190001Link · crackedDURING INSPECTION FOUND WHITE, YELLOW, AND BLACK MAIN ROTOR TENSION LINKS CRACKED.SDR F3LA202603190383Power Supply · failedDISCREPANCY: REFERENCE LP532313#3 EPSU BATTERY (12WL) FAILED EMERGENCY LIGHT TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK.
CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY (12WL) IAW AMM 33-51-38-0SDR F3LA202603190382Battery Pack · failedEPSU BATTERY (13WL) FAILED EMERGENCY LIGHT TEST. AC WAS NOT GROUNDED. REMOVED AND REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-000/400-002-A. OPS CHECK GOOD. AC OK FOR SERVICE.SDR F3LA202603190381Battery Pack · failedEPSU BATTERY (11WL) FAILED EMERGENCY LIGHT TEST. ACFT WAS NOT GROUNDED. REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000/400-002-A. OPS CHECK GOOD. AC OK FOR SERVICE.SDR SWIA2026031877381Frame · corrodedLOWER FRAME SECTOR AT BS 863, STR 25L - 25R WAS CORRODED OUT OF SCOPE. REPLACED LOWER FRAME SECTOR AT BS 863, STR 20R - 20L IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND DWG SH670-37060, REV F.SDR SWIA2026031877350Bulkhead Web · corrodedRIGHT LOWER WEB AT FS 280 HAS CORROSION. REPAIRED RT LOWER WEB AT FS 280 IAW SRM 53-11-10-201-003-A01 REPAIR B.SDR SWIA2026031876340Skin · corrodedEXTERNAL SKIN IS CORRODED AT SEVERAL LOCATIONS SURROUND SCREW HOLES COMMON TO PANEL 195BB. REPAIRED EXTERNAL SKIN COMMON TO PANEL 195BB IAW REO 601R-53-00-937 REV --. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026031876319Skin · gougedLEFT EXTERNAL SKIN IS GOUGED BETWEEN BS 559+96 - 574, STR 19L - 21L. REPAIRED LT EXTERNAL SKIN IAW REO 601R-53-00-937, REV--. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR AALA202605225667Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 67 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.SDR AALA202605185733Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE ARE L= 0.9540 INCHES W= 0.900 INCHES D=0.010 INCHES. MAINTENANCE REPLACED SHEAR PLATE LOCATED STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM SDR U2RA2026051200025Stringer · crackedFCD 744-53-0025 OPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS WHILE PERFORMING STA L/H 1160 AND STRINGER 10L REPAIR CARRIED OUT PER BOEING 8100-9 DATED MAY 12, 2026 REF BCS 0632095SDR AALA202605083174Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: #1 ENGINE INBOARD FAN COWL FORWARD HINGE FITTING MOUNTED ON THE PYLON IS WORN ALLOWING BUSHING HAS MIGRATED. MAINTENANCE REPLACED THE HINGE FITTING PER AMM 71-13-11.SDR REXA2026050700536Floorbeam · corrodedCORROSION ON CROSSBEAM LH AT FS 280.00 CROSSBEAM LH AT FS 280.00 WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01SDR REXA2026050700535Fitting · corrodedAFTER DISCONNECT FWD HANDRAIL ACTUATOR ROD, CORROSION ON FWD FITTING WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. FWD FITTING AT SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02, FITTING P/N SH670-31905-5 WAS VERIFIED PSDR REXA2026050700509Bracket · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-SDR REXA2026050700508Bracket · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-SDR REXA2026050700507Web · corrodedAFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-SDR REXA2026050500493Floorbeam · corrodedAFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE OVER FS 280.00, IT WAS DETECTED CORROSION ON RH CROSSBEAM AT FS 280.00 AT LBL 9.00. CORROSION ON RH CROSSBEAM AT FS 280.00 AT LBL 9.00. WAS EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-10-06-001-0SDR REXA2026050500492Floor Support · corrodedCORROSION ON INTERNAL STRUCTURE OVER STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE DAMAGE ON STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-SDR REXA2026050500491Strap · corrodedCORROSION IN STRAP MACHINED FS=349.00 AND STGR17 LH (LOWER AFT DOOR L1 CORNER). DUE TO EXCESSIVE DAMAGE IN STRAP MACHINED FS=349.00 AND STGR17 LH (LOWER AFT DOOR L1 CORNER) WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR REXA2026050500474Stringer · corrodedCORROSION ON INTERNAL STRUCTURE OVER STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE DAMAGE ON STGR25RH BTW FS280.00 / FS295.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-SDR AALA202605040066Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SHEAR PLATE STR 23 L BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE OF CORROSION IS L= 2.494 INCH W= 0.539 INCH D= 0.015 INCH. MAINTENANCE REPLACED SHEAR PLATE LOC. AT STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SDR VNAA20260501021Fitting · wornWEAR ON FITTING FROM STA FS 1051.30 , STRINGER 12RH OF AFT BAGGAGE-BAY DOOR, WEAR ON FITTING FROM STA FS 1051.30 , STRINGER 12RH WAS REPAIRED REO 690-53-61-1757 REV - -.SDR VNAA20260501014Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LH WING. CRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LT WING WAS REPAIRED PER REO 690-57-41-240 REV - -.SDR VNAA20260501013Seat Track · corrodedCORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY ,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27 ,BTW STA FS 1000 TO STA 1069. CORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY ,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27 ,BTW STA FS 1000 TO STA SDR 3EJA2026050100826Hose · failedTHE YAW DAMPER AND AUTOPILOT DISCONNECTED. WE HAD A YELLOW IAS MISCOMPARE INDICATION. R&R #2 PITOT HOSE, R&R LH/RH STATIC DRAIN PACKINGSSDR BAGA2026043000008Frame · corrodedHVY CHECK SUBMISSION - REAR BARREL WAS DOUIBLER AT FRAME 75 FOUND CORROSION, TEMP REPAIR CARRIED OUT AS PER BREEZE EA.