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.
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 CALA2026082518906Light · inoperativeAILSE EMERGENCY LIGHT AT 29ABC OUT. R & R EMERGANCY FLOOR POROXIMITY LIGHT AT ROW 29ABC IAW AMM TASK 33-51-11-960-802.SDR IPXA2026082507726Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)SDR IPXA2026082508532Slide · unwanted deploySLIDE DEPLOYED L1 DOOR SLIDE PLACED ON MEL 52-11-01-2-3, PLACARD INSTALLED, DI LOG UPDATED. DMP COMPLIED WIITH. (SLIDE REMOVED). VERIFIED SAFETY PIN REMOVED AND PRESSURE ON SLIDE IAW GMM 04-02.SDR JR2R20260825350Carriage · gougedRH MAIN FLAP CARRIAGE NR 2 HAS PITTING IN BOLT HOLE FOR O/B UPPER RUB PAD. REPAIRSDR JR2R20260825346Carriage · gougedLH MAIN FLAP CARRIAGE #2 HAS PITTING IN BOLT HOLE FOR I/B LOWER RUB PAD. REPAIRSDR DALA2026082504819Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS INOP IN MID CABIN. REMOVED AND REPLACED BATTERY PACK M1695 PER B737 AMM 33-51. EMERGENCY LIGHTS OPS CHECK GOOD. (8771431) AIRCRAFT WAS GROUNDEDSDR IXXA20260825001Support · damagedDURING INSTALLATION OF PANEL 661KB, FOUND A HOLE PARTIALLY DRILLED INTO THE RIGHT WING TRAILING EDGE HINGE POINT STRUCTURE. REPAIRED IAW AMES REA 47739REA12 WITH 8110-3 APPROVAL. REFERENCE AMES WO N761CX-57 NR 195166-0600-0140.SDR DALA2026082504815Shear Web · crackedFWD CARGO SHEAR WEB CRACKED AT STGR 44LH FR20-FR21. REPAIRED PER ERA 636283-14 REV ORIGINAL. (1775386) AIRCRAFT WAS GROUNDED.SDR DALA2026082504814Seat Track · corrodedCABIN SEAT TRACK FOUND CORROSION AT FR73-FR77 Y1137.1. REPAIRED PER ERA 635985-14 REV ORIGINAL. (1775376) AIRCRAFT WAS GROUNDED.SDR DALA2026082504813Seat Track · corrodedCABIN SEAT TRACK FOUND CORROSION AT FR73-FR77 - Y1137.1. REPAIRED PER ERA 635984-14 PRI REV 0. (1775359) AIRCRAFT WAS GROUNDED.SDR FDEA202608251224Skin Panel · crackedLH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS REMOVED, FABRICATED AND INSTALLED IAW B757 SRM 51-40-02-0G AND B-DWG 114N4077 REV DSDR DALA2026082504811Unknown · odorENTERING THE AIRPLANE, SEVERE CIGAR LOUNGE SMOKE LOUNGE ODOR THAT GETS WORSE TOWARDS THE BACK OF CABIN. NOT A BURNING OR CHEMICAL ODOR. REPLACED O-ZONE CONVERTER GEN AS PRECAUTION. AIRCRAFT OKAY FOR SERVICE. (LP 8441274 - AIRCRAFT WAS GROUNDED)SDR K11A2026082500385Computer · failedREJECTED TAKEOFF AFTER THROTTLES WERE STABILIZED + TOGO BUTTON PUSHED AIRCRAFT BEGAN TO YAW RIGHT UNCONTROLLABLE, TILLER HAD NO EFFECT IN THE CORRECTION. PERFORMED PULLED AND SECURED THE AUTOTHROTTLE CIRCUIT BREAKERS ON THE P18-1 PANEL. CAT: C. PLACARDS INSTASDR 2026F00183Idg · faultedAFTER ENGINE 1 START, GEN 1 FAULT ON ECAM RESET UNSUCCESFULSDR SIMA20260825001Unknown · odorDETECTED AN ELECTRICAL BURNING SMELL IN THE FLTDECK DURING APPROACH, FAS WERE ABLE TO CONFIRM ELECTRICAL BURNING SMELL IN THE CABIN. NO EICAS MSG OR ABNORMAL SYSTEM ALARMS ACTIVATED, ALL BREAKERS IN. C/W ITEMS 1 THROUGH 8 OF TRIAD WORK SCOPE WAS UNABLE TO DUSDR SIMA20260825002Unknown · odorBURNING SMELL EXPERIENCED INFLIGHT. BOTH COCKPIT AND CABIN EXPERIENCED THE SMELL. CABIN SAW SLIGHT HAZE DURING ARRIVAL/APPROACH. ALL SYSTEMS LOOKED NORMAL AND NO ALARMS OR ABNORMAL INDICATIONS. (EMERGENCY DECLARED) C/W ITEMS 1 THROUGH 8 OF WORK SCOPE, UNABLE SDR 2026F00184Fitting · corrodedREMOVED NOSE LANDING GEAR ACTUATOR FITTING ASSEMBLY DUE TO LEVEL 2 CORROSION. INSTALLED NEW FITTING PER SR-680A-ATA53-33739 REV. A, STANDARD REPAIR - NLG ACTUATOR FITTING REPLACEMENT, DATED 28 NOV 2023. SUPPORTED BY 8100-9 FORM DATED 29 NOV 2023.SDR ABXA20260825374Fire Loop · fault messageR ENG FIRELOOP 2 STATUS MSG. DEFERRED PER MEL ABX-26-11-1-1. A/C RETURNED TO SERVICE.SDR 2026FA0000665Fuel Sys · abnormalTHE AIRCRAFT HAS BEEN MODIFIED WITH STC ST03382NY, WHICH CONVERTS A DRY BAY IN EACH WING TO AN EXTENDED RANGE AUXILIARY FUEL TANK. STANDING FUEL WAS NOTED IN THE DRY BAY ADJACENT TO THE BAY MODIFIED INTO AN AUX FUEL TANK. THE FUEL WAS TRAPPED BY STRINGERS AND SDR 2A6R2026082575402Frame · crackedTWO CRACKS APPROXIMATELY 6MM IN LENGTH EACH WERE DISCOVERED ON THE LH UPPER FRAME 5 MEDICAL INTERIOR MOUNT LOCATION. BOTH CRACKS PROPAGATED FROM THE SAME RIVET HOLE AT APPROXIMATELY FS: 4780, WL: 2400, AND BL: -710. THE CRACKS WERE LESS THAN 1.5” IN LENGTH ANSDR VNAA202610280027Bushing · wornIN REFERENCE TO TRFKE00BN3TF: FABRICATE OVERSIZE BUSHING (3EAS) ON HINGE FITTINGS R1, R2 AND R6 AT AILERON RT. OVERSIZE BUSHING (3EAS) ON HINGE FITTINGS R1, R2 AND R6 AT AILERON RH WERE FABRICATED PER REO 670-57-61-237 REV -.SDR VNAA202610280023Bearing · corrodedAFTER REMOVAL BUSHINGS AND BEARINGS ON AILERON RH IN REF TRFKEOOBN3TF CORROSION WAS FOUND ON CENTER HIGUE FITTING R5 AND R6. CENTER HINGE FITTING R6 WAS CLEANED PER SRM 51-26-00-001-001-A01 THEN INSPECTIONED PER NDT MANUAL 51-20-009-210 CONFIG A01 AND NOT DAMSDR REXA2026101601947Support · corrodedCORROSION ON LOWER SUPPORT BTWN BS 761.85 - 797 RT & LT SIDES AT INTERNAL OVERWING. LOWER SUPPORTS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR , EA CRJ953-23262, REV IR, & EA CRJ953-23263, REV IR, EA CRJ953-2326SDR REXA2026101601938Support Plate · corrodedCORRODED CONNECTOR SUPPORT PLATES LT / RT (PX33, PX17, PX34, PX19) ON LT & RT MAIN WHEEL WELL SUPPORT PLATE RH (PX33, PX17, PX34, PX19) ON RT MAIN WHEEL WELL WAS REPLACED IAW SRM 51-42-21-001-001-A01. CORROSION ON SUPPORT PLATE LH (PX33, PX17, PX34, PX19) ON SDR REXA2026101601930Floorbeam · crackedCRACKED FLOORBEAMS (2 EA) BTWN LBL 12 - RBL 12, BS 280 & 265. THE FLOORBEAMS MANUFACTURED IAW DWG CC670-33199, REV B, & DLA 5039 & WERE REPLACED IAW SRM 51-42-21-001-001-A01, & SRM 51-42-06-001-001-A01.SDR REXA2026101601929Floorbeam · crackedCRACKED FLOORBEAMS (2 EA) BTWN LBL12 - RBL12, BS 280 & 265. THE FLOORBEAM REMOVED IAW DWG CC670-33199 REV -B & DLA 5039. THE FLOORBEAMS WERE REPLACED IAW SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.SDR REXA2026101601928Stringer · corrodedCORRODED STRINGER 25R, BTWN BS280 & 295 IN THE E/E COMPARTMENT. THE STRINGER WAS REMOVED IAW SRM SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, AND WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR REXA2026101601927Beam · corrodedCORROSION ON LONGITUDINAL BEAM LBL 9, BS 1000 - 1088 IN THE AFT BAGGAGE BAY. THE BEAM WAS REPAIRED IAW SRM 53-00-41-201-001-A03.SDR REXA2026101601926Fitting · crackedCRACKED LOWER SIDE POST FITTING OF THE LT & RT WINDSHIELD FRAME IN THE COCKPIT. THE SIDE POST FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.SDR REXA2026101601925Fitting · crackedCRACKED LOWER SIDE POST FITTING OF THE LT & RT WINDSHIELD FRAME IN THE COCKPIT. THE SIDE POST FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.SDR REXA2026101601924Support Angle · crackedCRACKED SUPPORT ANGLE ON EXTRENAL SERVICE PANEL. THE SUPPORT ANGLE WAS REPAIRED IAW EA CRJ953-23097, REV IR, & SRM 51-41-02-001-001-A01.SDR REXA2026101601923Web · crackedCRACKED WEB BTWN BS 195 - 205, WL79.5, LT SIDE IN THE FWD HYDRAULIC BAY. THE WEB WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR REXA2026101601922Floor Support · crackedCRACKED FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPAIRED & REO 690-53-11-2249, REV --.SDR REXA2026101601921Angle · corrodedCORRODED ANGLE CAP OF LOWER SILL AREA IN THE PASSENGER DOOR CUTOUT. THE ANGLE CAP WAS REMOVED IAW SRM 51-21-06-001-001-A01, & WAS EVALUATED OUT LIMITS IAW SRM 51-10-06-001-001-A01, REPLACED IAW SRM 51-41-02-001-001-A01.SDR REXA2026101601920Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CSDR REXA2026101601919Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CSDR REXA2026101601918Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CSDR REXA2026101601917Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CSDR REXA2026101601916Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797, RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILLS WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA SDR REXA2026101601915Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797 RT & LT SIDES AT INTERNAL OVERWING LONGERON ASSEMBLIES. THE SILL WERE REPAIRED IAW EA CRJ953-23259, REV IR, EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CRJSDR REXA2026101601914Angle · corrodedCORROSION ON LOWER SILL BTWN BS 761.85 - 797 RT & LT SIDES. THE SILL WAS REPAIRED IAW EA CRJ953-23259, REV IR , EA CRJ953-23260, REV IR, EA CRJ953-23261, REV IR, EA CRJ953-23262, REV IR, EA CRJ953-23263, REV IR, EA CRJ953-23264, REV IR , EA CRJ953-23265, REVSDR HNAA2026101500993Rib · damagedWHILE PERFORMING HFEC INSPECTION ON LT WING SPAR I LOWER FLANGES AT RIB 9 FOUND A RELEVANT INDICATION. REPAIRED LH WING SPAR I LOWER FLANGE AT RIB 9 IAW SRM 57-20-05RE, ITEM 2, FIG 201 SHEET 2 (CASE 3) DET C AND PIEDMONT EO1-57-26-0457.SDR HNAA2026101500990Rib · crackedRIGHT WING RIB 5 IS CRACKED. R & R RIGHT WING RIB 5 IAW AERNNOVA TI-145-26-139 IAW ETD-2026-145-014875 REV.A. AND EO1-57-26-0487SDR SIMA20260824006Battery Pack · inoperativeCOCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE. SEE AML PAGE NUMBER 103302168 FOR ORIGINAL WRITE UP. RAR FWD RH EMERGENCY LIGHT POWER UNIT IAW AMM TASK 33-50-01. OPS CHECK GOOD. MEL RESTORED.SDR SWIA2026082477331Landing · dentedLEFT ELEVATOR, LEADING EDGE NUTPLATE LANDING, UNDER PANEL 334AB IS DENTED. REPAIRED DAMAGE TO THE LT ELEVATOR FRONT SPAR LOWER FLANGE IAW REO 601R-51-00-309 REV B.SDR 2026FA0000799Door · brokenAIRCRAFT WAS IN CRUISE AT 6000' WHEN ALL 4 CYLINDERS EXPERIENCED ABNORMAL EGT RISE, SLIGHT REDUCTION IN CHT, AND ENGINE SURGING. DIVERTED TO NEAREST AIRPORT. REMOVED MAIN ENGINE AIR FILTER AND DISCOVERED 600118-015 ALTERNATE AIR DOOR WITH CRACKS EMANATING FRSDR SWAA2026092996069Web · crackedCRACKED SHIELD WEB, BTWN BS 767 - 787, STR 25R. REPLACED THE SHIELD WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 146A0081, SHEET 49, REV A.SDR SWAA2026092919174Fitting · crackedCRACKED FITTING, BS 947.5, STR 26L. REPLACED THE FITTING IAW SRM 51-40-02, AND DWG 149A8103, SHEET 8, REV- .SDR SWAA2026092854601Stringer Clip · crackedAFT CARGO COMPARTMENT. FOUND A STRINGER CLIP CRACKED, STA 727D, STR 23L. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 145A1201, REV A.SDR SWAA2026092854390Sidewall Support · corrodedAFT CARGO COMPARTMENT- CORROSION WAS FOUND ON THE FLOOR TO SIDEWALL SUPPORT BETWEEN STA 727C+10 AND 727G+10, RBL 22 AND WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT SECTION BETWEEN BS727C+10 AND BS767 RBL22 WL156 IAW SRM 53-00-53-2R-6 AND DWG 146A750