Service difficulty reports
1,771,154 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 IPXA2026062203992Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 10.5" FROM AFT EDGE AND 45" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BOND THE SPACER WITH FILM ADHESISDR IPXA2026062203971Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM AFT EDGE AND 24" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURSDR IPXA2026062203947Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 5:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 19.5" FROM UPPER EDGE AND 11.5" FROM AFT EDGE, AT 5 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). BONDED THE SPACER WITH FILM ASDR IPXA2026062203822Nose Cowl · dentedDENT - SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 4:00 POS. (REPAIR) CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0 REV. 95.SDR IPXA2026062203799Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE , 29" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ASDR IPXA2026062203788Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 50.5" FROM OUTBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESSDR IPXA2026062102849Skin · crackedCRACKED SKIN, LT WING T/E NR 3 FLAP AFT FAIRING INBD. (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6 INCHES ALL AROUND. RESULT: NO DEFECT FOUND.SDR IPXA2026061903308Bracket · chafedCHAFED BRACKET, NR 2 ENG RT T/R CLOSURE DOOR T/E AREA. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96 C/W REVIEWSDR DXTA2026062208500Brake Sys · faultedBRAKES PULSATE OR GRAB AND RELEASE UNDER LIGHT TO MODERATE BRAKING WHILE TAXING. THEY STOP WELL WITH HEAVY BRAKING. THE GRABBING IS MOST NOTICEABLE WHEN BRAKES ARE WARM AFTER LANDING. BRAKES PULSATE OR GRAB & RELEASE UNDER LIGHT TO MODERATE BRAKING WHILE TASDR DXTA2026062208490Transducer · shearedDURING INITIAL CLIMB AT APPX. 400 FT. AGL, CREW RECEIVED A BRAKE LT FAULT CYAN CAS ACCOMPIANIED BY AN AMBER FLT CTRL NO DISPATCH CAS. LT INBOARD WHEEL SPEED TRANSDUCER LOST ROTATION. FAULT CODE: 32410. ARRIVED AND ACCESSED THE ACFT. PERFORMED POWER CHECKS ANDSDR DXTA2026062208488Link · corrodedRIGHT MLG HAS CORROSION LEACHING . FOUND PITTING AROUND TRAILING LINK / BRAKE MATING SURFACE. REPLACED TRAILING LINK. OPS CHECK GOOD. IAW MM 32-10-15.SDR DXTA2026062208484Link · corrodedRIGHT TRAILING LINK ASSEMBLY CORROSION, LINK PIN DAMAGE AND AXLE CHIPPINGSDR AALA202606221968Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT HSS 138.70, 8 INCHES FORWARD OF AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.SDR AALA202606222935Slide Raft · no testAIRCRAFT IN BASE MAINTENANCE: GROUND SCANNING REPORT REVEALED CIDS1 EPSU EXT LOAD FWD L 33-51-38, AND CIDS1 EPSU INT LOAD FWD L 33-51-38. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202606192507) AND THE FORWARD RIGHT DOOR SDR AALA202606222507Power Supply · no testAIRCRAFT IN BASE MAINTENANCE: GROUND SCANNING REPORT REVEALED CIDS1 EPSU EXT LOAD FWD L 33-51-38, AND CIDS1 EPSU INT LOAD FWD L 33-51-38. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 (AALA202606192507) AND THE FORWARD RIGHT DOOR SDR UIEA2026061800528Bulb · inoperativeBOTH FORWARD OVERWING ESCAPE LIGHTS ON RH WING INOPERATIVE. RELAMPED FORWARD OVERWING ESCAPE LIGHTS ON RH WING IAW AMM 33-51-06-902-082. OPS CHK GOOD. NO DEFECTS NOTED.SDR YENA2026062200484Unknown · odorFLT 1471 LGA-FLL. STRONG PERSISTENT FUMES FROM 12,000 UNTIL LANDING. DIRTY SOCK ODOR. ATTEMPTED TO ISOLATE PACK 1 WAS UNSUCCESSFUL. SMELLED BY BOTH PILOTS. FA'S DID NOT ODOR IN THE CABIN. LEVEL II FUME EVENT; COMPLIED WITH INFO/ NOTICE 2017-T015. IDENTIFISDR YENA2026061700484Unknown · odorFLT 1471 LGA-FLL. STRONG PERSISTENT FUMES FROM 12,000 UNTIL LANDING. DIRTY SOCK SMELL. ATTEMPTED TO ISOLATE PACK 1 WAS UNSUCCESSFUL. SMELLED BY BOTH PILOTS. FA'S DID NOT SMELL IN THE CABIN. LEVEL II FUME EVENT; COMPLIED WITH INFO/ NOTICE 2017-T015. IDENTSDR DALA2026062203692Oxygen Panel · openPASSENGER OXYGEN MASK PANEL OPENED IN FLIGHT ABOVE SEATS 2C AND D. FWD TO MEL 35- 21-01A. M PROCEDURE C/W AND PLACARD INSTALLED. SEATS 2 C AND D UNUSABLE. RESECURED O2 CONTAINER DOOR AT 2CD PER AMM 35-21. M PROCEDURES REVERSED. MEL PLACARD REMOVED. OK FOR SESDR AALA202606210290Pump · inoperativeAIRCRAFT WAS GROUNDED: ENGINE FAILURE NR 1 ENGINE ON FINAL APPROACH. SINGLE ENFINE OPERATION WAS CONFIRMES AT 1 MINUTE 51 SECONDS. MAINTENANCE REPLACED FUEL PUMP IAW AMM 73-11-11.SDR DALA2026062103687Stiffener · unsecureDURING M2 AND WHILE INSPECTING PER 5316-01052-05B THE HORIZONTAL STIFFENER OF LATERAL WINDOW FR4 RHS WAS FOUND COMPLETELY REMOVED DUE TO PREVIOUS REWORK PER THIS ER/A ORIGINAL REVISION. PER SECTION IV OF 573692-14 REV B, ACCOMPLISH SECTION IV REPETITIVE INSPESDR AALA202606205697Light · faultedAIRCRAFT WAS NOT GROUNDED: LEFT OVER WING EMERGENCY EXIT LIGHT IS FLICKERING AND LIGHT STRIP SHOWING A RAINBOW SET OF LIGHTS. MAINTENANCE REPLACED EMERGENCY ROW SIDEWALL LIGHT IAW AMM 33-21-00SDR DALA2026061903677Skin · scratchedSCRATCH ON LOWER SKIN OF AFT MOVABLE VANE (3 INCHES FROM T.E. AND 6 INCHES FROM INBRD EDGE APPROX) AT RT WING. LOWER SKIN OF AFT MOVABLE VANE WERE REPAIRED IAW SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND IAW SRM 51-70-02-0G PROCEDURE GENERAL. (LP 1651992 - AIRCSDR DALA2026061903676Skin · out of limitsHOLES OUT OF LIMITS ON LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE. LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE WAS REPAIRED PERSDR KCSA20260619733Oil System · lowON DESCENT NOTICED STRONG ODOR OF OIL ON UPPER DECK AND MAIN DECK CREW REPORTED LOW OIL ON ENG 4, INDICATED 4 QUARTS. PERFORMED CONDITIONAL INSPECTION OF #4 ENG IAW FIM 21-00 TASK 810 NO EXTERNAL LEAKS FOUND. SERVICED ENG OIL IAW AMM 12-13-03.SDR IPXA2026061903879Support Angle · crackedCRACKED SUPPORT ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -SDR IPXA2026061903908Bracket · crackedCRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR IPXA2026061903869Support Angle · crackedCRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 REV: - AND SH 76 REV: -SDR IPXA2026061904932Bracket · crackedCRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.SDR WX0A2026061932855Fan · odor(AIRCRAFT NOT GROUNDED) AT 23:00Z 45 MIN FROM LANDING AT ATW AT 35,000 CRUZE FWD FA AND FLIGHT DECK CREW SMELLED ELECTRICAL BURNIG SMELL FROM FORWARD AREA OF PLANE. IT DISAPATED WITHIN 2 MIN OF THE INITIAL SMELL. PERFORMED TSM 21-21-00-810-803-A THRU STEP 4A2SDR WX0A2026061932854Epsu · inoperative(AIRCRAFT NOT GROUNDED) EPSU BATTERIES REQUIRE REPLACEMENT FAIL EPSU TEST. REMOVED AND REPLACED EPSU BATTERY 10WL, 11WL, 12WL, 13WL REF AMM 33-51-38-000-002-A AND 33-51-38-400-002-A OPS CHK GOOD.SDR DALA2026061903670Power Supply · inoperativeEMERGENCY LIGHTS ON SEATS INOP 18F - 21F. REMOVED AND REPLACED M1695 POWER SUPPLY IAW AMM 33-51. ALL LIGHTS OPS CHECKED GOOD. (LOG 8607054 - AIRCRAFT WAS GROUNDED).SDR JJBA20260619015Light · inoperativeAISLE CEILING EMERGENCY LIGHT AT ROW 3 INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHT AT ROW 3. OPS CHECK SAT.SDR DALA2026061903669Hook And Loop · faultyINSPECT 4L DOOR SLIDE MFG S/N 1488RP OF HOOK AND LOOP CONDITION. PERFORMED INSP OF SLIDE AND FOUND HOOK AND LOOP BAD. R & R L4 SLIDE IAW WORK CARD 2566-9001-4L. (1652338) AIRCRAFT WAS GROUNDED.SDR DALA2026061903666Seat Track · crackedSHIP 5807 N REF TO AMDS 2525-0062: WHILE ACCOMPLISHING CIC APPLICATION, CRACK WAS FOUND ON LH OUTBD SEAT TRACK BS 550 AT FLOOR PAX CABIN STRUCTURE. LT OTBD SEAT TRACK BS 550 AT FLOOR PAX CABIN STRUCTURE WAS REPAIRED IAW SRM 53-00-52-2R. (1652305) AIRCRAFT WAS SDR AALA202606195352Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202606193763Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.SDR CALA2026061917197Sensor · faultedFLAPS ASYMMETRY ALT FLAPS EXTENSION FLAPS 5 LANDING FAULTS UPLOADED. REMOVED AND REPLACED NR 7 FLAP SKEW SENSOR. REF AMM 27-59-01. OPS CHECKS GOOD, NO FAULTS NOTED.SDR CALA2026061917192Unknown · odorCREW AND PAX SMELL ELECT RIC BURN SMELL UPON ARRIVAL TO A/C, NO ELECTRICAL BURN ODOR WAS PRESENT. DEBRIEFED FLIGHT CREW, FLIGHT ATTENDANTS REPORT SMELL WAS IN THE FWD GALLEY. PILOTS DID NOT SMELL IT. PERFORMED INSPECTION REF AMM 05-51-26-800-801-C1. NO DEFECTSSDR CALA2026061917190Unknown · odorSTRONG FUEL SMELL NOTED IN FLT DECK AFTER BOTH ENGINES STARTED AFTER SHUTDOWN FROM RETURN TO GATE NOTED A SLIGHTLY STRONGER FUEL ODOR FROM E1 THAN E2. OPENED FAN AND REVERSER COWLS REF AMM 71-11-04/78-31-00 TO INSPECT E1, NO DEFECTS NOTED, CLOSED ACCESS. INSPSDR CALA2026061917184Web · corrodedCORROSION: AFTER REMOVAL OF FWD CARGO DOOR CUTOUT PLATE ASSY FOUND WEB WITH UPPER SURFACE CORROSION IN SEVERAL AREA REF AAR N/R 100035713. REMOVED AND REPLACED FWD CARGO SILL WEB FROM APPROX BS 440 - 492.4, RBL 30 IAW SRM 51-40-02-0G-0 DWG 143A8120.SDR CALA2026061917182Access Panel · corrodedCORROSION, NOSE WHEEL WELL INTERNAL THRU LEFT O/B AFT ACCESS PANEL 113BW LWR CHORD CORRODED AT BS 277 BELOW STR 25. REF AAR N/R 100038745. REMOVED AND REPLACED LOWER CHORD AT NOSE WHEEL WELL INTERNAL STRUCTURE BETWEEN BS 225.4 TO 294.5 BELOW STR 25L IAW SRMSDR YENA2026061900484Ignition Sys · warning messageFLT 411, JFK-LAS. (ETOPS) ENGINE 1 IGNITION B FAULT (IGNITION SYSTEMS SYSTEM B ). PERFORMED OPS CHK THROUGH CFDS IAW AMM 74-00-00-710-802-A. OPS CHK OK. MDDR CLEARED. MX-4 UPDATED.SDR 6CBA2026061926001Engine · unknownDURING CRUISE FROM KIAD TO KCEU, CREW NOTED A LOUD BANG FROM THE ENG AREA. THE CREW DIVERTED TO KCLT & ATC DECLARED AN EMER, LANDING UNEVENTFUL. TECHS VISUALLY INSPECTED THE ENG FOR DEFECTS & COMPLIED WITH A BORO INSP IAW EMM 72-00-00 & FOUND IN LIMITS. ISDR SCNA20260619254Light · inoperativeL4 SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED L4 EMERGENCY SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SCNA20260619253Charger · inoperativeAFT OVERWING, L3 SLIDE LIGHT, AND INTERIOR AREA LIGHTS INOP. REMOVED AND REPLACED CHARGER ASSY UNDER ROW 21ABC IAW AMM 33-51-06-960-806 AND AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD AT THIS TIME.SDR ASAA2026061766836Door · no discrepancyCATERING REPORTS DIFFICULTY OPENING L2 DOOR. GROUNDED - YES. REF AMM 52-13-00-860-801/-860-802, OPENED AND CLOSED L2 DOOR WITH EXTERIOR HANDLE W/ NO DEFECTS NOTED. NO ABNORMAL DOOR WARNING LIGHTS NOTED ON FLIGHTDECK OVERHEAD PANEL.SDR ASAA2026061766832Cover · wrong partEXIT ROW 16A HAS WRONG SIGNAGE ON EMERGENCY LT COVER. GROUNDED - YES. REPLACED EXIT ROW EMERGENCY SIGN COVER IAW AMM 33-51-04.SDR ASAA2026061766830Lens · wrong partWHILE WORKING TC 78233001 FOUND INCORRECT LENS INSTALLED FOR INTERIOR EMERGENCY EXIT LENS AT ROW 16 DEF. (MISSING ARROW INDICATION). GROUNDED - YES. DURING LENS REPLACEMENT FOUND LENS SUPERGLUED TO ASSY, BREAKING ATTACHMENT POINT. REMOVED & REPLACED L1207 EMERSDR ASAA2026061766829Lamp · inoperativeEMERGENCY LIGHT (EXTERIOR) NEXT TO R1 DOOR NOT ILLUMINATED WHILE ACCOMPLISHING T/C. GROUNDED - YES. RELAMPED EXTERIOR R1 EMERGENCY LIGHT IAW AMM 33-51-04 OPS CHECK GOOD.