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 IPXA2026071311366Brake · indicationEMERGENCY DECLARED, UPON LOWERING THE GEAR FOR LANDING, BRAKE RELEASE SIGNAL FOR WHEELS 5 & 8 WAS MISSING. CYCLED THE ANTI-SKID SWITCH AND ELECTED TO FOLLOW ANTISKID FAULT CHECKLIST. REPLACED BSCU (29GG) IAW AMM 32-42-72/401 OPS CHECKS NORMAL PER AMM 32-42-00/SDR DALA2026071304104Bottle · low pressureR2 DOOR ASSIST LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (8513698) AIRCRAFT WAS GROUNDED.SDR DALA2026071304100Fitting · crackedCRACKS WERE FOUND IN THE RH KEEL BEAM FITTING. REPAIRED PER ERA 635419-14AD. (1694589) AIRCRAFT WAS GROUNDED.SDR DALA2026071304097Bottle · low pressureDOOR 4R ASSIST BOTTLE LOW. SERVICED DOOR BOTTLE PER A330 AMM 52-15. (9219574) AIRCRAFT WAS GROUNDED.SDR DALA2026071304094Skin · crackedHOLE H378 CRACKED AT THE FITTING LAYER OF FR 40 LOWER SHELL PANEL JUNCTION ON THE LH SIDE. IT IS AT THE 11 O`CLOCK DIRECTION. AND HOLE H362 CRACKED AT THE SKIN LAYER OF FR 40 LOWER SHELL PANEL JUNCTION ON THE LH SIDE. IT IS AT THE 5 O`CLOCK DIRECTION. CORRECTISDR DALA2026071304093Frame · crackedCRACK AT FWD DIRECT OF THE FASTENER HOLE 555 OF FRAME 40 LEFT SIDE. REPAIRED PER ERA 634953-14 REV ORIGINAL. (1693250) AIRCRAFT WAS GROUNDED.SDR DALA2026071304092Frame · corrodedFRAME LOWER CHORD AT FR53.3, BETWEEN STGR-49L AND STGR-50L OF THE AFT CARGO BILGE AREA FOUND CORROSION. REPAIRED PER ERA 635421-14. REV ORIGINAL. (1693203) AIRCRAFT WAS GROUNDED.SDR FDEA202607110913Control Valve · odorFUME EVENT DESCEND THROUGH 20-25K. IT WAS A DIRTY OILY SOCK SMELL. PERFORMED INSPECTION OF HIGH PRESSURE DUCT & INTERMEDIATE PRESSURE DUCT ON BOTH ENGINES. REMOVED AND REPLACED LEFT WATER EXTRACTOR ASSY LEAK AND OPS CHECK GOOD. REMOVED AND REPLACED LEFT PSDR FDEA202607110912Skin · dentedDENT ON LOWER SKIN OF INBOARD AFT FLAP AT 41 IN. INB EDGE AND 2 IN. TRAILING EDGE ON LEFT WING INBOARD AFT FLAP AT 14". INB EDGE AND 2". TRAILING EDGE ON LT WING WAS REPAIRED IAW SRM 57-53-01-2R, FIGURE 201, SHEET 4, AND SRM 51-70-03-0G, PAR. 5.L FIG. 16, SHSDR FDEA202607110911Floor Panel · damagedBROKEN FIBERS AT FLOOR PANEL 241WFF OF MAIN DECK CARGO COMPARTMENT (11 LOCATIONS) FLOOR PANEL 241WFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC.15/2025SDR FDEA202607110910Floor Panel · puncturedPUNCTURES AT FLOOR PANEL 241FFF OF MAIN DECK CARGO COMPARTMENT (4EA) FLOOR PANEL 241FFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC.15/2025SDR FDEA202607110909Floor Panel · damagedBROKEN FIBERS AT FLOOR PANEL 251CFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251CFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC.15/2025.SDR FDEA202607110908Floor Panel · puncturedPUNCTURE AT FLOOR PANEL 231KFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231KFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC.15/2025SDR FDEA202607110907Floor Panel · damagedBROKEN FIBERS AT FLOOR PANEL 251DFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251DFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC.15/2025SDR FDEA202607110906Door · no discrepancyLEFT ENTRY DOOR WILL NOT CLOSE AND ARM. AMM 52-11-00-2 OPERATED L ENTRY DOOR FROM INSIDE AND OUTSIDE, DOOR ARMED AND DISARMED, A/C OK FOR SERVICE.SDR FDEA202607110905Floor Panel · crackedBROKEN FIBERS AT FLOOR PANEL 252LFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL252LFF WAS ASSESSMENT IAW SRM 53-00-50-1A REV. 94 DEC 15/2025 AND WAS REPAIRED IAW.SRM 53-00-50-2B FIG. 201 SHEET 1 AND FIG. 202 REV. 94 DEC 15/2025.SDR FDEA202607110904Floor Panel · crackedPUNCTURES AT FLOOR PANEL 251SFF OF MAIN DECK CARGO COMPARTMENT. (2EA) FLOOR PANEL 251SFF OF MAIN DECK CARGO COMPARTMENT WAS ASSESSMENT I.A.W. B767 S.R.M. 53-00-50-1"A REV. 94 DEC 15/2025 AND WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R FIG 201 AND 202 SHEETSDR FDEA202607110903Floor Panel · crackedBROKEN FIBERS AT FLOOR PANEL 242SFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242SFF OF MAIN DECK CARGO COMPARTMENT WAS ASSESSMENT I.A.W. B767 S.R.M. 53-00-50-1"A REV. 94 DEC 15/2025 AND WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R FIG 201 AND 202 SHEET 4 SDR FDEA202607110902Support Beam · crackedCRACK ON UPPER PANEL SUPPORT BEAM, WS 1054 INNER ACCESS PANEL 561QB, LH WING UPPER PANEL SUPPORT BEAM, WS1054 INNER ACCESS PANEL 561QB, LH WING WAS REPLACED AND FASTENERS, SHIM S AND CHORDS WERE INSTALLED I.A.W. E.O. #: H-5720-E0353920 C (P5) RELEASE DATE: SDR HNAA2026071300594Hydraulic System · lowHYD 1 LOW DISPLAYED IN FLIGHT. SERVICED NR 1 HYD SYSTEM IAW AMM 12-13-01. OPS CHECK GOOD AT THIS TIME. OK FOR SERVICESDR HNAA2026071300593Warning Message · false indicationCABIN ALT AND CABIN RATE OF CHANGE INDICATION DASHED ON GROUND AND IN FLIGHT. CABIN PRESSURE ACQUISITION MODULE. MX PDPU A/C AND ALL INDICATIONS CAME BACK ROA UPON FURTHER INVESTIGATION ALL DISPLAYS WERE FOUND TO FUNCTION PROPERLY. OPS CHECKED PRESSURIZATIOSDR YENA2026071300561Pin · missingFLT # 345, BOS-BCN. (ETOPS) " ENG NR 1 1XTHRUST REVERSER INHIBITION PIN MISSING ( THRUST REVERSER INHIBITION PIN )" (SUPPLEMENTAL INFORMATION TO FOLLOW).SDR YENA2026071300560Warning Message · illuminatedFLT # 7, JFK-LHR. (ETOPS) "CLASS 2 FUEL MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY FUEL )" (SUPPLEMENTAL INFORMATION TO FOLLOW).SDR SIMA202607131001Glowstrip · inoperativeFWD RT PHOTOLUMINESCENT STRIP DOES NOT GLOW. . DEFERRED MEL 33-32 AUTH 070644-C. OPENSDR SCNA20260713293Hinge · deformedEVERY 7 DAYS CHECK LAVATORY "D" DOOR FOR DIFFCULT OPERATION, SHARP EDGES AROUND LOWER MODIFIED HINGE, HINGE CENTER HAS DEFORMED AND BENT AWAY FROM LAVATORY DOOR. CONTACT INTERIORS ENGINEERIF ANY OF THE ABOVE OCCUR. ( LIFE LIMITED REPAIR PER AMM/ENG ) PERFORMESDR SCNA20260713292Latch · stuckFORWARD FA EMERGENCY EQUIPMENT CABINET DOOR LATCH STUCK. PERFORMED OPS CHECK OF EMERGENCY EQUIP CABINET DOOR LATCH IAW AMM 25-24-70 OK FOR SERVICE.SDR SCNA20260713291Apu · damagedAPU EXHAUST SHOOTING SPARKS, SMOKE ODOR IN CABIN/COCKPIT. FOUND MANY TURBINE BLADES TORN AND BENT ALONG THE AFT TIPS. APU WAS DEFERRED ON L/P 848721 ITEM 2.SDR SCN2026F00002Apu · failedAPU EXHAUST SHOOTING SPARKS, SMOKE ODOR IN CABIN/COCKPIT. FOUND MANY TURBINE BLADES TORN AND BENT ALONG THE AFT TIPS. APU WAS DEFERRED ON L/P 848721 ITEM 2.SDR DALA2026071304086Floor Support · crackedCRACK FLOOR STRUCTURE BEAM LOCATED BTW FR 20 TO FR 21 AT LEVEL -Y 189 AT FWD GALLEY AREA. REPLACED FLOOR STRUCTURE BEAM -Y189 LOCATED BTW FR 20 TO FR 24 AT LEVEL FWD GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-72-11, DWG D53111406 RELEASE DATE:20-DEC-96 ISSUSDR DALA2026071204078Strap · crackedCRACK STABILIZER STRAP ON BS 720 & 24 RBL AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT. STABILIZER STRAP ON BS 720 & 24 RBL AT CEILING STRUCTURE OF FWD CARGO COMPARTMENT WAS REPAIRED IAW SRM. 53-00-51-2R PROCEDURE 13 REPAIR 13. (LP 1694520 - AIRCRAFT WAS GRSDR ABXA20260711316Circuit Card · unknownL ENG FIRE LOOP 1 STATUS MESSAGE AC GROUNDED ,CONDUCTED T/S PER FIM 26-11 FT 804, CONTINUITY CHECK PASS. INTEGRITY RESISTANCE FROM AFOLTS CARD M681 PINS 20 & 21 14.1 OHM. PER BLOCK 102, SWAPPED M681 AND M682 AFOLTS CARDS, MESSAGE DID NOT RETURN. A/C VERIFIED SDR AALA202607126053Light · faultedAIRCRAFT WAS NOT GROUNDED: 17A EMERGENCY EXIT HATCH LIGHT FLICKERS. MAINTENANCE REPLACED OVERWING EXIT LIGHT ASSEMBLY AT SEAT ROW 17 IAW AMM 33-21-00-960-802.SDR AALA202607126715Lamp · inoperativeAIRCRAFT IN BASE MAINTENANCE: MCL BAR AT DR 3 R EXIT SIGN ( AMBER) NO ILLUMINATION. MCL BAR AT DR 3R EXIT SIGN (AMBER). MAINTENANCE REPLACED LAMP AND TEST NORMALAS PER AMM 33-25-02 REV.264 DATED 25 JUN 2026.SDR AALA202607125458Lamp · inoperativeAIRCRAFT IN BASE MAINTENANCE: MCL BAR AT DR 1 EXIT SIGN (BLUE) NO ILLUMINATION. MCL BAR AT DR 1 EXIT SIGN (BLUE). MAINTENANCE REPLACED LAMP AND TEST NORMAL IAW AMM 33-25-02 REV.264 DATED 25 JUN 2026.SDR AALA202607124031Heatshrink · missingAIRCRAFT WAS NOT GROUNDED: GIRT BAR ON LEFT AFT DOOR SLIDE MISSING RED HEAT SHRINK. MAINTENANCE REPLACED MISSING HEAT SHRINK ON AFT LH GRIT BAR IAW AMM 52-10-00SDR ABXA20260711315Test Panel · malfunctionedF/U-CHECK CONNECTORS & WIRING AT FIRE-OVHT TEST PANEL FOR HISTORY OF FIRE/OVHT SYS MESSAGES. IF NFF, REPLACE FIRE/OVHT TEST PANEL. PERFORMED GVI OF FIRE OVHT TEST PANEL CONNECTORS AND WIRING IAW B767 AMM 20-60-03 ALL WIRES LOOK SATISFACTORY WITH NO DAMAGE NOTESDR ABXA20260711313Audio Panel · malfunctionedDURING SERVICE CHECK FOUND CAPTAINS OXYGEN MASK MICROPHONE INOP. SWAPPED CAPTANS AUDIO PANEL WITH FIRST OBSERVERS, IAW AMM 23-12-02 OPS CHECK GOOD. AND DEFERRED . FIRST OBSERVER SEAT POS. IAW MEL 25-11-2-1A. RETURNED AC TO SERVICE.SDR AALA202607115240Slide · faultedAIRCRAFT WAS NOT GROUNDED: AFT LEFT ENTRY DOOR GIRT BAR DIFFICULT TO ARM. MAINTENANCE REPLACED L2 DOOR SLIDE ASSY IAW WORKCARD 08L22125001.SDR 2026FA0000761Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR 2026FA0000760Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR IPXA2026082702249Frame · crackedRIGHT FR 47 VERTICAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE N IN ALL LAYERS AT 6 O' CLOCK POSITION. ACCOMPLISHED THE REPAIR PER EO-98116-REQ1 AND EA 300-5710-27-A4553, REV-.SDR IPXA2026081401622Support · corrodedAFT CARGO CEILIING SUPPORT AT FR 57 BETWEEN Y-1959 TO Y-953 SI CORRODED. REMOVED AFT CARGO CEILING SUPPORT FR57 IAW SRM 51-40-21. INSTALLED ALL NUT PLATES TO AFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y-1959 TO Y-953 IAW SRM 51-40-21. INSTALLED AFT CARGO CEISDR IPXA2026082601638Support · corrodedAFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y-953 TO Y953 IS CORRODED. REMOVED AFT CARGO CEILING SUPPORT AT FR57 IAW SRM 51-40-21. INSTALLED NUT PLATES IN AFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y-953 TO Y953 IAW SRM 51-40-21. INSTALLED AFT CARGO CEILING SSDR IPXA2026082601642Support · corrodedFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y953 TO 1959 IS CORRODED. REMOVED AFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y953 TO 1959 IAW SRM 51-40-21. INSTALLED NUT PLATES IN AFT CARGO CEILING SUPPORT AT FR 57 BETWEEN Y953 TO 1959 IAW SRM 51-40-21. INSTALLED ASDR IPXA2026082401671Support · corrodedAFT CARGO CEILING SUPPORT AT FR 58 BETWEEN Y-953 TO Y953 IS CORRODED. REMOVED AFT CARGO CEILING SUPPORT AT FR 58 BETWEEN Y-953 TO Y953 IAW SRM 51-40-21. INSTALLED NUT PLATES TO AFT CARO CEILING PANEL SUPPORT AT FR 58 BETWEEN Y-953 TO Y953 IAW SRM 51-20-41.SDR IPXA2026082701557Support · corrodedAFT CARGO CEILING SUPPORT AT FR 54.2 BETWEEN Y-1959 TO Y-953 HAS SEVERAL SPOTS OF CORROSION. REMOVED CEILING SUPPORT IAW SRM 51-40-21-001. INSTALLED NUT PLATES TO NEW CEILING SUPPORT STRUCTURE AT AFT CARGO 54.2 BETWEEN -Y1959 TO Y-953 IAW AMM SRM 51-21-10. ISDR IPXA2026090101703Support · corrodedAFT CARGO CEILING SUPPORT AT FR 54.2 BETWEEN Y-953 TO Y953 WITH SERVAL SPOTS OF CORROSION. REMOVED CEILING SUPPORT IAW SRM 51-40-21-001. INSTALLED NUT PLATES TO NEW AFT CARGO CEILING SUPPORT AT FR 54.2 BETWEEN Y-953 TO Y953 IAW A300-600 SRM 51-21-10. INSTALLSDR IPXA2026091401737Floorbeam · corrodedAFT CARGO FLOOR SUPPORT ON FR 65 BETWEEN Y0 TO Y953 IS CORRODED DOT 50011-016. REMOVED PARCIALY ROLLER TRACK Y140, Y805, Y1470, Y-140, -Y805 AND -Y1470 AND REMOVED CROSSBEAM FR65 FOR EXCESSIVE CORROSION. INSTALLED NEW NUTPLATES (23 EA) IN FLOOR SUPPORT IAW A3SDR 2026FA0000732Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWSDR IPXA2026091101718Intercostal · crackedAFT CARGO INTERCOSTAL WEB BETWEEN FR 64 TO 65 Y1959 IS CRACKED. INSTALLED NEW INTERCOSTAL WEB, AFT CARGO BETWEEN FR 64 TO 65. IAW SRM 51-40-21.