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 SWAA2026032076433Shield · corrodedCORROSION ON R/H FLOOR TO SHIELD STA 767-787; RBL 22; WL 155 AT VARIOUS SPOTS. IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED. INSTALLED NEW SHIELD BS 767-787, RBL 22, WL 155 IAW SRM 51-40-02-0G AND DRAWING 146A0081, REV A.SDR IPXA2026031600239Support Angle · corrodedAFT CARGO COMPT RIGHT LOWER BULKHEAD SUPPORT AT STA.1640 SHOWS EVIDENCE OF CORROSION AND A CRACK DOT 47-11 INSTALLED 2 ANGLES IAW SRM 51-40-02.SDR VE7A202603190040Skin · crackedTHE MECHANIC WAS COMPLYING WITH THE ZONE 3 TRANSMISSION INSPECTION WHEN HE FOUND A CRACK. THE CRACK WAS EMANATING FROM THE FORWARD RIGHT HAND PYLON BEAM ATTACHMENT POINT. IT WAS FOUND BECAUSE OF BLACK OIL AROUND THE AREA. HE CLEANED THE AREA AND COMPLETED A DYSDR AALA202603187782Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 5 RH. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 5 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603189676Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 2 RH. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 2 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603186895Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 6 RH. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 6 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603184277Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 4 RH. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 4 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603182887Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 3 RH. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 3 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR SIMA20260303004Flashlight · missingFA2 FLASHLIGHT MISSING . RAR FLASHLIGHT ASSY AT FA2 IAW 33-51-01 OPS CHECKED GOOD MEL RESTORED.SDR SWAA2026031776207Seal · crackedRIGHT HORIZONTAL STAB FORWARD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SLIDER SEAL AND COTTER PINS PER AMM 53-31-31.SDR AALA202603130450Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 1 RH. MAINTEANCE REPLACED ELEVATOR HINGE ARM END FITTING 1 RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR IPXA2026031289808Bracket · crackedCRACKED BRACKET, NR 2 ENG LT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 11:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-55, REV 141.SDR IPXA2026031289779Stiffener · crackedCRACKED BRACKET, NR 2 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT BRACKET NEAR 3:00 POSITION. INSTALLED A NEW STIFFENR IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-60, REV 141.SDR YENA2026031100286Apu · odorFLT 1142 PBI-BDL, AFTER ROTATION AND THROUGHOUT THRUST REVOLUTION OIL ODOR IN COCKPIT. CABIN CREW DID NOT NOTICE THE ODOR. COMPLIED WITH INFO NOTICE 2017-T015, STEPS 1 AND 2. INDENTIFIED ODOR TYPE 1- APU DECONTAMINATION LEVEL C WAS ACCOMPLISHED PER AMM 36-10SDR IPXA2026031089949Angle · crackedCRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALLED A NEW CLIP I.A.W SRM 51-40-02-0G REV.94 AND DWG 313T2303, SH 136, REV -, & DWG 313T2303, SH 131, REV -.SDR CALA2026031014459Power Supply · failedCIDS 1 EPSU SYS TEST SHOWS "EPSU (12WL) EXT R" MESSAGE. TEST OF THE EPSU SHOWS "UNIT FAILED" FAULT. R & R THE EPSU BATTERIES TWICE. NO GOOD. INSPECTED FOR BURNT OUT LIGHTS. ALL EMERGENCY LIGHTS OPERATIONAL. RESEATED CONNECTOR PLUG. NO GOOD. NO ECAM MESSAGE. ENSDR 6JPA2026F00025Uplock Switch · out of adjustON CLIMBOUT AT LEVEL OFF NOSE GEAR INDICATED UNLOCK/MISCOMPARESDR SWIA2026030375431Bracket · damagedDAMAGE TO THE MCD PULLEY MOUNTING BRACKET AND SKIN (FLIGHT 4696) PERFORMED PERMANENT REPAIR TO PAX DOOR INNER SKIN AND FORMER AT FS347.25 AND BTW DATUM #3 AND #5 IAW REO 601R-52-11-3088 REV-- DATE 2026-03-03 STEPS 4-21. SEE CP 31820099 FOR STEPS 1 AND 2 OF RSDR SWAA2026030976539Engine · odorBIRD STRIKE, NO ABNORMAL ENGINE INDICATIONS. ODOR OF HOT OR SOMETHING COOKING IN COCKPIT & CABIN. C/W BIRDSTRIKE CONDITIONAL INSP IAW AMM 05-51-18. REF DEFECT LGPG 3025472. INSPECTED PER AMM 05-51-18-210-801-NG-01.SDR SWAA2026030976238Bulkhead Web · crackedCRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB.SDR SWAA2026030976279Seat · out of adjustPAX CABIN AT SEAT ROW 14D MUST BE NOT RECLINE. PERFORMED ADJUSTMENT ON HYDRAULIC LOCK STROKE ON SEAT ROW 14D AT PAX CABIN IAW CMM 25-22-46-3500, REV 9. FITS AND CLEARANCES STEP 6. PSDR SWAA2026030976249Battery · inoperativeAFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE BATTERIES AND 2 LIGHT ASSY IAW AMM 25-64-00. OPS CHECKED GOOD.SDR SWAA2026030977905Flashlight · inoperativeTHREE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERIES AND 2 LIGHT ASSY IAW AMM 25-64-00. OPS CHECKED GOOD.SDR SWAA2026030976248Sign · brokenCEILING EXIT SIGN MID-CABIN BROKEN. R & R CEILING EXIT LIGHT ASSY IAW AMM 33-51-01.SDR SWAA2026030976062Lamp · inoperativeRIGHT EXTERIOR OVER WING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED & REPLACED THE LAMP IAW AMM 33-51-04-960-801-NG. OPS CHECKED GOOD.SDR SWAA2026030976250Light · unsecurePHOTOLUMINESCENT FLOOR PROXIMITY LIGHT STRIP LIFTING AT 12C. SECURED WITH DOUBLE SIDED TAPE IAW AMM 33-51-15.SDR SWAA2026030975892Battery Pack · dischargedEMERGENCY BATTERY M1676 INOPERATIVE. CHARGED THE BATTERY PACK M1676 AND OPS CHECKED GOOD IAW AMM 33-51-06-610-802, & AMM 33-51-00-710-801.SDR SWAA2026030976137Access Panel · damagedACCESS PANEL 194BL HAS ELONGATED FASTENER HOLE. PREPPED AND PAINTED ACCESS PANEL 194BL REF M/M 51-21-99. PANEL READY FOR INSTALLATION. REF TTG8Q01ARDBG FOR PANEL 194BL INSTALLATION.SDR SWAA2026030975959Slider · crackedR/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL IS CRACKED. R & R RIGHT UPPER SLIDER IAW AMM 53-31-31.SDR SWAA2026030975917Fastener · pulledLEFT WING UPPER T/E PANEL O/B OF NR 5 FLAT SPOILER HAS 2 EA. PULLED FASTENERS ABOVE AND FWD OF FLAP DEFLECTION BEAM . R&R LEFT WING UPPER T/E PANEL O/B OF NR 5 FLAT SPOILER 2 RIVETS ABOVE AND FWD OF FLAP DEFLECTION BEAM IAW SRM 51-40-02.SDR REXA2026030900201Skin · corrodedFOUND POSSIBLE CORROSION UNDER BED SEAL FOR PANELS 196DR AND 195EL. REPAIRED FUSELAGE SKIN IAW ENDEAVOR AIR EA CRJ953-21442 REV IR DATED 2/7/2026.SDR DALA2026030901601Plate · corroded(LOG 1477217) CORROSION ON LH SIDE PLATES FROM STA 500D TO STA 500L AT FWD CARGO COMPARTMENT. LH SIDE PLATE FROM STA 500D TO STA 500L AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-900 SRM 51-40-02-0G.SDR DALA2026030901608Module · failed(LOG 8521544) EMERGENCY LIGHTS FROM MODULE M1676 INOP. RPLD MODULE M1676 AND BATT PACK AT 11DEF PER B737 AMM 33-51. OPS CKS GOOD.SDR DALA2026030901607Battery Pack · inoperativeSEVERAL EMERGENCY EXIT PATH LIGHTS INOP IN FWD GALLEY. REMOVED AND REPLACED THE ASSOCIATED BATTERY PACK IN THE FWD GALLEY CEILING PER B737 AMM 33-51.SDR DALA2026030801587Tailpipe · fireTAILPIPE FIRE ON ENG 2. INFORMATION WAS FORWARDED FROM ANOTHER CREW ALL START INDICATIONS ON ECAM NORMAL. PERFORMED FADEC 2A/B OP TEST PER A319 AMM-NO FAULTS NO LAST LEG FAULTS.RAN ENGINE 2 PER A319 AMM 71-00-00 NO DEFECTS. (LP: 8280298)SDR DALA2026030801580Floorbeam · damagedMISSING MATERIAL FLOOR BEAM LOCATED BTW FR 20 TO FR 21 AND - Y 250 AT FWD GALLEY AREA. REPLACED FLOOR BEAM -Y189 AND FASTENERS LOCATED BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53111406 RELEASE DATE: 20/DEC/96 ISSSDR DALA2026030801579Fitting · damagedENGINE NR 2 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACED ENGINE # 2 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. REPLACED #2 PYLON LOWER SPIGOT FITTIN G IAW A319 SRM TASK 54-51-12-300-001 REV 155 DATED 17 NOV 2SDR DALA2026030801578Fitting · damagedENGINE NR 1 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACE ENGINE NR 1 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. (LP: 1477390)SDR DALA2026030801577Seat Track · corrodedUPPER FUSELAGE, FR 16, Y+765, LH LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK AT UPPER FUSELAGE, BETWEEN FR12 AND FR24, Y+765 IAW A319 SRM 53-11-15-01A FIGURE 001, ITEM 015-A REV 155.00 DATED 17/NOV/25 AND REFRENCE AIRBUS DWG #D53112813, ISSUE B, ITEMSDR AALA202603076934Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL AT BS 767 AND RBL 30. REPLACED THETRANSITION PANEL PER SRM 51-40-02.SDR R61A2026030300057Mau · failedAVNX MAU 1A FAIL IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED NIC PROC 1 MODULE.SDR SWAA2026030675813Battery · no testAFT LT OTBD FA UNDERSEAT FLASHLIGHT FAILS TO TEST. OKAY TO CONTINUE PER MEL 25-64-02A AUTH# 308512 SP1B. REMOVED AND REPLACED AFT L/H O/B FA FLASHLIGHT BATTERY; OPS CHECK AND TEST GOOD REF AMM 25-64-00.SDR SWAA2026030676175Flashlight · no testFWD ATTENDANT OUTBOARD FLASHLIGHT DOES NOT TEST FWD ATTENDANT O/B FLASHLIGHT DOES NOT TEST<[01] REMOVE AND REPLACED FWD ATTENDANT OUTBOARD FLASHLIGHT PER AMM 25-64-00.SDR SWAA2026030676169Girt Bar · looseL1 GIRT BAR LOOSE THIS IS A TEST<[01] RESECURED FASTERNER PER MM 20-50-11SDR AALA202603061176Oil System · leakingAIRCRAFT WAS GROUNDED: SMELL OF WET SOCKS BY MAIN CABIN ENTRY DOOR DURING ALL PHASES OF FLIGHT AS REPORTED BY THE FLIGHT ATTENDANTS. MAINTENANCE FOUND THE APU LEAKING OIL AT THE V BAND SEAL AND REPLACED THE APU PER JOB CARD 26L310449003.SDR DXTA2026030607107Switch · faultedDURING DESCENT, ON ARRIVAL INTO PBI AROUND 24000 FT, GOT STAB TRIM & MACH TRIM ICAS ON PROCEEDED WITH CHKLIST & TRIED TO RE-ENGADED NO SUCCESS. AS WE WERE SLOWING DOWN, GETTING HEAVIER & HEAVIER NOSE DOWN, DECLARED EMERGENCY, AROUND 10000FT ON SHORT FINAL TSDR CALA2026030614385Fuel Cap · missingFUELER REPORTED BOTH FUEL CAPS MISSING. INSPECTION CARRIED OUT IAW AMM 05-51-59-202-001. NO DEFECTS.SDR CALA2026030614378Web · corrodedAFT CARGO DOOR CUTOUT LOWER SILL THE WEB HAS CORROSION ON UPPER AND LOWER SURFACE, REMOVED CORROSION AT AFT CARGO DOOR CUTOUT LOWER SILL WEB MAT.ORIG INAL IS .045 REMAINING MATERIAL IS .038 LOSS OF .007 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1, REMOVESDR GTIA2026030539290Oil System · leakingMODERATE ODOR FROM AIR CONDITIONING LIKE EXHAUST DURING CLIMB DISIPATED AT LEVEL OFF. ISOLATED PACK 1. NO FURTHER ODOR UNTIL DECENT ON BASE LEG THEN STRONG DIRTY SOCK SMELL IN CABIN WITH PACK 2 ONLY. SOURCE, CABIN AIR SUPPLY VENTS. FWD, MID, AND AFT CABIN.SDR DALA2026030501545Seat Track · damaged(LOG 1477750) RIGHT OTBD SEAT TRACK TANG DAMAGED AT SEAT ROW 12DEF. COMPLIED WITH ER/A 632334-14 REV A.