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 CALA2026052816591Floor Panel · corrodedAFT CARGO PIT FLOOR PANEL 140BF HAS MULTIPLE GOUGES AND CORROSION. FABRICATED NEW FLOOR PANEL 140BF, GOUGE OUT OF LIMITS. APPLIED ALODINE AND PRIME IAW SRM 53-00-53-1A-1, 53-60-53-0I-1, 51-20-01 AND GMM 07-35-05.SDR DALA2026052803225Not Reported · crackedREF STEP #8 RC AA5530-01048-02 AND AD 2018-10-08 4 CRACK INDICATIONS BELOW ZFS = 52.267. REPAIRED ON ERA 564482-14AD (8342877) (AIRCRAFT GROUNDED)SDR DALA2026052803222Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA 1087 LONG 14 RH. REPAIRED PER PRI 634296-14 (1606252) (AIRCRAFT GROUNDED)SDR DALA2026052803221Cusp Web · crackedIAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1606106) (AIRCRAFT GROUNDED)SDR DALA2026052703212Percussion Mech · faultedL1 DOOR SLIDE DEPLOYED (PARTIAL DEPLOYMENT). R & R L1 DOOR SLIDE ASSY IAW AMM 52-11. R & R DIAPHRAGM IN PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREW DOOR IAW AMM 52-10. ALL RII STEPS ACCOMPLSIHED. (LP: 8881442SDR DALA2026052703211Fitting · damagedDURING M2 AND WHILE ACCOMPLISHING EM 2515-01014-02A, MATERIAL BURR WAS FOUND IN THE LT LWR LATERAL FITTING OF RACK FIN 80VU. PER SECTION II OF ER/A 633192-14AD ACCOMPLISH SECTION II INITIAL INSEPCTION WITHIN 19,500 FC FROM SECTION I (22MAY26). REPEAT SECTION SDR FDEA202605220635Skin · delaminatedRH WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE DELAMINATED. 38MM*13MM*0.98MM. COMPLIED WITH EA 6-5750-T0387449 P1 REPAIRED THE DELAMINATION ON RT WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE. EA TITLE: WING - FLIGHT SUSDR 2026FA0000432Fadec · faultedPART 91 FLIGHT, NO PAX ONBOARD. FLIGHT LEVEL 27,000 PILOT RECEIVED A FADEC NO DISPATCH, AND THEN SUBSEQUENTLY FADEC FAIL. HAD RED X’S ON MULTIPLE ENGINE DATA READOUTS, BUT NO ENGINE PERFORMANCE CHANGE. PILOT WAS ENROUTE TO ADDISON, HE FOLLOWED ONBOARD CHESDR CALA2026052716554Support · crackedPANEL 671 BT WITH CRACK ON SUPPORT STRUCTURE. REMOVED PANEL 671BT & BEAM SPRT RH WING, EVAUATED FOUND TO BE OUT OF LIMITS, VERIFIED MATERIAL, FABRICATED NEW SUPPORT, LOCATED AND DRILL NEW SUPPORT, APPLIED ALODINE, APPLIED PRIMER, APPLIED TOP COAT ON SUPPORT, ISDR CALA2026052616544Liner · damagedHOLE IN ENGINE 2 FAN CASINGFOUND LOCATION OF HOLE TO BE LOCATED IN RT SIDE APPROXIMATELY 3'O CLOCK POSITION WITH CARBON PLIES SHOWING THROUGH ON NO.2 ENGINE INSIDE THE ABRADABLE LINER INNER BARREL SKIN SECTION "B" LENGTH OF HOLE 0.50" DEPTH OF HOLE 0.22" REF ASDR CALA2026052616527Power Supply · inoperativeEMERGENCY LIGHTS - OPS CHECK EMERGENCY LIGHTS, OVERHEAD MOUNTED AISLE LIGHTS, RT AFT ESCAPE EXTERIOR LIGHT, & RIGHT OVERWING ESCAPE GROUND ILLUMINATION LIGHT (L00007, L00548, L01507, L01513, L01517) INOP. SLAVED IN NEW EMERGENCY BATTERY PACK, NO HELP. REPLACESDR CALA2026052616526Wire · broken32ABC EMERGENCY IN SEAT PATH LIGHT INOP REPAIR BROKEN WIRE ON EMERGENCY HARNESS CONNECTOR. REF SWPM 20-30-12. OPS CK GOODSDR DALA2026052703180Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D PER ER/A 633743-14AD FOR MIRROR FITTING INSTALLATION AND CONTI NUITY FITTING REPLACEMENT. SECTION I IS LIMITED TO 60000FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/CSDR DALA2026052703179Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR MIRROR FITTING REPAIR AND CONTINUITY FITTING REPLACEMENT PER ER/A 633743-14AD. C/A: SECTION I IS LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATESDR DALA2026052703178Fitting · not reportedER/A 633743-14AD ISSUED FOR CONTINUITY FITTING REPLACEMENT AND MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-633743 ADDED FOR AC 3168. (LP: 1607258) AIRCRASDR AALA202605277663Skin · crackedAIRCRAFT IN BASE MAINTENANCE: DURING THE CURRENT MAINTENANCE VISIT IN PIT, WHILE ACCOMPLISHINGJC 26T22053007, AFATIGUE CRACK RADIATING FROM A FASTENER HOLE WAS FOUND AT FR13/14 AND Z+780-Z+950 ONTHE RH SIDE. MAINTENANCE REPAIRED SKIN IAW EA 375396.SDR SWIA2026052276030Window · crackedCP SIDE WINDOW HAS ~3 INCH CRACK IN THE INNER PANE (FLIGHT 3792) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32308780 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED THE CA SIDE WINDOW WITH REFERENCE TO AMM 56€“12€“01 & TASK CARD 56-220-1000-SKSDR SWAA2026052605806Retainer · looseFORWARD SERVICE DOOR GIRT BAR LOOSE. INSPECTED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR AND BAR RETAINER CLIPS OP CHECK GOOD PER AMM 25-66-01.SDR SWAA2026052606582Girt Bar · looseFORWARD SERVICE DOOR GIRT BAR LOOSE. INSPECTED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR AND BAR RETAINER CLIPS OP CHECK GOOD PER AMM 25-66-01.SDR SWAA2026052605627Flashlight · not seatedEMERGENCY FLASHLIGHTS NOT TESTING. RE-SEATED AFT GALLEY FLASHLIGHT IAW AMM 25-64-00. OPS CHECK GOOD.SDR SWAA2026052605371Isolator · crackedPASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED.<[01] R&R AFTER SLIDE MOUNT ISOLATOR PER SRM 51-40-02;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.SDR SWAA2026052605808Lens · missingFA REPORTS RH FWD EMERGENCY EXIT SIGN LIGHT ASSY COVER MISSING. INSTALLED FWD RH EMERGENCY EXIT SIGN LENS PER AMM 20-50-11; OPS CHK GOOD PER AMM 33-51-00.SDR SWAA2026052605630Light · looseEMERGENCY EXIT LIGHT, CEILING. CAPTAINS SIDE ROW 19 WAS FALLING OUT OF SOCKET. SECURED EMERGENCY AREA LIGHT IAW AMM 33-51-03.SDR SWAA2026052605504Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF R1 DOOR IS INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT LAMP AFT OF R1 DOOR IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.SDR SWAA2026052605474Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. R & R RT UPPER HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.SDR KCSA2026052229Switch · faultedSTAB TRIM 2, STAB TRIM 3, EMERGENCY DECLARED FOR STAB TRIM 2 & 3. REMOVED AND REPLACED CAPTAINS STAB MANUAL TRIM CTRL WHEEL SWITCH IAW AMM 27-41-11 AND WDM 27-41-11. OPS CHECKS GOOD. AUTOLAND UNIQUE GROUND TEST PASSED IAW AMM 22-10-00. THIS A/C REMAINS CAT ISDR AALA202605266747Proximity Sensor · faultedAIRCRAFT WAS NOT GROUNDED: ECAM MESSAGE FOR DOOR LEFT AFT EMERGENCY EXIT DISPLAYED WHILE CLIMBING THROUGH 8000FT AND DISAPPEARED IN A FEW SECONDS. MAINTENANCE REPLACED THE DETECTOR PROXIMITY SWITCH FOR THE 3L EMERGENCY EXIT DOOR PER AMM 52-71-13 AND ACCOMPLSDR AALA202605263577Proximity Sensor · illuminatedAIRCRAFT WAS NOT GROUNDED: DOOR LEFT AFT EMERGENCY EXIT ECAM ON DURING CRUISE OCCURED DURING ANOTHER FLIGHT PER THE FLIGHT CREW. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY EXIT DOOR DETECTOR PROXIMITY SENSOR PER AMM 52-71-13 AND ACCOMPLISHED A SATISFACTORY SDR AALA202605260085Proximity Sensor · illuminatedAIRCRAFT WAS NOT GROUNDED: DOOR LEFT AFT EMERGENCY EXIT ECAM AT FL 340. FLIGHT CREW REPORTED THAT PRESSURIZATION AND CABIN VS LOOKED NORMAL. REPLACED THE LEFT AFT EMERGENCY EXIT DOOR DETECTOR PROXIMITY SENSOR PER AMM 52-71-13 AND ACCOMPLISHED A SATISFACTORYSDR AALA202605262110Mechanism · stickingAIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR HARD TO OPEN. MAINATENANCE CLEANED / LUBRICATED THE FLIGHT DECK DOOR LOCKING MECHANISMS PER AMM 52-51-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA202605264940Battery · no testAIRCRAFT WAS NOT GROUNDED: MEGAPHONE AT STATION D AFT AIRCRAFT LEFT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE MEGAPHONE.SDR AALA202605267148Battery · no testAIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 11WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.SDR IPXA2026052613721Brake Assy · inoperativeON LANDING USING MED AUTOBRAKES AND THEN MANUAL BRAKING NO LEFT MAIN GEAR BRAKING ENGAGED. LEFT MAIN GEAR TEMPS ALL REMAIN ZERO. THE ORIGINAL FAULT IS CORRECTED AND THE LH MLG BRAKES TEMP FAULT IS DEFERRED IAW MEL 32-47-02. REF BARCODE: T3F18E008W57X. R/R LH MSDR IPXA2026052614211Power Supply · inoperativeASPSU WILL NOT TEST. CYCLED AIRCRAFT POWER. PERFORMED TEST OF THE ASPSU IAW A300 AMM 52-73-00. OPS CHECK GOOD.SDR IPXA2026052613816Carabiner · missingCARABINER MISSING FROM 1 EMERGENCY DESCENT BODY BAG. INSTALLED NEW CARABINER IAW MM 25-61-00.SDR DXTA2026052608193Engine · failedON CLIMBOUT SHORTLY AFTER TAKEOFF, RECEIVED A STRONG VIBRATION FOLLOWED BY A L ENG EXCEEDANCE CAS & A OVERTEMP ON ITT. REDUCED THUST LEVER TO BRING ITT DOWN. RECEIVED A LT ENG VIBRATION CAS FOLLOWED BY A LT ENG FLAMEOUT CASS. VIBRATION DECREASED BUT NEVER WENSDR DXTA2026052608198Pin · out of rigMAIN CABIN DOOR VERY DIFFICULT TO LATCH CLOSED BOTH FROM THE INSIDE AND OUTSIDE. ONLY OCCURS INTERMITTENTLY BUT MORE THAN HALF OF THE TIME. SOMETIMES IT'S PERFECTLY NORMAL, OTHER TIMES IT TAKES EXCESSIVE FORCE AND TWO PEOPLE. NO VISIBLE DAMAGE TO THE DOOR NOR SDR DALA2026052603169Bottle · dischargedR4 DOOR PRESSURE LOW ON FAP. SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (8830712) AIRCRAFT WAS GROUNDED.SDR DALA2026052603164Skin · damagedSKIN DAMAGE AT STR 19R JUST AFT OF FRAME 500H. COMPLIED WITH ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS, ENSURE ALL ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS ARE COMPLETEDSDR DALA2026052603163Stringer · dentedSTRINGER DENTED AFT OF FRAME 500H @ STRINGER 19R. COMPLIED WITH ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS, ENSURED ALL ER/A ER/A 634485-14 REV ORIGINAL PRI REV "0", "1", "2", "3" REPAIR INSTRUCTIONAL STEPS ARE COMPLSDR DALA2026052603165Bolt · looseROW 15 ABC BOLT SECURING SEATS TO FLOOR MISSING. RE-SECURED HARDWARE , VERIFIED SEAT SECURITY, PER B737 M/M 25-21 CHK NML. (LOG 8435378 - AIRCRAFT WAS GROUNDED).SDR DALA2026052603158Skin · damagedWHILE IN SEA, MTC REPORTED 3 LIGHTNING STRIKES ON FWD NOSE FUSELAGE AT STA 181, LBL 21. ALL THREE ARE IN THE SAME OPEN BAY. MAINTENANCE REPAIRED DAMAGE PER ERA 634548-14. (LOG 1606265 - AIRCRAFT WAS GROUNDED).SDR AALA202605265959Slide · dislodgedAIRCRAFT WAS NOT GROUNDED: L1 SLIDE PACK FELL OUT OF STORAGE ASSEMBLY WHEN AGENT OPENED L1 DOOR. REMOVED AND REPLACED SLIDE. PER JOB CARD 08L22125001.SDR UIEA2026052600350Seal · damagedEXTERIOR EMERGENCY LIGHT AT L1 DOOR NEEDS RESEALED. RESEALED EXTERIOR EMERGENCY LIGHT LENS AT L1 DOOR IAW B767 AMM 33-51-06. NO DEFECTS NOTED</P>)SDR SWAA2026052605569Unknown · odorCUSTOMER REPORTED SMOKE SMELL IN AFT CABIN. PERFORMED SOMOKE OR FUMES IN THE CABIN CONDITIONAL INSPECTION PER FIM 21-00 TASK 806. COULD NOT DUPLICATE. NO FURTHER DEFECTS NOTED.SDR DALA2026052603152Indicator · inoperativeSLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. FWD TO MEL 52-73-01 (1606206) (AIRCRAFT GROUNDED)SDR SIMA20260522002Door · lack of lubeFA AND GATE AGENT REPORT ISSUES OPENING/CLOSING F1 MAIN CABIN DOOR. "STICKY" LUBRICATED THE L1 FORWARD-PASSENGER-DOOR COMMAND-RAMP ROLLER-SHAFT AND ITS BUSHING IAW AMM 53-10-21. OPC GOOD.SDR SIMA20260522001Unknown · odorIRRITATING/ HARSH SMELL NOTED IN COCKPIT ON DEPARTURE. SMELL DISSIPATED AND RETURNED PERIODICALLY IN FLIGHT AND RETURNED PERSISTENTLY AT TOP OF DESCENT. (REPEAT EVENT) FOLLOWED FIM 21-20-00-810-801-A PER WORKSCOPE PROVIDED, A/C HAD COMPRESSOR WASH DONE TO E1 OSDR HBKA202605260587Fire Detector · false activationWHILE CRUISING AT 38,000 FEET IN AND OUT OF CLOUDS NO PRECIPITATION OR TURBULENCE. RIGHT ENGINE FIRE INDICATION PUSH BUTTON ILLUMINATED AND "FIRE" ANNUNCIATOR IN THE N1 INDICATION CAME ON. THE FLIGHT CREW PERFORMED MEMORY ITEMS OF: THROTTLE TO IDLE AND WAIT FOSDR REXA2026052600610Bearing · damagedFOUND 1 EA. R/H AILERON SIDE BEARING LUG LABELED H TO BE PREVIOUSLY OVERSIZED REPAIRED IAW CRJ 900 MHIRJ REO 690-57-61-514 REV -- DATED 2026-05-08