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 SCNA20260529219Girt Bar · bindingR1 GIRT BAR HARD TO INSERT INTO BRACKET MC NOTIFIED JB 7665 ACTIVATED DOOR MOUNT ESCAPE SYSTEM THEN DEACTIVATED DOOR MOUNT ESCAPE SYSTEM AR R1 DOOR REF 25-66-00 NO ISSUE WITH INSERTS FOUND OK FOR SERVICE.SDR ABXA20260528231Antenna · defectiveWHILE DESCENDING THRU FL 280 AND BELOW, GEAR NOT DOWN EICAS WARNING AND CONFIG LIGHT CAME ON WHEN THRUST LEVERS ARE AT IDLE. REMOVED AND REPLACED LH RA RCVR AND XMTR ANTENNAS IAW 767 AMM 34-33-02. OPS CHECK GOOD. A/C DOWNGRADED CAT I PENDING 30/40 TESTS REF LPSDR ABXA20260528230Warning Message · false activationCREW GOT AIR/GND DISAGREE STATUS MESSAGE IN FLIGHT. PERFORMED B767 FIM TASK 810 1803. NO FAULTS WITH PROX INDICATION FOUND AT THIS TIME. ACFT OK FOR RETURN TO SERVICE REF FIM TASK.SDR HNAA2026052900439Elec Connector · shortedAPU FIRE WARNING WITH BELL DURING TAXI. C/W QRH. FIRE BOTTLE BLOWN. MEL 28MAY26 17:44 APU FIRE EXTINGUISHING. T/S IAW FIM 26-22-00-810-802A. FOUND SHORTED CANNON PLUG AT APU FIRE EXTINGUISHER BOTTLE. R & R ELECTRICAL CONNETOR IAW SWPM 20-50-00. REMOVEDSDR 2026FA0000467Window · crackedPILOT REPORTED BIRD STRIKE TO LOWER LEFT-HAND WINDOW. MAINTENANCE FOUND CRACK DAMAGE REQUIRING REPLACEMENT OF WINDOW.SDR 2026FA0000466Display · failedIN RESPONSE TO YOUR REQUEST, PLEASE FIND BELOW A DETAILED PILOT-IN-COMMAND (PIC) REPORT REGARDING THE EVENT THAT OCCURRED ON MAY 10, 2026, INVOLVING LEARJET 60, N269GJ. FOLLOWING THE OCCURRENCE, I ALSO REVIEWED THE EVENT WITH BOTH FLIGHT CREWMEMBERS IN MY CAPASDR GIRA20260528001Battery Pack · faultedR1 DOOR EMERGENCY LIGHT BATTERY FAILS DEEP CYCLE; REMOVED AND REPLACED BATTERY PACK AND OPS CHECK PASSED NO DEFECTS NOTED.SDR SWIA2026052876107Sensor · faultedA-I WING 1 LEAK WARNING IN CLIMB. RAN QRH AND MESSAGE CLEARED. SYNOPTIC PAGE SHOWED LEFT WING ANTI ICE AMBER, 15 DEGREES C. WING ANTI ICE WAS OFF AT TIME OF MESSAGE.C: MEL 30-11-0 DEFERRED DUE TO HISTORY AND RECENT REPLACEMENT OF SLAT 2 TEMP SENSOR.CAT C DUE 0SDR DALA2026052803242Bottle · low pressureR2 DOOR ASSIST LOW. SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. OK FOR SERVICE. (8834753) AIRCRAFT WAS GROUNDED.SDR AALA202605282358Diaphragm · leakingAIRCRAFT WAS GROUNDED: R2 EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE AT ZERO. MAINTENANCE FOUND THE DAMPER AND EMERGENCY OPERATION CYLINDER PERCUSSION MECHANISM DIAPHRAGM LEAKING AND REPLACED IT PER AMM 52-22-00.SDR AALA202605282858Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052003.SDR AALA202605288801Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: RIGHT AFT EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052003.SDR DALA2026052803240Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND (1 EA) ON RH CONTINUITY FITTING OF THE WINDSHIE LD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 5311-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RSDR DALA2026052803239Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L=0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONT SDR DALA2026052803238Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONTSDR DALA2026052803237Window Frame · crackedAIRCRAFT 3241, CRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE RH FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.079 INCHES, CRACK DIRECTION 2 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-02. AD RELATED, WORK CARD 531 1-01236-02. CORRECTIVE ACTION: PERSDR DALA2026052803230Window Frame · crackedAIRCRAFT 3236, DURING M2 CHECK AT AEM (SAL), WHILE EXECUTION OF HFEC INSPECTION OF THE WINDSHIELD CENTRAL NODE CONTINUITY FITTINGS AND WINDSHIELD FRAMES ON LH AND RH SIDES AS PER JOB CARD 5311-01226-01 (IN ORDER TO COMPLY WITH FAA AD 2020-17-03 AND SB A320-53-SDR QR9R2026052800001Bolt · crackedHEX BOLT FAILED NDI INSPECTION. CRACKED IN THREAD AREA AROUND COTTER KEY HOLE.SDR IPXA2026052888790Landing Gear · malfunctionedDIVERTED, LANDING GEAR WOULD NOT GO TO THE RETRACT POSITION.GEAR WOULD NOT RETREACT. DIVERT TO RFD REF T3F18E008VCC3, REPLACEMENT OF GEAR MICRO SWITCH (GEAR HANDLE) AND PROX DETECTOR UNIT. LANDING GEAR NORMAL EXTENSION AND RETRACTION TREATS NORMAL ON BOTH SYSSDR AALA202605286613Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5 AND LBL 9. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR AALA202605286105Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5 AND RBL 9. REPAIRED ANGLE PER SRM 57-10-10-2R-5.SDR UIEA2026052800367Light · inoperativeMULTIPLE OVERWING EMERGENCY LIGHTS INOP. REMOVED & REPLACED LIGHT ASSY IAW AMM 33-51-03. OPS CHECK GOOD.SDR FDEA202605280642Gust Lock · brokenL1 DOOR GUST LOCK BROKEN. REMOVED BROKEN PIECES OF GUST LOCK, BAGGED AND PLACED IN GALLEY COMPT WITH 02 DEMO MASK. NO ADDITIONAL DAMAGE FOUND. RELEASED FOR SERVICE PER MEL : 52-11-01-A COMPLIED WITH MEL PROCEDURES. A/C OK FOR SERVICE. REMOVED AND REPLASDR FDEA202605280641Hydraulic Line · leakingCLIMBING THROUGH FL200 COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM. DECLARED AN EMERGENCY AND RETURNED TO MEMPHIS. FOLLOWED QRH PROCEDURES, LANDED UNEVENTFULLY, AND WAS TOWED TO GATE. FOUND FLEX LINE GOING TO LH MANIFOLD-DUAL CONNECTING BLOCK DAMAGED. REMOVED SDR FDEA202605280640Gust Lock · damagedL1 DOOR HOLD OPEN LOCK IS BROKEN. TROUBLESHOOTING REQUIRED PRIOR TO INSTALLING IPC EFFECTIVITY VERIFICATION IS ALSO REQUIRED. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK COLLAR AND OPS CHKD GOOD IAW AMM 52-11-08-4.SDR 2026FA0000446Stiffener · crackedAFT FUSELAGE LOWER SKIN STIFFENER FOUND CRACKED. REPLACED WITH NEW STIFFENER.SDR 2026F00218Window · smokeDIVERTED FLIGHT TO SLCB ON ROUTE IQQ/VVI DUE TO SMOKE IN CABIN CONCKPIT. DURING CRUISE PHASE A SMELL CAME AND A SPARK GENERATED SMOKE FOR THE RIGHT WINDOW HEAT. CORRECTIVE ACTION: REMOVED AND REPLACED SIDE WINDOW RHSDR SWIA2026052777196Frame · corrodedBS 319 FRAME WAS CORRODED BTWN STR 20L - 21L. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-21 & 51-42-06. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.SDR 2026FA0000697Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEW.SDR 4VAA202605270028Skin · corrodedDURING INSPECTION, THE LEFT NACELLE INSIDE SKIN WAS FOUND CHAFED AND CORRODED. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.SDR SWIA2026052776823Roller · damagedLEFT WING SLAT TRACK 3-2, INBD FWD SIDE ROLLER DAMAGED. REMOVED AND REPLACED LT WING SLAT TRACK 3-2 INBD FWD SIDE ROLLERS, IAW AMMS 27-81-44-000-803 A01 AND 27-81-44-400-803-A01. ALL CHECKED GOOD.SDR SWIA2026052776819Roller · damagedRIGHT SLAT TRACK OTBD FWD SIDE ROLLER AT SLAT TRACK 1-2 DAMAGED OUT OF LIMITS. REMOVED INBD FWD SIDE ROLLER IAW AMM 27-81-44-000-801-A01. REINSTALLED INBD FWD SIDE ROLLER IAW AMM 27-81-44-400-801-A01. REMOVED INBD AFT SIDE ROLLER IAW AMM 27-81-44-000-801-A01.SDR SWIA2026052776818Roller · damagedRIGHT SLAT TRACK OTBD AFT SIDE ROLLER AT SLAT TRACK 2-2 DAMAGED OUT OF LIMITS. INSTALLED NEW OTBD AFT SIDE ROLLER AT RT SLAT TRACK 2-2. IAW AMM 27-81-44-400-802-A01. PERFORMED TWO OPS TESTS OF THE SLAT SYSTEM IAW AMM 27-50-00-710-801-A02. SLATS OPERATE SMOOSDR SWIA2026052776817Roller · damagedRIGHT SLAT TRACK INBOARD FORWARD SIDE ROLLER AT SLAT TRACK 3-2 DAMAGED/OUT OF LIMITS. INSTALLED A NEW INBD FWD SIDE ROLLER AT RT SLAT TRACK 3-2 IAW AMM 27-81-44-400-803, (CONFIG A01). PERFORMED TWO OPS TESTS OF THE SLAT SYSTEM IAW AMM 27-50-00-710-801-A02. SLSDR SWIA2026052776809Bracket · crackedLEFT UPPER TRANSCOWL OTBD -A- BRACKET CRACKED. REPLACED OTBD STAND OFF ANGLE ON LT UPPER TRANSCOWL, IAW EO CN624-2005, SNIEO S26 AND REO 670-54-21-971, REV. B.SDR SWIA2026052776799Stand Off · crackedLEFT UPPER TRANSCOWL INBD -A- BRACKET STANDOFF CRACKED. REPLACED INBD STAND-OFF ANGLE. ON LT UPPER TRANSCOWL, IAW REO 670-54-21-971, REV. B, & EO CN624-2005, SNIEO S27. SKY CARD 51-900-1002 SKY.SDR SWIA2026052776790Stand Off · crackedRIGHT UPPER TRANSCOWL INBD A BRACKET STANDOFF IS CRACKED. REPLACED INBB STAND-OFF ANGLE ON R/H UPPER TRANSCOWL, REF. EO CN624-2005 SNIEO S23 AND REO 670-54-21-971, REV. B 2023-11-28. COMPLIED WITH TAS CARD 51-900-1002-SKYSDR SWIA2026052776768Rivet · shearedLH UPPER TRANSCOWL Z STIFFENER RIVETS ARE SHEARED. REPAIRED UNDERLYING HOLES COMMON TO ZED STIFFENER CN624-2038-203 AND INNER PERFORATED SKIN ON LT UPPER TRANSCOWL IAW REO 670-54-21-1830, REV-.SDR REXA2026080401472Stringer · corrodedCORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R BTW FS 295 AND FS 310 AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUATED OUT OF LIMITS, THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-SDR REXA2026080401441Door Sill · corrodedCORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT. CORROSION ON LOWER SILL AT AFT BAGGAGE BAY DOOR CUT OUT WAS EVALUATED OUT LIMITS PER SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND 51-42-13-SDR REXA2026080401434Plate · corrodedCORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STGR24L AND STGR26L) OF FWD AND CTR DOOR LOWER SURROUND STRUCTURE AT FWD BAGGAGE BAY COMPARTMENT. DUE TO NOT ALLOWABLE CORROSION ON FWD AND AFT GUSSET PLATES ALSO CORROSION ON PLATES (BTW STGSDR REXA2026080401433Stringer · corrodedINITIAL INSPECTION: CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR18R FROM FS629 TO FS661 AND FROM FS661+62 TO FS661+90 AT FWD BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-SDR REXA2026080401432Stringer · corrodedINITIAL INSPECTION: CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND FROM FS597 TO FS613 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STGR20R (LONGITUDINAL JOINT AREA); FROM FS485 TO FS533, FROM FS565 TO FS581 AND FSDR REXA2026080401431Bracket · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND SUPPORT PLATE LSDR REXA2026080401430Stringer Splice · corrodedCORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR19R, BTW FS 437 AND FS 453 AND BTW FS 469 AND FS 485 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-21-03-101-007-A01SDR SWAA2026061507012Fan Cowl · crackedNUMBER 2 ENGINE O/B FAN COWL IS CRACKED AT FWD LOWER CORNER 3 INCHES FROM LEADING EDGE. REMOVED AND REPLACED PER AMM 71-11-02.SDR SWIA2026052776651Skin · dentedDURING JACKING PROCEDURES, TAIL JACK STAND SLIPPED OFF JACK PAD AND CAUSED A DENT RIGHT OF THE TAIL JACK PORT. REPAIRED DAMAGE ON REAR FUSELAGE CLOSE TO JACKING POINT IN BETWEEN STRINGERS 28R AND 29L, IAW ETD 2026-170-009310, REV.: A DISPOSTION 001- REAR FUSELSDR AALA202607060594Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR AALA202607066660Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR AALA202607063038Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR WEB AT FR 20 AND S23R. REPLACED WEB PER SRM 51-42-11.