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 FDEA202605140595Skin · debondedLEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE SDR N6WA2026051511Skin · dentedDENT IN FUSE SKIN FS 1117 STRG 17R-18R. PERFORMED EXTERNAL PERMANENT REPAIR ON FUSELAGE SKIN FS 1117 STGR 17 - 18 RH IAW CRJ EO C550-53MR-122 REV. OSDR N6WA2026051508Buttstrap · corrodedPOSSIBLE CORROSION ON FS280 BETWEEN STGR27 AND STGR26RH NEEDS EVALUATION. PERFORMED REPAIR ON BUTT STRAP AT FS280 BETWEEN STGR21R AND STGR26L IAW STS EA 129-2026-096.SDR REXA2026051500587Lamp · inoperativeLAMPS INOP IN RIGHT EXIT ROW FLOOD LIGHT. R+R 5 LAMPS FROM RIGHT EXIT ROW FLOOD LIGHT REF AIPC 33-51-05 P/N: 6100928.SDR AALA202605157928Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: EMERGENCY DOOR DAMPER CYLINDER FOUND ON YELLOW SERVICE BAND ON RH EMERGENCY EXIT DOORS 843 AND 844. MAINTENANCE SERVICED EMERGENCY DOOR DAMPER CYLINER AT EMERGENCY RH EXIT DOORS 843 AND 844 WITH N2 GAS SERVICED TO GREEN BAND AS REQUISDR AALA202605155291Accumulator · low pressureAIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY CYLINDER PRESSURE LOW. 900 PSI, 80 DEGREES. MAINTENANCE SERVICED R1 ACCUMULATOR IAW J/C 26L80052001.SDR ABXA20260514204Bracket · missingDURING MAINTENANCE POST FLT INSP, PORTABLE ELT MISSING CABLE BETWEEN RED TAB & WALL BRACKET. REPLACED ELT BRACKET ASSY. (CABLE COMBS ATTACHED TO BRACKET) I.A.W. AMM 20-11-00. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR YENA2026051500461Battery · no testFLT 1752, SJU-TPA. EMERGENCY LIGHT BATTERY FIN 12WL FAILED TEST, REMOVED AND REPLACED EMERG LIGHT BATTERY FIN 13WL IAW AMM 33-51-38.SDR YENA2026051500460Battery · no testFLT 1501, JFK-FLL. EMERGENCY LIGHTS BY L1 DOOR NOT TURNING ON; R & R EPSU BATTERY ABOVE L1 DOOR REF 33-51-38 OPS CHECK GOOD.SDR YENA2026051500459Battery · failedFLT 1501, JFK-FLL. EMERGENCY LIGHTS ON L/H SIDE OF CABIN NOT TURNING ON, REMOVED AND REPLACED EPSU BATTERY L/H MID CABIN REF 33-51-38 OPS CHECK GOOD.SDR DALA2026051403010Bottle · low pressureSHIP 3413 AT DOOR 3L THERE IS A CHECK DOOR PRESSURE MESSAGE WITH AN AMBER INDICATION. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (8836800) AIRCRAFT WAS GROUNDED.SDR YENA2026051500457Warning Message · illuminatedFLT 1634, SFO-BOS. (ETOPS) CLASS II AIR BLEED MSG ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY AIR BLEED ) ; T/S PER TSM 36-00-00-810-804-A. SUBTASK (B) CYCLE OF FWC C/B'S. MESSAGE DOES NOT SHOW ANYSDR YENA2026051500456Fire Detector · illuminatedFLT 32, AMS-BOS. (ETOPS) ENG L FIRE LOOP B FAULT ECAM AFTER LANDING. ENGINE FIRE DETECTION SYSTEMS LOOP B. FAULT HAS NOT SHOWED IN 3 DAYS PER MCC AC OK FOR SVC REF LP 4398668 ITEM 1 (FOUND PYLON RAIL ASSY BROKEN. R & R PYLON FIRE DETECTOR RAIL ASSY IAW AMM SDR ABXA20260514202Lamp · inoperativeEQUIPMENT COOLING SMOKE DISCRETE LIGHT WON'T ILLUMINATE DURING TEST ON GROUND BY MTC. RELAMPED EQUIPMENT COOLING SMOKE DETECTOR LAMP PER B767 AMM 21-58-19. OPS CHECK SATISFACTORY. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR AALA202605150861Power Supply · no testAIRCRAFT IN BASE MAINTENANCE: BAT/EPSU (15WL) MID L FAILED DURING CIDS TEST. MAINTENANCE REPLACED EPSU BATTERY(15WL) IAW AMM 33-51-38.SDR AALA202605153262Power Supply · no testAIRCRAFT WAS NOT GROUNDED: BAT/EPSU (10WL) FWD L FAILED DURING CIDS TEST. MAINTENANCE REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38.SDR AALA202605156391Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY CYLINDER FOUND TO LOW PRESSURE. MAINTENANCE REPLACED EMERGENCY DAMPER CYLINDER DIAPHRAGM AT L1 PAX DOOR REF. AMM 52-10-00.SDR HNAA2026051500381Engine · failedENGINE #2 REV DISAGREE FOLLOWED BY ENGINE FAILURE ENGINE #2 SHUTOFF. ( OVERHEARD DISP SUPER HE WAS AT 1,000 FEET ABOVE THE GROUND ABOUT TO LAND WHEN THE ENGINE #2 FAILED ON HIM, HE DECLARED AN EMERGENCY BUT WAS ABLE TO LAND THE AIRCRAFT.) R & R ENGINE IAW W/C SDR SCNA20260515200Oven · dirtyAFT OVEN RACK TO SMALL SMOKEY AND NEEDS CLEANING. INFORMED CATERING FOR NEW OVEN INSERTS AND RACKSSDR SCNA20260515199A/C Pack · odorSTRONG ODOR OF JET FUEL WHEN TRANSITIONING TO APU BLEED AS PACK SOURCE AFTER LANDING. DISSIPATES WITHIN A COUPLE OF MINUTES. MC NOTIFIED. TURNED OFF PACKS FOR 5 MINUTES. RESUPPLIED CONDITIONED AIR TO THE AIRCRAFT IAW AMM 21-00-00. COULD NOT DUPLICATE SMELL OFSDR 2026FA0000383Flap System · asymetricTHE INITIAL SQUAWK WAS FOR THE FLAP ACTUATORS NOT LOCKING IN THE FULLY RETRACTED POSITION. THE FLAPS WOULD DROOP DURING TAXI AND/OR WHILE PARKED. DURING THE SERVICE EVENT. THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS SDR 2026FA0000371Flap System · asymetricINITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OFSDR 2026FA0000370Flap System · asymetricINITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OFSDR 2026FA0000369Flap System · asymetricINITIAL SQUAWK WAS FOR FLAPS NOT LOCKING IN THE UP POSITION. THE FLAPS WERE DROOPING WHILE TAXING OR PARKED. DURING SERVICE THE TECHNICIANS REPORTED THE FLAP ACTUATORS WERE UNLOCKING AT DIFFERENT PRESSURES. THIS WOULD CAUSE A MOMENTARY ASYMMETRIC DEPLOYMENT OFSDR UIEA2026051400320Repair · not reportedEXISITNG REPAIR ON FUSELAGE SKIN BETWEEN STA 1787 AND STA 1800, NEAR S-34R. REMOVED EXISTING PARTS IAW SRM 57-40-02-0G-0 REV 106. ACCOMPLISHED REPAIR ON THE FUSELAGE SKIN IAW EI T2026A53M-976 REV 1. JOB ACCOMPLISHED AND CONDITION CHECK NORMAL.SDR QR9R2026051400001Control Lever · out of limitsRECEIVED FROM AIRBUS UNSERVICEABLE. MEASURED .026'' AROUND SLIP BUSHING, MAX ALLOWED IS .019".SDR 2026FA0000364Windshield · failedLH WINDSHIELD SHATTERED DURING CLIMB PASSING THROUGH FL 280 AIRSPEED 280 KNTS. OATAPPROXIMATELY -34 DEGREES C. NO IMPACT OBSERVED TO CAUSE BREAK.SDR 2026FA0000363Windshield · failedLH WINDSHIELD SHATTERED DURING CLIMB PASSING THROUGH FL 280 AIRSPEED 280 KNTS. OAT APPROXIMATELY -34 DEGREES C. NO IMPACT OBSERVED TO CAUSE BREAK.SDR CALA2026051416254Control Unit · faultySAFA INSPECTION FOUND FLOOR PROXIMITY LIGHTNING AT SEATS 30, 31 AND 32 INOP ON BOTH SIDES. FULL EMERGENCY LIGHT GROUND TEST SHOWS FAULT 33-11624 LOCKED FOR MX FERRY SLAVED WCU 26 FROM SEAT 39D INTO WCU 24 POSITION AT SEAT 22D, NO JOY. INSTALLED WCU IN ORIGINALSDR CALA2026051416252Smoke Detector · faultedLAV T SMOKE DETECTOR CHIM VERY LOW. REMOVED AND REPLACED LAV D SMOKE DETECTOR IAW AMM 26-14-01-000/400-802, OPS CK GOOD.SDR CALA2026051416250Smoke Detector · faultedLAV E SMOKE DETECTOR CHIM VERY LOW. REMOVED AND REPLACED LAV E SMOKE DETECTOR IAW AMM 26-14-01-000/400-802, OPS CK GOOD.SDR ABXA20260514200Generator · faultedDURING TAXI, APU RANDOMLY DROPS OUT ON PUSHBACK (2 TIMES). CREW RETURNED TO GATE (BTB). MTC DEFERRED APU GENERATOR IAW ABX MEL 24-00-2A NO DEACTIVATION REQUIRED PLACARD INSTALLED AC REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR JR2R20260514222Floorbeam · corrodedFWD WET AREA LH FR17 CROSSBEAM FLOOR SUPPORT CORRODED. REPLACEDSDR SWIA2026051377298Mount · gougedRIGHT WING HINGE BOX AT WS 178 WAS GOUGED ON AFT WING MOUNT FITTING. BLENDED DAMAGE TO A SMOOTH CONTOUR AT RT WING HINGE BOX AT WS 178 AFT WING MOUNT FITTING AND REPAIRED IN COMPLIANCE WITH STEPS 1-5 OF REO 601R-57-21-4095, REV -.SDR 4VAA202605130035Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PRESSURE BULKHEAD AFT ANGLE. THE ANGLE WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060703.SDR 4VAA202605130026Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR SUPPORT. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060641.SDR 4VAA202605130025Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT HAND NACELLE FIRE FLOOR ANGLE. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060704.SDR 4VAA202605130023Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE WEB ABOVE THE CARGO DOOR. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060682.SDR SWIA2026051376997Hinge · nickedTHE RUDDER'S MIDDLE BOTTOM HINGE IS NICKED AND CHAFED ON ITS TOP LUG. REPAIRED RUDDER PCU HINGE FITTING BY COMPLYING WITH ALL REPAIR STEPS PROVIDED IN REO 601R-55-41-319, REV-.SDR SWIA2026051376991Hinge · chafedTHE RUDDER'S MIDDLE CENTER HINGE IS CHAFED BETWEEN THE LUGS. REPAIRED RUDDER PCU HINGE FITTING BY COMPLYING WITH ALL REPAIR STEPS PROVIDED IN REO 601R-55-41-319 REV-.SDR SWIA2026051376990Hinge · damagedLEFT WING SIDE AILERON HINGE NR 4 INBD HAS A PREVIOUSLY OVER SIZED LUG LABELED -G-. CURRENT LUG INTERNAL DIAMETER MEASURES 0.8270. NOMINAL LUG INTERNAL DIAMETER IS 0.8120. FABRICATED AND INSTALLED BUSHINGS ON LT WING SIDE AILERON HINGE NR 4 IAW REO 601R-57-5SDR SWIA2026051376873Skin · dentedADM N796SK-9240 MCD TWO DENTS ON OUTER SKIN 24.5" FROM TOP, 11" FROM FRONT LEADING EDGE. 1ST DENT IS 11.5" FROM LEADING EDGE OF DOOR .750" TALL, .187" WIDE, .025" DEEP. 2ND DENT IS 11.0" FROM LEADING EDGE OF DOOR 1.250" TALL, .375" WIDE, .115" DEEP. SRM 52-11SDR SWAA2026061598287Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK LBL 25 WL 208 STA 500A+10 WELL; STA 500D+10 TOP; STA 500D+10 WELL. REMOVED AND REPLACED SEAT TRACK AT 480-520 LBL25 IAW SRM 51-40-02-0G-0 AND EA 26-153-01350.SDR SWAA2026061598289Rib · crackedCRACKED RIB RT INSPAR HORIZ STAB STA 120.30 COMMON TO UPPER RETURN FLANGE AND FWD SPAR. REPAIRED PER EA 26-155-01306. THIS IS A CATEGORY A REPAIR IAW SRM 51-00-06.SDR SWAA2026071398281Attach Angle · crackedLEFT AC BAY BS 663, LBL 9 HAD A CRACK ON THE VAPOR BARRIER ATTACH ANGLE, HFEC VERIFIED. CW EA 26-157-01403.SDR SWIA2026051376414Floor Support · crackedRT COCKPIT FLOOR SUPPORT ANGLE BETWEEN BS 265 - 280 CRACKED. REMOVED AND REPLACED WITH NEW RT COCKPIT FLOOR SUPPORT ANGLE BETWEEN BS 265 - 280 IAW SRM 51-42-21-001-001-A01 REV 380, SRM 51-42-06-001-001-A01 REV 38& DWG CC670-34010 REV -K. COMPLIED WITH ALL STSDR SWIA2026051376397Floor Support · crackedLEFT COCKPIT FLOOR SUPPORT ANGLE BETWEEN FS 265.00 - FS 280.00 HAS CRACK. REMOVED AND REPLACED WITH NEW LT COCKPIT FLOOR SUPPORT ANGLE BETWEEN BS 265 - 280 IAW SRM 51-42-21-001-001-A01 REV 38, SRM 51-42-06-001-001-A01 REV 38 & DWG CC670-34010 REV -K. COMPLIESDR SWIA2026051376394Stringer · corrodedCORROSION ON STGR 23L BETWEEN FS517 AND FS533. REMOVED AND REPLACED CORRODED STGR23L BETWEEN FS517.00 AND FS533.00 WITH NEW STRINGER (P/N SH670-33225-1A) USING ALL NEW FASTENERS, REF MHIRJ REO 670-53-31-1209 REV--, DATED 2026-06-09. COMPLIED WITH NOTES 20 ANDSDR SWAA2026062998078Skin · debondedPANEL 192AL OUTER SKIN IS DISBONDED. REPAIRED OUTER SKIN DISBOND IAW SRM 51-70-05-2R-2-A00733. (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRAME - PERMANENT)SDR SWAA2026062901514Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK RBL 39, BS 663+2, L: 0.300. REPAIRED HORIZONTAL PRESSURE DECK AT BS 663 - BS 675; RBL 39 - RBL 62 IAW SRM 53-40-51-2R-2, REPAIR 2.