Service difficulty reports
1,770,704 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 SWAA2026092514349Fuel Sys · faultedDURING CRUISE, NR 2 FUEL GAUGE PROGRESSED TO 400 LBS MORE THAN NR 1 TANK WITH CONSISTENTLY SLIGHTLY HIGHER FUEL FLOW. CROSSFED TO 200 LBS HIGHER IN NR 2 TANK, THEN NR 2 TANK EQUALIZED TO NR 1 TANK READINGS. SUSPECT INDICATING ERROR ON NR 2 TANK GAUGE. PERFOSDR SWAA2026092573795Light · inoperativeCABIN SIDEWALL LIGHTING ADJACENT TO ROWS 25, 26, 27 SEATS DEF WERE INOPERATIVE. R & R WINDOW LIGHTS AT ROWS 23DEF & ROW 16DEF IAW AMM 33-21-00.SDR SWAA2026092507623Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK M1673 IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M1673 IAW AMM 33-51-06-960-805. OPS TESTED GOOD.SDR SWAA2026092570312Sign · looseRIGHT EMERGENCY EXIT SIGN LOOSE. REPLACED EXIT SIGN IAW MM 33-51-01.SDR SWAA2026092591258Cradle · no testAFT CAPTAIN`S SIDE OTBD FA FLASHLIGHT WILL NOT TEST. REPLACED THE FLASHLIGHT BRACKET IAW AMM 25-64-00. OPS CHKD GOOD.SDR SWAA2026092587649Megaphone · no discrepancyF/A AFT MEGAPHONE NOT TESTING. P ERFORMED FUNCTIONAL CHECK OF F/A AFTER MEGAPHONE IAW MM 25-64-01, NO DEFECTS NOTED.SDR SWAA2026092538079Scuff Plate · crackedREMOVED THE R1 GALLEY DOOR LOWER MAIN SILL SCUFF PLATE FOR PERMANENT REPAIR IAW AMM 53-11-01. REPLACED THE SCUFF PLATE IAW 51-40-02. PERFORMED A CABIN PRESSURE LEAK TEST IAW AMM 05-51-91. LEAK TESTED GOOD.SDR SWAA2026092538116Light · unsecureRIGHT AFT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. SECURED RT AFT EMERGENCY DOOR COVER AND LIGHT IAW AMM 33-51-03. OPS CHECKED GOOD.SDR AALA202609254793Light · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT ROW 16ABC SEAT-MOUNTED EMERGENCY LIGHT IS INOPERABLE (OPEN)SDR AJXA2026092500048Flap System · warning messagePILOT REPORTED AMBER CAS MESSAGE FLAP FAIL AND DIVERTED TO KIAHSDR DXTA2026092509841Light · inoperativeEMERGENCY LIGHT TOE KICK SEAT 3 INOPERATIVE. REPLACED LIGHT BAR. OPS CHKD GOOD. IAW AMM 25-20-22-10.SDR DXTA2026092509835Strut · dischargedDURING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR INDICATED IN TRANSIT AND NEVER FULLY RETRACTED. LG LEVER DISAG CAS MESSAGE DISPLAYED. HYDRAULIC PRESSURE WAS NORMAL. ALL GEAR EXTENDED NORMALLY WHEN SELECTED DN. SERVICED NLG STRUT. OPS CHECK GOOD. IAW PHENOSDR CALA2026092519801Panel · missingFOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW AMM 54-57-22.SDR CALA2026092419800Module · faultedON TAKEOFF ROLL ENCOUNTERED AN OVHT/DET LIGHT AS WELL AS A FIRE WARN LIGHT AND BELL. ALL OF THE LIGHTS ILLUMINATED JUST LIKE WHEN THE OVHT FIRE TEST. WHEEL WELL LIGHT. ENGINE 1 ENGINE 2 AND APU FIRE BOTTLE DISCHARGE LIGHTS. ENGINE 1 AND EMGINE 2 OVERHEAT LIGHTSDR N6WA2026092407None · no discrepancyBIRD STRIKE ON T/O @100KTS. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-25. NO DAMAGE NOTED.SDR HNAA2026092500911Structure · damagedBIRD STRIKE TO L/H SIDE OF NOSE. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. REPAIRED IAW SRM 51-40-02, 51-40-06, CPM 51-21-04, AND 51-21-05SDR AALA202609248207Controller · inoperativeAIRCRAFT WAS GROUNDED: AUTO PRESSURIZATION AND ALTERNATE FAIL IN FLIGHT. QRH ACCOMPLISHED. AS A PRECAUTION EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CPC #2 #2 IAW AMM 21-31-01-400-801.SDR AALA202609245051Controller · inoperativeAIRCRAFT WAS GROUNDED: AUTO PRESSURIZATION AND ALTERNATE FAIL IN FLIGHT. QRH ACCOMPLISHED. AS A PRECAUTION EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CPC'S #1 IAW AMM 21-31-01-400-801.SDR AALA202609245386Oxygen Gen · activatedAIRCRAFT IN BASE MAINTENANCE: DOOR 4R OXYGEN GENERATOR FIRED. DOOR 4R OXYGEN GENERATOR REPLACED AS PER AMM 35-21-11 AND AFMM 20-11-11.SDR AALA202609245463Lamp · inoperativeAIRCRAFT IN BASE MAINTENANCE: DOOR 2L EXTERNAL EMERGENCY LIGHT DIM. DOOR 2L EXTERNAL EMERGENCY LIGHT LAMP REPLACED AND CHECKED IAW AMM 33-51-04.SDR AALA202609246226Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOD LIGHT ABOVE SEAT 6L INOP. RELAMPED IAW AMM 33-51-03.SDR AALA202609248832Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT AT RIGHT GALLEY F6, AFT SIDE INOP. RELAMPED IAW AMM 33-51-07.SDR AALA202609245012Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT OUTBD OF GALLEY F3, AFT SIDE INOP. RELAMPED IAW AMM 33-51-05.SDR AALA202609249969Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOD LIGHT ABOVE LAV 3F-2R INOP. RELAMPED IAW AMM 33-51-00.SDR AALA202609240693Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH LIGHT OUTBD OF FWD CLOSET, LEFT SIDE INOP. REMOVED AND REPLACED EMERGENCY LT ASSY IAW AMM 33-51-05.SDR DALA2026092405335Blades · dentedFOUND TWO BLADES DENTED ON NR 2 ENG. FOUND BLADES 29 AND 30 DENTS TO BE OUT OF LIMITS IAW AMM 72 -21-00-320-001-Q, DAMAGE EXCEEDS A DEPTH OF 1 INCH IN SECTION D INTO SECTION C. REROMVED SPINNER FRONT & REAR CONE IAW AMM 72-21 REMOVED AND REPLACED THE FAN BSDR CALA2026092419778Power Supply · faultedCHRONIC EMERGENCY EXIT LIGHTS AT OVERWING EXIT AND SEAT 20 AND 21 D,E,F ILLUMINATING RANDOMLY. REMOVED AND REPLACED POWER SUPPLY & BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.SDR CALA2026092419768Fitting · corrodedFRAME 68 HAS A DRILLED OUT FASTENER WITH CORROSION AROUND IT AFT CABIN. REMOVED AND REPLACED FITTING AT AFT CABIN FLOOR IAW SRM 51-42-11.SDR I5PA2026092168812Valve · faultyETOPS SIGNIFICANT REPORT, LT ENGINE PNEUMATIC HEALTH CHECK REQUIRED - PERFORMED PNEUMATIC HEALTH CHECK PER AMM, FOUND HPSOV FAULTY. REPLACED HPSOV PER AMMSDR YENA2026092300899Pylon · no discrepancyDURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RH PYLON; (RESOLVED ON W/O: 1477496 TASKCARD: NR-00012 ) FUR-A320-54-03371, REF AEROMAN N/R 2026-432556, PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE ENSDR YENA202609230089Pylon · no discrepancyDURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ON FWD MOUNT OF RT PYLON. PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RT PYLON IAW NTM 51-90-00 AND FOUND NO ELONGATED HOLE ONLY FOUND EXISTING REWORKSDR YENA2026092300898Floor Support · corrodedDURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT +Y1292, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, & DWG D53110876.SDR YENA2026092300897Floor Support · corrodedDURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, AND DWG D53110876.SDR YENA2026092300896Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT +Y765. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN FR 66 - 70 IAW SRM 51-72-11, SRM 51-42-11, DWG D53472794, DWG D53472777, AND DWG 53472809804.SDR YENA2026092300895Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 RT SIDE. CRACK DIRECTION IS 9 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERFORMED SDR YENA2026092300894Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE 7 LOCATED AT DOUBLE JOGGLE AREA, FR 20 R H SIDE. CRACK DIRECTION IS 3 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERMANESDR YENA2026092300893Frame · crackedDURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN DOUBLE JOGGLE AREA, FR 16. CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00. PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53SDR YENA2026092300892Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT -Y464.8 IN AFT GALLEY. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, & SRM 51-42-11.SDR YENA2026092300891Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION ON FLOORBEAM -Y765 IN THE AFT GALLEY AREA. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 51- 42-11, DWG D53472809, DWG D53472777, & DWG D53472195.SDR YENA2026092300890Fitting · corrodedDURING HEAVY MAINTENANCE, CORRODED CENTER FITTING, BTWN FR 66 - 68, STR 23R. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53480505.SDR YENA2026092300889Shear Plate · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR PLATE BTWN FRAMES 69 TO 70, STR 23R. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11, SRM 51-42-11, & DWG D53474180.SDR YENA2026092300888Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON EXTERNAL SKIN UPPER SURFACE BTWN RIBS 2 & 3, STR 11 RT WING. TOOK MEASURES OF CORROSION L= 1.023 IN, W= 0.826 IN, MEASURES AFTER REWORK ARE L= 2.780 IN, W= 2.418 IN. EVALUATED REWORK ON SKIN & FOUND WITHIN LIMITS IAW SSDR YENA2026092300887Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION UPPER SKIN, BTWN RIBS 8 & 9, LT WING T/E. MEASURES OF CORROSION ARE L=3.377IN W=1.465IN , REWORKED CORROSION ON LT WING UPPER SKIN IAW SRM 51-74-00 AND MEASURES AFTER REWORK ARE P1 L=4.042IN, W=2.842IN, EVALUATED REWORK &SDR YENA2026092300886Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON UPPER SKIN, BTWN RIBS 6 - 7, STRINGER 11, LT WING. REWORKED POINTS OF CORROSION (3E/A) IAW SRM 51-74-00, MEASURES OF POINTS OF CORROSION AFTER REWORK ARE P1 L= 1.858 IN, W= 1.232 IN, P2 L= 2.063 IN, W= 1.354, P3 L= 2.1SDR YENA2026092300885Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 30L, BTWN FR 61 - 62, IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 30L IAW SRM 53-00-13-300-001. THIS REPAIR IS CAT B.SDR YENA2026092300884Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 57 - 59 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 57 - 58 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.SDR YENA2026092300883Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 60 - 61. IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 +14 INCHES, & 2 INCHES AFT FACE OF FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.SDR YENA2026092300882Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L. BTWN FR 60 - 61 IN THE CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 + 14 INCHES & 2 INCHES AFT FACE FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B.SDR YENA2026092300881Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION IN STRINGER 33L, FR57 - 58 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L BTWN FR 57 - 58 IAW SRM 53-00-13-300-001. THIS REPAIR IS CLASSIFIED CATEGORY B.SDR YENA2026092300880Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 33L LOCATED AT FR59 IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L, FR 59 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B,