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 AALA202605041145Power Supply · faultyAIRCRAFT WAS NOT GROUNDED: DURING J/C 26L00025011 FOUND FWD EPSU BATTERY FAULT. MAINTENANCE REPLACED FWD EPSU AND FWD EPSU BATTERY IAW AMM 33-51-38.SDR WX0A2026050432804Epsu · failed(AIRCRAFT NOT GROUNDED) DURING WEEKLY FOUND EPSU (11WL) EMER L MESSAGE. REMOVED AND REPLACED EPSU BATTERY WITH REPAIRED BATTERY IAW AMM 33-51-38-000/400-002-A. OPS CHECK GOODSDR WX0A2026050432803Epsu · no test(AIRCRAFT NOT GROUNED) DURING EPSU BATTERY TEST, EPSU 11WL FAILED / REMOVED AND REPLACED EPSU (11WL) IAW AMM 33-51-38-000/400-002-A"SDR WX0A2026050432802Epsu · faulted(AIRCRAFT NOT GROUNED) DURING WEEKLY INSP (W/O 549885), FOUND EPSU SYS TEST FAILS, EPSU 11WL EMER LIGHT. PERFORMED TSM 33-51-00-810-822-A, OBSERVED DURING TEST RED EXTERIOR LIGHTS FAULT ILLUMINATED. REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A / AMM 33-SDR 2026FA0000316Intake Duct · looseON 3 MAY 2026, APPROXIMATELY 11:55 AM, N123NP DEPARTED BIL FOR FBL AND FOUND THAT THE RIGHT ENGINE WOULDN'T MAKE RED LINE MAP AND ABORTED HIS TAKEOFF. MAINTENANCE FOUND A COUPLE INDUCTION TUBE CLAMPS LOOSE. THE MECHANIC TIGHTENED BOTH CLAMPS AND AND THE PILOT SDR DALA2026050402790Compressor · stalledFLT. 0431 ATB-DEN-ATL DECLARED AN EMERGENCY AND RETURNED TO DEN DUE TO RIGHT ENGINE COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION WITH NO FINDINGS. IP CHECK VALVE REMOVED AND REPLACED, OPS CHECK NORMAL. (LP 8699470, 8699472 - AIRCRAFT WAS GROUSDR FDEA202605030535Door · no discrepancyWHEN ARRIVED AT A/C TO MOVE JET POST B-CHECK FOUND R1 OUTER DOOR HANDLE INOPERATIVE. OPERATED DOOR SEVERAL TIMES THROUGH FULL RANGE OF LATCHING MOTION USING OUTER HANDLE . DOOR HANDLE CYLED, LATCHED AND FUNCTIONED AS REQUIRED EACH TIME. COULD NOT DUPLICATSDR FDEA202605030534Skin · dentedFOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 127 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGSDR FDEA202605030533Skin · dentedFOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 231 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGUSDR SCNA20260504184Battery Pack · inoperativeFWD CABIN LT SIDE EMERGENCY LIGHTS INOP. R & R LT FWD CABIN EMERGENCY LIGHT CHARGER ASSY IAW AMM 33-51-06-960-806 AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD AT THIS TIME.SDR SCNA20260504183Battery Pack · inoperativeFWD R/H SECTION OF EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED LONGER THAN 30 SECONDS. R & R BATTERY PACK IAW AMM 33-51-06-960-805, OPS CHECK GOOD AT THIS TIME.SDR SCNA20260504182Retainer · out of limits-FWD ENTRY EMERGENCY ESCAPE SYSTEM COMPARTMENT RETAINER CLIPS WITH MEASUREMENTS OUT OF LIMITS.SDR SCNA20260504181Girt Bar · bentUPPER FUSELAGE, FWD GALLEY EMERGENCY ESCAPE SLIDE PACK, GIRT BAR RETAINER CLIPS (2EA) BENT AND WITH DEFORMATION. WORK ACCOMPLISHED: WO 90084 NR13: REPLACED GIRT BAR RETAINER CLIPS (2EA) LOCATED AT FWD GALLEY EMERGENCY ESCAPE SLIDE PACK IAW BCF SRM 51-10-02SDR SCNA20260504180Door Frame · damagedFWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING WITH SHARP EDGES. DEBURRED SHARP EGES LOCATED AT FWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING IAW AC5300-1 SECTION 11-2-2 REV K DATED 05-11-2018SDR SCNA20260504179Lamp · inoperativeRIGHT FWD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. CHECKS GOOD. REF MM 33-51-04.SDR SCNA20260504178Potable Water · contaminatedWATER HAS A TOXIC SMELL. COFFEE/ HOT WATER SMELLS LIKE CHLORINE AND HAS A CHECMICAL TASTE AND MAKES EYES BURN. SERVICED POTABLE WATER SYSTEMPER AMM 38-42-00-800-802.NO SMELLED FOUND. FLUSHED POTABLE WATER SYSTEM AND RESERVICED PER AMM 38-10-00-860-005.SDR JR2R20260503364Handle · chafedFWD ENTRY DOOR CHAFED ON DOOR HANDLE AND HANDLE CUTOUT. REPAIRED.SDR JR2R20260503363Handle · chafedFWD ENTRY DOOR CHAFED ON DOOR HANDLE AND HANDLE CUTOUT. REPAIRSDR JR2R20260503796Rib · corrodedLEFT WING NR 1 MAIN FLAP INSIDE TORQUE TUBE ACCESS PANEL, CORRODED AFT OF 3RD NUTPLATE. REPAIRED.SDR JR2R20260503814Beam · corrodedAFT WET AREA RBL11 FR84 CORRODED FASTENER / BEAM. REPAIRED.SDR JR2R20260503920Panel · corroded195ML PANEL CORRODED. REPAIRED.SDR JR2R20260503821Gusset · corrodedAFT WET AREA FR90 LBL0 CENTER GUSSET CORRODED. REPLACEDSDR JR2R20260503805Fitting · corrodedFORWARD WET AREA, FR16 LH FLOOR FITTING CORRODED. REPAIRED.SDR JR2R20260503813Fitting · corrodedFORWARD WET AREA FLOOR FITTING LBL30 - 36 BETWEEN FR19 AND FR20 CORRODED. REPAIREDSDR SWIA2026050277509Angle · damagedDURING INSTALLATION OF FASTENERS EDGE DAMAGE CREATED ON REINFORCEMENT ANGLE BS 333, BETWEEN STR 21R TO 22R. REPAIRED REINFORCEMENT ANGLE IAW REO 670-53-21-2883, REV -.SDR REXA2026070301008Angle · corrodedCORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE DUE TO EXCESSIVE CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE (KICKPLATE) WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01SDR REXA2026070301005Rib · crackedCRACK ON PARTIAL RIB AT LEFT INBOARD FIXED LEADING EDGE SS27.75 PARTIAL RIB AT LEFT INBD FIXED LEADING EDGE SS27.75 WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01.SDR SWIA2026050276425Door Sill · corrodedSERVICE DOOR SURROUND LOWER SILL CORRODED AT FORWARD DOOR STOP FITTING. REMOVED AND INSTALLED NEW ONE MOUNTING ANGLE AND SEAL STRIKER IAW SRM 51-42-06-001-001-A01 AND DWG. SH670-31950 REV Y. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR R61A2026050200162Elec Connector · disconnectedEMERGENCY LIGHT ON CEILING BETWEEN ROW 8 IS INOP. FOUND ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED.SDR 2026FA0000500Fuel Control · failedLEFT ENGINE ROLL BACK AT FL410, CO-PILOT ENGAGED FUEL BOOST PUMP AND DIVERTED TO KICT. TROUBLESHOT DOWN TO FAULTY FUEL CONTROL, REMOVED AND REPLACED.SDR DALA2026060903469Rib · corrodedLH WING / EM 5753-01164 / GEAR RIB 6 / FWD LUG CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 632580-14AD. (1573516) AIRCRAFT WAS GROUNDED.SDR SWAA2026060894902Support Bracket · corrodedCORROSION ON SUPPORT BRACKET FOR THE WATER SERVICE DOOR. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 147A7221, SHEET 23, REV -.SDR IPXA2026051584157Stringer · crackedSTRINGER CRACKED, AFT SIDE OF STA 2180 S-36R. ACCOMPLISH THE REPAIR I.A.W SRM 53-60-03-2R-3 REV.48 AND EGAT EI NO.F2026A53M-1159 REV.0 AND EGAT WORK SHEET NO.60346 AND UPS EO-97410-REQ0019 REV.1SDR SWAA2026060394989Scuff Plate · crackedCRACK ON SCUFF PLATE FWD SERVICE DOOR. REPAIRED THE SCUFF PLATE FWD SERVICE DOOR IAW BOEING SRM 53-10-15-2R-2; REPAIR 2 PARAGRAPH 4.B. AND BAC 5975.SDR HNAA2026060200470Seat Track · corrodedF124214 LH OTBD #6 SEAT TRACK HAS CORROSION ON MULTIPLE SPOTS. REMOVED AND REPLACED LH OTBD #6 SEAT TRACK IAW EMB 145 AMM 53-01-06.SDR SWAA2026060194855Rib · crackedCRACKED TRAILING EDGE ON DEFLECTION CONTROL RIB ORSS 280 AT RT WING. PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB AT RT WING IAW SRM 57-51-02-2R-3 REPAIR 3.SDR SWAA2026060194856Web · crackedCRACK WEB TRAILING EDGE LOCATED ORSS 261 TO ORSS 280 LT WING. REPLACED WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 280 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.SDR SWAA2026060194857Access Panel · crackedCRACK SEAL BLADE ACCESS PANEL 441AL AT RT PYLON. REPLACED SEAL BLADE LOCATED ON ACCESS PANEL 441AL AT RT PYLON IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SDR SWAA2026052894991Filler · crackedCRACK ON EXISTING REPAIR AT EXTERNAL POWER ACCESS DOOR CUTOUT. REPLACED FILLER LOC. AT EXTERNAL POWER ACCESS DOOR CUTOUT LOWER SIDE IAW SRM 51-10-02; SRM 51-40-02 AND SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204 SHEET 3 AND 4; ZONE 2; ALTERNATIVE 2.<SDR SWAA2026052894913Angle · crackedCRACKED ANGLE, BS 400, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, AND DWG 143A7505, SHEET 117, REV -.SDR SWAA2026052894912Gusset · crackedCRACKED GUSSET, BS 500D, STR 19R, IN THE FWD CARGO BAY. REPLACED THE GUSSET IAW SRM 51-10-02 AND SRM 51-40-02 AND DWG 143A7902, SHEET 259, REV-.SDR SWAA2026052894914Gusset · crackedCRACKED GUSSET, BS500D, STR 19L IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A7902, SHEET 259, REV -.SDR SWAA2026052894992Drain Mast · crackedCRACK APU DRAIN MAST ASSY ACCESS PANEL 194FL AT LOWER FUSELAGE. REPLACED APU DRAIN MAST ASSY ACCESS PANEL 194FL AT LOWER FUSELAGE IAW AMM 28-25-07-020-801 AND AMM 28-25-07-420-801.SDR AALA202605289829Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT STA 500I BETWEEN LBL 24 AND RBL 24. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.SDR AALA202605281968Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL AT STA 500B PLUS 19 INCHES AND AT RBL 24. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR SWAA2026052694951Skin · crackedFUSELAGE HAS A .45 VERTICAL CRACK AT BS 727A; APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. .26-153-01210SDR SWAA2026052694952Skin · crackedFUSELAGE HAS A .95 VERTICAL CRACK AT BS 727B; APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. REFER TO FAULT TTG8Q01BZXU WHERE EA 26-153-01210 WAS ADDED AS A SUBTASK. SDR SWAA2026052694953Skin · crackedFUSELAGE HAS A .50 VERTICAL CRACK AT BS 727D APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02<[01] REFER TO FAULT TTG8Q01BZCYK WHERE EA 26-153-01211 WAS ADDED AS A SUBTASSDR SWAA2026052694954Skin · crackedFUSELAGE HAS A .72 VERTICAL CRACK AT BS 727E APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. C\W 26-153-01211.SDR SWAA2026052694660Skin · crackedSUSPECTED CRACK AT BS727A AND APPROX 3IN ABOVE S14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED PAINT FROM BS727A APPROX 3 IN ABOVE STR14R<BR>REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6, 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRA