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 CALA2026080518303Retainer · crackedCRACKED LT WING T/E DEFLECTION CONTROL RIB FIXED PANEL LOWER HORIZONTAL BULB SEAL WEB RETAINER OTBD END. R & R THE RETAINER AT L/W T/E DEFLECTION CONTROL RIB FIXED PANEL LOWER HORIZONTAL IAW SRM 51-40-02-0G-0, AND DWG 115A2512.SDR CALA2026080518301Floorbeam · corrodedFWD OF R2 DOOR AREA FLOORBEAM APPROX RBL 45.5 BS 947 HAD CORROSION, ACCOMPLISHED PERMANENT REPAIR TO THE FLOORBEAM BS 947.5 RBL 35 - 59 IAW ESR-WI 9-15473 , ECRA 5370-01246 AND SRM 53-70-51-2R-5, REP 5, ALTENATIVE 2, FIG 206.SDR CALA2026080518298Lamp · inoperativeL4 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04, OPS CHKD GOOD.SDR CALA2026080518297Lamp · corrodedDURING EMERGENCY LIGHT TEST, PTP SHOWS FAULT EPSU EXT LOAD EMER. RESET POWER TO ASSOCIATED EPSU. NO FIX. COMPLETED BITE OF EPSU UNIT IAW TSM 33-51-00-810-822-A. BITE SHOWED EXTERIOR LIGHTS FAULT. WIRING CHECKED IAW TSM 33-51-00-810-822-A, FOUND RED LED EXSDR CALA2026080518296Light · splitDURING OPS CHECK OF THE EMERGENCY POWER SUPPLY UNITS PTP DISPLAYS FAULT MESSAGE EPSU EXT LOAD EMR R. FOUND AFT RT OVERWING LIGHT TO BE BURNED OUT. WHEN INSPECTING THE LIGHT FOUND LIGHT HOUSING SPLIT IN HALF. REPLACED OVERWING LIGHT ASSY IAW AMM 33-51-15-400-SDR CALA2026080518295Smoke Detector · no discrepancySMOKE ODOR CONDITIONAL INSPECTION REQUIRED IAW AMM 05-51-XX DUE TO AN INCIDENT REPORTED BY THE CREW. REAR LAVATORY SMOKE DETECTOR TRIGGERED AND FIRE PROTECTION ACTIVATED ALARM WENT OFF DUE TO ACCIDENTAL DISCHARGE OF SUBSTANCE. INSPECTED LAVATORY ALL CHKS GOODSDR CALA2026080518290Rib · crackedLEFT WING, DURING OK TO CLOSE OF ACCESS PANEL 524AT, OBSERVED THE END RIB CRACKED AT NR 3 SLAT. OSS 684 - 043 (INBD END OF SLAT 3). REMOVED, FABRICATED, & INSTALLED THE RIB, WAS ACCOMPLISHED IAW NR 3601211.SDR CALA2026080518288Profile · corrodedAFT CARGO, FR 63-65, S38R FLOOR PROFILE HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOOR PROFILE PANEL IAW SRM 51-42-11/001.SDR CALA2026080518286Profile · corrodedFWD CARGO, RT PROFILE PANEL AT S38R, FR 30 CORRODED. REMOVED AND REPLACED THE FLOOR PROFILE PANEL IN THE FWD CARGO IAW AMM 25-54-41-00-001A.SDR CALA2026080518284Battery · dischargedFWD FLASHLIGHT BLINKING RED AND INOP. FOUND FLASHLIGHT BATTERY DISCHARGED. REPLACED BATTERY AND RESEALED. OPS CHECKED NORMAL.SDR CALA2026080518282Profile · corrodedAFT CARGO FR 54 - 52 S35R MIDDLE FLOOR PROFILE HAS MULTIPLE SPOTS OF CORROSION. INSTALLED THE PROFILE AND PROTECTED REPAIR AREA IAW SRM 51-42-11.SDR CALA2026080518280Profile · corrodedAFT CARGO BAY, PROFILE FR 65 S38L-38R WAS CORRODED. REMOVED AND REPLACED PROFILE PANEL IN AFT CARGO FR65 STR 38L TO 38R IAW SRM 51-42-11/001.SDR CALA2026080518278Air Filter · faultySTRONG DIRTY ODOR FROM AIR CON, STARTED AROUND 15K FT & LASTED UNTIL LANDING. FOUND OIL PUDDLE IN AFT TURBINE SECTION ON NR 1 ENGINE. PERFORM CONDITION INSP IAW AMM 05-51-26-800-801 -C1 ODOR STILL PRESET NOT AS STRONG WITH RT PACK OFF, NO SMOKE ODOR. ABSERSDR CALA2026080518276Bulb · no testEMERGENCY LIGHTS OPS CHECKED, LT OVERWING, FWD EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB, OPS CHECKED GOOD.SDR JR2R20250804140Cam · chafedFWD CARGO DOOR, BOTH FWD AND AFT VENT FLAP CAMS ARE CHAFED OUT OF LIMITS. REPAIREDSDR 2026FA0000618Pump · failedENGINE DRIVEN FUEL PUMP FAILURE ALLOWED FUEL TO FLOOD ENGINE CRANKCASE. FOUND ON GROUND BEFORE FLIGHT.SDR AALA202608046997Connector · disconnectedAIRCRAFT WAS NOT GROUNDED: SEAT ROW 13ABC EMERGENCY LIGHT ON SEAT INOPERATIVE. MAINTENANCE FOUND THE L1 AND K3 HARNESS WAS DISCONNECTED UNDERNEATH THE SEATS AT THE FLOORBOARD - SIDEALLW THRESHOLD AND RECONNECTED THE ELECTRICAL CONNECTOR PER AMM 33-51-00. A SATSDR AALA202608047557Sign · disconnectedAIRCRAFT WAS NOT GROUNDED: ROW 11 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY EXIT SIGN UNPLUGGED AND PLUGGED IN THE SIGN PER AMM 33-51-16SDR AALA202608048569Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001SDR AALA202608040697Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L2 EMERGENCY EXIT DOOR DAMPER REQUIRES SERVICING. MAINTENANCE SERVICED L2 EMERGENCY EXIT DOOR DAMPER PER JC 26L80052003.SDR 141A2026080400001Circuit Breaker · trippedLEFT VENT BLOWER CIRCUIT BREAKER POPPED OUT. SMELL OF SMOKE IN COCKPIT. DID A GATE RETURN.SDR EE4Y2026080424824Fitting · damagedDURING THE EXECUTION OF ALLEGIANT WORK CARD A32X-25-127-003/001 AT THE LOWER FUSELAGE, E&E COMPARTMENT: IT WAS FOUND OVALIZATION ON THE 80VU RACK L/H AND R/H LOWER LATERAL FITTINGS. REPAIR ACTION ACCOMPLISHED: PER CUSTOMER EO A32X-STR-25-EO-00203. REV 01 AD202SDR HNAA2026080400646Bleed Air Sys · leakingCREW NOTIFIED CLT MX OF EXHAUST FUMES IN COCKPIT. CLT MX CREW REPORTED SMELL IN COCKPIT, CABIN NORMAL, FUTHER TROUBLESHOOTING FOUND APU BLEED CAUSE OF FUMES AND WAS PUT ON MEL. A/C DEPARTED WITH NO FURTHER ISSUES IN FLIGHT.SDR JR2R20260804573Mount · scratchedSTARLINK MOUNTING AREA SCRATCHES ON DOUBLER. REPAIRSDR FDEA202608041082Battery · failedBETWEEN 16-18000 FT GOT LT, RT, & CENTER IRS DC FAILED. TRIED STARTING APU TO VERIFY HOT BATTERY BUS STILL WORKING. WHEN APU REACHED SPEED GOT EICAS APU FUEL VALVE & RT FUEL SPAR VALVE. MAIN BATTERY CHARGER MSG ILLUMINATED. BTWN IRU FAILS & EICAS MGS NOTICESDR FDEA202608041081Skin · abnormalRIGHT HAND WING DROOPED LEADING EDGE UPPER AFT SURFACE FOUND WITH EXISTING REPAIR XDLE 329.774. RIGHT HAND WING DROOPED LEADING EDGE UPPER AFT SURFACE EXISTING REPAIR AT XDLE 329.774 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-01-2R FIGURE 20SDR ABXA20260804347Module · defectiveAT APPROXIMATELY 300FT AGL THE FLIGHT CREW RECEIVED THE AURAL WARNING, TOO LOW, FLAPS. BOTH THE FO AND PILOT CONFIRMED FLAPS 25 WAS INDICATED. THE PILOT CALLED FOR A GO-AROUND ANYWAY AND THEY EXECUTED A MISSED APPROACH. THE SECOND APPROACH RESULTED IN A SAFESDR KCSA202608041105Angle · crackedNR 5 LT OTBD AILERON HINGE FITTING LOWER ANGLE CRACKED AT FWD END. APPROX WS 1310SDR SWIA2026080377541Frame · corrodedFS1015 FOUND TO HAVE CORROSION BETWEEN STGR 27 TO 25L, STGR 22L TO 21L REQUIRES REPLACEMENT C-CHECK RO 10062026REPLACED FRAME FS1015 BETWEEN STRINGER 26R TO 19L IAW REO 670-53-61-2744 REV-- DATED 2026-08-11 AND CRJ-700 SRM 51-42-06-001-001-A01 AND 51-24-36SDR COEA2026092809807Skin Panel · dentedWO 275319 NR 3 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE SKIN BETWEEN FRAMES 5-6 STRINGERS 11R-12R DENTED. CORRECTIVE ACTION: REPAIRED PER SRAS-00054254-01 ISSUE A, DATED 8/18/2026.SDR AALA202609241034Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOCATED ON STRINGER 26L, AROUND FASTENER HOLE APPROXIMATELY STA 819. STRINGER P/N 146A-3233-47 REPLACED IAW AARD 51-00-05, SRM 53-00-03-2R AND BOEING DWG 146A3230.SDR AALA202609231034Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LOCATED ON STRINGER 26L, AROUND FASTENER HOLE APPROXIMATELY STA 819. STRINGER P/N 146A-3233-47 REPLACED IAW AARD 51-00-05, SRM 53-00-03-2R AND BOEING DWG 146A3230.SDR CNMA2026080006Floorbeam · corrodedCORRODED FLOORBEAM AT BS 1197+132 APPROX BELOW AFT CARGO COMPARTMENTSDR REXA2026091601817Skin · crackedCRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL. SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL WAS REPAIRED PER EA CRJ952-22930 REV BSDR REXA2026091601816Skin · crackedCRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL WAS REPAIRED PER EA CRJ952-22930 REV BSDR MASA202609142026Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF CFIII WET AREA, CORRODED FLLOR SUPPORT PANEL, AT FR88 TO FR90 L/H, LBL 45. REMOVED AND REPLACED IAW SRM 51-41-01, AND SRM 51-43-01. NRC 4502680-1000-0057. REV 45, AND REV 46.SDR REXA2026091001784Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS RBL9 BTW FS349 TO FS485 AT PAX CABIN. FLOOR SEAT RAILS RBL9 BTW FS349 TO FS485 AT PAX CABIN WAS REPLACED PER CRJ-900 AMM 53-00-49.SDR SWAA2026090826109Tie Clip · crackedCRACKED TIE CLIP, BS 277 STR 8R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 141A1110, SHEET 55, REV -, AND DWG 141A8380, SHEET 33, REV-.SDR SWAA2026090871291Tie Clip · crackedCRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-40-02, DWG 141A1110, SHEET 55, REV -, & DWG 141A8380, SHEET 21, REV -.SDR SWAA2026090836458Plate · crackedCRACK TRAILING EDGE CORRUGATED PLATE AT LEVEL ORSS 219 AT RT WINGREPLACED TRAILING EDGE CORRUGATED PLATE AT LEVEL ORSS 219 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG 115A2001 SHEET 78 REV A. DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM 57-51-02-1A-1.SDR SIMA2026090803003Seat Track · chafedCENTER FUSELAGE III RH LATERAL SEAT TRACKS HAS MULTIPLE AREAS OF SCRATCHES AND CHAFFING ON TEETH, CENTER AND EDGES, ALONG ENTIRE LENGTH. (MAJOR REPAIR). BLENDED DAMAGED AREAS ON CENTER FUSELAGE III RH LATERAL SEAT TRACK PER SRM 51-10-03. DEEPEST BLENDED AREA OSDR SIMA2026090803002Seat Track · corrodedLEVEL 2 CORROSION CENTER FUSELAGE III LH LONGITUDNAL SEAT TRACK HAS MULTIPLE AREAS OF CORROSION, SCRATCHES AND CHAFFING ON TEETH, CENTER AND EDGES, ALONG ENTIRE LENGTH. (MAJOR REPAIR). BLENDED MULTIPLE AREAS OF CORROSION ON CENTER FUSELAGE III LH LONGITUDINAL SDR SIMA2026090803004Seat Track · corrodedLEVEL 2 CORROSION CENTER FUSELAGE III RH LONGITUDNAL SEAT TRACKS HAS MULTIPLE AREAS OF CORROSION, SCRATCHES & CHAFING ON TEETH, CENTER & EDGES, ALONG ENTIRE LENGTH. (MAJOR REPAIR). BLENDED CORRODED AREAS ON CENTER FUSELAGE III RH LONGITUDINAL SEAT TRACK CROWN SDR SWIA2026080377076Slide · crackedEMER EVACUATION SLIDE ASSY RESTORE 60M - EMERGENCY EVACUATION SLIDE ASSEMBLY DUE RESTORATION. COMPLY WITH ONE OF THE FOLLOWING TASK CARDS DEPENDING ON SLIDE POSITION: PN 4A4030-7 - FWD TASK CARD: 25-65-01-001-FWDLH OR 25-65-01-001-FWDRH OR PN 4A4011-7 - AFT TASDR AALA202609026715Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORROSION ON STRINGER 26L AROUND FASTENER HOLE APPROXIMATELY BS 777. REPLACED STRINGER FROM FS 777 TO FS 837; IAW SRM 53-00-03-2R-1, AARD 51-00-05 AND BOEING DWG 146A3230.SDR SWAA2026090184244Floor Panel · damagedELONGATED HOLES ON FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT 2026-472681 FABRICATED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 PARAGRAPH 1.F AND DWG 453A2610 SHEET:2 REV: C MATERIAL USED CONOLITE P/N:A90RG1W P/O:2025-281119.SDR SWAA2026082737942Skin · damagedNR 2 ENGINE INLET HAS PULLING FASTENERS AT 3 AND 9 O'CLOCK POSITIONS REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.SDR SWAA2026082715244Skin · damaged#1 ENGINE INLET HAS PULLING FASTENERS AT THE 3 O'CLOCK POSITION REMOVED AND REPLACED NR 1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCESDR SWAA2026082541242Baffle · crackedBAFFLE FROM BS 500D - 500E, RBL 25 WAS CRACKED. R & R THE RT FCB BAFFLE BS 500D - 500E, RBL 25, WL 156 IAW SRM 51-40-02, & DWG 143A7505 REV -.SDR AALA202608184388Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND Y1292 LEFT - REPLACED BEAM-SEAT TRACK PER SRM 51-42-11