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.

SDR EE4Y2026030924073Doubler · misinstalledDURING STRUCTURAL INSPECTION, THE CUSTOMER FOUND AN EXTERNAL REPAIR DOUBLER AT FR74 + 105 MM AND STR 24L + 85 MM, REPORTEDLY INSTALLED IN ACCORDANCE WITH EMB IC2009-190/05358C DATED 09-JUL-2009. ONCE THE AVAILABLE DOCUMENTATION LACKED ESSENTIAL INFORMATION, THMar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/SkinSDR EE4Y2026030924072Skin · damagedWAS REPORTED THAT DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR32 AND JUST ABOVE STR-26LH. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETMar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/SkinSDR EE4Y2026030924071Skin · damagedDURING THE STRUCTURAL INSPECTION, AN EXISTING BLEND-OUT WAS FOUND IN THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 86-87 AND STRINGERS 27R-28R. SINCE NO PREVIOUS RECORD OF THIS BLEND-OUT EXISTS, IT WAS INSPECTED AND EVALUATED. THE CONDITION WAS FOUND TO BEMar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/SkinSDR QR9R2026030900001Bolt · crackedNDI INSPECTION OF THE SECONDARY BOLT REVEALED A CRACK IN BETWEEN 4TH AND 5TH THREAD FROM TOP THREAD OF BOLT.Mar 9, 2026 · Bolkms BK117C2 · Main Rotor HeadSDR DALA2026030901624Battery Pack · inoperativeDURING SVC CHECK FOUND ROWS 33-38 EMERGENCY LIGHTS OUT. REPLACED EPSU BATTERY ON AFT GALLEY AND LEFT AND RIGHT CENTER CABIN EPSU. REPLACED AFT GALLEY EPSU, FOUND BROKEN WIRE AT ROW 36. SPLICED BROKEN WIRES IAW A321 AWM 33-51-08. AND SPWM CHAP 20. FOUND EPSU Mar 9, 2026 · N539DN · Airbus A321271NX · Emergency LightingSDR EE4Y2026030924069Skin · damagedCUSTOMER REPORTS LIGHTNING STRIKE DAMAGE AFFECTING THE CENTER FUSELAGE III SKIN, LOCATED AT FR74 AND STR 28L. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BMar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/SkinSDR AALA202603091505Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT CREW DOOR SILL BEAM FLOOR STRUCTURE AFT FASTENER HOLE, REPAIRED DOOR SILL BEAM PER SRM 53-41-14-300-001.Mar 9, 2026 · N413AN · Airbus A321253NX · Fuselage Main, StructureSDR AALA202603091227Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT CREW DOOR SILL BEAM FLOOR STRUCTURE AFT FASTENER HOLE, REPAIRED DOOR SILL BEAM PER SRM 53-41-14-300-001.Mar 9, 2026 · N413AN · Airbus A321253NX · Fuselage Main, StructureSDR AALA202603096715Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.Mar 9, 2026 · N189UW · Airbus A321211 · Passenger/Crew DoorsSDR AALA202603093848Wire · brokenAIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND BROKEN GROUND WIRE BETWEEN LH SIDE ROWS 29 AND 30. SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRE PER ESPM 20-43-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SMar 9, 2026 · N461AN · Airbus A321253NX · Light System WiringSDR AALA202603094128Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: LEFT AFT EMERGENCY EXIT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER WORK CARD 26L00005005.Mar 9, 2026 · N987AM · Airbus A321231 · Emergency ExitsSDR AALA202603096832Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABLIZER LOWER SKIN AT STABILIXER STA 120.30, 18 INCHES FROM THE FRONT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R.Mar 9, 2026 · N990AN · Boeing 737823 · Horizontal Stabilizer, Plate/SkinSDR IXXA20260309001Bracket · cracked#2 PYLON HYDRAULIC BAY DOOR SUPPORT CRACKEDMar 9, 2026 · N307AZ · Boeing 767338 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2026030877461Former · corrodedPASSENGER DOOR FORWARD FORMER HAS CORROSION BETWEEN DD5 AND DD6. REPLACED WITH NEW PASSENGER DOOR FORWARD FORMER IAW SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026030877452Stringer · corrodedCORROSION FOUND ON STRINGER 24L, BS 280 TO 333. REPLACED THE STRINGER IAW DWG SH670-31630, REV K, SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026030877439Stringer · corrodedCORROSION FOUND ON STR23L FROM FS280 TO FS333. REPLACED STR23L WITH NEW STRINGER REF DRAWING SH670-31630 REV K AND SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026030877433Beam · corrodedEXTERNAL FUSELAGE, LEFT BUTTSTRAP BETWEEN BS 834-847, HAS CORROSION AROUND FASTNER HOLES, REPLACED THE BEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-36290 REV U.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026030877424Stringer · corrodedCORROSION FOUND ON STR 21R, BTWN BS 333 - 379. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, REV 38, SRM 51-42-13-001-001-A01, & DWG SH670-31350, REV A.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026030877397Skin · damagedICE DETECTORS SURROUND HAD TOOLING MARKS, ON BOTH LT & RT. REMOVED SCRATCHES ON FUSELAGE EXTERIOR SKIN ICE DETECTOR SURROUNDS, BOTH RT & LT SIDES IAW SRM 51-12-00-001-001-A01, REWORKED AREAS ARE WITHIN LIMITS PER REO 670-53-11-2295, REV -.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026030877395Stringer · corrodedCORROSION FOUND ON STRINGER 23R, BS 333 - 379. REPLACED THE STRINGER IAW DWG SH670-31350, REV A, & SRM 51-42-06-001-001-A01.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026030877393Stringer · corrodedCORROSION FOUND ON STRINGER 24R, BS 280 - 333. REPLACED STRINGER 24R IAW DWG SH670-31630, REV K, & SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026030877366Intercostal · corrodedPASSENGER DOOR MID DD6 INTERCOSTAL HAS CORROSION ON LOWER SIDE. REPLACED WITH NEW PASSENGER DOOR MID DD6 INTERCOSTAL AND CLEAT IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N.Mar 8, 2026 · N611SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026030877341Frame · fomREMOVE AND REPLACE FRAME FS333 STR20R TO STR20L TO FOM C-CHECK RO 9302026REMOVED AND REPLACED FRAME WITH NEW PART AT FS333 STR20R TO STR21L REF DWG SH670-32420 REV E AND CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 COMPLIED WITH ALL STMar 8, 2026 · N611SK · Cndair CL6002C10 · Standard Practices/StructuresSDR CALA2026090119142Skin · crackedCRACK FOUND ON THE LT HORIZONTAL STAB HSS 166.30 ,LOWER SKIN, 15" FROM REAR SPAR, INBD ROW. SKIN REPAIRED IAW SRM 55-10-01-2R-11, REPAIR 11, FIGURE 204.Mar 8, 2026 · N53442 · Boeing 737924ER · Horizontal Stabilizer, Plate/SkinSDR COEA2026072327803Fitting · corrodedHORIZONTAL TO VERTICAL STAB AFT RT FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.Mar 8, 2026 · N803FX · Aerosp ATR72212 · Horizontal Stabilizer, Attach FittingsSDR COEA2026072224803Fitting · corrodedHORIZONTAL TO VERICAL STAB AFT L/H FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.Mar 8, 2026 · N803FX · Aerosp ATR72212 · Vertical Stabilizer Miscellaneous StructureSDR SCNA20260623259Smoke Goggles · crackedSMALL CRACK IN THE MIDDLE SECTION OF THE GLASS ON CAPTAINS SMOKE GOGGLES (BW #9425 MC NOTIFIED). REMOVED AND REPLACED CA SMOKE GOGGLES IN REF AMM 25-64-00. OKAY FOR SERVICE.Mar 8, 2026 · N826SY · Boeing 7378F2 · Emergency EquipmentSDR SWIA2026030876152Angle · corrodedPAX DOOR KICK PLATE ANGLE IS CORRODED IN 2 SPOTS. PAX DOOR KICK PLATE ANGLE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 DUE TO MULTIPLE FACTORSINCLUDING PROXIMITY OF DAMAGE TO FASTENERS, MORE THAN 30 PERCENT OF PART DAMAGED, AND MULTIPLE CROSS SECTIONS OF DAMAMar 8, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026030876144Hinge · chafedPAX DOOR HINGE (FUSELAGE SIDE) HAS CHAFING DAMAGE BETWEEN SEVERAL LUGS. REMOVED AND REPLACED A/C SIDE PAX DOOR HINGE WITH NEW SERVICEABLE HINGE IAW SRM 53-21-23-201-007-A01. PERFORMED REO 670-53-21-2844 REV -A FOR 3EA. DISCREPANT HOLES FOR ACFT SIDE PAX DOORMar 8, 2026 · N716SK · Cndair CL6002C10 · Fuselage, Door HingeSDR REXA2026050400443Fitting · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026050400442Doubler · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400441Fitting · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026050400440Bracket · corrodedINITIAL INSPECTION: CORROSSION AND WEAR ON SENTLEMENT AREA OF WHEEL BIN LH (3 LOCATIONS) AND RH (5 LOCATIONS). NEW WHEEL BEAM STABILIZER P/N: CC670-39221-4 WAS FABRICATED PER DWG CC670-39221 REV NC & EA CRJ953-21866 REV IRMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400439Bracket · corrodedINITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LH/RH) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400438Bracket · corrodedINITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LT/RT) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-8Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400424Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026050400423Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026050400417Latch · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Accessory Compartment DoorsSDR REXA2026050400416Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR HNAA2026042100320Bushing · migratedF111352 HAT BUSHING IS MIGRATING ON LH AILERON PCA OTBD HINGE. REMOVED AND REPLACED LH AILERON PCA ATTACHMENT HINGE FITTING IAW EMB 145 SRM 51-40-02.Mar 8, 2026 · N905JH · Emb EMB145LR · Wing Main, Frame StructureSDR SWAA2026042077659Web · crackedCRACKED WEB, BS 344 - 360, RBL 33, WL 208.1 REPLACED THE WEB LOCATED IAW SRM 51-40-02, AND DRAWING 141A5400, SHEET 33, REV -.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077658Web · crackedCRACKED WEB, BS 277 TO 294.5, RBL 1, WL 208.1. REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 WL 208.1 AT FWD GALLEY AREA IAW SRM B737-800 SRM 51-10-02 ITEM 9 AND DWG :141A5400 SHEET:20 REV:-.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077663Floor Support · corrodedCORROSION FLOOR SUPPORT BTW BS 947 TO BS 967 AT LBL 51 AND WL 208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 147A5650, SHEET 55, REV A.Mar 8, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077664Floor Support · corrodedCORROSION FLOOR SUPPORT BTW BS 947 TO BS 967, RBL 51, WL 208.1. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A5650, SHEET 71, REV A..Mar 8, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077809Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9111 SHEET 10 REV-.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077660Web · crackedCRACK INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA. REPLACED THE INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA IAW. B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 46 REV A.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077662Angle · crackedCRACKED ANGLE, TRAILING EDGE, ORSS 270, RT WING REPLACED THE ANGLE DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR CRACK ON SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1. LENGTH CRACK IS 0.734?.Mar 8, 2026 · N8630B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026042077655Angle · crackedCRACK ON ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 33 REV.-.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077656Angle · crackedCRACK ON ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01AV4EG.Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042077657Angle · crackedCRACK ON INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA. REPLACED INNER CHORD AND FASTENERS LOCATED BTW BS270 TO BS360 AT LEVEL STR 17L IAW SRM 51-40-02 AND DWG 141A8110 SHEET 10 REV.A, DWG 141A8110, SHEET 11, REV-. & DWG 142A0050 SHEET 15Mar 8, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous Structure