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 VNAA20260512015Fitting · corrodedCORROSION ON MID CAP ANGLE OF PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON MID CAP ANGLE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND IS OUT OFF LIMITS PER CRJ-700 SRM 53-21-23-101-001-A01 AND MID CAP ANGLE WAS REPLACED PER CRJ-700 SRM 51-41-02-00May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260512014Fitting · corrodedINITIAL INSPECTION: CORROSION ON FRAME FITTING FS 319 STGR 17RH AT CPAX. FRAME FITTING WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE IT IS OUT LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260512013Bracket · corrodedCORROSION ON BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGR 25LH AT FORDWARD BAGGAGE BAY. WERE EVALUATED,DUE NOT ALLOWABLE DAMAGE BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGRMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260512012Panel · crackedCORROSION AND CRACK ON DIVERTER PANELS (3EAS). REPAIRED PER EA 5321-2026-0502 REV - -, EA 5321-2026-0501 REV - - AND EA 5321-2026-0488 REV -.May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA20260512011Seat Track · corrodedCORROSION AND GOUGES ON SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER CABIN. SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER WERE REPLACED PER CRJ 700 SRM 53-00-49-400-May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260512010Seat Track · corrodedCORROSION AND GOUGES ON SIDE SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGER CABIN. SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGEMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260512009Skin · damagedPERM REPAIR - PANEL 196DR NUT PLATE ASSEMBLY OVERSIZED HOLE 1. WITHIN 1556 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACE NUT PLATE ASSY. MMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260512008Hinge · wornIN REF TO TRFKE00EQGM3: PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007-A01. SEND E-MAIL REQUEST TO DL_PSA_MAINTENANCE_PROGRAMS@PSAAIRLINES.COM TO COMPLETEMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA20260512006Web · crackedCRACK ON FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER CRJ 700 SMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260512007Drip Tray · crackedIN REF TO TRFKE00CFJVX: 4790FH PERM REPAIR - DAMAGE DRIP TRAY DRAIN TUBE FITTING WITHIN 4790 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACEMay 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260512005Plate · crackedCRACKS ON MOUNTING PLATE FWD/AFT CORNERS OF JB6 AT FWD EQUIPMENT COMPARTMENT. MOUNTING PLATE WAS REPLACED PER SRM 51-42-06-001-001-A01.May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260512004Angle · crackedCRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR. CRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01 AND SRM 51-41-02-001-001-A01May 12, 2026 · N541EA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA20260512003Retainer Seal · crackedCRACKED UPPER SEAL RETAINER AT PASSENGER DOOR. UPPER SEAL RETAINER AT PASSENGER DOOR WAS REMPLACED PER CRJ-700 SRM 51-42-10-001-001-A01May 12, 2026 · N541EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR 2026F00104Stringer · corrodedCENTER STRINGER UNDER PANEL 164BC HAS 3 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 3 AREAS AND VERIFIED CORROSION LOCATED INSIDE FUSELAGE BAY 164BC ON CENTER STRINGER. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSIONMay 12, 2026 · N361QS · Cessna 680A · Fuselage Main, Longeron/StringerSDR 2026F00103Landing · corrodedCORROSION ON PANEL LANDS FOR PANEL 164AC. REPAIRED CORROSION ON PANEL LANDS FOR PANEL 164AC IN REFERENCE TO NETJETS REQUEST FOR TECHNICAL SERVICES (RFTS): RFTS-117178 REV. 0; TITLED: N361QS (680-0235) PANEL 164AC NUTPLATE CORROSION; DATED: 11 MAY 2026.May 12, 2026 · N361QS · Cessna 680A · Fuselage Main, StructureSDR 2026F00102Stringer · corrodedCENTER STRINGER UNDER PANEL 164AC HAS 5 AREAS OF CORROSION. REMOVED BUBBLED PRIMER FROM 5 AREAS LOCATED IN FUSELAGE BAY 164AC ON CENTER STRINGER AND VERIFIED CORROSION. MECHANICALLY REMOVED CORROSION AND PITTING PER CESSNA 680 SRM 21-70-02. FOUND CORROSION BLEMay 12, 2026 · N361QS · Cessna 680A · Fuselage Main, Longeron/StringerSDR VNAA20260512002Handle · crackedCRACKS (4 EAS) ON EXTERNAL HANDLE FLAPER CORNERS AT PASSENGER DOOR. EXTERNAL FLAP HANDLE AT PASSENGER DOOR WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND PLACARD WAS INSTALLED PER CRJ-700 AMM 20-60-04-400-801.May 12, 2026 · N541EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20260512001Hinge Fitting · corrodedCORROSION ON HINGE FITTINGS (2 EAS) AND HARDWARE OF AFT LAVATORY SERVICE DOOR. CORROSION ON HINGE FITTINGS (2 EAS) OF AFT LAVATORY SERVICE DOOR WERE REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE IT IS OUT OF LIMITS PER CRJ-700 SRM 53-00-00-101-00May 12, 2026 · N541EA · Cndair CL6002C10 · Fuselage, Door HingeSDR 2026FA0000351Tail Wheel · faultyPILOT REPORTED PROGRESSIVELY SEVERE TAILWHEEL SHIMMY DURING LANDING ROLLOUT, LEADING TO LOSS OF CONTROL AND GROUND LOOP WITH SIGNIFICANT DAMAGE TO AIRCRAFT. POST ACCIDENT INSP FOUND THE TAILWHEEL SPRING HAD AN EXISTING CRACK FROM THE TAILWHEEL HEAD MOUNTING BOMay 12, 2026 · N5235D · Cessna 180A · Nose/Tail Landing GearSDR PN1R202605120001Bolt · unserviceableON TWO SEPARATE OCCASIONS, ON THE AS350B3, 6EA MAIN ROTOR STARFLEX ATTACHMENT BOLTS WERE FOUND TO BE UNSERVICEABLE. NOTE: THE STARFLEX IS ATTACHED TO THE MAIN ROTOR SHAFT USING 12EA BOLTS AND 12EA BARREL NUTS.May 12, 2026 · N568AE · Aerosp AS355* · Main Rotor BladesSDR DALA2026051202968Inlet · damagedAIR TURN BACK DUE TO LEFT ENGINE VIBRATIONS WITH AN ASSOCIATED ODOR REPORTED BY THE FLIGHT CREW. MAINTENANCE REPLACED THE LEFT ENGINE DUE TO INLET DAMAGE IAW T/C 7100-004423LH ON LOG PAGE 1578973. OPS AND LEAK CHECK GOOD. (LOG 7984276 - AIRCRAFT WAS GROUNDEDMay 12, 2026 · N3771K · Boeing 737832 · Engine Air Intake SystemSDR SCNA20260512195Girt Bar · disengagedL1 GIRT BAR WILL NOT DISENGAGE FROM HOLDER ON FLOOR. PERFORMED OPERATIONAL CHECK OF THE FLOOR MOUNTED ESCAPE SLIDE BRACKET INSTALLATION IAW AMM 25-66-02. OPS CHECKS GOOD. NO DEFECTS NOTED. ACFT OK FOR SERVICE.May 12, 2026 · N5167A · Boeing 73783N · Emergency EquipmentSDR IXXA20260512001Angle · crackedFOUND CRACK ON UPPER ANGLE ON FRONT SPAR ABOVE PDU LES150-148May 12, 2026 · N409AZ · Boeing 7673P6 · Wing Miscellaneous StructureSDR KCSA202605121038Escape Reel · damagedNR 1 EMERGENCY DESCENT DEVICE REQUIRES REPLACEMENTMay 12, 2026 · N767CK · Boeing 747481F · Emergency EquipmentSDR SWIA2026051177300Bracket · crackedPILOTS SIDE WINDSHIELD CENTER POST LWR BRACKET CRACKED. REMOVED & REPLACED THE PILOTS SIDE WINDSHIELD CENTER POST LWR BRACKET IAW SRM 51-42-21-00, & DWG 601R33007, REV U.May 11, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR 2026FA0000764Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.May 11, 2026 · N309TX · Cessna 172S · Main Landing Gear Attach SectionSDR 4VAA202605110031Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT ELEVATOR TOP AND LOWER LEADING EDGE. THE ELEVATOR WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060677.May 11, 2026 · N749SA · Saab 2000SAAB · Elevator, Plate/SkinSDR 4VAA202605110021Spar Cap · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE RIGHT HAND WING TRAILING EDGE TOP SPAR CAP AT HINGE NUMBER 3. THE RIGHT HAND WING TRAILING EDGE SPAR CAP WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060668.May 11, 2026 · N749SA · Saab 2000SAAB · Wing SparSDR SWIA2026051177013Frame · crackedTHE FORWARD SIDE OF THE FRAME AT F.S. 574 BETWEEN STRINGER 26R AND 27R FOUND TO BE CRACKED AND REQUIRES REPLACEMENT OR REPAIR. (C-CHECK RO 08/28/2026) COMPLIED WITH MAJOR REPAIR OF THE FORWARD SIDE OF THE FRAME AT F.S. 574 BETWEEN STRINGER 26R AND 27R FOUNDMay 11, 2026 · N477CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWAA2026061597617Baffle · crackedBAFFLE ANGLES CRACKED BS 500C AND BS 400 AFT SIDE OF FRAMES, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLES IAW SRM 51-40-02-0G-0, AND DWG 143A7505, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597628Baffle · crackedBAFFLE ANGLE CRACKED BS 500C FWD SIDE OF FRAME, LBL 25, WL 155. REMOVED AND REPLACED BAFFLE ANGLE IAW SRM 51-40-02-0G-0; AND DWG 143A7505, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597457Strap · corrodedCORROSION ON STRAP AT BS 1019-1032 LBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5600, SHEET 32, REV B.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597458Strap · corrodedCORROSION ON STRAP AT BS 1025 RBL 3 WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597462Floor Support · crackedCRACKED FLOOR SUPPORT AT BS 344 - 360, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 141A5400, SHEET 46, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597464Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380 - 400, LBL 16, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597465Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380-400, RBL 40, WL 208. EMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A5400, SHEET 109, REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597616Stringer Clip · crackedBS 727B, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597623Stringer Clip · crackedBS 727E, STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597624Stringer Clip · crackedBS 727B STRINGER CLIP 6R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1106 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597625Stringer Clip · crackedBS 727B, STRINGER CLIP 7L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP IAW NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597613Stringer Clip · crackedBS 685, STRINGER CLIP 2L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 144A1106 REV A.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597615Stringer Clip · crackedBS 727A, STRINGER CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597621Stringer Clip · crackedBS 727A, STRINGER CLIP 5L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101 REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597622Stringer Clip · crackedBS 727A STRINGER CLIP 5R UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1101; REV-.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597461Floor Support · crackedCRACKED INTERCOSTAL AT BS 344-360 BL 0 WL 208<[01] OK TO INSTALL GIVEN FOR STEP 2 ITEM 2;[02] REMOVED AND REPLACED NEW INTERCOSTAL BS344-BS360 BL 0 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV:-;[03] VERIFIED; CORRECTIVE ACTION STATEMENT # 2. TASKMay 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597463Floor Support · crackedCRACKED INTERCOSTAL AT BS 312-328 RBL 31 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-328 RBL 31 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 39 REV - DATE: 08/13/96;[02] VERIFIED CORRECTIVE ACTION 1May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026061597460Tee Fitting · corrodedCORROSION AT BS 986, RBL 43, WL 208. TASK CARD C/W. REMOVED AND REPLACED PREVIOUS REPAIR TEE FITTING SECTION, RBL14 - RBL50, WL 208 IAW SRM 51-40-02-0G-0 AS SHOWN IN EA 1-753-30047 REV IR ; SRM 53-70-51-2R-4 WITHOUT DEVIATION.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026061597618Stringer Clip · crackedSTA 727E STR CLIP 7L UPPER CORNER CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1112; REV-May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597626Stringer Clip · no discrepancySTA 727B STR CLIP 8L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 727B; S-8L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061597627Stringer Clip · no discrepancySTA 767 STR CLIP 10L UPPER CORNER CRACKED. HFEC INSPECTED STRINGER CLIP AT 767; S-10L IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 AND FOUND NO CRACKS PRESENT.May 11, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach Fittings