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 REXA2026070301065Skin · corrodedCORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGE SKIN SETTLEMENT AREA OF FAIRINGS 195AB, 195BB, 195AL, 195DL, 196DR AND 196AR AT LOWER FUSELAGE STRUCTURE BTW FS847.00 TO FS942.00 AND LBL 45.00 TO RBL 45.00. CORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGESDR REXA2026070301064Plate · corrodedCORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-SDR REXA2026070301063Bracket · corrodedCORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-SDR REXA2026070301061Bracket · corrodedCORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001-SDR REXA2026070301042Seat Track · corrodedCORROSION ON SEAT TRACK BTW FS375.00 TO FS485.00 LBL9.00 AND FS349.00 TO FS485.00 RBL9.00 ALSO CORROSION ON SIDE SEAT RAIL BTW FS785.15 TO FS847.00+16 AND STGR 15LH/15RH AT PASSENGER CABIN SEAT RAIL BTW FS375.00 TO FS485.00 LBL9.00 AND FS349.00 TO FS485.00 RBSDR REXA2026070301034Door Frame · crackedCRACK ON UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR. UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01SDR SWIA2026051976395Intercostal · corrodedPASSENGER DOOR INTERCOSTAL, DD5 IS CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL AT DD5 WITH NEW PASSENGER DOOR INTERCOSTAL DD5 USING NEW FASTENERS. REF. SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG 601R31702 REV -N. SEE CONTINUATION SSDR SWIA2026051976391Intercostal · corrodedPASSENGER DOOR INTERCOSTAL DD3 IS CORRODED. REMOVED AND REPLACED CORRODED PAX DOOR INTERCOSTAL DD3 WITH NEW PASSENGER DOOR INTERCOSTAL DD3 REF. SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG 601R31702 REV -N. SEE CONTINUATION STEPS FOR MORE DETSDR SCNA20260630272Pressure Deck · crackedTHREE CRACKS WERE FOUND ON THE RT WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB, BS 663.75, RBL 25 TO RBL45: BETWEEN RBL31.83 AND RBL 40.00 CRACK 1=1.1125IN LENGH, CRACK 2=1.060IN LENGTH, BETWEEN RBL 40.00 AND RBL 45.64 CRACK 3=3.0IN LENGTH, IN REFESDR AALA202606285845Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 56 AND FR 57 AT S43L. REPAIRED STRINGER PER EA 375950.SDR SWAA2026062204302Floor Panel · pulledFLOOR PANEL 231HF LOWER SKIN HAS AREAS OF PULLED STRANDS. FABRICATE REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2026062204303Floor Panel · pulledFLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2026062204318Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241RF FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2026062204311Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 146A5810.SDR SWAA2026062204315Floor Panel · pulledFLOOR PANEL 242EF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-0-B00275, REPAIR GENERAL.SDR SWAA2026062204316Floor Panel · pulledFLOOR PANEL 242FF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DWG 146A5810.SDR SWAA2026062204317Floor Panel · pulledAFT FLOOR PANEL 242D UPPER SKIN HAS AN AREA OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-B00276, REPAIR 1.SDR SWAA2026062204308Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS PULLED STRANDS ALONG THE AFT EDGE. FWD FLOOR PANEL 222CF WITH UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026062204309Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS PULLED STRANDS ALONG THE FWD EDGE. FWD FLOOR PANEL 222DF DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026062204620Shield · corrodedCORROSION ON ACB FWD SHIELD WEB BETWEEN BS 767 - 792, RBL 25, WL 156. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.SDR SWAA2026062204523Threshold Web · corrodedCORROSION ON FCB SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 25, WL 156. P 5 REJECT DUE TO COMMON STRUCTURE TO SUB-THRESHOLD HAS BEEN COUNTERSINK. REMOVED AND REPLACED FCB THRESHOLD WEB IAW SRM 51-40-02-0G-0, DWG 143A8330, REV B.SDR SWIA2026051976257Striker · corrodedSERVICE DOOR LOWER SEAL STRICKER IS CORRODED. REPLACED SERVICE DOOR LOWER SEAL STRIKER IAW DWG SH670-31950, REV Y, & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.SDR FDEA202605190780Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0377102 A P2 PERFORMED HFEC INSPECTION TO CONFIRM THE CRACK IN LH WING CENTER FLAP RIB26 UPR FLANGE BETWEEN STGR2.7 AND STGR2.8 AND REMOVEDSDR SWAA2026061804587Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231KF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.SDR SWAA2026061804517Floor Support · crackedCRACKED ANGLE FLOOR STRUCTURE, BS 380 TO 400, LBL 50 IN PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE IAW DWG 143A5400, SHEET 140, REV- AND SRM 51-40-02-0G-0.SDR SWAA2026061804516Floor Support · crackedCRACKED FLOOR SUPPORT LOCATED BETWEEN BS 380 - 400, LBL 13. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 184, REV -.SDR HNAA2026061800549Frame · crackedRT FR25 FRAME CRACKED AT BTW STR15-16R. REPAIRED IAW ETD 2026-145-008920 AND EO 1-53-26-0265.SDR REXA2026061700970Lug · damagedDURING BUSHING INSTALL BORE 1 AND 6 WERE FOUND OVERSIZE ON RH AILERON LUGS R1 AND R6 AT CENTER FITTING ON RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A0, AND REPAIRED PER REO 670-57-61-237 REV. - - & REO 690-57-61-516 REV. -ASDR AALA202606132655Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON THS COMPARTMENT ACCESS DOOR 312AR CUTOUT INTERNAL STRUCTURE ANGLE AT FR 71 BETWEEN S27R AND S32R. REPLACED ANGLE PER SRM 51-42-11.SDR SWAA2026061104758Floor Panel · failedFLOOR PANEL 241EF UPPER SKIN HAS A FAILED PREVIOUS REPAIR. FLOOR PANEL 241EF WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026061104577Lamp · inoperativeEXTERIOR EMERGENCY LIGHT BY AFT LEFT SERVICE DOOR IS INOPERATIVE. REPLACED THE LAMPS EXTERIOR EMERGENCY LIGHT BY AFT LEFT SERVICE DOOR IAW AMM 33-51-04. OPS CHECKED GOOD.SDR SWAA2026061104576Lamp · inoperativeEXTERIOR EMERGENCY LIGHT BY FWD SERVICE DOOR IS INOPERATIVE. REPLACED THE LAMPS EXTERIOR EMERGENCY LIGHT BY FORWARD SERVICE DOOR IAW AMM 33-51-04. OPS CHECKED GOOD.SDR SWAA2026061104505Fairing · crackedNR 6 CANOE FAIRING CRACKED. INSIDE CENTER BOTTOM. REPAIRED PER E/A M 21-157-01063. INSPECTION C/W FOR CORRECTIVE ACTION NR 1. REPAIRED IAW E/A M 21-157-01063.SDR AALA202606115541Handle · missingAIRCRAFT IN BASE MAINTENANCE: R1 CREW/PASSENGER DOOR ESCAPE SLIDE-RAFT ASSEMBLY MISSING PULL HANDLES. REPLACED SLIDE RAFT ASSEMBLY PER TASK CARD 26C84152006.SDR SWAA2026061004183Baffle · crackedFWD CARGO RT TRANSITION ANGLE SUPPORT BAFFLE BETWEEN STA.500G TO 500H IS CRACKED. REMOVED AND REPLACED NEW FWD CARGO R/H TRANSITION ANGLE SUPPORT BAFFLE BETWEEN BS 500G TO 500H PER SRM 51-40-02.SDR SWIA2026051976214Seat Track · nickedRH LATERAL SEAT TRACK FROM FR 22-43 HAS NICKS/SCRATCHES. REMOVED AND REPLACED RH LATERAL SEAT TRACK FR 23-34 WITH NEW IAW SRM 51-40-08. REPLACED WITH OEM PART.SDR VNAA202606060017Lug · corrodedCORROSION WAS FOUND ON LUG BORE #5 OF LH AILERON. REPAIRED PER REO 670-57-61-237 REV.-.SDR CALA2026060316799Coffeemaker · leakingGALLEY COFFEEMAKER LEAKS. COFFEEMAKER BAG BROKE OPEN SO NOW HS GROUNDS IN IT AND SMELLS FUNNY WHEN HEATING UP FWD GALLEY COFFEEMAKER INOP LEAKS IN USE CLEANED EXCESS GROUNDS AND AREA. PLACE ON NEF 2522AK BREAKER COLLARED AND PLACARD IN PLACE. APPROVED FOR NESDR AALA202606039349Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-42-11.SDR AALA202606032186Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.SDR HNAA2026060300482Floor Support · corrodedLEFT OMEGA BEAM CORRODED AT 2 ANCHOR NUT LOCATIONS BTW FR 59-61. REPAIRED IAW SRM 53-24-10.SDR SWAA2026060104617Cartridge · crackedCRACK FOUND ON LT OUTBOARD AFT FLAP INBOARD CARTRIDGE INNER SURFACE. LEFT WING OUTBOARD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW B737 CMM 57-53-08. ASSEMBLY 2.C.(2);SDR AALA202606014391Warning Light · intermittentAIRCRAFT WAS NOT GROUNDED: 4L DOOR SLIDE ARMED INDICATION INTERMITTENT IN FLIGHT. **SUPPLEMENTAL REPORT FOR AALA202605224391 SUBMITTED 5/22/2026 BY TUL: MAINTENANCE REPLACED THE L4 DOOR SLIDE ARMED INDICATOR LIGHT PER AMM 52-73-21 AND ACCOMPLISHED A SATISFACTOSDR IPXA2026052861067Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL 232XWF HAS EDGE DAMAGE. FABRICATION OF MAIN CARGO COMPT FLOOR PANEL 232XWF IAW SREO-9692-REQ001. REVIEWED.SDR 2026FA0000447Stiffener · crackedAFT FUSELAGE LOWER SKIN STIFFENER FOUND CRACKED. REPLACED WITH NEW STIFFENER.SDR DEMA202605270001Fuel Control · uncontrollableLOSS OF ENGINE THROTTLE RESPONSE FOLLOWED BY AN UNCOMMANDED ENGINE SHUTDOWN ON THE TAXIWAY PRIOR TO TAKEOFF. THE AIRCRAFT FUEL SYSTEM WAS CHECK FOR CONTAMINATION WITH NO APPRECIABLE WATER OR DEBRIS FOUND IN WING TANKS OR RESERVOIR. FIREWALL FUEL FILTER ASSEMSDR FDEA202605190633Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB3 BETWEEN REAR SPAR ASDR FDEA202605190632Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND STGR2.8 & BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND SDR FDEA202605190631Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB13 BETWEEN STGR2.6 ANSDR FDEA202605190630Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. EA TI