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 CALA2026041315303Baffle · damagedFWD CARGO BAFFLE UNDER Z CHANNEL AT STA 500D TO 500W RT SIDE IS BENT/DAMAGED. REMOVED AND REPLACED DAMAGE BAFFLE AT FWD CARGO BTW STA 500D TO STA500E R/H SIDE I.A.W B737-800 SRM 51-40-02-0G-0.SDR CALA2026041315301Baffle · damagedFWD CARGO BAFFLE UNDER Z CHANNEL AT STA 500E TO 500F RT SIDE IS BENT/DAMAGED. REMOVED AND REPLACED DAMAGE BAFFLE AT FWD CARGO BTW BS 500E AND STA 500F R/H SIDE I.A.W B737-800 SRM 51-40-02-0G-0.SDR CALA2026041315298Stringer · corrodedAFTER EVALUATION OF DAMAGE CORROSION AT STRINGER LOCATED BETWEEN BS 947.5 & 967, S23R & S27R. FOUND DAMAGE TO BE OUT OF LIMITS. AFTER EVALUATION OF DAMAGE CORROSION AT STRINGER 25R. FOUND DAMAGE TO BE OUT OF LIMITS. REPAIRED THE STRINGER IAW SRM 53-00-03-SDR CALA2026041315294Life Vest · missingLIFE VEST CHECK. 1L ADULT LIFE VEST MISSING. NEW LIFE VEST INSTALLED IAW DWG 2560DD15305 & AMM 25-62-99-900-801.SDR CALA2026041315290Wire Harness · inoperativePASSENGER CABIN SEATS, GENERAL VISUAL INSPECTION PROCEDURE, INSEAT AISLE PATH LIGHTING INOP 10ABC. REMOVED AND REPLACED AISLE PATH LIGHTING HARNESS ON SEAT IAW CMM 25-21-57. OPS CHKD GOOD.SDR CALA2026041315287Housing · missingROW 23 LEFT SIDE EMERGENCY PATH INDICATOR HOUSING/LIGHT MISSING REPLACED EXIT PATH EMERGENCY LIGHT HOUSING AND EMERGENCY LIGHT AT SEAT 23C, TESTS GOOD.SDR AALA202604131140Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE BETWEEN STA 500G AND STA 500H AT RBL 25. REPLACED BAFFLE PER AARD 51-00-05-1.SDR AALA202604131323Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT FORWARD SIDE OF STA 500G, AT RBL 23. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR AALA202604135698Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT AFT SIDE OF STA 500G, AT RBL 23. REPLACED BAFFLE CLIP PER AARD 53-00-01-6.SDR DALA2026041302316Web · corrodedCORROSION WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWG D53112545 RELEASE DATE 30-JUN-98 ISSUE: F00 AND DWG D53114392 RELEASE DATE: 01- FEB-SDR DALA2026041202312Seat Track · corrodedAFT CABIN-SEAT TRACK LBL43.5 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342701. (LP 1539725 - AIRCRAFT WAS GROUNDED)SDR DALA2026041202311Seat Track · corrodedAFT CABIN-SEAT TRACK RBL23 NEAR LAV MOUNT FR72 HAS CORROSION. (M) REF SSI 53-61-43-01. REMOVED DAMAGED SEAT TRACK AND INSTALLED REPAIR PARTS, COMPLIED WITH ER/A 632950-14 PRI REV 0, REV 1, ERA 623169-14TR REV. A, AND FINAL ER/A 632950-14 REV ORIGINAL, AND ERSDR DALA2026041202305Floor Support · corrodedCORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY A REA (SSI 534147). REPLACED FLOOR BEAM Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM 51-42-11 AND DWG D53472815 RELEASE DATE 18-DEC-06. ISSUE G. MEASURSDR KCSA202604111030Battery · inoperativeFO'S EMERGENCY FLASHLIGHT INOPSDR KCSA202604111029Battery · inoperativeCA'S EMERGENCY FLASHLIGHT INOP.SDR IXXA20260411001Support Angle · crackedRIGHT WING TRAILING EDGE STRUCTURE SUPPORT ANGLE IS CRACKEDSDR SWIA2026041077774Door Frame · crackedRIGHT HINGE FRAME IS CRACKED ON AFT EQUIPMENT BAY DOOR. REMOVED AND REPLACED FRAME AT RT OTBD SIDE AT THE AFT EQUIPMENT BAY DOOR SURROUND WITH NEW IAW SRM 51-42-06, AND DWG 601-36004, REV K.SDR SWIA2026041077768Skin · dentedAT APPROX BS 663 ON STRINGER 23L THERE WERE 2 EXTERNAL DENTS IN CLOSE PROXIMITY TO EACH OTHER. REPAIRED BS 663 SKIN STRINGER 23L, IAW REO 601R-53-61-8602, REV-. COMPLIED WITH 51-900-1003-SKY.SDR SWIA2026041076337Hinge Fitting · corrodedUPON REMOVAL ON JOB HN00303104 CAMP 31954799, FOUND LT ELEVATOR L/E HINGE FITTING ASSY, ES 16.52 TO HAVE PITTING CORROSION IN BEARING BORES ON BOTH HINGE HALVES. REPLACE HINGE FITTING ASSY. INSTALLED 1 EA NEW L/E HINGE FITTING ASSY ON L/H ELEVATOR AT ES16.52 SDR SWIA2026041076282Crossbeam · crackedDURING AUDIT OF 1C TASK CARD 53-140-509, DETAILED INSPECTION OF THE BS 280 CROSSBEAM, DRAIN PANS AND DRAIN TUBES, FOUND A SUSPECTED CRACKED ANGLE ON THE AFT SIDE OF THE BS 280 CROSSBEAM OTBD OF RBL 9 SHEAR BOX. REMOVED OLD ANGLE & REPLACED WITH 1 EA OF NEW ANSDR SWIA2026041076211Floorbeam · damagedFLOOR BOARD LANDING IS DAMAGED AT FS559+48 ON RBL27.5 OUTBOARD SIDE. (C-CHECK RO 06/04/2026)REPAIRED DAMAGED FLOOR BOARD LANDING AT FS559+48 ON RBL27.5 OUTBOARD SIDE IN REFERENCE TO SRM 53-00-43. PERFORMED EDDY CURRENT INSPECTION IN REFERENCE TO NDTM PART 1 5SDR IPXA2026050238789Adapter · corrodedCLS ADAPTER AT Y0 FRAME 28 R/H WITH CORROSION. DOT AC-017. INSTALL 2 EACH CLS ADAPTER PER DRAWING B53774150 AT FR28 Y0 LT & RT LOCATION. IAW SRM 51-40-21-001.SDR CALA2026052916610Stop Fitting · gougedL-2 CABIN ENTRY DOOR FWD UPPER DOOR STOP FITTING IS GOUGED. L-2 DOOR STOP FITTING REPAIRED, REMOVED DAMAGED FITTING IAW B737-800 SRM 51-40-02 AND INSTALLED NEW STOP FITTING IAW SRM 51-40-02 AND RESTORED SURFACE PROTECTION IAW AMM 51-21-73.SDR 2026FA0000441Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTESDR IPXA2026050736877Support · crackedFAULT: STR- Z410- NO.1 ENGINE TOP OF PYLON PRESSURE RELIEF DOOR SUPPORT IS CRACKED INSTALLED #1 ENGINE TOP OF PYLON PRESSURE RELIEF DOOR SUPPORT IAW A300-AMM 54-52-61/401 ITEM C (4).SDR AALA202605226506Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE BETWEEN STA 767 AND STA 787, OUTBOARD SIDE OF S26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR AALA202605222271Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 747 AND STA 767, AT S26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA 374893.SDR AALA202605222836Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 847 AND STA 887, AT S22R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-10-02 AND EA374838.SDR HNAA2026052000411Shear Tie · crackedF118310 CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L HAS CRACK. REMOVED AND INSTALLED NEW CARGO SHEAR CLIP AT FR-65 BETWEEN STGRS 6L/7L IAW EMB-145 SRM 51-40-02.SDR HNAA2026052000410Shear Tie · corrodedCARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP ABOVE LWR CENTER SILL IS CORRODED. RE-ACCOMPLISHED CARGO DOOR FUSELAGE CUT-OUT FR-65 SHEAR CLIP SPLICE PATCH REPAIR ABOVE LWR CENTER SILL IAW ETD2016-145-072133 AND SRM 53-31-04RE, ITEM4. AND EO1-53-26-0224.SDR HNAA2026052000409Hinge Fitting · wornRUDDER I UPPER HINGE ATTACHMENT FITTING TRIANGLE FITTING ATTACHMENT TANGS WORN. REMOVED AND REPLACED WORN RUDDER I UPPER HINGE ATTACHMENT FITTING/ TRIANGLE FITTING ASSY IAW SRM 51-40-02 AND AMM 20-10-01. EASI 4484. PAINTED FASTENERS AS REQUIRED IAW CPM 51-21-SDR HNAA2026052000407Door Sill · corrodedCARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR FUSELAGE CUT-OUT LWR CENTER SILL IAW SRM 51-40-02.SDR IPXA2026051230823Floor Support · crackedAFT CARGO DOOR SILL FLOOR SUPPORT BETWEEN C60 AND C61 HAS CORROSION. SILL FLOOR SUPPORT AFT CARGO ENTRANCE REMOVED AND REPLACED IAW A300-600F SRM 51-72-10-001.SDR IPXA2026050731344Seal Depressor · gougedAFT CARGO DOOR SEAL DEPRESSOR HAS MULTIPLE GOUGES FROM 3" TO 24" ABOVE THE FWD LWR CORNER. REMOVED AND REPLACED DOOR SEAL DEPRESSOR IAW SRM 51-40-21-001.SDR IPXA2026050544404Skin · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL HAS (1EA) CRACK. REMOVED SKIN FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SKIN PANEL IAW A300-600 SRM 51-40-21-001.SDR IPXA2026050544443Bracket · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL, CURVED SUPPORT BRACKET HAS (1EA) CRACK. REMOVED CURVED SUPPORT BRACKET FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-21-001.SDR U2RA2026051200026Frame · cracked1EA CRACK FOUND AT BS2598 BULK HEAD RHS FRAME SUPPORT HOLE D AS PER BOEING SR MUA-MUA-26-0022-07B REPAIRED CARRIED OUT PER BOEING 8100-9 DATED MAY 12 2026 AND PER BOEING BCS 202603210023-0016SDR IPXA2026041337727Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 TO 1060, RBL 46 IS EXFOLIATED AROUND NUTPLATE LOCATIONS. INSTALLED NEW TEE FITTING AND REINSTALLED 1EA ANGLE AND REINSTALLED 1EA BONDING JUMPER IAW SRM 51-40-02-0G-0.SDR SWAA2026051188148Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 183 REV -.SDR SWAA2026051197570Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 183 REV -.SDR SWAA2026051188150Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 140 REV -.SDR SWAA2026051197571Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET 140 REV -.SDR SWAA2026051188146Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 154 REV - MESDR SWAA2026051197572Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENER LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 154 REV - MEASSDR SWAA2026051188147Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 184 REV -.SDR SWAA2026051197573Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A5400 SHEET 184 REV -.SDR SWAA2026051188149Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN AND FASTENER IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 115 REVSDR IPXA2026041036299Stiffener · crackedSTIFFENER BETWEEN FRAMES 38.1-38.2 R/H SIDE WITH CRACK. INSTALLED FLOOR ANGLE AT MAIN CABIN FR38.1 TO FR38.2 IAW SRM 51-40-21-001 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02. REPLACED STIFFENER IAW SRM 51-40-21-001.SDR IPXA2026050536213Stiffener · crackedSTIFFENER BETWEEN FRAMES 37-38 R/H SIDE WITH CRACK. REPLACED STIFFENER BETWEEN FRAME 37-38 R/H IAW SRM 51-40-21-001.SDR SCNA20260508189Floor Support · crackedCRACKED PASSENGER FLOOR SUPPORTS (2 EAS) ON STA 540, BTW RBL 2 & LBL 2 WNG BOX AREA. (PAX CAB) - - NEW FLOOR SUPPORTS (2 EAS) ON STA 540, BTW RBL 2 & LBL 2 WNG BOX AREA. (PAX CAB) WERE REPLACED PER B737-800 SRM 51-40-02-0G-0