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 SWIA2026052377000Floor Support · corrodedTHREE OFF AREAS OF BLENDED CORROSION DAMAGE ON LT PRESSURE FLOOR SUPPORT, 2 AT BS 449.85 AND 1 AT BS 484) BEYOND LIMITS OF GREO 601R-53-41-666 REV C. PERFORMED MAJOR REPAIR ON 3 AREAS OF BLENDED CORROSION DAMAGE ON LT PRESSURE FLOOR SUPPORT BEYOND LIMITS OF GSDR IPXA2026052530789Skin · missingLEFT WING INBOARD SLAT HAS APPROX 8" X 6" SQ AREA OF THE SLAT HAS MISSING SKIN. COMPLETED ALL STEPS OF PRELIMINARY REQ 3 AS REQUIRED. VERIFIED ALL STEPS OF EO-97577REQ5 HAS BEEN COMPLETED. MAJOR REPAIR.SDR AALA202608217175Flashlight · no testAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT PORTABLE FLASHLIGHT INOP. MAINTENANCE INSTALLED NEW FLASHLIGHT AS REQUIRED.SDR SWIA2026052376874Skin · erodedRH ENG INLET LEADING EDGE ERODED. REMOVED AND REPLACED NOSE COWL LIPSKIN AT RT ENG INLET LEADING EDGE IAW SRM 54-11-05, AMM 71-61-01, SRM 51-42-06, REO 670-54-11-1456 REV - , REO 670-54-11-1456 REV -A AND SRM 51-21-11.SDR REXA2026080401440Thrust Reverser · crackedCRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE CRACK ON RH LOWER THRUST REVERSER TORQUE BOX FRAME AT LH ENGINE WAS REPAIRED PER REO 690-54-22-130REV. - -SDR VNAA202608010011Door Frame · corrodedCORROSION ON BULKHEAD DOOR POSTS LOWER SECTION AT FS280.00 (LBL12 & RBL12). BULKHEAD DOOR POSTS LOWER SECTION AT FS280.00 LBL12 & RBL12 WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ 900 SRM 51-10-06-001-001-A01 AND BULKHEAD DOOR POSTS LBL12 & RBL12 WERE REPAISDR VNAA202608010009Drip Tray · corrodedCORROSION ON DRIP TRAY LT AT CROSSBEAM BS 280. DRIP TRAY LT AT CROSSBEAM BS 280 WAS REPAIRED PER REO 690-53-22-055 REV -.SDR SWAA2026061505713Glowstrip · brokenBROKEN PHOTOLUMINESCENT STRIP LH SIDE AT PASSENGER CABIN (6EA). REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.SDR SWAA2026061505710Glowstrip · brokenBROKEN PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6EA). REPLACED PHOTOLUMINESCENT STRIP RT SIDE IAW AMM 33-51-15-400-802.SDR SWAA2026061505851Access Panel · crackedCRACKED ANGLE ACCESS PANEL 551FB AT LT WING REPLACED ANGLE ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND SRM-51-40-02-0G-0.SDR SWAA2026061505944Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING REPAIRED ACCES PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026061505945Access Panel · damagedELONGATED HOLES ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026062905869Angle · crackedCRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT STR 19R AT FWD CARGO BAY IAW SRM 51-10-01, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.SDR SWAA2026062905870Angle · crackedCRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 174, REV-, AND DWG 143A9481, SHEET 2, REV A.SDR SWAA2026062906012Stringer · crackedCRACKED STRINGER 15L BTW BS 294.5 - BS 303.9 IN FWD GALLEY AREA. PERFORMED PERMANENT REPAIR LOCATED ON STR 15L BETWEEN BS 277 MORE 10 INCHES TO BS 294.5 AT FWD GALLEY AREA IAW SRM 53-00-03-2R-1. REPAIR 1.SDR SWAA2026062906011Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 141A1311, SHEET 1, REV C.SDR IPXA2026062532624Swivel · corrodedRT MLG, SIDE STRUT SWIVEL (PART OF THE MLG SUPPORT BEAM ASSEMBLY) HAS CORROSION AROUND AND UNDERNEATH THE O/B BUSHING, FLL-005, REMOVE CORROSION OF RH MLG, SIDE STRUT SWIVEL INSIDE LUG BORE, CHANFER AND AROUND AREA OUTSIDE OF SPOTFACE IAW B767-300F SRM 51-10-SDR SWAA2026062505863Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 WL 208.1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2026062505868Angle · crackedCRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS LOCATED FWD FACE BS 500C AT LEVEL STR 26L IAW SRM 51-40-02-0G-0 AND DWG 143A7505; SHEET 82; REV.-.SDR SWAA2026062506013Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS, BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0; DWG 141A1110 SHEET: 18 REV: - AND DWG 141A8380, SHEET: 21 REV:-SDR SWAA2026062505865Gusset · crackedCRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D STR 19L AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 174; REV - .SDR SWAA2026062305973Seal · crackedRIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL WAS CRACKED. REMOVED AND REPLACED SLIDER SEAL IAW SRM 51-40-02.SDR SWAA2026062305975Seal · crackedLEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SLIDER SEAL IAW SRM 51-40-02.SDR SWAA2026062305969Panel · crackedSTABILIZER REMOVABLE LE PANEL 341A INTERNAL FIBERGLASS WEB HAS A CRACK AT A FWD RIVET. REMOVED NUT PLATES; FOR FURTHER INSPECTION IAW SRM 51-40-02. REMOVED PAINT IN SUPPOSED DAMAGED AREA. NO DEFECTS NOTED TO PLY'S ON FWD AND AFT SIDE. CRACK ARE LINES IN THESDR SWIA2026052376260Floorbeam · corrodedFLOORBEAM ANGLE AT BS 280, RBL 11 CORRODED. REPLACED FLOOR BEAM ANGLE/CLIP AT BS 280, RBL 11 WITH NEW. IAW SRM 51-42-06-001-001-A01 & DWG CC670-34191, REV NC, DWG CC67033052 REV -G AND DWG CC670-34010 REV -J. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SDR SWAA2026061805909Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241ABF AT AFT GALLEY AREA. REPAIRED FLOOR PANEL 241ABF AT AFT GALLEY AREA IAW SRM 53-00-50-2R-7 REPAIR 7 AND B737-800 SRM 53-00-50-2R-0 REPAIR GENERAL.SDR IPXA2026061634755Skin · corrodedLH RUDDER SURFACE CONDUCTIVE FRAME ABOVE STA. 380 SHOWS EVIDENCE OF CORROSION. DOT 65-001 INSTALLED FAIRING P/N 173N2603-3, FAIRING P/N 179N1000-7, BRACKET SUPPORT P/N 173N2507-9001 AND STATIC DISCHARGE. IN LH RUDDER SURFACE CONDUCTIVE FRAME ABOVE STA. 380. IASDR SWAA2026061105657Angle · crackedAFT CARGO COMPARTMENT BS 867, LBL 13, ANGLE BRACKET FOR PANEL 141QW PILLAR IS CRACKED. REMOVED AND REPLACED AFT CARGO COMPARTMENT BS 867, LBL 13.SDR ASAA2026052366544Transition Panel · crackedFWD CARGO RT TRANSITION PANEL BS 500B TO 500H HAS MULTIPLE CRACKED AREAS. GROUNDED - YES. REMOVED AND REPLACED RT TRANSITION PANEL AND SPLICE BS 500B TO 500H IAW SRM 53-00-53-2R-6.SDR MASA20260608148Shear Panel · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE CFIII, AFT WET AREA, CORROSION ON LT SHEAR PANEL AT FR 87, LBL 13 TO LBL 46 REMOVED BY BLENDING IAW SRM 51-10-03, MAX MATRL REMOVED .002". FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10 AD 03.10X MAG C/OUT, NO FAULT FOUND. BSDR AALA202606082712Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606044619Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606043334Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR DALA2026060403382Transmitter · faultyDUE TO TAKEOFF CONFIG WARNING FLAPS. REPLACED FLAP LEVER POSITION TRANSMITTER AND FLAP PDU POSITION TRANSMITTER. REPLACED TE FLAP POSITION TRANSMITTER AND FLAP POSITION DRIVE. (LP 1608832 - AIRCRAFT WAS GROUNDED)SDR AALA202606033652Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202606038152Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR 2026FA0000474Control Unit · faultyBRAKE CONTROLS MAINT MSG 32-32300, AFT INVESTIGATION FOUND BSCU LEFT FAULTY SAME REPLACED I.AW AMM DMC-B787-A-32-42-03-01A-520A-A AND DMC-B787-A-32-42-03-01A-720A-A .SDR AALA202606027001Baffle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT BAFFLE AT STA 771 AND RBL 34. REPLACED BAFFLE PER SRM 51-10-02.SDR AALA202606018498Plate · crackedAIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER DOOR GIRT BAR FITTING PLATE ASSEMBLY CRACKED. REPLACED GIRT BAR FITTING PLATE.SDR FDEA202605230659Floor Support · corrodedMAIN DECK - FWD COURIER AREA FR11-FR14 Y1456 LONGITUDINAL FLOOR SUPPORT CORRODEDSDR CALA2026060116682Door Sill · corrodedCORROSION ON INNER CHORD AT R1 DOOR CUTOUT LOWER SILL. REMOVED AND REPLACED R1 DOOR LOWER SILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8310. REMOVED AND REPLACED R1 DOOR LOWER SILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8310.SDR CALA2026060116680Support Beam · crackedRIGHT WING PANEL 671DB HAS A CRACK. INSTALLED PANEL 671 DB IAW B737-800 SRM 51-40-02-0G-0. REMOVED PANEL 671DB & BEAM SPRT RH WING, EVAUATED FOUND TO BE OUT OF LIMITS, VERIFIED MATERIAL, FABRICATED NEW SUPPORT, LOCATED AND DRILL NEW SUPPORT,APPLIED ALODINESDR FDEA202605230649Web · crackedMDC - UNDER FLOOR WEB CRACKED AT FR47 Y-953 - Y-1456. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-1SDR DALA2026052803227Slide · detachedUPON ARRIVAL & OPENING 1L DOOR, EMERGENCY SLIDE SEPARATED FROM DOOR & FELL INTO JET BRIDGE. SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR SLIDE IAW B717 AMM 25-61. AC OK FOR SVC. (8235878) (AIRCRAFT GROUNDED)SDR DALA2026052803226Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 BTW. PERMANENT REPAIR AND PER PRI 634510-14 (1609411) (AIRCRAFT GROUNDED)SDR DALA2026052803224Longeron · crackedCRACKED LONGERONS 5R, 6R, 7R AND 8R AT BS 1022. REPAIRED PER SRM 53-00-05 (1607816) (AIRCRAFT GROUNDED)SDR DALA2026052803223Skin · crackedCRACK ON FUSELAGE SKIN BTW STA. Y=1037 & LONG 14R AT RH PYLON. REPAIRED PER ER/A 634213-14 (1607725) (AIRCRAFT GROUNDED)SDR DALA2026052703215None · noneER/A 589110-14AD REV 'A' ISSUED FOR REPAIR AT FR16RH & DOOR STOP 1. FOLLOW ON ACTION REQUIRED. PERFORM SECTION IV EVERY 11500FC AFTER SECTION III. THIS SUPERSE DES LOG 1704322. ASSOCIATED ER/A 14-589110 ADDED FOR AC 3251. (LP: 1608765) AIRCRAFT WAS GROUNDEDSDR DALA2026052703213Window Frame · damagedDURING M2 AND WHILE INSPECTION PER EM 5311-01236-02, CRACK FOUND IN THE UPPER JUNCTION FASTENER HOLE OF FR4 LATERAL WINDOW FRAME, RHS, AT THE INTERFACE WITH RHS FRONT WINDSHIELD FRAME. PER SECTION DTE OF 633157-14AD THE REPAIR OF SECTION I IS LIMITED TO 26,60SDR DALA2026052703203Fitting · cracked*DTE* DURING M2 AND WHILE ACCOMPLISHING EM 5311-01246-01, BOTH LH/RH CONTINUITY FTGS FOUND CRACKED AND ALSO FRONT WINDSHIELD FRAME HOLE D1 CRACKED. C/A: *DTE* PER SECTION DTE OF 633213-14AD, THE REPAIR OF SECTION I IS LIMITED TO 60,000 TOTAL FC (FROM A/C FIRST