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 VNAA202607120007Skin · damagedWEAR ON EXTERNAL SKIN AT FS 910 AND FS 919, STRINGER 27 ON CENTER FUSELAGE. WEAR ON EXTERNAL SKIN AT FS 919 STRINGER 27 ON CENTER FUSELAGE WAS BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND FOUND WITHIN LIMITS PER CRJ900 SRM 53-51-01-101-003-A05 AND WEAR SDR VNAA202607120006Box Beam · damaged800FH PERM REPAIR - TEMPORARY REPAIR FOR DAMAGED HOLE TO LH NLG BOX SIDE BEAM BETWEEN FS228.42-FS235.00 THIS TEMPORARY REPAIR IS ACCEPTABLE FOR 800 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. // ENGINEERING COMMENTS: FWD FITTING STR 26A LH (PN CC6SDR VNAA202607120005Fairing · dented3801.90FH PERM REPAIR - LH FLAP STUB FAIRING (171DL) WITHIN 3801.90 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH FLAP STUB FAIRING (171DL) WAS REPAIRED PER EA NO: 53SDR VNAA202607120004Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT SDR VNAA202607120003Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER SRM 55-31-00-201-001-A01SDR VNAA202607120002Angle · crackedRACK AFT ANGLE ON PASSENGER DOOR. CRACK AFT ANGLE ON PASSENGER DOOR WAS REPAIR PER SRM 52-11-04-201-002-A01.SDR VNAA202607120001Handle · wornWEAR ON HANDLE FRAME AT AFT BAGGAGE BAY DOOR. DOOR WAS REPAIRED PER REO 670-52-31-031 REV. - BV. - BSDR SWAA2026070608365Lens · brokenBROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-801, STEP 2.C.(4).SDR SWAA2026070608238Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AR AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9 REPAIR 9.SDR SWAA2026070608363Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN. REPLACED THE SUPPORT BRACKET & FASTENERS LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN. IAW SRM 51-40-02, SRM 51-10-02, AND DWG 146A7901, SHEET 66, REV A.SDR SWIA2026060176369Intercostal · corrodedPASSENGER DOOR INTERCOSTAL DD7A IS CORRODED. REMOVED AND INSTALLED PASSENGER DOOR INTERCOSTAL DD7A REF. SRM 51-42-06-001-001-A01 REV 38 AND DWG 601R31702 REV -N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002. LEAK CHKD GOOD AT THIS TIME.SDR R61A2026063000177Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RH LOWER WING SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18. RT WING LOWER SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18 REPAIRED IAW ETD2026-170-009575.SDR R61A2026063000176Skin · damagedDURING HEAVY CHECK MAINTENANCE FOUND LIGHTENING STRIKE THICKNESS REDUCTION AT FR02. CARRIED OUT PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN AT FWD FUSELAGE FR2 BETWEEN CENTER STRGR AND STGR 2L IAW ETD2025-170-922426 REV B.SDR HNAA2026063000560Skin · corrodedLEFT SKIN STRAP CORRODED AT STR19L BTW FR 60-61. REPAIRED IAW SRM 53-00-02RESDR SWAA2026062908234Rib · crackedCRACK LEADING EDGE RIB LOC LE STA 95.96 AT LT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOC LE STA 95.96 AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND DWG 186A1303, SHEET 1, REV A, & DWG 186A1001, SHEET 19, REV-.SDR R61A2026062900173Beam · corrodedDURING HEAVY CHECK MULTIPLE AREAS OF CORROSION AROUND PREVIOUSLY BLENDED AREAS OF AFT PAX DOOR THRESHOLD BEAM LOCATED AROUND THE FWD AND AFT EVACUATION SLIDE GIRT BAR CUTOUT, FWD AND AFT SERRATED SHIMS. L2 AFT PAX DOOR THRESHOLD BEAM HAS BEEN REPLACED IAW SRM SDR SWAA2026062408446Bracket · crackedCRACKED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING. REPLACED DEFLECTION CONTROL RIB TRAILING EDGE BRACKET LOCATED ORSS 272 LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV.SDR SWAA2026062308223Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN. REPLACED SUPPORT ANGLE BS 867 BETWEEN S2R TO S3R PASSENGER CABIN IAW SRM 51-40-02-0G-0, & DWG 146A7901, SHEET 58, REV-.SDR SWAA2026062308323Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SIMA20260601003Floorbeam · corrodedSSI 53-23-005 AFT GALLEY RIGHT CENTER FLOOR BEAM AT FR 86 IS CORRODED. (LVL 2 CORROSION) (MAJOR REPAIR) ACCOMPLISHED A PERMANENT REINFORCING REPAIR ON AFT GALLEY RIGHT CENTER FLOOR BEAM AT FR 86 IAW ERS-EJ-53MR-5459SDR AALA202606223403Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL AT STA 500 AND S26R. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.SDR AALA202606226884Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN STA 460 AND STA 500I AT S26L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.SDR AALA202606227573Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHIELD AT BS 500A AT S26R. REPLACED SHIELD PER AARD 51-00-05-01.SDR AALA202606223006Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM AROUND FASTENER HOLE AT STA 986.5 AND LBL 43. REPAIRED FLOORBEAM PER EA 375815.SDR CALA2026062217204Floorbeam · corrodedB737-MP-2000-53-410-00-01 MAIN CABIN FLOOR BEAM STA 947.5 HAS CORROSION ON THE UPPER SURFACE AT APPROX LBL53. REMOVED DAMAGED CHORD (UPPER) REPLACED & INSTALLED NEW REPAIR PARTS AT STA 947.5 FROM LBL41 TO LBL58.6 WL 208 IAW SRM 53-70-51-2R-5 REPAIR 5 ALTERNASDR IPXA2026061648877Support · crackedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, INTERCOSTAL IS CRACKED AT BS 990. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR IPXA2026061148884Tee Angle · corrodedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, TEE ANGLE HAS EXFOLIATED CORROSION, BTWN BS 1040 AND BS 1060 AT RBL 68. INSTALLED NEW TEE ANGLE RT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, BTWN BS 1040 AND BS 1060 AT RBL 68 IAW SRM 51-40-02-0G.SDR IPXA2026061249095Frame · corrodedRIGHT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, FRAME-WEB HAS CORROSION AT BS 1200 RBL 60. INSTALLED 1 EA FRAME WEB IAW SRM 51-40-02.SDR IPXA2026060648764Support Bracket · crackedLEFT MLG WHEEL WELL, 1EA BRACKET SUPPORT IS CRACKED AT THE 1180 BULKHEAD LWR SECTION. INSTALLED WEB REMOVED FOR ACCESS IN STEP 1 AND NEW BRACKET SUPPORT P/N UP-144N2503-133 INSTALLED IAW 757-200 SRM 51-40-02SDR IPXA2026060949184Support Angle · crackedFAULT-STR-Z100- R/H WING TO BODY FAIRING SUPPORT STRUCTURE AT BS 1300, UPPER T-CHORD BRACKET SUPPORT IS CRACKED. DOT 21-14 INSTALLED NEW ANGLE SUPPORT P/N UP-149N7665-8 IAW 757-200 SRM 51-40-02SDR IPXA2026060946378Floor Panel · corrodedCORROSION UPPER DECK WET AREA FLOOR PANEL WEB EXTERNAL SURFACE AT BS 520 - BS 540, LBL 45.83. INSTALLED FABRICATED PARTS IAW SRM 51-40-02-0G, REV 106, AND DWG 141U5420, SH3, REV-, & DWG 141U5420, SH4, REV F.SDR AALA202606126968Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT STA 540 AND RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202606122980Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT STA 540 AND LBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR HNAA2026061100494Plate · crackedNLG BAY, INTERNAL STRUCTURE, UNDER LH AND RH WHEEL STOPPER PLATE FOUND CRACKED. REPAIRED PLATE IAW SRM 53-11-10SDR CALA2026061016962Skin · corrodedAFT GALLEY DOOR FUSELAGE CUTOUT HAS EVIDENCE OF CORROSION AT DOOR EAL MATING AREA AT STA 992.8 NEAR STR 16R. PERFORMED THE REPAIR TO THE FUSELAGE SKIN P/N 147A3110-4 AND BEAR STRAP P/N: 147A3120-11 IAW ECRA 5370-01242, THE REPAIR IAW PART 1 IS A CATEGORY B RSDR SCNA20260609245Door Frame · crackedL1 DOOR, FOUND FRAME DAMAGED WITH 2 CRACKS AND SEVERAL DAMAGED FASTENERS AT UPPER AFT CORNER OF THE DOOR FRAME. REMOVED AND REPLACED L1 DOOR FRAME IAW SRM 51-40-02-0G-0/ DWG NO. 141A6101.SDR DALA2026060903435Door Frame · corrodedCORROSION ON ANGLE DOOR JAM BTW BS 370 TO 389 APROX AT FWD CARGO COMPARMENT. REPAIRED IAW SRM 51-40-02 (1625046) (AIRCRAFT GROUNDED).SDR SWAA2026060808105Battery Pack · inoperativeINOPERTIVE LIGHTS ASSOCIATED TO EMERGENCY BATTERY PACK M2335. REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK M2335 AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805.SDR IPXA2026060248829Splice Plate · corrodedRT LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, SUPPORT WEB HAS CORROSION AT BS 860 BL0. SURFACE PROTECTION RESTORATION COMPLIED WITH IAW SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR IPXA2026060249026Angle · corrodedR/H LOWER WING TO BODY FAIRING SUPPORT STRUCTURE, T-CHORD "L" ANGLE HAS CORROSION AT BS 1040 AT RBL 68. VERIFIED STEP 3.INSPECTED SURFACE PROTECTION RESTORATION COMPLIED WITH IAW B757-200 SRM 51-20-01-0G-0, AMM 51-21-14-370-801 AND AMM 51-21-15-370-801.SDR IPXA2026060847254Skin Panel · crackedCRACKED SKIN, RT WING T/E OUTBD AILERON PNL 691CB AREA WS 1325. FABRICATE SKIN PANEL PER DWG NO.:65B02108 SH 3 REV."A";PL REV."H", PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 15.2 REQUIREMENT<BR>2. INSTALL FABRICATE THE SKIN PANEL ISDR BAGA2026060800002Sensor · faultedDURING DESCENT THE RIGHT OUTBOARD BRAKE INDICATIED HIGH TEMP SEVERAL TIMES. REMOVED AND REPLACED TEMP SENSOR ON RH OUTBOARD BRAKE ASSEMBLY.SDR 2026FA0000491Safety Valve · defectiveLANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING.SDR 2026FA0000490Safety Valve · defectiveLANDING GEAR EMERGENCY FREE-FALL VALVE FOUND TO BE LEAKING.SDR DALA2026060803420Light · inoperativeL2 ARM LIGHT INOP. FOUND LIGHT ASSY BASE DETACHED, RE-ASSEMBLED LIGHT BASE TO HOUSING, OPS CKS GOOD REF B767 AMM 52-11. (8877306) (AIRCRAFT GROUNDED)SDR 2026FA0000480Windshield · crackedDURING CRUISE FLIGHT OF 150 KIAS, SIC NOTICED WHAT LOOKED LIKE TO BE CRACKS IN SEALANT LOCATED ON THE PIC WINDSCREEN LOCATED AT THE TOP RIGHT CORNER ABOUT A 1/3 OF THE WAY DOWN AS YOU ARE LOOKING AT THE WINDSCREEN FROM THE SIC SEAT, WITH LIGHT VISIBLE THROUGH SDR DXTA2026060508308Strut · malfunctionedAFTER TAKE OFF LG LEVER DISAGREE CAS MESSAGE WAS DISPLAYED. RECYCLED THE LANDING GEAR AS PER THE QRH. IT SHOWS 3 GREEN ON EXTENSION. ON RETRACTION INDICATES A NOSE LANDING MALFUNCTION. LANDING GEAR GRAVITY EXTENSION WAS PERFORMED AS PER PROCEDURE. PLACED AIRCSDR VNAA2026060518401Shutoff Valve · unserviceableL BLEED CAUTION MSG IN FLIGHT / FOUND B1 006926 T/S IAW FIM 36-12-01-810-805. REMOVED AND REPLACED LH HPSOV IAW CRJ900 AMM 36-12-05-000/400-801. OPS CHECK GOOD, LEAK CHECK GOOD.SDR DALA2026060503397Unknown · odorPASSANGERS IN 15 D AND 15E REPORTED OCCASIONAL WHIFS OF BURNING OIL SMELL THAT THEY REPORTED AT TOP OF DESCENT TO THE FLIGHT ATTENDANT. I SPOKE TO THE PASSANGERS AND THEY SAID THEY HAD NO ILLNESS SYMPTOMS AND CONFIRMED INTERMITTANT WHIFFS. INSPECTED PSU PANELSDR DALA2026060503396Oxygen Mask · deployedOXYGEN MASKS OVER 17 A,B,C NEED TO BE RESTOWED. FOUND 17 ABC O2 GENERATOR PIN PULLED AND DEPLETED. R & R O2 GENERATOR AND STOWED MASKS PER AMM 35-21. (LP: 8925703, AIRCRAFT WAS GROUNDED)