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 VNAA2026040920125Slat Track · chafedRH WING SLAT 2 TRACK 1 WEAR ON UPPER SURFACE. LOCATION 12.5" FROM SLAT ATTACHMENT POINT.SDR VNAA2026040920123Slat Track · chafedLH WING SLAT 1 TRACK 1 HAS DAMAGE.SDR VNAA2026040920127Slat Track · gougedRH SLAT 3 TRACK OBD HAS 3 SMALL GOUGES ON THE FLANGES OF THE TRACK UPPER SURFACE.SDR VNAA2026040950052Skin · damagedDAMAGE ON SKIN LH OBD FLAP FS179.96 UPR BAY.SDR VNAA2026040920559Cradle · wornR/H INBOARD FLAP, VANE ACTUATOR CRADLE ASSY, L/H INSIDE TRACK SHOWS WEAR.SDR VNAA2026040920149Crossbeam · corrodedCORROSION FOUND ON CROSSBEAM FS333 RH SIDE 5 IN FROM EDGE OF THE MEMBER P/N:SH670-32127-5.SDR VNAA2026040920122Slat Track · gougedLH WING, SLAT 3 OBD TRACK HAS 4 MARKS IN TRACK UPPER SURFACES OF FLANGES.SDR VNAA2026040920077Floorbeam · corrodedDURING MAINTENANCE INTERGRANULAR CORROSION WAS FOUND ON BEAM LOCATED AT FLOOR SUPPORT STRUCTURE FS280. ALL CROSS THE UPPER SURFACE OF BEAM, WL72.5 . ADJACENT FINDING OF CORROSION ON ANGLE CAPS LBL11.128 FS280 AND RBL11.128SDR CALA2026040915234Gusset · damagedLEFT FR 66 GUSSET NR 7, HOLE NR 1, GUSSET NR 8, HOLE NR 2, HAS AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 66 GUSSET NR 7 & 8 WITH PART 2EA D534 800207 5802 IAW SRM 51-72-11-911-001 SRM 51-42-11/001.SDR SWIA2026032775679Beam · corrodedAFT WET ARE RT BEAM ATFRAME 87 Y+10.748 HAS CORROSION PRESENT. REMOVED AND REPLACED AFT WET AREA RT BEAM AT FR 87 Y+ 10.7" IAW SRM 51-40-08. PN 170-65669-004 PO# 345038.SDR 2026FA0000256Static Inverter · failedELEC LIGHT ON, C/B RESET IAW AMM 24-31-00-740-801. STATIC INVERTER WAS REPLACED IAW AMM 24-34-21-000-801/400-801.SDR 2026F00061Current Limiter · faultedR & R CURRENT LIMITER OPS CHECK GOOD IAW 24-30-25 RTS CHECKS COMPLETESDR TSAA2026032700002Skin · damagedFELT TAIL STRIKE ON ROTATIONSDR CALA2026040114995Rib · crackedLEFT HORIZONTAL STAB INTERNAL RIB AT STA 111.10 HAS A CRACK AT THE BOTTOM OF THE NR 3 VERTICAL STIFFENER ON THE INBD FACING SIDE OF THE OF THE RIB. REPAIRED RIB NR 3 VERTICAL STIFFENER PER SRM 55-10-09 2R REPAIR 4SDR CALA2026040114994Rib · crackedLEFT HORIZONTAL STAB INTERNAL RIB AT STAB STA 111.10 HAS A CRACK AT THE BOTTOM OF THE NR 4 VERTICAL STIFFENER ON THE INBD FACING SIDE OF THE RIB. REPAIRED RIB NO.4 VERTICAL STIFFENER @ STA 111.10 PER B737-900 SRM 55-10-09-2R REPAIR 4.SDR CALA2026040114993Floorbeam · corrodedMAIN CABIN AFT WET AREA FLOOR BEAM HAS CORROSION ON UPPER SURFACE AT BS 1016 APPROX LBL 34.5. ACCOMPLISHED STA 1016 FLOORBEAM STRAP REPAIR IAW UAL ECRA 5375-01020 AND AAR REO-G25844 REV IR.SDR CALA2026040114992Floorbeam · corrodedMAIN CABIN AFT WET AREA FLOORBEAM HAS CORROSION ON UPER SURFACE AT BS 986.5 APPROX LBL45. ACCOMPLISHED STA 986.5 FLOORBEAM SPLICE REPAIR IAW UAL ECRA 5375-01019 AND AAR REO-G25834 REV IR.SDR VNAA2026040115401Pitch Control · faultedPITCH FEEL CAUTION AND STAB CH 1 INOPERATIVE. STATUS MESSAGE IN FLIGHT. PERFORMED SPOST IAW AMM 27-61-05-740-801-A03-PSA. FAULTS EXTINGUISHED.SDR DALA2026040102120Radome · damagedSHIP 3247 DISC: BIRDSTRIKE WHILE FLARING TO LAND IN SMF RWY 35R. APPEARED TO BE DOVE SIZED. WALK-AROUND SHOWED STRIKE ON RADOME CAPT'S SIDE DIVERTER STRIP. CONTRACT MX NOTIFIED. C/A: PERFORMED BIRD STRIKE INSP PER A320 AMM 05-51, NO OTHER DAMAGE NOTED. REMOVEDSDR DALA2026040102119Skin · corrodedDURING M2 AND WHILE INSPECTING PER JIC 5320-6010-DE, CORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. AT REV A STAGE II DTE IS COMPLETE. STAGE III PENDING. C/A: *DTE* PER SECTION DTE I, THE REPAIR OF SECTION SDR SWAA2026033183842Skin · delaminatedLEFT WING AFT OTBD FLAP, AFT FLAP ASSY INBD UPPER SKIN WAS DELAMINATED, LENGTH: 9', WIDTH: 4-1/2, PERFORMED TIME LIMITED REPAIR IAW EA 26-157-00845 TO LT OTBD AFT FLAP.SDR DALA2026033102112Anti-Ice Valve · faultedAIRCRAFT DIVERTED TO LAX DUE TO RIGHT ENGINE STATOR ANTI-ICE VALVE CLOSED FAULT. FLIGHT UNABLE TO CONTINUE DUE TO ICING. PERFORMED RIGHT ENGINE FADEC SYSTEM TEST PER A350AMM, TEST OK AND MESSAGE CLEARED. (LP# 8376425)SDR DALA2026033102111Elec Connector · loosePER CREW REPORT EMERGENCY EXIT LIGHT ABOVE DOOR 2L INOP. FOUND CONNECTOR ON LIGHT LOOSE, RESECURED CONNECTOR OPS TEST GOOD AT THIS TIME. (LP# 8181924)SDR AALA202603311878Battery · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT (AALA202603300492) AND BATTERY (AALA202603311878). PER AMM 25-64-00.SDR AALA202603310492Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR (AALA202603300492) SUBMITTED 03/30/2026 BY DFW: REPLACED FLASHLIGHT (AALA202603300492) AND BATTERY (AALA202603311878). PER AMM 25-64-00**(CLOSED).SDR AALA202603318454Power Port · burnedAIRCRAFT WAS GROUNDED: ELECTRICAL SMELL FROM ROWS 19-20 DESCRIBED AS PLASTIC BURNING SMELL AND PERSISTENT FROM MULTIPLE PEOPLE. COULD NOT ISOLATED INCLUDING TURNING OFF AND OUT ALL ELECTRICAL DEVICES. SOURCE IDENTIFIED TO 19F, REMOVED AND REPLACED POWERPORTS ASDR AALA202603315039Power Port · burnedAIRCRAFT WAS GROUNDED: ELECTRICAL SMELL FROM ROWS 19-20 DESCRIBED AS PLASTIC BURNING SMELL AND PERSISTENT FROM MULTIPLE PEOPLE. COULD NOT ISOLATED INCLUDING TURNING OFF AND OUT ALL ELECTRICAL DEVICES. SOURCE IDENTIFIED TO 19F, REMOVED AND REPLACED POWERPORTS ASDR AALA202603316791Power Port · burnedAIRCRAFT WAS GROUNDED: ELECTRICAL SMELL FROM ROWS 19-20 DESCRIBED AS PLASTIC BURNING SMELL AND PERSISTENT FROM MULTIPLE PEOPLE. COULD NOT ISOLATED INCLUDING TURNING OFF AND OUT ALL ELECTRICAL DEVICES. SOURCE IDENTIFIED TO 19F, REMOVED AND REPLACED POWERPORTS ASDR AALA202603313509Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT 4R INBOARD FLIGHT ATTENDANT SEAT INOPERATIVE DUE TO FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT. PER AMM 25-64-00.SDR AALA202603316584Light · detachedAIRCRAFT WAS NOT GROUNDED: SEAT 10C EMERGENCY LIGHT IS DANGLING. (OPEN).SDR AALA202603318596Sign · dislodgedAIRCRAFT WAS NOT GROUNDED: AFT CABIN OVERHEAD EXIT SIGN FELL FROM CEILING. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. PER AMM 33-51-01. OPS CHECK GOOD.SDR AALA202603312668Power Port · burnedAIRCRAFT WAS GROUNDED: ELECTRICAL SMELL FROM ROWS 19-20 DESCRIBED AS PLASTIC BURNING SMELL AND PERSISTENT FROM MULTIPLE PEOPLE. COULD NOT ISOLATED INCLUDING TURNING OFF AND OUT ALL ELECTRICAL DEVICES. SOURCE IDENTIFIED TO 19F, REMOVED AND REPLACED POWERPORTS ASDR DALA2026033102107Window Frame · crackedWINDOW INSPECTION FOUND CRACK ON R3 LOWER FWD FRAME. COMPLIED WITH B737-800 / WINDOW / RHS NO. 3 FLIGHT COMPARTMENT WINDOW FRAME CRACK PERMANENT REPAIR - ER/A 620149-14ADTR REV. ORIGINAL.SDR DALA2026033102106Window Frame · crackedWINDOW INSPECTION FOUND CRACK ON L1 UPPER LT FRAME. COMPLIED WITH WINDOWS / FLIGHT COMPARTMENT FIXED LH NO.1 WINDOW FRAME UPPER CORNER CRACK PER ERA 620146-14. (LOG 1514547)SDR DALA2026033102105Window Frame · crackedWINDOW INSPECTION FOUND CRACK ON R1 WINDOW UPPER RT FRAME. COMPLIED WITH B737-800 WINDOWS FLIGHT COMPARTMENT FIXED RH NO.1 WINDOW FRAME UPPER CORNER CRACK PER ERA 620147-14.SDR DALA2026033102104Pin · detachedSEAT 2C EMERGENCY LIGHTS INOP. RECONNECTED EMERGENCY LIGHT PINS FOR SEAT 2C PER STANDARD WIRING PRACTICE MANUAL 20-30. OPS CHECKED GOOD. (LOG 8267790)SDR DALA2026033102103Rod · disconnectedFA AND JET BRIDGE OPERATOR UNABLE TO OPEN L1 DOOR. FOUND HANDLE MECH CONNECTION ROD DISCONNECTED. RECONNECTED ROD. OPS CHK GOOD.SDR YENA2026033100363Skin · damagedDURING HEAVY MAINTENANCE: AFT FUSELAGE/ TAILCONE/ SKIN PANEL BTWN FR84-85 AND STGR16R/20R/ EXISTING REPAIR DOUBLER AND DISPREPANT HOLES/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0025-26 COVER & PART 1 /2/ AIRBUS RDAF 70574427/048/2026#A /3/ MX244. DESCRSDR YENA2026033100362Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / LHS LOWER LATERAL PANEL / BTWN FR5-FR6 / EXISTING REWORKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0027-26 REV. 0 (COVER + PARTS 1-2) /2/ AIRBUS DOSSIER 81764255 /3/ AIRBUS RDAF 81764255/004/20SDR YENA2026033100361Structure · wornDURING HEAVY MAINTENANCE. WEAR ON VERTICAL MEMBER Y254 LOC ON FR24A ON FWD CARGO COMPARTMENT; REMOVED AND REPLACED VERTICAL MEMBER Y254 LOC FR24A ON FWD CARGO COMPARTMENT IAW AMM 25-54-81-400-801-A.SDR YENA2026033100360Structure · wornDURING HEAVY MAINTENANCE: WEAR ON VERTICAL MEMBER Y765 FR24A ON FWD CARGO COMPARTMENT; REMOVED AND REPLACED VERTICAL MEMBER Y765 FR24A ON FWD CARGO COMPARTMENT IAW AMM 25-54-81-400-801-A.SDR YENA2026033100359Skin · dentedDURING HEAVY MAINTENANCE: DAMAGE ON CAPT SIDE FUSELAGE BTWN FR 5 & 7 LOWER HALF DENTED. ACCOMPLISHED REPAIR OF EXISTING REWORKS NOSE FWD FUSELAGE LT LOWER LATERAL PANEL BTW FR 5 TO 6 IAW EA 53-0027-26, REV 0, & RDAF 81764255/004/2026, ISSUE A, & EC A26-248-SDR CALA2026033114984Heater · faultedCREW REPORTS R ELEVATOR PITOT HEAT MSG INFLIGHT. FOUND RIGHT ELV PITOT CB POPPED AT P18-3 D4 RESET POPED AGAIN WHEN POWER APPLIED. REMOVED AND REPLACED RIGHT ELEVATOR PITOT TUBE IAW AMM 27-31-94-400-801, HEATER TESTED OK IAW AMM 30-31-00-730-801, LEAK TESTEDSDR 2026FA0000242Crossbeam · corrodedAFT CARGO COMPARTMENT AT FRAME 65 CROSS BEAM, T-SHAPE LATCH AT RIGHT HAND SIDE FWD BELOW SURFACE FOUND CORROSION.SDR DALA2026033002093Dummy Rail · corrodedCORRODED DUMMY RAIL Y503.2 LOCATED BTW FR 12 TO FR 16 FWD GALLEY AREA. REPLACED THE DUMMY RAIL IAW SRM 51-42-11, SRM 51-72-11, DWG D53112825, ISSUE E00. DWG D53112758, ISSUE F00, & DWG D53110984, ISSUE C00. TOOK MEASUREMENT OF CORROSION: L: 0.543 INCH, WSDR DALA2026033002086Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y765, BTW FR 66 & FR 70 IN AFT GALLEY AREA. INSTALLED SPLICES ON FR 66 IAW SRM 51-42-11, AND DWG D53472816, ISSUE A. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472816, ISSUE A. TOOK MEASURESDR DALA2026033002085Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 69 & FR 70 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472780, TOOK MEASUREMENT OF CORROSION: L=1.014 IN, W= 0.840 IN, D= 0.044 IN, (LP: 1515362)SDR WX0A2026033032772Apu · odor(AIRCRAFT NOT GROUNDED) AFT FA'S REPORT A CHEMICAL OR DIRTY SOCK OR DIRTY SOCK SMELL ON APPROACH INTO KJKA. THEY REPORTED THE SMELL WAS NOTICABLE IN THE AFT GALLEY AND LAST FOR APPX 10 MIN / PERFORMED TC 21-000-001 AND FOUND SOURCE OF SMELLÏ¿½COMING FROM THESDR 2026FA0000241Uplock · contaminatedAFTER TAKE OFF LANDING GEAR NOT UPLOCKED AND AFTER LANDING : LANDING GEAR SYS DISAGREE NOSE LANDING GEAR UNLOCKED RED INDICATION AND ON SD RED TRIANGLE DURING INITIAL CLIMB. IAW TSM 32-31-00-810-865-A THE GREASE CONTAMINATION OF THE UPLOCK N.L.G PROXIMITY SESDR AALA202603300492Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. (OPEN).