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.

SDR N6WA2026041304Seat Track · corrodedFOUND CORROSION ON SEAT RAIL AT LBL 9 BETWEEN FS581-FS693 NEEDS TO BE REPLACED. REMOVED AND REPLACED SEAT RAIL AT LBL9 BETWEEN FS581-FS693 IAW CRJ AMM 53-00-45.Apr 13, 2026 · N659CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026041303Seat Track · corrodedFOUND CORROSION ON SEAT RAIL AT STGR 15R BETWEEN FS477-FS581 NEEDS TO BE REPLACED. REMOVED AND REPLACED SIDE SEAT RAIL AT STGR 15R BETWEEN FS477-FS581 IAW CRJ AMM 53-00-49.Apr 13, 2026 · N659CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026041302Seat Track · corrodedFOUND CORROSION ON SEAT RAIL AT STGR 15L BETWEEN FS581-FS669 NEEDS TO BE REPLACED. REMOVED AND REPLACED SIDE SEAT RAIL AT STGR 15L BETWEEN FS581-FS669 IAW CRJ AMM 53-00-49.Apr 13, 2026 · N659CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026041301Seat Track · corrodedFOUND CORROSION ON SEAT RAIL AT STGR 15L BETWEEN FS477-FS581 NEEDS TO BE REPLACED. REMOVED AND REPLACED SIDE SEAT RAIL AT STGR 15L BETWEEN FS477-FS581 IAW CRJ AMM 53-00-49.Apr 13, 2026 · N659CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WX0A2026041332784Battery Pack · inoperative(AIRCRAFT NOT GROUNDED) EPSU 10WL BATTERY FAILS EMERGENCY LIGHT CHECK / REMOVED AND REPLACED EPSU BATTERY 10WL IAW AMM 33-51-38-000-002A AND 33-51-38-400-002A OPS CHECK GOOD."Apr 13, 2026 · N301NV · Airbus A319112 · Emergency LightingSDR IPXA2026041371289Fitting · noneNR 2 WING STRUT SUPPORT CLEVIS FITTING FREEZE PLUG - PERMANENT REPAIR. CONDITION CHECK NORMAL. PAPER FINAL CHECK OK.Apr 13, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame StructureSDR GTIA2026041339352Megaphone · inoperativeFWD MEGAPHONE INOP .-R & R FWD MEGA PHONE REF AMM 25-65-51. NO DEFECTS NOTED.Apr 13, 2026 · N626NK · Airbus A320232 · Emergency EquipmentSDR DALA2026041302328Seat Track · corrodedCABIN SEAT TRACK AT FR36 RBL 61.12 FOUND WITH CORROSION. REPAIRED PER ERA 632442-14 REV ORIGINAL. (1542053) AIRCRAFT WAS GROUNDED.Apr 13, 2026 · N819NW · Airbus A330323 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026041302327Rib · corrodedRIGHT MLG RIB 6 FWD LUG BORE CORROSION. COMPLIED WITH ERA 632186-14AD REV ORIGINAL. (1542006) AIRCRAFT WAS GROUNDED.Apr 13, 2026 · N816NW · Airbus A330323 · Wing, Landing Gear Attach FittingsSDR QR9R2026041300002Display · failedPILOT'S PFD SYMBOLOGY SCRAMBLES AND GOES ON AND OFF ON BATTERY POWER. UNABLE TO GO INTO MAINTENANCE MODE. REMOVED AND REPLACED PILOT'S PFD IAW AMM 31-61-00, 4-1.Apr 13, 2026 · Bolkms BK117C2 · Central DisplaySDR ABXA20260413161Module · faultedAFTER BLOCK OUT AND LT & RT ENGINES STARTED, RUDDER RATIO EICAS CAUTION MESSAGE APPEARED. ACFT RETURNED TO GATE AND MTX GROUNDED ACFT . MTX RESET LT & RR RUDDER RATIO MODULE AND PERFORMED ENGINE RUNS AND NO RUDDER RATIO FAULT IAW FIM 27-09 FT 814 AND AMM 71-00Apr 13, 2026 · N1427A · Boeing 767306 · Rudder Control SystemSDR 2026FA0000266Bearing · brokenFOUND THE LEFT AND RIGHT HAND OUTBOARD NOSE GEAR TRUNNION ASSY BEARINGS BROKEN AT THEIR FLANGES RESULTING IN MUCH SIDE-TO-SIDE PLAY IN THE NOSE LANDING GEAR. INSPECTION OF THE O.D. OF THE TRUNNION ASSY IN WHICH THE BEARINGS ARE INSTALLED WAS IN TOLERANCE. NO OApr 13, 2026 · N445BG · Piper PA44180 · Fuselage, Landing Gear Attach FittingsSDR MASA2026041300015Flashlight · inoperativeAFT EMR FLASHLIGHT INOP. R & R AFT FA FLASHLIGHT ASSY, OPS CK GOOD.Apr 13, 2026 · N85320 · Emb ERJ170200LL · Emergency EquipmentSDR QR9R2026041300001Gcu · faultedGEN DISCON CAUTION LIGHT INTERMITTENT ILLUMINATION DURING HOVER TAXI, NO OTHER INDICATION. GEN OUTPUT WITHIN NORMAL PARAMETERS. THIS WAS THE SECOND TIME WITH SAME CAUTION WITHIN LAST 2 FLIGHTS. REMOVED AND REPLACED #1 GCU IAW AMM 24-30-00, 4-1.Apr 13, 2026 · Bolkms BK117C2 · DC Generating SystemSDR 2026FA0000265Blades · mismanufacturedTHE ENGINE (PT6A-60A, P/N 3102700-01 S/N PCE-PK0793) WAS UNDERGOING A REPAIR I.A.W. P&WC LIGHT OVERHAUL CRITERIA AND WAS TESTED AT EURAVIA. THE ENGINE SUBSEQUENTLY PASSED TEST AND AS PER EURAVIA STANDARD PRACTICE A BORESCOPE POST-TEST WAS PERFORMED. DURING THEApr 13, 2026 · Turbine SectionSDR SWIA2026041277775Skin · chafedLEFT AILERON LEADING EDGE SKIN CHAFED AT MULTIPLE SPOTS. INSTALLED NEW LEADING EDGE SKIN IAW DWG CC670-13000, REV D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22.Apr 12, 2026 · N917SW · Cndair CL6002B19 · AileronsSDR SWIA2026041276857Cap · crackedRIGHT WING WHEEL WELL, FIRST BATT RIB IN MLG CUTOUT CRACKED AT TWO LOCATIONS. REMOVED AND INSTALLED NEW SERVICEABLE CAP ON R/H WING WHEEL WELL, FIRST BATT RIB IN L/G CUTOUT IAW CRJ 200 SRM 51-42-21.Apr 12, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026041276854Channel · crackedLEFT MLG WHEEL WELL, SECOND BATT RIB OTBD, BRACKET CRACKED ON FWD END OF RIB. PERFORMED A MAJOR REPAIR BY REPLACING 2ND BATT RIB CHANNEL , AND ATTACHING ANGLES, OTBD IN LT MLG WHEEL WELL. IAW SRM 51-40-11, 51-42-21, & 51-42-06 COMPLETED SKYWEST RII TASK CAApr 12, 2026 · N926SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 3EJA835JS041226Valve · failedON TAKEOFF CLIMB PRESS FLUCTUATIONS UP TO 4300 ON THE RATE AND BACK DOWN AND BACK UP AGIN ACCOMPANIED WITH A ACM OVERHEAT: REMOVED AND REPLACED LH BILEVEL VALVE IAW AMM 21-11-00. OPS & LEAK CHECKED GOOD.Apr 12, 2026 · N835JS · Cessna 560XL · Cabin Cooling SystemSDR SWIA2026041276298Floor Support · corrodedPASSENGER DOOR FLOOR SILL ANGLE BETWEEN BS 310 TO BS 349 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW MID CAP ANGLE TO PAX DOOR LOWER SILL ANGLE REF DWG. SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA2026041276291Floorbeam · crackedCOCKPIT FLOORBEAM AT BS 280, RBL 12 CRACKED AND CORRODED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM AT BS 280, RBL 12 IAW SRM 53-11-43-201-003-A01.Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR SWIA2026041276266Stringer · corrodedCORROSION ON STRINGER 20L BETWEEN BS 319 AND 333. REMOVED AND REPLACED STRINGER 20L BETWEEN BS 310 AND 349 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH67031810 REV. Y. INSTALLED FASTENERS TO NEW STRINGER 20L BETWEEN BS 319 AND 333 IAW Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR SWIA2026041276255Frame · crackedCRACK AT BS 333 BETWEEN S1R AND S2R. CRACK AT BS 333 BETWEEN S1R & S2R. REPAIRED BS 333 FRAME BETWEEN STRINGERS 1R - 2R. IAW REO 670-53-21-2863, REV -. ALSO COMPLIED WITH 51-900-1002-SKY.Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, FrameSDR SWIA2026041276254Cup · corrodedPASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS342.00 CORRODED. INSTALLED NEW AFT CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY Apr 12, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026041276252Fitting · corrodedPASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS 314 CORRODED. INSTALLED A NEW FWD CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG.SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY TAApr 12, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR VNAA202606120061Stiffener · corrodedCORROSION ON ANGLE BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM. ANGLE (STIFFENER) BTW STGR 25LH/25RH AT BTW 55.265% AND 67.50 % SPAR DATUM WAS REPLACED PER SRM 51-42-06-001-001-A01.Apr 12, 2026 · N649NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR IPXA2026060367876Retainer · crackedFAULT: APG-800-MDC DOOR UNDERNEATH NR 2 LATCHING HOOK HAS STRUCTURE DAMAGE. 33-040 ACCOMPLISHED PERMANENT REPAIR PER EA 300-5236-27-A4484 REV. -.Apr 12, 2026 · N141UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR AALA202606052909Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.Apr 12, 2026 · N9013A · Airbus A319115 · Landing Gear DoorsSDR AALA202606053270Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.Apr 12, 2026 · N9013A · Airbus A319115 · Landing Gear DoorsSDR AALA202606051445Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.Apr 12, 2026 · N9013A · Airbus A319115 · Landing Gear DoorsSDR AALA202606058484Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.Apr 12, 2026 · N9013A · Airbus A319115 · Landing Gear DoorsSDR FJ7A202605270001Control Unit · intermittentON APRIL 12, 2025, WHILE AIRCRAFT N171AM WAS TAXIING FROM THE RAMP AT FORT LAUDERDALE EXECUTIVE AIRPORT (FXE), THE FLIGHT CREW OBSERVED AN EICAS MESSAGE INDICATING “STAB CH 2 INOP.” THE CREW ATTEMPTED TO RESET THE SYSTEM; HOWEVER, THE RESET WAS UNSUCCESSFUL. TApr 12, 2026 · N171AM · Cndair CL6002B16 · Stabilizer Control SystemSDR HNAA2026052000391Floor Support · corrodedRIGHT FLOOR SILL 3 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT FLOOR SILL 3 IAW SRM 51-40-02.Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026052000390Floor Support · corrodedLEFT FLOOR SILL 4 HAVE CORROSION IN MULTIPLE AREAS. R & R LT FLOOR SILL 4 IAW SRM 51-40-02.Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026052000389Floor Support · corrodedLEFT FLOOR SILL 6 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT FLOOR SILL 6 IAW SRM 51-40-02.Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026052000388Seat Track · corrodedLEFT UPPER SEAT TRACK 5 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED LT UPPER SEAT TRACK 5 IAW AMM 53-01-06.Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026052000387Seat Track · corrodedRT UPPER SEAT TRACK 4 HAS CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED RT UPPER SEAT TRACK 4 IAW AMM 53-01-06.Apr 12, 2026 · N655AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026051989213Seal · crackedRIGHT STABILIZER, UPPER BODY-TO-HORIZONTAL STABILIZER SLIDING SEAL CRACKED. REMOVED AND REPLACED RT UPPER SLIDER SEAL IAW AMM 53-31-31.Apr 12, 2026 · N8538V · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026051288539Tail Cone · crackedNUMBER 3 FLAP TRACK FAIRING TAILCONE 542EB TIP IS CRACKED. DUE TO THE EXTENT OF DAMAGE; REPLACED #3 FLAP TRACK FAIRING TAILCONE 542EB IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 27-51-18-01 ITEM 430.Apr 12, 2026 · N8639B · Boeing 7378H4 · Trailing Edge FlapsSDR ASAA2026041265945Cargo Track · corrodedAFT PIT CARGO TRACK HAS CORROSION IB OF DOOR AT STA 787-827. GROUNDED - YES. REPLACED AFT PIT CARGO TRACK I/B OF DOOR AT STA 787-827 IAW B737-800 SRM 53-00-53-2R-3W- 1" O- .070" R- .040" L- 2" D- .030".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026041265944Support · corrodedFWD PIT LOWER AFT BULKHEAD SUPPORT R/H IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER AFT BULKHEAD SUPPORT R/H I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.C.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265943Support · corrodedFWD PIT LOWER L/H AFT BULKHEAD SUPPORT IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER L/H AFT BULKHEAD SUPPORT I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.C.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR SWAA2026050888603Flap Track · corrodedAFTER REMOVED BEARING CORROSION FOUND ON INNER BORE OF OB AFT FLAP TRACK 2 AT LT WING. REPLACED OB AFT FLAP TRACK 2 AT LT WING IAW B737-800 AMM 27-51-26-000-801 AND AMM 27-51-26-400-801.Apr 12, 2026 · N8637A · Boeing 7378H4 · Leading Edge DevicesSDR HNAA2026050500377Bracket · crackedCRACKED BRACKET IN ZONE 155 JUST AFT OF PANEL 155BZ THAT HOLDS SYSTEM 1 PRESSURE AND RETURN HYDRAULIC TUBES. REMOVED AND REPLACED WITH NEW BRACKET IN ZONE 155 JUST AFT OF PANEL 155BZ IAW SRM 51-40-02-PR.Apr 12, 2026 · N654AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026050500376Door · gougedGOUGES ON THE PAX MAIN DOOR AFT BOTTOM SIDE. COMPLIED WITH REPAIR ON MAIN DOOR AFT BOTTOM SIDE SKIN PER EMB 145 ETD2026-145-006635 AND EO1-05-26-0171Apr 12, 2026 · N654AE · Emb EMB145LR · Passenger/Crew DoorsSDR ASAA2026041265822Support · corrodedFWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE PIECE IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.CW- 1" O- .063" R- 0" L- 2" D- .063".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265821Web · crackedFWD PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .045" R: .039" L: 2" D: .006".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265813Web · corrodedAFT PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .050" R: .043" L: 2" D: .007.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265812Plate · corrodedFWD PIT SIDEPLATE R/H SIDE IS CORRODED AT STA 500A-500I. GROUNDED - YES. REMOVED AND REPLACED FWD PIT SIDEPLATE R/H SIDE AT STA 500A-500I IAW BOEING 737-800 SRM 53-00-53-2R-5W: 1" OT: 0.040" RT: 0.032 L: 2" D: 0.008".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265811Plate · corrodedFWD PIT LT SIDEPLATE HAS CORROSION AT STA 500H-500I. GROUNDED - YES. REMOVED AND REPLACED FWD PIT L/H SIDEPLATE STA 500H-500I. IAW B737-800 SRM 51-40-02-0G-0W 1" O .040 R .036 L 2" D .014.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, Structure