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.

SDR VNAA20260623018Bracket · corrodedL/H WHEEL WELL HYD LINE BRACKET IS CORRODED BETWEEN W.S. 0.00 TO W.S. 29.00. REMOVED AND INSTALLED NEW SERVICEABLE HYDRAULIC LINE BRACKET IN LT WHEEL WELL BETWEEN W.S. 0.00 TO W.S 29.00 IAW SRM 51-41-02-001-001-A01 AND AMM 20-22-00-910-801-A01.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20260623017Seat Track · corrodedLBL9 SEAT TRACK BETWEEN BS 985 - BS 1000 FOUND TO BE CORRODED. REMOVED UNSERVICEABLE LBL 9 SEAT TRACK, BTWN BS 985- 1000 IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICABLE LBL9 SEAT TRACK IAW AMM 53-00-49-400-801-A03.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260623016Seat Track · corrodedLEFT SIDE SEAT TRACK BS 713 - 761 SEGMENT IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260623015Fitting · corrodedWHILE PERFORMING INSPECTION OF LT THRUST FITTING IAW AMM 71-22-01-400-801-A01 STEP 4.A.(1). FOUND FRETTING CORROSION ON LT PYLON OUTBD RIB THRUST FITTING HOUSING. REPAIRED LT PYLON OUTBOARD RIB REO 670-54-51-089, REV -.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR VNAA20260623014Fitting · corrodedWHILE PERFORMING INSPECTION OF LH THRUST FITTING IAW AMM 71-22-01-400-801-A01 STEP 4.A.(1) FOUND EVIDENCE OF FRETTING CORROSION ON INTERFACE (MATING SURFACE) OF THRUST FITTING AND DAMAGE FOUND AROUND THE TABS OF THE THRUST FITTING ON THE INTERFACE. (MATING SURJun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260623013Skin · corrodedFUSELAGE EXTERNAL SKIN IS CORRODED BETWEEN BS 517 TO 533 AT STR 27 (UNDER ADF ANTENNA). REPAIRED FUSELAGE SKIN IAW REO 670-53-31-1127, REV -.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260623012Floor Support · corrodedLBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 1000 TO BS 1031. REPAIRED FLOOR SUPPORT IAW SRM 53-0041-201-001-A01, FIGURE 53-00-41-991-830.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260623011Floorbeam · corrodedLBL 27 FLOORBEAM IS CORRODED BETWEEN BS 1000 TO 1031. REPAIRED FLOORBEAM IAW SRM 53-0041-201-001-A01, FIGURE 53-00-41-991-830.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20260623010Cargo Track · corrodedRBL 27 FLOOR SEAT TRACK IS CORRODED BETWEEN BS 985 TO 1000. INSTALLED NEW SERVICEABLE CARGO TIE DOWN FLOOR TRACK ON IAW REO 670-53-00-812 REV -.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260623009Stringer · corrodedSTRINGER 26R CORRODED BETWEEN BS 985 TO BS 1000. COMPLIED WITH REPAIR OF STR 26R BY INCORPORATING REO 670-53-61-2626 REV-.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260623008Frame · corrodedBS 1000 FRAME IS CORRODED BETWEEN S26R TO S25R. REPAIRED CORRODED AREA OF FRAME IAW REO 670-53-61-2626 REV. P1.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260623007Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED BETWEEN BS 1031 TO 1047. INSTALLED NEW SERVICABLE AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260623006Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED BETWEEN BS 364 TO 379. REPAIRED RIGHT FLOOR SILL IAW REO 670-53-00-390 REV -.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260623005Seat Track · corrodedSEAT TRACK AT LBL.9 APPROX BS 830 TO 985 HAS SIGNS OF CORROSION. INSTALLED NEW SEAT TRACK BETWEEN IAW 53-00-49-400-801(CONFIGA03).Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260623004Frame · corrodedBS 333 FRAME IS CORRODED BETWEEN STR 27 TO STR 25L. REMOVED, FABRICATED NEW FRAME SECTOR FROM FRAME IAW 670-53-21-277 REV-. LOCATED AND DRILLED IAW SRM 51-40-11-001-001-A01, AND INSTALLED A NEW FRAME SECTOR IAW REO 670-53-21-2779 REV —, AND SRM 51-42-21-001-Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260623003Angle · corrodedPASSENGER DOOR SILL MID CAP ANGLE IS CORRODED. REMOVED AND REPLACED PASSENGER DOOR SILL MID CAP ANGLE IAW SRM 51-42-13-001-001-A01 AND 51-42-02-001-001-A01.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR HNAA2026062400553Relay · faultedICE CONDITION, ANTI ICE INOP, ENG REF ANTI ICE DISAG, ICE CONDITION DISPLAYED ON TAKEOFF AT 76KTS. R & R RELAYS K0264, K0532, K0531, K0323 IAW AMM 20-13-02. PERFORMED OPS CHKD IAW 30-00-00 AND 30-21-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.Jun 23, 2026 · N932AE · Emb EMB145LR · Engine Anti-Icing SystemSDR VNAA202606230002Seat Track · corrodedLEFT SIDE SEAT TRACK FS861-969 SEGMENT IS CORRODED. REMOVED LT SIDE SEAT TRACK AT FS861-969 IAW AMM 53-00-49-000-801-A03 AND INSTALLED NEW SERVICEABLE LH SIDE SEAT TRACK AT FS861-969 IAW AMM 53-00-49-400-801-A03.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260623001Seat Track · corrodedLEFT SIDE SEAT TRACK FS785-861 SEGMENT IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026062403744Unknown · odorUPON REACHING CRUISE ALTITUDE FL360 RECEIVED CALL FROM FWD. FA ( S) VERY STRONG (C) FORWARD CABIN (E) NO PHYSICAL EFFECTS (N) DIRTY SOCK SMELL (T) LASTED FROM INITIAL CLIMB, COMPLETED QRH SMOKE/FUMES/AVNCS SMOKE WITH AIR COND SMOKE/FUMES SUSPENDED. AFTER CAB FJun 23, 2026 · N339NB · Airbus A319114 · Air Distribution SystemSDR DALA2026062403745Floor Support · corrodedLEVEL 2 CORROSION, PPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR SUPPORT CORRODED AT Y1292, BETWEEN FR67 AND FR68. REPLACED LONGITUDINAL FLOOR SUPPORT AT UPPER FUSELAGE AFT PAX CABIN BETWEEN FR66 AND FR68 Y1292 IAW SRM 51-72-11-911-001 REV 158 AND DWG D53Jun 23, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR 2026FA0000537Autothrottle Sys · abnormalPILOTS HAVE REPORTED MULTIPLE INSTANCES OF AUTOTHROTTLE INDUCED WARNING/RED TORQUE INDICATIONS OCCURRING DURING TAKEOFF, GO-AROUND, AND CLIMB PHASES OF FLIGHT ON SIX DIFFERENT AIRCRAFT (S/N BY-472 AND UP). THREE INSTANCES WERE SEVERE ENOUGH TO ACTIVATE THE MASJun 23, 2026 · Beech B200GT · Auto Throttle SystemSDR YENA2026062300490Unknown · odorFLT 1323, BOS-STI. STRONG MAGIC MARKER ODOR PASSING THROUGH 14K ON DESCENT; IAW INFO NOTICE 2017-T015M A/C INSPECTED & ODOR IDENTIFIED AS TYPE 5, APU INSPECTED AND NO OBVIOUS SIGN OF OIL CONTAMINATION FOUND, DECONTAMINATION LEVEL B C/W PACK 2 OPERATED NO ODOR Jun 23, 2026 · N965JT · Airbus A321231 · Air Distribution SystemSDR DALA2026062303739Lamp · inoperativeFLIGHT DECK O/H EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-11. (LP 7959221 - AIRCRAFT WAS GROUNDED)Jun 23, 2026 · N981AT · Boeing 717200 · Emergency LightingSDR DALA2026062303738Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP WEB UPPER SIDE BTW X=-56 AND BS 304-310, BS 456-463, BS 570-577, STA 797-811 AND STA 944. CORROSION LEVEL 2, CUSP WEB UPPER SIDE BTW X=-56 AND BS 304-310, BS 456-463, BS 570-577, BS 797-811 AND 944 WERE REPAIRED IAW SRM 53-00-5Jun 23, 2026 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR IPXA2026062398212Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.Jun 23, 2026 · N304UP · Boeing 76734AF · Passenger/Crew DoorsSDR DALA2026062303727Girt Bar · fodSHIP 3304 2L DOOR WILL NOT ARM. LEVER IS STUCK. REMOVED FOD FROM GIRT BAR AREA. OPS CHECK GOOD. (8315656) AIRCRAFT WAS GROUNDED.Jun 23, 2026 · N804NW · Airbus A330323 · Passenger/Crew DoorsSDR FDEA202606230791Girt Bar · out of adjustRT ENTRY DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL : 52-11-01-A. R1 DOOR OR SLIDE INOP. ADJUSTED R1 DOOR GIRT BAR REF AMM 25-66-10-2. OPS CHECKED GOOD.Jun 23, 2026 · N996FD · Boeing 7572Q8 · Emergency EquipmentSDR JR2R20260623896Seat Track · corrodedEXISTING REPAIR DOUBLER ON SEAT TRACK BEAM RBL11 FR17 CORRODED. REPLACED REPAIRJun 23, 2026 · N86324 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR JR2R20260623895Seat Track · corrodedEXISTING REPAIR DOUBLER ON SEAT TRACK BEAM RBL11 FR16 CORRODED. REPLACED REPAIRJun 23, 2026 · N86324 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR MASA2026062300031Power Supply · looseTWO EMERGENCY CEILING LIGHT FWD CABIN INOPERATIVE. FOUND PWR SUPPLY LOOSE, RESECUREDJun 23, 2026 · N86350 · Emb ERJ170200LL · Emergency LightingSDR JR2R20260623904Seat Track · corrodedEXISTING REPAIR DOUBLER ON SEAT TRACK BEAM LBL11 FR18 CORRODED. REPLACED REPAIRJun 23, 2026 · N86324 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026062303725Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INOP. R & R MT1694 BATTERY PACK PER B737 AMM 33-51. (6457647 - AIRCRAFT WAS GROUNDED).Jun 23, 2026 · N886DN · Boeing 737932ER · Emergency LightingSDR R61A2026062300166Skin · corrodedDURING HEAVY CHECK FOUND AFT CARGO LWR SKIN PANEL STRINGER 29R, FR 75-79 HAS NUMEROUS AREAS OF CORROSION.Jun 23, 2026 · N653RW · Emb ERJ170100SE · Fuselage Main, Plate/SkinSDR R61A2026062300165Shear Tie · corrodedDURING HEAVY CHECK FOUND AFT CARGO LOWER SKIN PANEL HAS 1EA CORRODED SHEAR CLIP AT FR 77, STGR 29L-29RJun 23, 2026 · N653RW · Emb ERJ170100SE · Fuselage Internal Mounting StructureSDR R61A2026062300164Seat Track · corrodedDURING HEAVY CHECK FOUND CENTER FUSELAGE 3 AT FR 84/85, RT SEAT TRACK HAS CORROSIONJun 23, 2026 · N653RW · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20260623277Extinguisher · unsecurePIN TO COCKPIT FIRE EXTINGUISHER NEAR LAV DISCOVERED ON FLOOR BY MTC. REATTACHED PIN TO FIRE EXTINGUISHER HANDLE USING BREAKAWAY WIRE. PLACARDS INSTALLED. ACFT RETURNED TO SERVICE.Jun 23, 2026 · N1489A · Boeing 76731K · Fire Bottle, PortableSDR R61A2026062300163Skin · crackedDURING HEAVY CHECK FOUND CRACK ON R/H WING LOWER SKIN OTBD OF RIB 4 DOUBLERJun 23, 2026 · N653RW · Emb ERJ170100SE · Wing, Plate/SkinSDR SWIA2026062277718Stringer · corrodedCORROSION FOUND ON STRINGER 26R, BS 280 - 333. EXFOLIATED CORROSION RESULTING IN 100 MATERIAL LOSS. INSTALLED A NEW IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG SH670-31630, REV K. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SJun 22, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2026062277717Bulkhead Web · corrodedRIGHT LOWER WEB AT BS 280 HAD CORROSION. EVALUATED THE RT LOWER WEB AND FOUND OUT OF LIMITS, REMOVED AND REPLACED THE RT LOWER WEB AT BS 280 IAW SRM 53-11-10-201-003-A01, REPAIR B, REV 38. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Jun 22, 2026 · N822SK · Cndair CL6002D24 · Fuselage Main, BulkheadSDR SWIA2026062277020Hinge Arm · out of limitsLH OB FLAP HINGE ARM WS178.00 INBD LEADING EDGE-SIDED BUSHING REQUIRES FABRICATION (C-CHECK RO 08/28/2026)PERFORMED A MAJOR REPAIR BY FABRICATING FREEZE PLUG AND DRILLING TO SIZE, AND INSTALLING SERVICEABLE BUSHING INTO HINGE ARM WITH BOMBARDIER REO 601R-57-5Jun 22, 2026 · N477CA · Cndair CL6002B19 · Trailing Edge FlapsSDR IPXA2026082091705Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT, DECK PLATE FLOOR STRUCTURE SUPPORT ANGLE ASSY HAS CORROSION ON NUT PLATE STRAP APPROX AT BS 1715, RBL 24. INSTALLED ONE NUT PLATE STRAP ASSY AT STA 1715 RBL 24 IAW SRM 51-40-02-0G-0. REQUEST OK TO RE-INSTALL PRESSURE DECK PLATE Jun 22, 2026 · N429UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR SWIA2026062276778Door Frame · out of limitsPAX DOOR FWD FRAME FORMER AT BS 311.75 HAD 7EA OVERSIZED HOLES FROM JO-BOLTS ON PREVIOUS REPAIR DOUBLER AT APPROX DD1. REPAIRED OVERSIZED HOLES ON PAX DOOR FWD FRAME FORMER BS 311.75 ON PREVIOUS REPAIR DOUBLER AT APPROXIMATELY DD1 IAW SRM 51-42-06-001-001-A01Jun 22, 2026 · N719SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026062276772Door Frame · crackedUPON REMOVAL OF INNER SKIN FOUND CRACK ON AFT FRAME FORMER BS 347.25 BETWEEN DD4 & DD5. REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER AT BS 347.25 BETWEEN DD4 & DD5 IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601RJun 22, 2026 · N719SK · Cndair CL6002C10 · Fuselage Main, StructureSDR AALA202608072944Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON POSITION 1 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY - REPLACED SUPPORT FRAME PER AMM 57-51-31Jun 22, 2026 · N827AW · Airbus A319132 · Wing Main, Frame StructureSDR AALA202608078041Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON POSITION 3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY - REPLACED SUPPORT FRAME PER AMM 57-51-31Jun 22, 2026 · N827AW · Airbus A319132 · AileronsSDR AALA202608062272Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON HINGE SUPPORT FRAME POSITION 1 HAS EXCESSIVE PLAY - REPLACED SUPPORT FRAME PER AMM 57-51-31Jun 22, 2026 · N827AW · Airbus A319132 · AileronsSDR SWIA2026062276723Skin · corrodedFUSELAGE LWR SKIN EXTERIOR FOUND SIGNS OF CORROSION BTWN BS 501 - 549, AROUND ADF ANTENNA CUT-OUT. REMOVED DAMAGE ON FUSELAGE LOWER SKIN EXTERIOR BETWEEN BS 501 - 549 AROUND ADF ANTENNA CUTOUT, FOUND TO BE STRUCTURALLY ACCEPTABLE IAW SRM 53-31-01, 51-42-06, RJun 22, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR AALA202607314056Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON HINGE SUPPORT FRAME #3 HS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.Jun 22, 2026 · N827AW · Airbus A319132 · AileronsSDR AALA202607313987Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON HINGE SUPPORT FRAME #5 HS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.Jun 22, 2026 · N827AW · Airbus A319132 · Ailerons