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 IPXA2026030469211Gimbal Joint · crackedTHS ACTUATOR UPPER GIMBAL IS CRACKED. INSTALLED TAB WASHER IN HINGE ARMS SECTION B-B ITEM (27) IAW AMM 55-16-36-401.Mar 1, 2026 · N162UP · Airbus A300F4622R · Stabilizer Control SystemSDR SWAA2026032375509Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING T/E. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.Mar 1, 2026 · N245WN · Boeing 7377H4 · Wing, Plate/SkinSDR IPXA2026031770646Panel · corrodedAFT CARGO STA 1540 ON LH SIDE FLOOR ANCHOR POINT HAS CORROSION AROUND FASTENER. INSTALLED NEW REPAIR DOUBLER, NEW SIDE PANEL IAW B757-200PF, SRM 51-40-02.Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWIA2026030175549Floor Support · corrodedLEFT LONGITUDINAL FLOOR BEAM JUST PASS THE LT AND CENTER SHEAR PANELS HAS CORROSION AROUND RIVET HEAD AT FRAME 87. REMOVED AND REPLACED LH LONGITUDINAL BEAM BETWEEN FR 86-89 REF EMB SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE.Mar 1, 2026 · N306SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR AALA202603199803Fitting · damagedAIRCRAFT IN BASE MAINTENANCE: AFT LEFT EMERGENCY EXIT DOOR ESCAPE SLIDE ENCLOSURE HAS DAMAGED PIPE FITTING. REPLACED SLIDE ASSEMBLY PER TASK CARD 26C15053012.Mar 1, 2026 · N413AN · Airbus A321253NX · Escape SlideSDR MASA20260318005Support · corrodedFWD WTBF SUPPORT STRUCTURE FOUND CORRODED AT FR45 BET. BLO.RBL36.FWD WTBF SUPPORT STRUCTURE AT FR45 BET. BLO-RBL36 REPLACED IAW ERJ-175 SRM 5141.02 RELATED TO YQG NRC # 4502565-1OOO-0031Mar 1, 2026 · N89321 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR AALA202603188109Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 986 AND RBL 32. REPLACED WEB PER SRM 51-40-02-0G.Mar 1, 2026 · N989AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR SWAA2026031775358Bezel · crackedPASSENGER CABIN: AFT PASSENGER COMPARTMENT CEILING HORSESHOE PANEL EMERGENCY LIGHT BEZEL CRACKED. INSTALLED NEW AFT PASSENGER COMPARTMENT CEILING HORSESHOE PANEL EMERGENCY LIGHT BEZEL (LENS) IAW AMM 33-51-03.Mar 1, 2026 · N8857Q · Boeing 7378 · Emergency LightingSDR IPXA2026031763179Support Channel · crackedLEFT MLG WW, TANG DOOR FWD CUTOUT, BRACKET SUPPORT AT LOWER SIDE HAS A CRACK. REMOVED DAMAGED BRACKET SUPPORT IAW SRM 51-40-02. INSTALLED PANEL 197DL, IAW AMM 53-36-02-404-006.Mar 1, 2026 · N416UP · Boeing 75724APF · Fuselage Main, StructureSDR SWAA2026031675506Scuff Plate · damagedMODIFY CENTER SCUFF PLATE TO BE INSTALLED ON FWD CARGO DOOR CUT OUT WITH A EXISTING REPAIR REPAIRED BY WELDING CENTER SCUFF PLATE ON FWD CARGO DOOR CUT OUT IAW SRM 53-30-15-2R-1 REPAIR 1.Mar 1, 2026 · N240WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202603135651Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Mar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR AALA202603131087Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-AMar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR AALA202603139792Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Mar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR AALA202603132438Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Mar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR AALA202603136427Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 4 ON LH HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING NO 4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Mar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR AALA202603134645Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 5 ON LH HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING NO 5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Mar 1, 2026 · N126UW · Airbus A320214 · Elevator StructureSDR SWAA2026031175526Shear Tie · crackedSHEAR TIE, BS 480 BTWN STRINGER 26R - 27R CRACKED. REMOVED AND REPLACED DAMAGED SHEAR TIE IAW SRM 51-40-02.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Internal Mounting StructureSDR SWAA2026031175455Shear Tie · crackedSHEAR TIE CRACKED AT BS 500 BTWN STRINGER 26R & 27R. REMOVED THE DAMAGED SHEAR TIE IAW SRM 51-40-02. REPAIRED PER EA 26-153-00626.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Internal Mounting StructureSDR SWAA2026031175456Stringer · crackedSTRINGER 27R CRACKED IN 2 PLACES, BS 440 - 460. STRINGER SHEARED THROUGH AT BS 460. REMOVED & REPLACED THE DAMAGED STRINGER IAW SRM 51-40-02.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Main, Longeron/StringerSDR SWAA2026031175525Shear Tie · crackedSHEAR TIE, BS 360 BTWN STRINGERS 22R - 23R CRACKED. REPAIRED IAW EA 26-153-00584.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Internal Mounting StructureSDR SWAA2026031175530Stringer Clip · crackedSTRINGER CLIP 22R, BS 360 IS CRACKED. REPAIRED IAW EA 26-153-00584.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Main, Attach FittingsSDR SWAA2026031175713Skin · crackedSKIN CRACKED BS 344, ABOVE STRINGER 22R. REPAIRED IAW EA 26-153-00584.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Main, Plate/SkinSDR SWAA2026031175714Stringer · deformedSTRINGER 22R DEFORMED IN TWO PLACES, BS 356 & 341. REPAIRED IAW EA 26-153-00584.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Main, Longeron/StringerSDR SWAA2026031175529Stringer Clip · crackedSTRINGER CLIP LOCATED AT STA 344, S22R BENT AND CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02. REPAIRED IAW EA 26-153-00584.Mar 1, 2026 · N8745K · Boeing 7378 · Fuselage Main, Attach FittingsSDR IPXA2026031166900Profile · crackedLEFT BTW FR73-76 Z-PROFILE HAS A CRACK. REMOVED Z-PROFILE BTW FR73- FR76 IN ZONE 200 L/H SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED L/H BTW FR73-76 Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026031170844Profile · crackedMDC AFT SECTION RH SIDE, Z PROFILE CRACKED AT FR 74. REMOVED Z-PROFILE BTW FR73- FR76 IN MDC AFT SECTION RT SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED RT Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026031170858Profile · crackedMDC AFT SECTION LT SIDE, Z PROFILE CRACKED AT FR 79. REMOVED Z-PROFILE IN MDC AFT SECTION IAW SRM 53-18-18, AND SRM 51-40-21. INSTALLED THE PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR 2026F00022O-Ring · leakingDURING INITIAL CLIMB THE ENGINE 1 INDICATES LOW OIL QUANTITY, SHOWING 3 IN TOTAL . WORK PERFORMED IAW AMM 79-00-00-200-802-F00 AND OIL LEAK WAS IDENTIFIED ON OIL NOZZLE PLUG. CONSIDERING THE FINDING WORKS PERFORMED IAW AMM 70-30-01-910-802-F00: REPLAEMENT Mar 1, 2026 · Boeing 737800* · Turbine Engine Oil SystemSDR SWAA2026030575655Handle · looseFORWARD SERVICE DOOR ASSIST HANDLE LOOSE. TIGHTENED THE ASSIST HANDLE IAW AMM 52-41-31-400-802.Mar 1, 2026 · N8610A · Boeing 7378H4 · Service DoorsSDR SWAA2026030575654Pin · disengagedSEAT ROW 14FED OVERHEAD EMERGENCY LIGHT INOPERATIVE. ON INVESTIGATION; FOUND PIN B NOT FULLY ENGAGED IN CONNECTOR D14816. TERMINATED IAW WDM 33-51-12 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-03-960-805, STEP 5.D.(3).Mar 1, 2026 · N8610A · Boeing 7378H4 · Light System WiringSDR AALA202603051816Stop Fitting · out of positionAIRCRAFT IN BASE MAINTENANCE: FORWARD ENTRY AFT FRAME 3RD STOP FROM TOP STOP FITTING INSERT ROTATING AND LOOSE IN STOP FITTING. ADJUSTED STOP FITTING INSERT. PER AMM 52-11-00.Mar 1, 2026 · N990AN · Boeing 737823 · Passenger/Crew DoorsSDR AALA202603053779Repair · expiredAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WHEEL WELL VAPOR BARRIER CRACK REPAIR EXPIRED. PERFORMED 2 INCH REPAIR. PER AARD 57-10-10-9 MAINTENANCE BASE ONLY PARAGRAPHMar 1, 2026 · N922AN · Boeing 737823 · Fuselage Main, BulkheadSDR IPXA2026030561754Former · crackedNOSE FORMER, LT WING L/E OTBD DOOR LINK INNER FORMER OF THE CRACK AT OSS 499. REMOVED DAMAGED FORMER IAW SRM 51-40-02-0G, REV 94. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2161, SHT 6, REV -, AND SREO-50900-REQ001, REV2. JOB COMPLETEMar 1, 2026 · N351UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026030561788Former · crackedLEFT WING L/E ATTACH INTERNAL FORMER CRACKED AT OSS 441, NR 5 SLAT. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 94. INSTALLED NEW FORMER IAW SRM 51-40-02-0G REV 94, AND DWG 114T2241 SH. 4 REV -, AND SREO-54290-REQ1, REV 2. JOB COMPLETED.Mar 1, 2026 · N351UP · Boeing 76734AF · Wing Main, Frame StructureSDR AALA202603051292Door · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT LAVATORY-D DOOR WILL NOT OPEN FROM INSIDE, FLIGHT ATTENDANT HAD TO OPEN DOOR FROM OUTSIDE. LUBE AFT LAVATORY-D DOOR. PER AMM 25-40-00.Mar 1, 2026 · N887NN · Boeing 737823 · Fixed Inner DoorsSDR DALA2026030501521Fuel Tank · crackedCRACKED WEB, FUEL TANK, X=56 APROX BS 696 AT LH CENTRAL FUEL TANK. : WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK WAS REPAIRED PER ERA 631718-14AD (1474080)Mar 1, 2026 · N949AT · Boeing 717200 · Fuel StorageSDR DALA2026030501520Frame · crackedCRACKED FRAME BS 1133, LONGERON 2 RT, AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW ERA 631717-14 REV. (1474071)Mar 1, 2026 · N949AT · Boeing 717200 · Fuselage Main, FrameSDR IPXA2026030462840Support Bracket · crackedCRACKED BRACKET, LT WING L/E COMPARTMENT TORQUE TUBE SUPPORT BRACKET. INSTALLED NEW BRCKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.Mar 1, 2026 · N351UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA2026030462846Support Bracket · crackedCRACKED SUPPORT, RT WING L/E NR.7 SLAT PNL NO. 611KB TORQUE TUBE SUPPORT. INSTALLED NEW BRCKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.Mar 1, 2026 · N351UP · Boeing 76734AF · Leading Edge DevicesSDR DALA2026030401501Packing · leakingAFTER 35 MIN FLIGHT FAS REPORTED BURNING PLASTIC SMELL FROM THE BACK GALLEY. SHORTLY AFTER WE ALSO SMELLED IN THE FLIGHT DECK DONNED MASKS AND EXPEDITED TO SLC AND COMPLETED QRH. C/W W/C 0550-2001 STEPS 1-10+13-16 COMPLETED STEP 11 OF W/C 0550-2001. C/W BSI OFMar 1, 2026 · N110DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2026030401498Oil System · overservicedDIRTY SOCK SMELL NOTICED IN THE FLIGHT DECK ON FINAL APPROACH SLOWING FROM 170 TO B6 KIAS IT WAS A MOMENTARY STRONG SMELL THEN SLOWLY DISSIPATED. FILLED OUT ODOR FORM. WORKING ON W/C 0550-2001 TO STEP 8. WILL REQUIRE HP ENGINE RUN NEXT. (613097) FOUND #1 ENGINMar 1, 2026 · N124DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2026030401497Seat · stuckLOOSE PART UNDER CAPTAIN SEAT GOT CAUGHT AT CRUISE AND SEAT STUCK IN FULL AFT POSITION, NOT SAFE FOR FLIGHT UNTIL FIXED. FOUND CABLE PULLEY AND BOLT DISCONNECTED & HARDWARE LOOSE, ALL PARTS INTACT . RESECURED MISSING HARDWARE IAW A220 AMP 25-11 , OPS CHECK GOOMar 1, 2026 · N121DU · Airbus BD5001A10 · Flight Compartment EquipmentSDR YENA2026030400267Skin · dentedDURING HEAVY MAINTENANCE: #1 RH SLAT DAMAGED; REFERENCES: /1/ STS EA 166-2026-004 /2/ MX-244. DESCRIPTION: DURING THE CURRENT C3 CHECK (02/2026) FOR A/C N988JT AT MLB, MX-INDUCED DAMAGE RESULTED IN A DENT ON THE RH WING SLAT 1(PN: D5746091000300, SN: SA8926) LMar 1, 2026 · N988JT · Airbus A321231 · Leading Edge DevicesSDR YEN2026F00002Floor Support · corrodedDURING HEAVY MAINTENANCE: CPCP TASK CABIN FLOOR BEAM Y -512.5 CONOSION DAMAGE ON AT FR67; FLOORBEAM Y-512.5 BETWEEN FR67 AND FR70 REMOVED AND REPLACED IAW A321 SRM 51-11-911-001 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0907.Mar 1, 2026 · N913JB · Airbus A321231 · Fuselage Miscellaneous StructureSDR DALA2026030401484Power Supply · inoperativeL4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND POWER SUPPLY M738 BAD. R & R M738 POWER SUPPLY IAW AMM 33-51-07. OPS CHKD GOOD. NO FAULTS. ACFT OK FOR SERVICE. (8450821)Mar 1, 2026 · N173DZ · Boeing 767332 · Emergency LightingSDR YENA2026030400265Floor Support · corrodedDURING HEAVY MAINTENANCE: CPCP TASK EVIDONCE OT CORROSION ON CENTRAL LINE FLOOR BEAM UPPER SURFACE TROM FR. '16 TO '18; ALL WORK ACCOMPLISHED ON STS WO W004054 NR N00492 REPLACED FLOORBEAM Y254 BTWN FR 12 TO FR 24 IAW A321 SRM 51-42-11 PAR 2E AND 2F.Mar 1, 2026 · N913JB · Airbus A321231 · Fuselage Miscellaneous StructureSDR YENA2026030400264Mount · corrodedDURING HEAVY MAINTENANCE: CPCP TASK FWD GALLEY MOUNTING POST @FR 14 ON Y-81 FLOOR BEAM CORRODED; REMOVED AND REPLACED FLOOR BEAM Y-81 AT FR 12 TO FR 16 IAW A321 SRTM 51-42-11 AND SRM 53-11-14-10-C ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0496.Mar 1, 2026 · N913JB · Airbus A321231 · Fuselage, Equipment Attach FittingsSDR YENA2026030400263Floor Support · corrodedDURING HEAVY MAINTENANCE: CPCP TASK MULTIPLE AREAS OF CORROSION ON FLOOR BEAM Y1292, FR 66-68 (L4 DOOR); REMOVED AND REPLACED FLOOR BEAM Y1292 FR 66 TO FR 68 (L4 DOOR) IAW A321 SRM 51-42-11 AND SRM 51-72-11 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N0521.Mar 1, 2026 · N913JB · Airbus A321231 · Fuselage Miscellaneous StructureSDR YENA2026030400262Floor Support · corrodedDURING HEAVY MAINTENANCE: CPCP TASK MULTIPLE AREAS OF CORROSION ON FLOOR BEAM .Y765, FR66, FLOORBEAM -Y765 BETWEEN FR 66 AND FR 70 REMOVED AND REPLACED IAW A321 SRM 51-72-11-900-001 ALL WORK ACCOMPLISHED ON STS WO W004054 NR N 0525.Mar 1, 2026 · N913JB · Airbus A321231 · Fuselage Miscellaneous StructureSDR YENA2026030400261Floor Support · corrodedDURING HEAVY MAINTENANCE: FLOOR BEAM Y-160.5, FRAME 67 TO 70, A321 SRM 53-41-14-15-H (|TEM 400); REMOVED AND REPLACED FLOOR BEAM Y-160.5 IAW A321 SRM 51-22-11-*901-001 AND EA 160-2025-008 REV IR RDAF# 81712104/002/2025#A JETBLUE EC # A25-1103-01 ALL WORK ACCOMMar 1, 2026 · N913JB · Airbus A321231 · Fuselage Miscellaneous Structure