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 I5PA2026020888801Brushes · wornAPU INOPERATIVE. FOUND APU STARTER BRUSHES WORN. R & R APU STARTER IAW AMM, OPS CHECKED NORMAL.Feb 8, 2026 · N888LT · Boeing 757230 · APU Start/Ignition SystemSDR G1IA20260208104Relay · failedVFR LANDING PHASE, ON BASE LEG FOR RUNWAY 32 AT XWA. COMMANDED GEAR DOWN. MAIN GEAR LOWERED & LOCKED INTO PLACE. VERIFIED 2 GREEN LIGHTS. NOSE GEAR REMAINED RED, UNSAFE/TRANSIENT POSITION. TURNED ACFT TO FINAL APPROACH & NOSE GEAR REMAINED RED, & AMBER HYDFeb 8, 2026 · N8421E · Pilats PC1245 · Landing Gear Retraction/Extension SystemSDR ABXA20260208063Failsafe · not reportedDURIING C6 CHECK, ON WO 15843154, REPAIRED RH FAILSAFE TRIM-OUT AND RE-ASSEMBLY, STA. 955 IAW ABX-EA-5350-0014-0013. (RH FAILSAFE) AND AMES DOC. 47207ORD04. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, StructureSDR ABXA20260208062Failsafe · not reportedDURIING C6 CHECK, ON WO 15843154, REPAIRED THE LT FAILSAFE TRIM-OUT AND RE-ASSEMBLY, BS 955 IAW EA-5350-0013-0013. LT FAILSAFE AND AMES DOC. 47207ORD03. C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, StructureSDR ABXA20260212061Floorbeam · not reportedDURING C6 CHECK, ON WO 15843154, ACCOMPLISHED ABX-REA-5300-65992-00 (MODIFY - STA 390 TO 720 MAIN DECK FLOORBEAMS AND LOWER DECK CEILING, FQIS WIRE SEPARATION PROVISION, B767). C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.Feb 8, 2026 · N1229A · Boeing 767306 · Fuselage Main, Floor BeamSDR SWAA2026021168977Potable Water · odorF/A STATED A FOUL WATER ODOR FROM AFT GALLEY COFFEE POT. RAMP DRAINED AND REFILLED WATER TANK IAW SIP.Feb 8, 2026 · N910WN · Boeing 7377H4 · Potable Water SystemSDR SWAA2026021168878Battery Pack · inoperativeOVERWING ESCAPE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CHARGER ASSY, & BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06.Feb 8, 2026 · N249WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026021169800Charger · faultedOVERWING ESCAPE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CHARGER ASSY, & BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06.Feb 8, 2026 · N249WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026021168978Handle · looseCREW REPORTS FWD GALLEY SERVICE DOOR ASSIST HANDLE LOOSE. SECURED THE FWD GALLEY DOOR ASSIST HANDLE PER AMM 52-41-31.Feb 8, 2026 · N8313F · Boeing 7378H4 · Service DoorsSDR SWAA2026021168884Lamp · inoperativeAFT RIGHT EMERGENCY LIGHT EXTERIOR OF R2 DOOR INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04.Feb 8, 2026 · N8325D · Boeing 7378H4 · Emergency LightingSDR SWAA2026021168865Battery Pack · inoperativeOVERWING DOOR, EMERGENCY LIGHTS INOPERATIVE. REMOVED & INSTALLED A NEW BATTERY PACK AND PERFORMED OPS CHECK IAW AMM 33-51-06-960-805. OPS CHECKED GOOD.Feb 8, 2026 · N8553W · Boeing 7378H4 · Emergency LightingSDR SWAA2026021168830Bulb · inoperativeAFT GALLEY OVERHEAD EMERGENCY EXIT SIGN BULB INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.Feb 8, 2026 · N8659D · Boeing 7378H4 · Emergency LightingSDR SWAA2026021168829Bulb · inoperativeAFT LEFT OVERWING DOOR EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.Feb 8, 2026 · N8659D · Boeing 7378H4 · Emergency LightingSDR SWAA2026021168880Tail Cone · damagedNUMBER 6 INBD FLAP SUPPORT, FORWARD FAIRING HAS SEVERAL OVERSIZED AND ELONGATED HOLES COMMON TO THE TAILCONE FROM FASTENERS PULLING THROUGH. R & R THE NR 6 FAIRING TAILCONE IAW SRM 51-40-02.Feb 8, 2026 · N249WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026021168789Flashlight · no testAFT OUTBOARD LT CABIN EMERGENCY FLASHLIGHT DOES NOT TEST. REMOVED AND INSTALLED A NEW AFT FLASHLIGHT ASSY IAW AMM 25-64-00, OPS CHECKED GOOD.Feb 8, 2026 · N8537Z · Boeing 7378H4 · Emergency EquipmentSDR DALA2026021101009Line · unsecureFA`S UNABLE TO ARM THE L2 MAIN ENTRY DOOR. SECURED A LOOSE MOORING LINE. OPS CHKD NORMAL. (8075516)Feb 8, 2026 · N583NW · Boeing 757351 · Emergency EquipmentSDR DALA2026021101008Rod End · brokenR1 DOOR, HARD TO OPEN, GIRT BAR FOOT ASSY BROKEN. R & R LIFTER ON R1 DOOR ASSY IAW IPC 52-11-20-24A. FOUND ROD END BROKEN IN BOTTOM END OF DOOR MECHANISM, REPLACED THE BROKEN LOWER HINGE DOOR MECHANISM IAW IPC 52-11-20-20A, ADJUSTED IAW AMM 52-11, DOOR OPS CFeb 8, 2026 · N687DL · Boeing 757232 · Passenger/Crew DoorsSDR DALA2026021101007Track · contaminatedL2 DOOR NOT ARMING CORRECTLY, KNUCKLE KNOCKER. FOUND DEBRIS IN DOOR TRACK, LUBRICATED AND PERFORMED OPS CHK WITH NO DEFECTS NOTED. (8422382)Feb 8, 2026 · N684DA · Boeing 757232 · Passenger/Crew DoorsSDR DALA2026021101005Proximity Sensor · contaminatedL3 DOOR LIGHT INOPERATIVE WHEN ARMING DOOR. CLEANED EXCESS GREASE FROM GIRT BAR PROX SENSORS CHKD OK IAW AMM 52-00. (8452231)Feb 8, 2026 · N554NW · Boeing 757251 · Door Warning SystemSDR DALA2026021100999Snubber · out of toleranceIN REFERENCE TO THE AMDS 2040-0191-1R STEP 7, OUT OF TOLERANCE LENGTH TO THE PIN EXTENSION ON ROTARY SNUBBER FLUID LEVEL L1 DOOR. R & R ROTARY SNUBBER IAW AMM 52-11-10. (1441836)Feb 8, 2026 · N821DX · Boeing 75726D · Passenger/Crew DoorsSDR DALA2026021100995Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 LBL 43.5 SHOWS SIGNS OF CORROSION. REPAIRED PER ER/A 623167-14TR, REV ORIGINAL. (LP# 1442279)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100994Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 RBL 23 SHOWS SIGNS OF CORROSION. " COMPLIED WITH A220 AMM 51-21-11 AND ERA 623169-14TR REV ORIGINAL. (LP# 1442029)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100993Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 LBL 23 SHOWS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0004:2500-2647/114 00148 COMPLIED WITH ER/A 623167-14TR REV ORIGINAL. (LP# 1442020)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100992Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 RBL 43.5 SHOWS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0004:2500-2647/112 00146 COMPLIED WITH ER/A 623170-14TR REV ORIGINAL. (LP# 1442019)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202602111753Pin · bentAIRCRAFT IN BASE MAINTENANCE: WELLS CONTROL UNIT DOES NOT ALIGN WITH POWER CONTROL UNIT, LOOSE PIN. MAINTENANCE REPLACE WCU AT M335051.Feb 8, 2026 · N885BP · Boeing 7878 · Emergency LightingSDR AALA202602111609Oxygen Bottle · leakingAIRCRAFT WAS GROUNDED: CKPT OXY 270 PSI. LEVEL DROPPING EXCESSIVELY MIA-DFW, POSSIBLE LEAK. DECESION MADE TO DIVERT TO DFW, NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O2 BOTTLE IAW AMM 35-11-41.Feb 8, 2026 · N9025B · Airbus A319115 · Crew Oxygen SystemSDR WX0A2026021132728Light · no discrepancy(AIRCRAFT NOT GROUNDED) EXIT LIGHT ON, PERFORMED OPS TEST OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00-710-009-A OPS TEST OK.Feb 8, 2026 · N208NV · Airbus A320214 · Emergency LightingSDR YENA2026021100194Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 14 INCHES BELOW LH SIDE STRI NGER AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00006) REF AE WO # 2025-414/1 NR # 2025-717347 EVALUATED DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 1Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100193Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR40L AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00007) REF AE WO # 2025-414/1 NR # 2025-717348 EVALUATED DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR4Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100192Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR70 TO FR71 BTW STR31R TO STR32R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00008) REF AE WO # 2025-414/1 NR # 2025-717299 PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOT FOUND DENT ONLY Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100191Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00009) REF AEROMAN WO # 2025=414/1 NR # 2025-717302 EVALUATED DENT ON EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE AND FOUND WITHIN LIMITS I.A.W A320 SRFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100190Skin · bulgedDURING HEAVY MAINTENANCE: BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19L TO STR20L ON UPPER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00010) REF AEROMAN WO # 2025-414/1 NR # 2025-717282 EVALUATED BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19LFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100189Skin · dentedDURING HEAVY MAINTENANCE: DENT SKIN LOCATED LOWER AREA DOOR R2 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00011) REF AEROMAN WO # 2025-414/1 NR# 2025-717349 EVALUATED DENTS LOCATED LOWER SKIN AREA DOOR R2 AT LOWER FUSELAGE AND FOUND WITHIN LIMITFeb 8, 2026 · N613JB · Airbus A320232 · Service DoorsSDR YENA2026021100188Frame · crackedDURING HEAVY MAINTENANCE: CRACK NDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 8, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.120INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O:Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100187Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100186Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 6, CRACK DIRECTION AT 11 O CLOCK LOOKING INBOARD, D=0.125 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100185Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00038Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100184Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 5 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.090 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00039Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100183Skin · deformedDURING HEAVY MAINTENANCE: DEFORMATION LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE; REF AEROMAN N/R 2025-717439, PERFORMED PERMANENT REPAIR LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE, THIS REPAIR IS CATEGORY A,Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026021100182Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1425349 TASKCARD: Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100181Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 2 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100180Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 3 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100179Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, AT AFT GALLEY AREA ( 1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00045) REF AE WO # 2025-414/1 NR # 2025-717399 PEFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100178Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, TRANSVERSAL FLANGE ARE A FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00046) REF AE WO # 2025-414Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026021100177Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (2 EA); REF AEROMAN N/R 2025-717397, ACCOMPFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100176Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SIDE. CRACK L= 0.109 INCH. CRACK DIRECTION 11 O CLOCK; REF AEROMAN N/R 2025-717306, ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMIFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100175Window Frame · crackedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVEFeb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021100174Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVEFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100173Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE AT LEVEL RIB 8 TO RIB 9 TRAILING EDGE ON RH WNG; REF AEROMAN WO 2025-414/1 NR # 2025-716950 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB7-RIB9 I.A.W EA 57-0135-2Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021100172Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER AREA BTW RIB8 TO RIB 9 ON RH WING; REF AEROMAN WO # 2025-414/1 NR # 2025-717170 PERFORMED PERMANENT REPAIR ON TRAILING EDGE UPPER SKIN LOWER AREA ON RIB 8 RH WING IAW EA # 57-0135-25 (COVER ANDFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin