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 UIEA2026020500032Skin · debondedDISBOND - RT WING OTBD AFT FLAP EXISTING DOUBLER ON LWR SURFACE. PERFORM PERMANENT REPAIR AT RH WING OTBD AFT FLAP LWR SURFACE NEAR WBL 548 IAW EGAT EI T2026A57M-080 REV 1. CONDITION CHECK IS GOOD</P>)Feb 5, 2026 · N481MC · Boeing 747443 · Trailing Edge FlapsSDR UIEA2026020500033Fairing · debondedDISBOND. RH WING OTBD AFT FLAP LWR SURFACE NEAR #8 FLAP TRACK FAIRING. PERFORM DISBOND AND CORROSION INTERIM REPAIR ON RT WING OTBD AFT FLAP LWR SURFACE BETWEEN WBL 731 AND WBL 747 IAW EGAT EI T2026A57M-094 REV 2. CONDITION CHECK IS GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Trailing Edge FlapsSDR UIEA2026020500034Spar Web · corrodedDAMAGE ON CENTER WING REAR SPAR WEB RH SIDE NEAR JETTISON PUMP AT STA 1240 RBL 93. ACCOMPLISHED EI T2026A57M-110 REV 1. JOB COMPLETED AND CONDITION CHECK GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Fuselage Main, StructureSDR UIEA2026020500035Door Frame · crackedPERFORM SB 4453A356 PART 1-3, FOUND CRACK HOLE AT DOOR NR 2 LH FWD EDGE FRAME, BS 800 S16L AREA. PERFORM EI T2026A53M-162 REV 0. ACCOMPLISH EI T2026A53M-162 REV 1. NO FURTHER DEFECTS NOTED.Feb 5, 2026 · N481MC · Boeing 747443 · Fuselage Main, StructureSDR UIEA2026020500036Doubler · corrodedLEFT WING INBD REAR SPAR OVERRIDE JETTISON PUMP TANK #2 FWD M222. REMOVE REWORKED DOUBLER IAW SRM 51-40-02-0G-0 REV R125. ACCOMPLISHED EI T2026A57M-113 REV 0 & W/S 69034 (DWG 65B19560 REV B). ACCOMPLISHED EI T2026A57M-113 REV 1. JOB COMPLETED AND CONDITIFeb 5, 2026 · N481MC · Boeing 747443 · Wing Main, Frame StructureSDR UIEA2026020500037Light · inoperativeFOUND OVERWING EMERGENCY LIGHT INOP AT L1870 FWD SIDE. IAW AMM 33-51-03-004-034 & 33-51-03-404-007 REV 115. R & R OVERWING EMERGENCY LIGHT (L1870). IAW AMM 33-51-03-404-007 REV 115 PERFORMED EMERGENCY LIGHT ASSY INSTALLATION TEST & THE RESULT WAS GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR UIEA2026020500038Indicator · crackedFOUND EMERGENCY EXIT INDICATOR LIGHT (M2989) BASE CRACK AT L2 DOOR. REF IPC 33-51-12-01A REV 91 & AMM 33-51-00-715-001 REV 115. R & R L2 DOOR EMERGENCY EXIT INDICATOR LIGHT ASSY (M2989) AND PERFORMED EMERGENCY LIGHTS OPS TEST, TEST WAS GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR UIEA2026020500039Power Supply · no testFOUND EMERGENCY LIGHT BATTERY (M5933) FUNCTION FAIL. IAW AMM 33-51-04-902-001-001 REV 115. R & R EMERGENCY LIGHT BATTERY POWER SUPPLY (M5933) & PERFORMED POWER SUPPLY INSTALLATION TEST, TEST GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR UIEA2026020500040Battery · no testFOUND EMERGENCY LIGHT BATTERY (M7928) FUNCTION FAILED. IAW AMM 33-51-04-902-001-001 REV 115. R & R EMERGENCY LIGHT BATTERY (M7928) & PERFORMED EMERGENCY LIGHT BATTERY INSTALLATION TEST, TEST WAS GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR UIEA2026020500041Light · no testFOUND CREW REST EMERGENCY LIGHT ASSY (M8925) FUNCTION FAIL. REF IPC 33-29-10-40B REV 91 & AMM 33-51-00-715-001 REV 115. R & R CREW REST EMERGENCY LIGHT (M8925) & PERFORMED EMERGENCY LIGHTS OPS TEST, TEST GOOD.Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR UIEA2026020500042Battery · inoperativeFOUND EMERGENCY LIGHT BATTERY (M7916) INOPERATIVE. IAW AMM 33-51-04-0902-001-001 REV 115, R & R EMERGENCY LIGHT BATTERY (M7916) & PERFORMED BATTERY INSTALLATION TEST, TEST GOOD</P>)Feb 5, 2026 · N481MC · Boeing 747443 · Emergency LightingSDR 2026FA0000084Engine · damagedALASKA AIRLINES LEAP-1B ESN 60A682 WAS REMOVED IN JAN 2025 AT ETSN/ECSN 10,132 FH / 2,895 FC FOR SB 72-0394 HPC STAGE 2 SEAL HONEYCOMB. ON OCT 15TH, 2025 (16:38 LOCAL TIME), ESN 60A682 EXPERIENCED A TEST CELL STALL/SHUTDOWN AT VILLAROCHE “MRO” TEST CELL DURFeb 5, 2026 · Engine (Turbine/Turboprop)SDR DALA2026020500840Proximity Sensor · faultedDOOR L AFT DOOR ECAM MESSAGE CLIMING OUT OF FL370. NO V/S ISSUES. R & R PROXIMITY SENSOR 23MJ & RIGGED TO 0.064 IN. DOOR INDICATION NORMAL. (8306806)Feb 5, 2026 · N805NW · Airbus A330323 · Door Warning SystemSDR AALA202602050487Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.Feb 5, 2026 · N150NN · Airbus A321231 · Emergency ExitsSDR FDEA202602050135Frame · unknownEXISTING REPAIR ON FUSELAGE FRAME AT FR28 BETWEEN STGR8LH AND STGR12LH REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-REPAIRED THE FRAME PER EA 6-5310-T0386358. TITLE: FUSELAGE - MAINFRAME - EXISTINFeb 5, 2026 · N658FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202602050134Floorboard · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED. FABRICATED NEW FLOOR PANEL MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 222BFF DENTED 222BFF, MPN 141T5856- 106,RBL33 - RBL 54.75, STATION 285 - 412 IN REF TO BOEING DWG 141T5856-106 AND SR67-53- 009.SEFeb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602050133Floor Panel · dentedMIAN DECK CARGO COMPARTMENT, FLOOR PANEL 251LFF DENTED. JM40 FABRICATED NEW FLOOR PANEL 251LFF, MPN: 146T5869-127, LBL 11- RBL 11, STA 1208-1351 IN REF. TO BOEING DWG 146T5869-127, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR.Feb 5, 2026 · N297FE · Boeing 7673S2F · Fuselage Structure (General)SDR FDEA202602050131Floorboard · delaminatedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS AREA OF DELAMINATION. FABRICATED NEW FLOOR PANEL 232MFF, MPN: 148T5875-19 RBL 54.75- RB L 77.5, STA 654-784.5 IN REF. TO BOEING DWG 148T5875-19, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR FDEA202602050130Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. JM39. (INCORRECT REF. AND REWORK PROCEDURE USED FOR DAMAGED AREAS.) FABRICATED NEW FLOOR PANEL 251KFF, MPN: 146T5869-9, LBL 77.50- LBL 86.75, STA 1087-1207 IN REF. TO BOEING DWG 146T586Feb 5, 2026 · N297FE · Boeing 76732LF · Fuselage Floor PanelSDR ABXA20260205049Pump · warning messageDURING TAXI OUT, L FWD FUEL PUMP EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL 28-22-1 CAT "C" MX PROCEDURES CW. PLACARD INSTALLED. MBCB 02/15/2026. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.Feb 5, 2026 · N762CK · Boeing 7673P6 · Fuel Boost PumpSDR IXXA2026020501Floor Panel · puncturedFIRST OFFICERS RIGHT RUDDER PEDAL FLOOR PANEL IS PUNCTUREDFeb 5, 2026 · N389AZ · Boeing 767319 · Fuselage Floor PanelSDR F3LA202602050355Battery · failedNR 3 EPSU BATTERY 13WL FAILED TEST. INSTALLED NEW EPSU BATTERY IAW AMM 33-51-38-400-001-A. EPSU BITE CHECK GOOD IAW AMM 33-51-00-710-001. CIDS POWER UP TEST GOOD IAW AMM 23-73-00-740-005. EPSU TEACH IN PROCEDURES GOOD IAW AMM 33-51-00-820-801. EPSU FIN CHANFeb 5, 2026 · N380FR · Airbus A320251N · Emergency LightingSDR CALA2026020413584Charger · failedR2 DOOR EMERGENCY LIGHT BATTERY CAPACITY CHECK FAILED. THE BATTERY AND BATTERY CHARGER WERE REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.Feb 5, 2026 · N77014 · Boeing 777224 · Emergency LightingSDR SWIA2026020476047Frame · corrodedCORROSION FOUND ON THE LOWER FLANGE OF FRAME APPROX FS847+16 BETWEEN STGR 26L AND 26R. FS.847+16 FRAME LOWER SECTOR DISREPANT SECTION BETWEEN STGR 25L - STGR 25R CUT AWAY AND FRAME REPAIRED WITH NEW SECTION & REPAIR SPLICES PER SRM 53-00-06-201-001-A03, DWG Feb 4, 2026 · N899SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2026020475611Intercostal · crackedDURING THE LH TRU LANDING INSTALLATION CRACK FOUND ON LH INTERCOSTAL ELECTRIC BAY FLOOR BETWEEN FS 173.00 AND FS 193.00 MX# 31653855 (C-CHECK RO 03/28/2026)REMOVED AND REPLACED INTERCOSTAL P/N CC670-33194-7. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-1Feb 4, 2026 · N726SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260326002Channel · corrodedCORROSION ON TWO NUT CHANNELS OF LT & RT P-SEALS OF BODY FARING PANELS AT MLG WW. THE NUT CHANNELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, EVALUATED, AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPLACED IAW SRM 51-41-02-001-001-A01.Feb 4, 2026 · N642NN · Bombdr CL6002D15 · Fuselage Main, StructureSDR VNAA20260326001Skin · corrodedTWO DENTS ON LOWER SKIN FLS60.00 OF INBD FLAP AT LT WING. THE DENTS WERE REPAIRED IAW SRM 57-52-01-201-001- A01.Feb 4, 2026 · N642NN · Bombdr CL6002D15 · Trailing Edge FlapsSDR 3EJA202603240001Oil Cooler · failedRECEIVED RED OIL PRESSURE INDICATION (POINTER AND DIGITS) LEFT ENGINE IN FLIGHT. SHUT DOWN LEFT ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO KCHS. FOLLOWED CHECKLIST PAGES D4 LOW OIL PRESSURE INDICATION, A2 ENGINE FAILURE/SHUTDOWN AND Y1 SINGLE ENGINE APPROACFeb 4, 2026 · N739JS · Cessna 525B · Engine Oil Distribution (Airframe Furnished)SDR 2026FA0000206Engine · damagedA LOUD BANG HEARD FROM RIGHT SIDE OF AIRCRAFT ON TAKEOFF FROM KFRG AT 600 FEET WHILE GEAR WAS GOING INTO WELL. CREW THOUGHT IT WAS A GEAR UPLOCK ISSUE. GEAR INSPECTED WITH NO DEFECTS FOUND.  A FEW DAYS LATER AFTER ENGINE DATA DOWNLOADS IT WAS DETERMINED THE NRFeb 4, 2026 · N350PD · Bombdr BD1001A10 · Engine (Turbine/Turboprop)SDR SWAA2026031667611Strap · corrodedCORROSION ON STRAP LOCATED APROX OFSS 345 LEADING EDGE AT LT WING 2026-112181<[01] PERFORMED REPAIR ON STRAP LOCATED APROX OFSS 90.49 TO OSS 163.95 LEADING EDGE AT LT WING IAW EA 26-157-00382 AND B737-800 SRM 57-20-01-2R REPAIR 3 SEE INDIVIDUAL SIGN OFF BELOW;Feb 4, 2026 · N8629A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SIMA2026031604004Skin · gougedLH WING L/E SKIN OUTBD OF #9 SLAT TRACK ON UPPER SIDE GOUGED. (MAJOR REPAIR) REMOVED AND REPLACED LH WING SKIN OUTBD OF #9 SLAT TRACK BETWEEN RIB 37 AND RIB 42 IAW ERJ 170 SRM 51-40-02.Feb 4, 2026 · N770JM · Emb ERJ170100LR · Wing, Plate/SkinSDR IPXA2026030841896Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 10 - 40 HAS CORROSION AT NUTPLATE HOLES. INSTALLED TEE-ANGLE AND PLATES AT RT WING TO BODY IAW SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026030243996Panel · crackedNR 2 PYLON GAP PANEL HAS A CRACK IN LOWER SURFACE. INSTALLED ONE DOUBLER & FILLER WASHERS IAW SRM 51-40-02, AND SRM 57-41-01-2R-3, REPAIR 3.Feb 4, 2026 · N427UP · Boeing 75724APF · Wing, Center BoxSDR VNAA202603130004Hinge Arm · corrodedCORRODED HINGE ARM (1 EA) AND HINGE FITTING (1 EA) ON SERVICE DOOR 195EL. HINGE ARM (1 EA) ON SERVICE DOOR 195EL WAS REPAIRED PER EA NO:5245-2026-0241 REV-- SECTION III PERMANENT REPAIR AND HINGE FITTING (1 EA) ON SERVICE DOOR 195EL WAS EVALUATED EXCESSIVE DFeb 4, 2026 · N635NN · Cndair CL6002D24 · Fuselage, Door HingeSDR VNAA202603130003Hinge Fitting · corrodedCORRODED HINGE FITTINGS (2 EAS) AND HINGE ARMS (2 EAS) AT SERVICE DOOR 196ER. HINGE FITTINGS (2EAS) AND HINGE ARMS (2 EAS) AT SERVICE DOOR 196ER WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND REMOVED AND INSTALLED PER CRJ900 AMM 52-45-01Feb 4, 2026 · N635NN · Cndair CL6002D24 · Fuselage, Door HingeSDR SWAA2026031267821Scuff Plate · crackedCRACKED ON FWD CORNER OF SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.Feb 4, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031267822Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.Feb 4, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWIA2026020475508Skin · damagedRIGHT INBD FLAP HAS 5 DISCREPANT NUT PLATE HOLES ON PANEL 684AB. COMPLETED REPAIR OF DISCREPANT HOLES IAW REO 601R-57-52-2542.Feb 4, 2026 · N913EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWAA2026031067601Seat Track · corrodedCORROSION ON SEAT TRACK, LBL 45, BS 480+11 TOP, BS 500+6 TOP, BS 500B WELL, 500D+15 TOP, & 500D+15 WELL, WL 208. THE SEAT TRACK WILL BE REPLACED ON TASK CARD TTG8Q01A8V2U.Feb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026031067602Seat Track · corrodedCORROSION ON SEAT TRACK LBL 25, BS 500+7 TOP, BS 500B+2 TOP, BS 500A+18 TOP, BS 500C+11 TOP, BS 500D+15, WELL, WL 208. THE SEAT TRACK TO BE REPLACED ON CCN TTG8Q01A8V2T.Feb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026031067808Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK, RBL 25, BS 578+16 TOP, BS 663+18 WELL, BS 683+3 TOP, BS 708+8 WELL, BS 727A+8 TOP, WL 208. REMOVED CORROSION ON SEAT TRACK IAW SRM 51-10-02-0G-0. TREAT AND PRIME WILL BE COMPLETED ON CARD: TTG8Q01A8V4NFeb 4, 2026 · N246LV · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026022839378Frame · dentedAFT CARGO FRAME AT BS 1500 RT, DENTED. VERIFIED ACCOMPLISHMENT OF EO-96676-REQ1, AND EA 757-5360-27-A4324, REV- AS RII IAW UPS GMM 04-02-01-15.Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, FrameSDR AALA202603076088Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT AT STA 951 AND LBL 20. REPLACED THE FLOOR SUPPORT PER ECO J1301.Feb 4, 2026 · N910AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202603078813Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BTW FR66 AND FR68, STR 23R AT AFT GALLEY AREA MEASURES OF CORROSION ARE: L=3.608IN W=0.556 IN AND D=0.090IN. MIANTENANCE REPLACED CENTER FITTING AND FASTENERS LOCATED BTW FR66 AND FR68 AT LEVEL STR 23RH AFFeb 4, 2026 · N9006 · Airbus A319115 · Fuselage Miscellaneous StructureSDR IPXA2026030443086Tee Fitting · gougedFAULT - STR - Z100 - LH UPPER WING TO BODY T-CHORD AT STA 1147 HAS GOUGE ON EDGE DOT 5698-08 INSTALLED T-CHORD AT LH WING STA 1147 I.A.W. B757 SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APF · Aerodynamic FairingsSDR ASAA2026020464679Stringer · corrodedFWD CARGO BAY, STRINGER 27L HAD CORROSION AT BS 540. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED STRINGER IAW SRM 53-00-03-2R-1W =.650 O= .045 R= .002 L= 2.25 D= .043.Feb 4, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/StringerSDR ASAA2026020464677Stringer · corrodedFWD CARGO BAY STRINGER 27R CORRODED AT BS 540. GROUNDED - YES. REMOVED CORROSIONN, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1. REPAIRED STRINGER IAW SRM 53-00-03-2R-1 W= .650 O= .045 R= .002 L= 1.25 D= .043.Feb 4, 2026 · N611AS · Boeing 737790 · Fuselage Main, Longeron/StringerSDR IPXA2026020942975Support · crackedLEFT MLG I/B SEAL RETAINER SUPPORT STRUCTURE HAS A CRACK IN THE CORNER AT BS 1060 VERIFIED INSTALLED SEAL RETAINER SUPPORT STRUCTURE AT LT MLG INBD BS 1060 IAW SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026022139192Frame · dentedMAJOR REPAIR, AFT CARGO FRAME AT STA 1300 RH IS DENTED. VERIFIED STEP 47. COMPLIED WITH EO-96677-REQ1, AND EA 757-5360-27-A4325, REV-.Feb 4, 2026 · N427UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2026030403971Spar · crackedRH WING FR47 CWB LOWER ANGLE. CRACK INDICATION NOTED ON HOLE T IN ALL LAYERS AT 3 O' CLOCK POSITION. REJECTED - EO-96608-REQ1 NOT ATTACHEDFeb 4, 2026 · N145UP · Airbus A300F4622R · Wing Spar