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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202607100894Floor Panel · puncturedMAIN DEXJ CARGO COMPARTMENT FLOOR PANEL 241BFF HAS PUNCTURE DAMAGE. JM29. REPAIRED FLOOR PANEL 241BFF MPN145T5876-97 LBL11-LBL33 STA 755 IN REF TO B767 53-00-50- 2R FIG 201, REPAIR 1 SHEET, 2 THIS IS A MAJOR REPAIR THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFTSDR FDEA202607100893Skin Panel · dentedUPPER FUSELAGE TAIL AREA BETWEEN B.S. 1918 TO B.S. 1941 TOP SECTION WITH 01 EA DENT. APPLIED PERMANENT REPAIR AT UPPER FUSELAGE TAIL AREA BS 1918 TO B.S. 1941 I.A.W B757 SRM 53-80-01-1A, TABLE I, NOTE 'C', FIG 101, SHEET 2 AND SRM 51-70-10-2R REP '4'SDR FDEA202607100892Access Panel · crackedLH WING #3 SLAT LOWER SKIN ACCESS PANEL 523GB AREA WITH 02 EA CRACK. 2EA CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523GB AREA WERE REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4SDR FDEA202607100891Skin · dentedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DSDR FDEA202607100890Access Panel · crackedLH WING #3 SLAT LOWER SKIN ACCESS PANEL 523FB AREA WITH 01EA CRACK. CRACK AT LH WING #3 SLAT LOWER COVE SKIN ACCESS PANEL 523FB AREA WAS REPAIRED IAW B-757 SRM 57-43-01-2R FIG 201 REPAIR 4.SDR FDEA202607100889Skin · unknownNEED TO REPAIR DAMAGE ON #4 SLAT, OTBD CLOSURE PANEL (MPN: 114T4151-7) AT OSS 641. REPAIRED #4 SLAT OTBD CLOSE OUT PANEL AT OSS 641 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SHT. 3, REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE JSDR FDEA202607100888Skin · delaminatedNEED TO REPAIR DAMAGE ON #4 SLAT, INBD CLOSURE PANEL (MPN: 114T4151-5) AT OSS 572. REPAIRED #4 SLAT INBD CLOSE OUT PANEL AT OSS 572 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SH 3 REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE JPF SDR DALA2026071304091Transceiver · faultyATB- RETURNED TO DTW DUE TO MULTIPLE FAULTS AFTER GEAR RETRACTION. REPLACED ALL RADIO ALTIMETER ANTENNAS AND BOTH TRANSCEIVERS. GEAR SWING AND RADIO ALTIMETER OPS CHECK GOOD. (6544512) (AIRCRAFT WAS GROUNDED)SDR SIMA20260710001Flap System · malfunctionedFLAP FAIL WHEN SELECTING FLAPS 2, SLATS WENT TO 3, FLAPS FAILED AT 1. RAN QRH NO FIX PERFROMED FLAP FAIL PER FIM TASK 27-51-00-810-802. CLEARED THE FLAP-ACE 1 CLEAR INHIBITS. CYCLED THE FAIL. FAULT DID NOT DISPLAY ON EICAS. NO DEFECT NOTED AT THIS TIME. OKAY SDR YENA2026071300559Transceiver · failedFLT # 2260, MAD-BOS. (ETOPS) "WX RADAR 1 TRANSEIVER FAILURE RED WXR R/T; T/S WXR1 RTU REMOVED + REPLACED RTU 1 REF AMM 34-41-51 PERFORMED BITE + OPS CK REF AMM 34-41-00-740-002 + TEST OK."SDR HNAA2026071300592Controller · faultedPRESSURE CLIMBED CONTINUOUSLY IN FLT. PRESS CONTROL AUTO AND MANUAL. R & R DIGITAL RESSURE CONTROLLER IAW AMM 21-31-01 OPS CHECKED IAW AMM 21-31-00, OPS CHECKED GOOD. THIS CLEARS MEL 21-12-3.SDR DXTA2026071308774Light · detachedCAPT'S MAP READING LIGHT IS DETACHED AND DANGLING FROM ITS WIRES. IT SPARKS AND SMOKES WHEN TURNED ON OR MOVED. REMOVED AND REPLACED CAPT'S MAP READING LIGHT DUE TO BEING BROKEN WITH CUSTOMER SUPPLIED NEW ONE OPS CHECKS GOOD.SDR DXTA2026071308778Light · inoperativeA SECTION OF EMERGENCY AISLE LIGHTING IS INOPERATIVE UNDER SEAT THREE. REMOVED DAMAGED THRESHOLD LED LIGHT ASSEMBLY AND INSTALLED NEW THRESHOLD LED LIGHT ASSEMBLY. PERFORMED OPS CHECKS WITH NO DEFECTS NOTED AT THIS TIME.SDR UIEA2026071000587Proximity Sensor · out of toleranceGEAR DISAGREE MSG, LT WING LANDING GEAR UP PRIMARY AND ALT PROXIMITY SWITCHES TARGET FAILED. JACKED AIRCRAFT TO CHECK PROX SENSOR RIGGING. FOUND PROX SENSORS S398 & S1638 OUT OF TOLERANCE. RESHIMMED BOTH SWITCHES IAW AMM 32-61-21. OPS CHECKED GOOD.SDR DALA2026071304085Seat Track · corrodedLEVEL 2 CORROSION, CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK - Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, AS PER A320 SRM 51-42-11 AND DWGD53112812; RELEASE DATE: 08-JAN-97; ISDR DALA2026071304080Oven · odorFORWARD GALLEY OVEN MOTOR SEVICE LIGHT ON AS WELL AS METAL BURNING SCENT COMING FROM OVEN. OVEN ISN'T HEATING MEALS UP AND THE OVEN TEMPERTURE WAS DECREASING AND INECRESING AT RANDOM POINTS DURING HEATING MEALS. OVEN BEING DEFFERED TO NEF 25-34-02 DUE TO BURNSDR DALA2026071304079Not Reported · not reportedTESTING DTE/AMOC ASSOCIATED ER/A 00-603239 ADDED FOR AC 3132. COMPLIES WITH ERA 00-603239. (LP: 1692281, AIRCRAFT WAS GROUNDED)SDR I5PA2026071088801Ldvt · faultyDEFERRED LT THRUST REVERSER DUE TO LT ENG REVERSER, LT ENG SEC CONT STATUS MSG. R & R LT ENG LDVT IAW AMM, OPS CHKD NORMAL.SDR QMLA2026071020044Fadec · failedNR 1 FADEC FAILURE IN FLIGHTSDR AALA202607129006Spring · missingAIRCRAFT IN BASE MAINTENANCE: L1 DOOR GIRT BAR NYLON SPRING LATCH MISSING OUTER SLEEVE. MAINTENANCE INSTALLED L1 DOOR GIRT BAR NYLON SPRING LATCH IAW 737 AMM 25-66-01.SDR DALA2026071104075Wire · miswiredDURING SERVICE CHECK FOUND FWD GALLEY OVERHEAD CENTER EMERGENCY LIGHT L26 AND FLOOD LIGHT M11430 INOP. FOUND FWD LT OVERHEAD LIGHT L891 P/N 0105938-001 WIRE TERMINAL ON INCORRECT SCREW TO LIGHT HOUSING, CAUSING POWER SUPPLY FUSE TO TRIP. RESECURED TERMINAL ASDR DALA2026071104074Angle · corrodedCORROSION LEVEL 2 IN ANGLE STA 438 LBL 58 AT CPAX. REPLACED ANGLE IAW SRM 51-40-02-0G. (LP 1692766 - AIRCRAFT WAS GROUNDED)SDR DALA2026071104073Seat Track · corrodedCORROSION LEVEL 2 ON SEAT TRACK INBD RH FROM STA 1290 TO STA 1320 AT CPAX. REPLACED SEAT TRACK PER BAC5300-1 REV (K), PER B757-300 SRM 51-40-05-0G, PER B757-300 SRM 51-40-08-0G, PER B757-300 SRM 51-40-02-0G AND PER B757-300 SRM 53-60-52-01- PROCEDURE 1. (LP SDR ABXA20260710314Warning Message · false activation"FIRE/OVHT SYS" EICAS CAUTION MESSAGE AFTER ENGINE NR 1 STARTED. ACCOMPLISHED QRH PROCEDURE AND MESSAGE DISAPPEARED PERFORMED ENGINE FIRE DETECTION SYSTEM TEST IAW B767 AMM 26-11-00. COULD NOT DUPLICATE. A/C REMAINS NO ETOPS. LP 39190-25/1 RETURNED TO SERVICSDR DALA2026071104071Battery Pack · faultedDURING SVC. EPSU BAT (17WL) FAULT ON CIDS. REPLACED 17WL BATTERY PER A321 AMM 33-51. FUNCTION TEST AND BITE TEST PASS. NO FAULTS. (LP 8765908 - AIRCRAFT WAS GROUNDED)SDR AALA202607110719Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: DURING PS CHECK FOUND EMERGENCY EXIT (RH AFT 844) DOOR DAMPER CYLINDER PRESSURE ON RED (LOW). MAINTENANCE CHARGE CYLINDER IAW JC 26L80052003 SERVICED DOOR ASSIST SERVICE PRESSURE IAW JC 26L80052003.SDR WX0A2026071032890Unknown · odor(AIRCRAFT NOT GROUNDED) BOTH FWD FLIGHT ATTENDANTS REPORT CHEMICAL/MILDEW SMELL FOR 20 MINS DURING CRUISE / TROUBLESHOT PER TSM 05-50-00-810-831-A FOR ODOR EVENT, PERFORMED TC A32X-21-000-001 NO DEFECTS NOTED AND NO SMELL WAS REPRODUCED. (FOLLOWUP - DI CLOSED)SDR DALA2026071004066Battery Pack · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AT M1670 IAW AMM 33-51-06. OPS CHECK GOOD. (8767583) AIRCRAFT WAS GROUNDEDSDR DALA2026071004065Battery Pack · inoperativeL2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M1673 IAW AMM 33-51-06. OPS CHECK GOOD. (8767582) AIRCRAFT WAS GROUNDEDSDR DALA2026071004060Battery Pack · defectiveFOUND ON SVC, EMERGENCY PATH LIGHTING INOP AT SEATS 11-15. REMOVED & REPLACED DEFECTIVE BATTERY PACK (M1676) IAW AMM 33-51 CHECKS NORMAL. (8722117) AIRCRAFT WAS GROUNDEDSDR DALA2026071004059Door Sill · corrodedAFT CARGO COMP DOOR SILL WEB CORRODED IN MULTIPLE LOCATIONS. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REMOVED AND REPLACED SILL WEB AT AFT CARGO DOOR IAW SRM 51-40-02. (1691919) AIRCRAFT WAS GROUNDED.SDR DALA2026071004058Floorbeam · corrodedRIGHT AFT WET AREA BS 888, RBL 20, CORRODED. PERFORMED FLOORBEAM TEE ANGLE REPAIR AT RT AFT WET AREA AT BS 947 IAW SRM 53-70-51-2R-5. (1691379) AIRCRAFT WAS GROUNDED.SDR IPXA2026071095408Compressor · stalledEMERGENCY DECLARED, LEFT ENG COMPRESSOR STALLED AND VIBRATION.SDR DALA2026071004052Hinge · damagedLEAVING FL210, WE RECEIVED APU CAUTION EICAS COMPLETED CHECKLIST & HAD DASHES ON OIL TEMP. FOLLOWED BY APU FAULT FOLLOWED BY APU SHUTDOWN. COMPLETED CHECKLIST FOLLOWING APU SHUTDOWN. UPON INSPECTION FOUND APU AIR INLET DOOR MISSING. REMOVED APU INLET DOOR ACCSDR REXA2026071001072Lamp · inoperativeTHREE EMERGENCY FLOODLIGHT LAMPS INOPERATIVE. R & R THE THREE EMERGENCY FLOODLIGHT LAMPS IAW AMM 33-51-05. OPS CHECKED GOOD.SDR 2026FA0000577Motor · wornDURING CRUISE FIGHT THE CREW RECEIVED A HYD CAWS ANNUNCIATION. THE LANDING GEAR DID NOT RESPOND TO THE NORMAL GEAR EXTENSION COMMAND. THE CREW EMERGENCY EXTENDED THE GEAR VIA THE MANUAL EXTENSION PUMP. DURING THE TROUBLE SHOOTING MAINTENANCE DISCOVERED THE HSDR DALA2026071004048Web · crackedCRACK ON AFT CABIN BULKHEAD DOOR WEB AND X= 12 L/H AT CPAX, R & R CABIN BULKHEAD DOOR PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51- 41-01-0G, B717-200 SRM 51-41-05-0G AND B717- 200 SRM 51-20-09-0G, B717-200 SRM 51-10-04-0G, B717-200 SRM 51-40- 04-0G. (16914SDR FDEA202607100887Test Switch · inoperativeR1 DOOR SLIDE PRESS TO TEST LIGHT IS INOPERATIVE AMM 25-61-04-4. R & R BATTERIES & BOTH LAMPS. NO HELP. R & R REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4. INDICATOR KIT BAD FROM STOCK. INDICATOR STILL INOP. SLIDE BOTTLE PRESSURE NORMAL. RELEASED FOSDR FDEA202607100886Lanyard · out of positionDURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM . DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARBINER STATIC LINE NO DEFECTS NOTED. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA202607100885Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 231QFF AT MDCC FLOOR PANEL 231QFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV.94 DEC 15/ 2025SDR FDEA202607100884Floorbeam · corrodedEXISTING REPAIR ON BULK CARGO COMPARTMENT FLOOR BEAM FR66, Y1456 - Y1456 REQUIRES EVALUATION FOR COMFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH DWR:A53974322(ISSUE:T).FOUND CORROSION ON THE FLANGE SURFACE.PERFORMED THE NEW REPAIR PER EA 6-5321-T03SDR FDEA202607100883Floor Panel · crackedMDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 2400SDR FDEA202607100882Web · crackedMDCC UNDER FLOOR PANEL FR47, Y0 - Y450 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 24000FC, SDR SWIA2026070977777Floor Support · corrodedLEFT PRESSURE FLOOR SUPPORT, BS 449.85 HAD ONE AREA OF CORROSION. REMOVED CORROSION, EVALUATED AND RESTORED IAW STEPS A-F OF REO 601R-53-41-666, REV C. COMPLIED WITH 51-900-1003-SKY.SDR SWIA2026070977737Angle · damagedDURING INSTALLATION OF FRAME SPLICE AT RT BS 379 FOUND REINFORCEMENT ANGLE SPLICE WITH ELONGATED HOLES. REPLACED REINFORCEMENT ANGLE SPLICE IAW SRM 51-42-06-001-001-A01, REV 38, AND DWG SH670-31401, REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR AALA202609247438Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: SIDEWALL UPPER PANEL LANDING HAS CORROSION BETWEEN STA 787 AND STA 807 ABOVE STR 20 L. REPLACED WITH P/N 146A9403-123 IAW AARD 51-00-05 AND BOEING DWG 146A9403.SDR AALA202609237438Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: SIDEWALL UPPER PANEL LANDING HAS CORROSION BETWEEN STA 787 AND STA 807 ABOVE STR 20 L. REPLACED WITH P/N 146A9403-123 IAW AARD 51-00-05 AND BOEING DWG 146A9403.SDR IPXA2026092183506Keelbeam · crackedCRACK FOUND ON LH KEEL BEAM ON AFT SIDE OF BREAK LINE BETWEEN FR 13A AND FR 14. LENGTH: 1 1/2". ACCOMPLISH THE REPAIR PER EO-98018-REQ1 AND EA 300-5312-27-A4549, REV-.SDR IPXA2026091783481Fitting · crackedFAULT: CRACK FOUND ON RH KEEL BEAM ON AFT SIDE OF BREAK LINE BETWEEN FR 13A AND FR 14. LENGTH: 1 1/4". COMPLIED WITH UPS EO-98017-REQ1 AND EA 300-5312-27-A4548, REV. _.SDR IPXA2026091783506Keelbeam · crackedCRACK FOUND ON LH KEEL BEAM ON AFT SIDE OF BREAK LINE BETWEEN FR 13A AND FR 14 LENGTH: 1 1/2" REJECT STEP 102, OPS CHECK PERFORMED AT T3F18E003Z5FL DOES NOT HAVE INSPECTION CERTIFY.