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 SWAA2026072477163Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 143A0060 SHEET: 64 REV: -.SDR SWAA2026072479476Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 52 IN THE AFT CARGO BAY. LOCATED THE SUPPORT ANGLE BTWN BS 727A - 727B, LBL 52 IAW SRM 51-10-02, SRM 51-40-02, SRM 51-70-11-2R-0, REPAIR GENERAL, DWG 149A9490, SHEET 24, REV-, & DWG 140A9861, SHEET 61, REV A.SDR SWAA2026072480551Web · crackedCRACKED WEB, BTWN BS 277 - 294.5, RBL 1, WL 208.1. REPLACED THE WEB AND FASTENERS IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 141A5400, SHEET 20, REV -.SDR SWAA2026072495381Intercostal · crackedCRACKED INTERCOSTAL, BTW BS 344 - 360, LBL 11, WL 208.1. REPLACED THE INTERCOSTAL IAW SRM 51-40-02, AND DWG 141A5400, SHEET 46, REV-.SDR SWAA2026072441073Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 867, RBL 54, IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, SRM 51-70-11-2R-0, REPAIR GENERAL, DWG 149A9490, SHEET 23, REV A, & DWG 149A9490, SHEET 14, REV -.SDR SWAA2026072441145Web · crackedCRACKED WEB LOCATED BTW BS 312 - 328, RBL 31, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02, & SRM-51-10-02-0G-0, ITEM 9, DWG 141A5400, SHEET 39, REV -.SDR HNAA2026072400601Cup · corrodedCORROSION AROUND THE WASTE DRAIN VALVE. REMOVED AND REPLACED WITH NEW WASTE DISCHARGE CUP ASSY PER EMB 145 SRM 51-40-02-PR STEP 4B.SDR U2RA2026072100044Frame · crackedCRACK FOUND IN OPEN HOLE INSPECTION AT RT STA 1120 TENSION TIE FRAME WEB 65B01749-22. REPAIRS COMPLETED PER BOEING BCS CASE 06372730SDR IPXA2026072010384Bracket · brokenBROKEN - BRACKET , LT WING INBD L/E CAVITY AIR DUCT LINK SUPPORT , ILES 1098 (REPLACE). IAW AMM 20-51-01-912-008 REV.117 INSTALLED LT WING L/E DUCT LINK ROD. CONDITION CHECK NORMAL.SDR U2RA2026072000041Frame · crackedA CRACK DAMAGED WAS FOUND ON THE FRAME WEB AT STA 1160 AND BETWEEN S-9R- 10R WHILE PERFORMING SERVICE BULLETIN 747-53A2702 REV 02. PERFORMED CLASS B REPAIR PER CASE 06372691SDR U2RA2026072000040Frame · crackedDURING OPEN HOLE INSPECTION, CRACK FOUND AT BS 800 BETWEEN S-16R & S-17R. PERFORMED PERMANENT REPAIR AIW BOEING BCS MUA-MUA-26-0081-09B AND DWG 65B26468.SDR U2RA2026072000039Frame · crackedDURING OPEN HOLE INSPECTION, 2 CRACKS FOUND AT BS800 BETWEEN S-15L TO S-17L. PERFORMED CLASS B REPAIR IAW BCS CASE # 06372411SDR IPXA2026071706780Bracket · crackedCRACKED DISCONNECT PANEL , NR 4 ENG R/H T/R FWD UPPER AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.107 AND AIPC 78-31-00-60 REV.61 AND SREO-62461-REQ1 REV.1 3.SDR IPXA2026071104567Retainer · corrodedLEFT ELEVATOR T/E COUNT FROM OTBD TO INBD NR 2 STATIC WICK BASE HAS CORROSION. REMOVED AND REPLACED NR 2 STATIC WICK BASE ( MOUNTING STATIC DISCHARGER) P/N 16335, BATCH 0004414980 AND WICK DISCHARGER P/N 10-900-25A, BATCH 0004493176 ON SUPPORT PLATE IAW AMM SDR AALA202607141745Reservoir · defectiveAIRCRAFT IN BASE MAINTENANCE: DURING DISARMING PROCESS ON RIGHT AFT DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY INFLATION BOTTLE DISARM PIN WILL NOT ENGAGE. MAINTENANCE SUCCESSFULLY DEPLOYED THE SLIDE RAFT AND REPLACED IT PER AMM 25-62-44.SDR SWIA2026061776622Seat Track · corrodedCORROSION ON LT SEAT TRACK AT FR 17, Y + 10.748. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.SDR SWIA2026061776621Beam · corrodedCORROSION ON THE BEAM AT FR 87, Y +10.748. REMOVED AND REPLACED BEAM AT FR 87, Y +10.748" PER SRM 51-40-08SDR SWIA2026061776620Seat Track · corrodedCORROSION ON AREAS OF RT INBD SEAT TRACK BETWEEN FR 18 AND FR 19. REMOVED AND REPLACED FWD RT INBD SEAT TRACK IAW SRM 51-40-08.SDR IPXA2026071106966Skin · debondedDEBONDED SKIN, LT AFT WING TO BODY FAIRING 193 BL. IAW SRM 53-60-70-2R-0 REFER TO SRM 53-00-70-2R-1 AND SRM 51-70-07-0G-0 REV.107. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026071007466Stiffener · crackedCRACKED BRACKET, NR. 4 ENG LT THRUST REVERSER TORQUE BOX AFT 10:00 POSITION. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV.107 AND AIPC 78-31-00-55 REV 61.SDR SWAA2026071013227Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR IPXA2026070219049Support Angle · crackedRIGHT AFT WTB PANEL LANDING UPPER SUPPORT ANGLE HAS A CRACK.
REMOVED SUPPORT ANGLE AT RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW SUPPORT ANGLE RT WING TO BODY UPPER AFT PANEL LANDING SUPPORT IAW SRM 51-40-02-OG-0.SDR SWAA2026070613250Skin · crackedFOUND TWO CRACK INDICATIONS ALONG THE LOWER L/H STAB SURFACE MEASURING ROUGHLY 1.5; AND 4. FOUND UNER WIP1 INSTRUCTIONS ON TTG8Q01CQFWN. REPLACED LT LOWER HORIZONTAL STAB SKIN IAW SRM 51-40-02-0G-0; SRM 51-40-04-0G-0; SRM 51-20-01-0-G-0; AMM 55-05-03-210-810SDR SWIA2026061776362Skin · gougedDURING THE RECONTOUR OF THE DENT ON FWD FUSELAGE SKIN AT FR 1-2, STGR 12R-17R, THE MECHANIC WAS USING A RIVET GUN AND BUCKING BAR TO KNOCK OUT SOME FASTENERS TO GAIN ACCESS FOR THE RECONTOUR. DURING REMOVAL, THE BUCKING BAR CHATTERED ON THE SKIN CAUSING GOUGINSDR CALA2026070117513Skin · damagedDUE TO NON ROUTINE 3493866 AND ECRA 5300-03218 REV. A PART 3: PERMANENT REPAIR, ITS NECESSARY TO COMPLY WITH B767 SRM 53-00-01-2R-1.ACCORDING TO NON ROUTINE 3493866 IT WAS ACCOMPLISHED PERMANENT R EPAIR ON THE UPPER FUSELAGE SKIN AT BS 522 AND 544, STR 6L & 7LSDR IPXA2026070110500Rub Strip · chafedCHAFED RUB STRIP, NR 3 ENG LT CORE COWL INNER FACE AFT UPPER EDGE. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47SDR DALA2026063003860Warning Light · illuminatedL1 DOOR SLIDE ARMED INDICATION LIGHT IS NOT ILUMINATED. MEL 52-11-01 (8895602)(AIRCRAFT GROUNDED)SDR SWAA2026062913478Vapor Barrier · damagedTHERE ARE THREE FASTENER HOLES ELONGATED ON THE REPAIR AREA, UNABLE TO PERFORM NDT BOLT HOLE INSPECTION, ON THE VAPOR BARRIER BS 661-95, LBL 34.79, THERE ARE 3 FASTENER HOLES ELONGATED ON THE REPAIR AREA UNABLE TO PERFORM NDT BOLT HOLE INSPECTION ON THE VAPORSDR CALA2026062917375Lamp · inoperativeDURING SAFA INSPECTION, REPORTED EMERGENCY LIGHT AT CEILING 21LK INOPERATIVE, CEILING AISLE EMERGENCY LAMP 21LK INOPERATIVE PER MEL 3351A. REPLACED THE LAMPS, CEILING AISLE EMER LAMP 21LK. REMAINED INOPERATIVE.SDR 8HBR20260628085Bearing · brinelledPILOTS REPORTED VIBRATIONS IN THE CYCLIC CONTROL. INSPECTION OF THE MAIN ROTOR BLADE SPINDLE BEARINGS SHOWED BRINELLED BEARINGS ON BOTH MAIN ROTOR BLADE SPINDLES.SDR ASAA2026061766943Channel · corrodedFOUND CORROSION ON FWD CARGO BAY L/H AND R/H SIDE Z CHANNELS NEAR AFT BULKHEAD. CORRODED IN MULTIPLE AREAS. GROUNDED - YES. REMOVED AND REPLACED ZEE CHANNELS IAW DWG 143A7500.SDR DALA2026062403764Girt Bar · lack of lubeWRITE UP FOR DOOR 4L ARMING ISSUES. ADJUSTED DISARM ROD LINK AND LUBED DOOR CONTROL AND GIRT BAR. ALL CKS FOOD PER B757 AMM 52-11. (1650893) AIRCRAFT WAS GROUNDEDSDR AALA202606243251Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN MOUNTING BRACKET AT BS 663 AND RBL 32 JUST BELOW UPPER PRESSURE DECK. REPLACED BRACKET PER SRM 51-40-02.SDR DXTA2026062208495Wire Harness · faultedWE RECIEVED AN ENG CNTRL FAULT R CAS MESSAGE DURING CRUISE. RAN THE QRH PROCEDURE BUT MESSAGE DID NOT CLEAR. POWERED UP ACFT VIA APU AND INTERROGATED CMC FOUND 2 FAULT CODES SA & SB. BOTH ISSUES HAPPENED AT CRUISE, CONTINUED. GAINED ACCESS TO DCU CONNECTOR INSDR 2026F00131Tire · damagedFLIGHT 624, CBB7LPB. MAIN TIRE 3 WITH PLY SEPARATION IN THE READ. TIRE DAMAGED. RH WING INBOARD FLAP, TRAILING EDGE, THE LOWER AFT FLAP WITH DENT 8.5" WIDHT, 3/16"DEPTH, 6"HEIGHT. RH WING INBOARD FLAP TRAILING EDGE WITH DENT. ACCESS PANEL 651FB PANEL ASSY LOSDR R61A2026061700162Wheel · failedON DEPARTURE OUT OF LGA WE HEARD A LOUD BANG ON ROTATION DURING CLIMB OUT, WE RECEIVED A BRK LT FAULT MSG AND WHEN WE EXTENDED THE GEAR, WE HAD A LG LEVER DISAGREE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED DAMAGED HYDRAULIC LINES, SIDESDR SWAA2026062313228Sign · brokenFOUND OVERWING MID AISLE; EXIT LIGHT HOUSING WITH BROKEN CUSHION. OVERWING MID AISLE LIGHT FOUND TO HAVE A BROKEN CUSHION ON THE HOUSING ASSY. REPLACED BROKEN OVERWING MID AISLE CUSHION ON HOUSING ASSY EXIT SIGN IAW AMM 33-51-01-960-802.SDR R61A2026061700161Warning Message · illuminatedPARKING BRAKE CAUTION INDICATION IN FLIGHT. QRH DID NOT CLEAR. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED EMERGENCY PARKING BRAKE PRESSURE SWITCH 1.SDR N6WA2026062209Idg · warning messageABORTED TAKEOFF AFTER IDG 1 CAUTION MESSAGE RECIEVED. AS PER TELECON WITH MXC, DEFERRED IDG 1 CAUTION MESSAGE ON OCN 70101614 PER MEL 24-11-01A CATEGORY ASDR SWAA2026062213428Charger · intermittentEMERGENCY EXIT LIGHT ABOVE FWD GALLEY DOOR ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT CHARGER.SDR QXEA2026062200144Lens · damagedFLIGHT 2141. AFT OVERHEAD EXIT SIGN BROKEN, OVER CENTER AISLE.. REMOVED FROM SERVICE. REPLACED AFT OVERHEAD EXIT LOCATOR SIGN LENS. CLEAR DEFECT RETURNED TO SERVICE.SDR QXEA2026062200143Fadec · malfunctionedENGINE 2 NO DISPATCH MESSAGE ON LANDING AND ALSO INTERMITTANT AUTOTHROTTLE FAIL AND FADEC FAULT. DISPLAYED FOR ABOUT 5 SECONDS AT TAXI TO THE GATE. AND FLICKERING AT PARKING. REMOVED FROM SERVICE. REMOVED AND REPLACED #2 ENGINE FADEC PER CF34-8 LMM TASK 73-00-SDR ASAA2026061766882Power Supply · inoperativeL1 AND L2 DOOR HEADER PANEL EXIT SIGNS ARE INOPERATIVE. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1675 IAW AMM 33-51-06-960-806. OPS CHECKED GOOD.SDR ASAA2026061766879Power Supply · inoperativeAFT LOWERED CEILING PANEL EXIT SIGN IS INOP. GROUNDED - YES. BATTERY PACK M2627 AND M1673 WERE REMOVED AND REPLACED IAW B737 AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2026061766878Power Supply · inoperativeFWD CLOSEOUT PANEL EXIT SIGN IS INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACKS M1676 AND M1671 IAW B737 AMM 33-51-06-960-806. OPS CHECK GOOD.SDR IPXA2026062204155Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 7:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 27" FROM OUTBD EDGE, AT 7 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). BOND THE SPACER WITH FILSDR IPXA2026062204145Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 21" FROM FWD EDGE, 18" FROM UPPER EDGE, AT 1 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESSDR IPXA2026062204122Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 11:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 18.5" FROM AFT EDGE, 24" FROM UPPER EDGE, AT 11 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH SDR IPXA2026062204106Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL BARREL NEAR 4:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 20" FROM FWD EDGE, 4" FROM LOWER EDGE, AT 4 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUSDR IPXA2026062203995Nose Cowl · dentedDENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 4.75" FROM AFT EDGE, 33" FROM LOWER EDGE, AT 9 O'CLOCK ON THE INNER BARREL OF NR 1 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURE