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.
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 SWAA2026032374933Seat Track · corrodedCORROSION ON SEAT TRACK CROWN, BS 639+13, 706+17, 727+15, RBL 25, WL 208. THE SEAT TRACK WAS REPLACED ON CUSTOMER CARD TTG8Q01AN5EX.SDR SWAA2026032374931Seat Track · corrodedCORRODED SEAT TRACK CROWN, BS 616+19, 662-664, 685+8-11, 727A+8, RBL 25, WL 208. REMOVED AND REPLACED THE DAMAGED SEAT TRACK, BS 540 - 727B, RBL 25, WL 208 IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0, & DWG 114A6300, REV E, REF AIPC 53-43-11-01. TOURQUED THSDR SWAA2026032374934Seat Track · corrodedCORRODED SEAT TRACK CROWN, BS 727C+2-4, 747+3-7, 767+13-16, 807+1-2, 827+14-19, LBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK BS 727B - 887, LBL45, WL 208 IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 146A5300, REV -.SDR SWAA2026032374924Support Beam · wornLEFT WING TRAILING EDGE SUPPORT BEAM ATTACHMENT HAS WEAR DAMAGE AND ELONGATED HOLE ON TWO FASTENER LOCATIONS. REPAIRED IAW SRM 57-51-02-2R-1-A01271, REPAIR 1.SDR SWAA2026032380585Fastener · shearedRIGHT INLET COWL LIP SKIN HAS SHEARED FASTENERS HEAD AT 2; 3 AND 10 O'CLOCK POSITIONS; MARKED<[01] COMPLETED STEP 1;[02] REMOVED AND REPLACED RH INLET COWL IAW AMM 71-11-01-400-802-F00 LEAK TEST GOOD;[03] VERIFIED CORRECTIVE ACTION 2.;[04] VERIFIED STEPS 2 ANDSDR SWAA2026032074532Floor Panel · pulledWHILE REMOVING FLOOR PANEL 241DF, IDENTIFIED A DAMAGED INSERT (PULLED THROUGH PANEL) AFT LH SIDE OF THE PANEL. FABRICATED OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.SDR 2026F00031Snubber · bindingL1 ENTRY DOOR ROTARY SNUBBER SERVICE INDICATOR OUT OF LIMITS. DOOR HARD TO OPEN. MAINTENANCE DISCOVERED OPENING DOOR. PRIOR TO DISCOVERY DURING MAINTENANCE THE FAILED SNUBBER COULD HAVE POSSIBLY IMPEDED EMERGENCY EGRESS IF NEEDED.SDR AALA202603187392Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: ACB RH UPPER MIDDLE FLOOR SUPPORT IS CRACKED AT CLIPNUT HOLE 6 INCHES AFT OF FR 62. MAINTENANCE REPLACED FLOOR SUPPORT AT ACB RH UPPER MIDDLE BETWEEN FR59-FR63 OER SRM 51-42-11 AND DWG D53974990.SDR AALA202603187546Web · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND CRACKED WEB AT LH Y1162.5, FR69-FR70. MAINTENANCE REPLACED WEB AT -Y1162 PER SRM 51-42-11-801 AND DWG D53474180.SDR QXEA2026031800065Doubler · corrodedFLOOR DOUBLER AT FRAME 19-20 LBL 20 IS CORRODED. REPAIRED IAW E175 SRM 51-40-08. FINISH RESTORED.SDR AALA202603170326Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA. MAINTENANCE REPLACED SHEAR PLATE STR 23 R LOC. BTW FR69 AND FR70 AT AFT GALLEY IAW A320 RM 51-42-11-801 AND DWG D53474180.SDR AALA202603176138Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT BRACKET AT BS 947.5 BETWEEN S25L AND S25R. REPLACED BRACKET PER AARD 51-00-05-1.SDR SWIA2026022675356Engine · odorIN FLIGHT FA REPORTED STRONG EXHAUST ODOR IN THE CABIN CAUSING HER THROAT AND HEAD TO HURT. DESCENDED TO FL240 AND SWAPPED TO THE APU BLEED. FA INITIALLY NOTED THAT THE SMELL IMPROVED BUT LATER CALLED US SAYING THE ODOR WAS BACK. PILOTS CONFIRMED THERE WAS A SDR IPXA2026031424391Splice Strap · corrodedWORKING FAULT T3F18E008B4MR FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1510 ATA 53-60 PRODUCTION AUDIT C/WSDR IPXA2026031424635Splice Strap · corrodedWORKING FAULT T3F18E008B4LL AFT CARGO FOUND CORROSION ON NUT PLATES AND DOUBLER DRILL HOLE ON FLOOR PANEL SPLICE STRAP STA.1470 PRODUCTION AUDDIT C/WSDR AALA202603126380Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD BETWEEN STA 767 AND STA 777 AT S25R. REPLACED SHIELD PER AARD 51-00-05-1.SDR AALA202603122779Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 947 AND 948 AT LBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR 2026FA0000176Bulkhead · crackedFOUND FORWARD PROPELLER BULKHEAD P/N 0550321-4 CRACKED AT ONE BOLT HOLE LOCATION.SDR ASAA2026022664788Shield · corrodedAFT PIT RH SIDE DOOR CUTOUT SHIELD PANEL HAS POSSIBLE CORROSION IN (5EA) SCREW HOLES AND UNDER NUTPLATES AT BETWEEN STA 787 TO 767 CIRCLES IN RED. GROUNDED - YES. REMOVED AND INSTALLED A NEW SHIELD PANEL AT AFT PIT R/H SIDE DOOR CUTOUT APROX STA 787 TO 767 IAWSDR SIMA20260226004Shear Tie · corrodedCENTER FUSELAGE III SHEAR CLIP AT FR 88 BETWEEN STGR 27R-28R CORRODED (LEVEL 2 CORROSION). RAR CENTER FUSELAGE III SHEAR CLIP AT FR 88 BETWEEN STGR 27R / 28R IAW ERJ 175 SRM 51-40-08SDR AALA202603074945Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR SUPPORT BETWEEN BS 991 AND BS 1016 AT LBL 31. REPLACED SUPPORT PER AARD 51-00-05-1.SDR AALA202603078969Elevator · vibrationAIRCRAFT WAS GROUNDED: SIGNIFICANT AIRFRAME VIBRATION ABOVE 300KTS / .78M. FL250-280 IN CLIMB. ENGINE VIBRATION WAS NORMAL. WHEN F/CTL WAS CALLED UPTHE RUDDER TRAVEL LIMIT WAS AMBER VERY BRIEFLY. MAINTENANCE REPLACED THE RIGHT HAND ELEVATORY ASSY.SDR IPXA2026030612569Seal · brokenBROKEN SEAL , NO. 1 PYLON AFT FAIRING PNL 436CL SPRING SEAL AREA. REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 2. INSTALL NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 16 REV.- 3. JOB COMPLETEDSDR IPXA2026022825145Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED BS 1420 RT OTBD LOWER SIDE ABOVE AFT LOWER CARGO DOOR VERIFIED STEP 17. FORMED TWO REPAIR ANGLES IAW SRM 53-00-51-2R-6.SDR IPXA2026030512672Angle · wornNR 1 PYLON TORQUE BOX PANEL 436AR INNER CABLE SUPPORT AREA ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 94. 2. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO: 311T1065 SH 8 REV. D. 3. JOB COMPLETED.SDR AALA202603050212Splice Plate · delaminatedAIRCRAFT IN BASE MAINTENANCE: FLOORBOARD SUPPORT BETWEEN PANELS AT STA 2021 CENTER LH FOUND DELAMINATED (ATTACHING PANEL 151W8723-3 VERIFIED A NEW SERVICEABLE SPLICE PLATE WAS INSTALLED ON FLOORBOARD 151W8723-3 IAW AMM 53-01-- 01SDR CALA2026030514369Skin Panel · damagedLEFT SKIN BTW BS 654+88 - 654+110, S29L-30L CREASED. THERE ARE NO ALLOWABLE LIMITS FOR THE CREASE IAW SRM 53-00-01-1A-1, PERFORMED A REPAIR IAW ECRA 5330-07699, PART 1 INTERIM REPAIR WITHOUT ANY DEVIATION.SDR AALA202603049409Heatshrink · missingAIRCRAFT WAS NOT GROUNDED: FORWARD SERVICE DOOR GIRT BAR IS MISSING A PLASTIC END ON THE BAR. REPLACED MISSING HEAT SHRINK ON THE FORWARD GALLEY SERVICE R1 DOOR GIRT BAR. PER AMM 25-66-01**(CLOSED).SDR AALA202603045037Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8719-3 HAS CORRODED INSERTS. MAINTENANCE INSTALLED NEW FLOORBOARD P/N 151W8719-3 IAW AMM 53-01-01 SO DY0H.SDR DALA2026030401483Door Sill · fodENTRY DOOR ARMING LEVER HARD TO OPERATE. REMOVED DEBRIS FROM DOOR SILL, OPERATED R2 DOOR ARMING. OP CKD NORMAL. (1468468)SDR DALA2026030401479Skin · crackedCRACK INDICATIONS WERE NOTED AT THE NR 5 HOLE OF THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR (R1) CUT OUT AFT LWR CORNER DURING NDT INSP. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REPAIRED THE R1 DOOR AFT LOWER CORNERSDR SWAA2026030374508Elec Connector · brokenAFT COVE BULLNOSE HAS BROKEN AISLE LIGHT CONNECTOR. REPLACED AISLE LIGHT CONNECTOR IAW SWPM 20-63-02, & WDM 33-51-14-13. FUNCTIONAL TEST WILL BE PERFORM IN TASK CARD TTG8Q01AJFUK.SDR AALA202603038969Unknown · vibrationAIRCRAFT WAS GROUNDED: SIGNIFICANT AIRFRAME VIBRATION ABOVE 300KTS / .78M. FL250-280 IN CLIMB. ENGINE VIBRATION WAS NORMAL. WHEN F/CTL WAS CALLED UPTHE RUDDER TRAVEL LIMIT WAS AMBER VERY BRIEFLY. (OPEN)SDR MASA20260303004Skin · dentedDURING C1, C3 SCHEDULED MAINTENANCE INSPECTIONS OF FWD FUSELAGE SKINS, MULTIPLE DENTS FOUND O RH SIDE (QTY 9). THE DAMAGES ARE OUTSIDE THE ALLOWABLE LIMITS DEFINED IN ERJ175 SRM 53-10-01, AD02. AS PER ETD2026-170-003152 DISPOSITION-001 THE 9 DENTS WHERE FOUNDSDR 2026F00019Fseu · malfunctionedFLIGHT 401, CIJ/LPB. EXECUTED GO-AROUND DUE TO TRAILING EDGE FLAP DISAGREE BETWEEN 5-10. FSEU BITE PROCEDURE PERFORMED. NO SHOW FAULTS FLAP POSITION INDICATOR PROBLEMSDR R61A2026022600056Warning Message · false activationL1 DOOR OPEN EICAS MSG IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED PRESSURE CHECKS. NO FAULTS FOUND. L1 DOOR EICAS MESSAGES PLACED ON DEFERRAL.SDR SWAA2026030274677Unknown · fumesFUMES IN COCKPIT AT TAXI THROUGH FL18.0; BOTH CLIMB AND DESCENT. RAN APU AND BOTH MOTORS FOR 5 MINUTES COULD NOT DUPLICATE PER FIM TASK 21-00 TASK 806SDR SWAA2026030274622Floor Panel · crackedRAMP REPORTED CRACK ON FLOOR IN AFT CARGO BAY. OK TO CONTINUE PER MEL 25-16-01. R & R AFT CARGO PANEL 140BF IAW AMM 25-52-01. R&R AFT CARGO PANEL 140BF IAW AMM 25-52-01.SDR SWAA2026030274686Lens · brokenRIGHT EMERGENCY EXIT SIGN BROKEN. R & R RT OVERWING EXIT EMERGENCY LIGHT LENS IAW MM 33-51-01. OPS CHKD OK IAW MM 33-51-00.SDR SWAA2026030274512Cowl Door · pulledNR 2 ENG INLET COWL HAS TWO PULLED THRU FASTENERS AND ONE MISSING FASTENER ON AFT BULKHEAD AT 3 O`CLOCK POSITION VIEWING AFT FACING FWD. R & R THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01.SDR AALA202603023699Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN AFT PASSENGER CABIN FLOOR STRUCTURE CLIP AT STA 2174 AND LBL 42.5. REPLACED CLIP PER AARD 200 51-00-05-1.SDR AALA202603027064Deu · faultedAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR 4L SLIDE PRESSURE AMBER CAUTION MESSAGE APPEARED DURING CRUISE FLIGHT. MAINTENANCE FOUND FAULT MESSAGE FOR DECODER ENCODER UNIT (DEU-B-300RH8) AND REPLACED IT PER AMM 23-73-47. A SATISFACTORY OPERATIONALSDR AALA202603028209Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.SDR DALA2026030201425Fuel Line · leakingFAINT SMELL OF JETT FUEL IN CABIN UPON ARRIVAL TO JET. JET WAS SHUTDOWN WITH EXTERNAL AIR HOOKED UP. FOUND RETURN TO TANK LINE & SHROUD LEAKING IN FWD RT AFT BAG BIN WALL. REPLACED ORINGS ON RETURN TO TANK LINE & SHROUD PER B717 AMM 28-26. (8558590)SDR DALA2026030201421Skin · crackedCRACK ON FUSELAGE SKIN STA Y = 1087 LONG 13 LH-14LH SIDE. REPAIR AND PRI 631743-14 (1469678)SDR DALA2026030201420Hinge Fitting · corrodedCORROSION WAS FOUND ON INB AND OUT HOLES (4EAS) UPPER AND LOWER HINGE FLAP ALSO ON SETTLEMENT AREA. REPAIRED PRI 631842-14 REV 2 AND ER/A 631842-14. (1469307)SDR DALA2026030201419Diaphragm · crackedSHIP 9500 CRACKS ON DIAPHRAGM BTW STA Y=160 TO STA Y= 170 X=8 TO X=9 AT PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER B717- 200 SRM 53-00-00 (1468333)SDR JJBA20260302075Battery · inoperativeEMERGENCY LIGHT TURNING ON AND OFF INTERMITTENTLY DURING FLIGHT SEAT 18CD. REMOVED AND REPLACED AISLE EMERGENCY LIGHT BULB AND REMOVED AND REAPLCED #4 EMERGENCY BATTERY. OPS CHECK SAT.SDR AALA202603023676Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 950, LBL 48.5. REPLACED INTERCOSTAL PER SRM 51-40-02.SDR AALA202603024286Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 986, LBL 43. REPAIRED CHORD PER SRM 53-70-51-2R-6.