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 SWAA2026042280031Access Panel · damagedELONGATED HOLE ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026042280125Access Panel · crackedCRACK ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026042280027Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2026042280028Scuff Plate · crackedCRACK HOLE ON THRESHOLD LOCATED AT FWD CARGO COMPARTMENT. REPAIRED THRESHOLD CENTER SCUFF PLATE LOCATED AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SDR SWAA2026042080023Support Angle · crackedCRACKED OXYGEN BOTTLE SUPPORT ANGLE, BS 360, STR 27R - 28R. REPLACED OXYGEN BOTTLE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9; MEASUREMENT OF CRACK: 0.0508.SDR SWAA2026042080120Access Panel · crackedCRACKED ANGLE ON ACCESS PANEL 844DZ ON THE AFT SERVICE DOOR. REPLACED THE ANGLE OF THE ACCESS PANEL 844DZ IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 411A2119, SHEET 71, REV-.SDR SWAA2026042080022Tie Clip · crackedCRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, AND FASTENERS IAW SRM 51-40-02 AND DRAWING 141A1110, SHEET 55, REV -.SDR SWAA2026042080118Access Panel · crackedCRACK ACCESS PANEL 333AT BLADE ANGLE AT LT HORIZONTAL STABILIZER 2026-182072<[01] REPLACED ACCESS PANEL 333AT BLADE ANGLE AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 186A3101 SHEET 24 REV -<BR><BR>MEASURE OF CRACK IS SDR REXA2026041700292Floorbeam · corrodedTHE RH FS 280 FLOOR BEAM IS CORRODED. BEGAN REMOVING CORROSION FROM RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-21-06-001-001-A01. PART IS HEAVILY CORRODED FROM BL0 TO RBL9 WITH MORE THAN 50% MATERIAL LOST AND DAMAGE STILL PRESENT. CROSSBEAM REQUIRES REPLACEMENTSDR SWAA2026041680108Shear Tie · corrodedCORRODED SUPPORT ANGLE, BS 520, STR 28L - 28R IN THE FWD CARGO BAY. REPLACED THE SHEAR TIE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 143A3230, SHEET 121, REV A, AND DWG 143A1215, SHEET 93, REV -.SDR SWAA2026041680111Angle · corrodedCORRODED ANGLE, BS 767 - 787, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A8123, SHEET 16, REV-.SDR SWAA2026041680018Angle · crackedCRACKED ANGLE LOCATED BS500D, STR 28R FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET: 126 REV: A.SDR REXA2026041600289Floorbeam · corrodedTHE LT FS 280 FLOORBEAM CORRODED REMOVED CORROSION FROM LT FLOORBEAM IAW SRM 51-21-06-001-001-A01. PART IS HEAVILY CORRODED FROM BL0 TO LBL9 WITH MORE THAN 50% MATERIAL LOST & DAMAGE STILL PRESENT. LOCATED & DRILLED A NEW FLOORBEAM IAW SRM 51-40-11-001-001-A0SDR SWAA2026041580017Stringer · corrodedCORRODED STRINGER 23R LOCATED BS540 WL165 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 23R LOCATED LOCATED BETWEEN BS 500D TO BS 540 WL165 AT FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1. REPAIR 1 AND DRAWING 143A3250 SHEET 109 REV A; DWG 143A1215 SHEET 94 REV.SDR SWAA2026041580019Stringer · crackedCRACKED STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER SECTION 26L LOCATED BETWEEN BS 500D MORE 10 INCHES TO BS 540 AT FWD CARGO COMPARTMENT I.A.W SRM 53-00-03-2R-1. REPAIR 1.SDR SWAA2026041480109Shield · corrodedCORROSION SHIELD WEB LOCATED BS767 TO BS794 RBL21 AND WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BS767 TO BS794 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET: 31; REV -.SDR SWAA2026041385063Cowling · corrodedON THE NR 2 OTBD FAN COWL; THE FWD HOLD OPEN ROD STOWAGE POINT HAS EVIDENCE OF CORROSION AROUND THE CENTER ATTACH POINT AND THE CENTER POINT SPINS. REMOVED AND REPLACED #2 O/B FAN COWL PER MM 71-11-02. REFERENCE TTG8Q01BDEQR FOR PARTS INFORMATION AND TTG8Q01SDR IPXA2026040685799Support Strap · corrodedCORROISION FOUND ON FWD CARGO CEILING GILL LINER SUPPORT STRAP UNDER NUT PLATE STA 820 LBL 45. FOUND WHILE WORKING EO.89712-REQ007 DECOMPRESSION PANEL.ATA 25. INSTALLED STRAP P/N STESAA7003345555-7 AT FWD CARGO CEILING SUPPORT STA 760 TO STA 840 LBL 45.5 PESDR HNAA2026040600268Gusset · corrodedDOOR GUSSET AT FR 20 AND FR 22 FOUND CENTER OMEGA BEAM CORRODED AROUND NUT PLATE HOLE. REPAIRED CORRODED AREAS WITH DOUBLER AND FILLER ON CENTER OMEGA AT FR22 IAW EMB 145 SRM 53-21-10-RE SECTION 3(G) SEE WO H10323 QN 2177 MAJOR EO# EO-1-53-26-0148SDR SWAA2026040179973Screw · missingGIRT BAR LATCH BUTTON HEAD SCREWS MISSING FROM L1 DOOR. REINSTALLEED GIRT BAR BRACKET HARDWARE IAW AMM 25-66-01.SDR IPXA2026032788116Hinge · corrodedRIGHT ECS BAY DOOR PNEUMATIC GROUND SERVICE DOOR HAS TWO EXFOLIATED HINGES. VERIFIED STEP 4. REMOVAL OF TWO CORRODED HINGE FROM DOOR PNEUMATIC GROUND SERVICE DOOR.IAW SRM 51-40-02. INSTALLED THE HINGES IN RT ECS BAY DOOR PNEUMATIC GROUND SERVICE DOOR IAW SRSDR AALA202604013199Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING OUTBOARD AFT FLAP UPPER AND LOWER SURFACE HAS EVIDENCE OF DELAMINATION AT INBOARD END. SUCCESSFULLY REPAIRED DELAMINATED AREAS FOUND AT RIGHT HAND WING OUTBOARD AFT FLAP UPPER AND LOWER SURFACE INBOARD END. PER B73SDR IPXA2026032783724Fairing · crackedCRACKED FAIRING, NR 2 ENG LT TRANSCOWL INNER LWR AREA. INSTALLED A NEW FAIRING IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-31, REV 94.SDR AALA202603315025Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603313651Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603313983Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603314567Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR AALA202603314135Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.SDR IPXA2026032588224Thrust Reverser · dentedFAULT-STR-Z400 #1 ENG O/B T/R C-DUCT ACOUSTIC INNER SKIN HAS A PUNCTURE (2 LOCATIONS), INSPECTED, REPAIRED DAMAGED AREA (2EA), FILLED HOLES 2(E/A) WITH ADHESIVE FILLER COMPOUND P/N:04-009-0146 B/N:0004667693, IAW B757-200 AMM 78-31-20-308-117.SDR FDEA202603150376Web · crackedMDCC UNDER FLOOR WEB AT FR47, BETWEEN Y0 AND -Y450 CRACKED. REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN Y0 AND -Y450 PER A300- 600F SRM53-15-15-201-C2. THIS REPAIR IS CATEGORY B PER A300-600F SRM53-15-15-201-C2, IT MUST BE INSPECTED AT DEFISDR FDEA202603150375Web · crackedMDCC UNDER FLOOR WEB AT FR47, BETWEEN Y0 AND Y450 CRACKED. REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN Y0 AND Y450 PER A300- 600F SRM53-15-15-201-C2. THIS REPAIR IS CATEGORY B PER A300-600F SRM53-15-15-201-C2, IT MUST BE INSPECTED AT DEFINEDSDR U5QA202603150168A/C Pack · inoperativeMEL 21-52-00-02 (CAT A NO EXT) R PACK FAIL AMBER CAS MESSAGE - SMOKE APPEARS IN THE CABIN NEAR R2 THEN 10 MINUTES LATER THE R PACK FAIL. MX C/A: RH AIR CYCLE MACHINE (ACM) REMOVED AND REPLACED.SDR KCSA202603261513Lamp · inoperative100234149: R1 DOOR EXTERNAL EMERGENCY LIGHT INOP. CORRECTIVE ACTION: RELAMPED R1 DOOR EMERGENCY LIGHT PER B777-300 AMM 33-51-04. OPS CK GOOD.SDR AALA202603249137Wire · disconnectedAIRCRAFT WAS NOT GROUNDED: ROW 18DEH SEAT MOUNTED EMERGENCY LIGHTS INOP ON BOTH SIDES OF AILSE. **SUPPLEMENTAL REPORT FOR SDR AALA202603189137 SUBMITTED BY ORD 3/15/26. **(CLOSED)** MAINTENANCE RECONNECTED WIRES AT PASSENGER SEAT TRACK COVER FOR L/H18 DEH ROW SDR AALA202603243671Unknown · odorAIRCRAFT WAS GROUNDED: STRONG SMELL OF BURNING OIL IN THE ENTIRE AIRCRAFT, SMELL GOT WORSE DURING INITIAL CLIMB OUT. NORMAL CLIMB CONFIGURATION. DECESION MADE TO RETURN TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHEDSDR DALA2026032401973Bottle · leakingR2 DOOR ASSIST PRESSURE LOW. R & R DOOR ASSIST CYLINDER AND SERVICE IAW AMM 52-15. OK FOR SERVICE. (1495689)SDR ASAA2026031563862Smoke Detector · faultedCRG SMK FWD FAIL, (1B). ( LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM DETECTOR UNITS [ONE DETECTOR AT EACH LOCATION MAY BE INOPERATIVE AND THE REMAINING PORTIONS OF THE SMOKE DETECTION SYSTEM MAY STILL BEUSED.] ). GROUNDED - YES. REMOVED AND RPELACED. FWD CSDR DALA2026031901909Light · inoperativeFOUND RT SIDE EXTERIOR SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED RT SIDE SLIDE ILLUMINATION LIGHT. (LP 7462391)SDR DALA2026031901906Seat Track · corrodedCABIN SEAT TRACKS UPPER FLANGE SURFACE FOUND CORRSION AT BS 1480, RBL 54.75. THE CORROSION ON SEAT TRACK UPPER FLANGE AT BS 1480, RBL 54.75. REMOVED AND MEASURED, FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, FIG 101, REV 77. THE DAMAGE SEAT TRACK WAS REPAIRESDR DALA2026031901905Skin · damagedSECTION 48 RT SKIN AT BS 1730, WL 200 FOUND ABRASION. THE ABRASION ON SECTION 48 RT SKIN AT BS 1730, WL 200. REMOVED AND MEASURED: FOUND OUT OF LIMITS IAW SRM 53-80-70-1A-1, FIG 101, REV 77. DAMAGE SKIN REPAIRED IAW SRM 53-80-01-2R-3, REV 77. (LP 1495387)SDR DALA2026031901904Skin · damagedSECTION 48 LEFT SKIN AT BS 1730, WL 200 FOUND ABRASION. ABRASION ON SECTION 48 LT SKIN AT BS 1730 WL200 REMOVED AND MEASURED, FOUND OUT OF LIMIT IAW SRM 53-80-70-1A-1, FIG 101, REV 77. THE DAMAGE SKIN REPAIRED IAW SRM 53-80-01-2R-3, REV 77. (LP 1495385)SDR BAGA2026031900004Elec Connector · unsecureFA REPORTS EMERGENCY LIGHTS FLICKERING AT OVERWING EXIT. RESECURED ELECTRICAL CONNECTOR, OPS CHECK GOOD.SDR AALA202603190216Elevator · excess playAIRCRAFT WAS GROUNDED: AIRCRAFT HAD A VIBRATION FELT ON THE FLIGHT DECK ON CLIMB OUT. VIBRATION WAS FELT FOR ABOUT 5 SECONDS AND THEN STOPPED FOR ABOUT A MINUTE. THIS OCCURRED FROM 12000 FT TO FL 240. IT THEN STOPPED AND DID NOT RETURN FOR THE REMAINDER OF THSDR DXTA2026031907263Engine · failedDURING THE TAKE OFF ROLL AROUND 30 KNOTS WE EXPERIENCED A RIGHT ENGINE FAILURE. WE HEARD 4-5 COMPRESSOR STALLS. ENGINE SHUT DOWN ON ITS OWN. WE PULLED OFF THE RUNWAY AND HAD THE AIRCRAFT TOWED TO SIGNATURE. UPON VISUAL INSPECTION WE DID NOT NOTICE ANY ABNOSDR DXTA2026031907268Control Lever · defectiveON APPROACH ATC ASKED FOR SLOWEST PRACTICAL SPEED. CREW STARTED TO CONFIGURE BY LOWERING FLAPS AND GEAR. FLAPS 2 WAS REQUESTED AND AN AMBER FLAP FAIL CAS WAS DISPLAYED. CREW DECLARED AN EMERGENCY AND CANCELLED APPROACH CLEARANCE. FLAP FAIL QRC WAS ACCOMPLISHEDSDR DALA2026031901883Stringer Splice · not reportedFUSELAGE STRINGER SPLICE 2R, FR 60 - 62. MAJOR REPAIR IAW ERA 632531-14. (1495930)SDR 2DYA202603150004Light · inoperativeFORWARD DOOR L3 EMERGENCY LIGHT INOP. APPLIED MEL 33-51-01 CAT C. . TROUBLE SHOOTING ON GOING.SDR SWAA2026031880169Flashlight · failedFA REPORTS FRONT GALLEY LOWER FLASHLIGHT NOT TESTING. REMOVED AND REPLACED IAW AMM 25-64-00-SWA-807-NG-01.SDR SWAA2026031879901Lamp · inoperativeFORWARD MOST LT FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECKED GOOD.SDR SWAA2026031879789Light · inoperativeEXTERIOR EMERGENCY LIGHT ON L1 DOOR INOPERATIVE. R&R THE LIGHT ASSEMBLY IAW AMM 33-51-04. OPS CHECKED GOOD.