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 AALA202603309358Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR YENA2026033000351Igniter · failedFLT 724 LAX-JFK (ETOPS), ENG 1 IGNITION A FAULT ( IGNITION SYSTEMS A) SYSTEM A ). REPLACED ENG 1 IGNITER PLUG IAW AMM 74-21-00 OPS CHK GOOD. THIS CLEARS THE MDDR. MX-4 UPDATED PLACARD REMOVED.SDR AALA202603305690Light · inoperativeAIRCRAFT IN BASE MAINTENANCE: FWD AISLE EMERGENCY LIGHT ON 6H FAILED TO ILLUMINATE. MAINTENANCE INSTALLED A NEW SERVICEABLE FLOOR PROXIMITY LIGHT IAW AMM 33-51-06.SDR AALA202603302980Latch · stuckAIRCRAFT WAS NOT GROUNDED: LAV D JAMMED DOOR. PASSENGER WAS BRIEFLY STUCK. MAINTENANCE LUBRICATED DOOR LATCH TO LAV "D". GRD OPS CHECK NORMAL.REF GPM 02-01-2.SDR YENA2026033000347Fire Loop · faultedFLT # 524 LAX-JFK (ETOPS). ENG 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS 1) LOOP A ). OPENSDR DALA2026033002063Girt Bar · damagedR3 DOOR GIRT BAR DAMAGED. REMOVED R4 SLIDE PER WORKCARD 2566-9001-4R. REMOVED AND REPLACED R4 GIRT BAR PER B757 AMM 25-66-10. REINSTALLED R4 SLIDER PER WORKCARD 2566-9001-4R. REPLACED 4R DOOR GIRT BAR PER B757 AMM 25-66-10. REINSTALLED REMOVED SLIDE PER AMDSSDR DALA2026033002055Wire Harness · shortedDIVERSION TO ATL DUE TO RIGHT ENGINE EGT EXCEEDANCE. ECU FAULTING T495 SENSOR. INSPECTED WIRING HARNESS AND FOUND JUNCTION BOX SHORTED. REPLACED MAIN JUNCTION BOX, OPS CHECK OK. (LP 8377943)SDR ABXA20260328136Fire Warning · false activationDURING LOADING, MAIN CARGO FIRE MESSAGE. VERIFIED NO FIRE PERFORMED OPS TEST IAW 26-14-00, FIRE DEPT. SCANNED A/C FOR FIRES, NO FIRE CONFIRMED. A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.SDR FDEA202603280380Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241HFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 241HFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET2 REV.SDR FDEA202603280379Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 232KFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 232KFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50.2R PAR 4-B FIG 201 SHEET2 REV. 94 DEC 15/2025SDR FDEA202603280378Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231UFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 231UFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET2 REV 94 DEC 15/2025SDR FDEA202603280377Floor Panel · damagedPUNCTURE ON FLOOR PANEL 231MFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 231MFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR CALA2026033014919Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE R/H WING INT ERSPAR LWR SKIN APB PANEL P/N 757-3401-2 REPLACEMENT BETWEEN WS 711.50 & 743.50 IS APPROVED AS TIME LIMITED FOR 18 MONTHS UNTIL PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA).SDR CALA2026033014917Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE RT WING APB SPLICE & ADJACENT LWR SKIN PANEL HOLES CRACKED INBD OF WS 711.5 0 & THE LWR SKIN PANEL L-8 STRINGER AT APPROX. WSTA 700 IS APPROVED AS TIME LIMITED.SDR CALA2026033014912Skin Splice · crackedRIGHT WING OTBD MAIN SKIN SPLICE WAS CRACKED. REMOVED AND REPLACED SKIN SPLICE IAW DWG 757-3400, SRM 51-40-02, ECRA 5720-03636 REV-, & REO G25831, REV IR.SDR CALA2026033014911Angle · crackedRT WING LOWER STR NO. 8 SPLICE PN 757-3403-4 PER REO G25831, REMOVED AND REPLACED STR 8 SPLICE. REMOVED AND INSTALLED FREEZE PLUGS AT DISCREPANT HOLE, RESTORED COATING REF B737NG 51-40-02, ECRA 57220-03636 REV - AND AAR REO G25831 REV IR.SDR CALA2026033014910Skin · crackedRIGHT WING OTBD FWD SKIN SPLICE WAS CRACKED. R & R THE SKIN SPLICE IAW DWG 757-3400, REV E, SRM 51-40-02, EC/RA 5720-03636 REV-, & REO G25831, REV IR.SDR DALA2026033002054Valve · faultedDIV - INTO BOS DUE TO INTERMITTENT DUAL BLEED ECAM FAULT. REPLACED BMC NR 1, NR 2 PRV, AND NR 2 PRV SENSE LINE. PERFORMED HEALTH CHECK ON BOTH SYSTEMS. OPS CHECK GOOD. (8506464)SDR F3LA202603280393Battery · no testNR 3 EPSU BATTERY (12WL) FAILED TO TEST, ACFT WAS NOT GROUNDED, SCHEDULED RON MAINTENANCE HEAVY CHECK. R & R THE EPSU BATTERY (12WL) IAW AMM 33-51-38-000-002-A, & 33-51-38-400-002-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR F3LA202603280392Battery · no testNR 2 EPSU BATTERY (11WL) EMERGENCY LIGHT FAILED TO TEST, ACFT WAS NOT GROUNDED. SCHEDULED RON MAINTENANCE HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (11WL) EMERGENCY LIGHT IAW AMM 33-51-38-000-002-A, & 33-51-38-400-002-A. OPS CHECKED GOOD. AIRCRAFT RESDR 2026FA0000236Support · corrodedLEVEL 2 CORROSION WAS FOUND ON LOWER FUSELAGE FAIRING SUPPORT STRUCTURE AND FFS575 LBL6SDR R61A2026032800070Skin · damagedDURING AAI INSP. FOUND - AAI DISCREPANCY ITEM NR 2 REPAIR NR 38 - FR 27-28, STGR 22R-23R, PROVIDES A REPAIR DISPOSITION OF SRM 51-75-11 FOR DAMAGE BETWEEN STGR 22R AND 23R; HOWEVER, SRM 51-75-11 IS NOT APPLICABLE BECAUSE THE DOUBLER CROSSES A RIVET ROW (STGR SDR R61A2026032800069Skin · chafedDURING HEAVY CHECK FOUND, SKIN UNDER AFT PAX DOOR 3 ISOLATORS, 2 ON TOP AND 1 ON BOTTOM AFT HAS CHAFING DAMAGE.SDR R61A2026032800068Plate · chafedRIGHT ENGINE OTBD THRUST REVERSER MIDDLE THERMAL INSULATION BLANKET WEAR PLATE IS GOUGED.SDR R61A2026032800067Plate · chafedLEFT ENG INBD THRUST REVERSER MID. THERMAL INSULATION BLANKET WEAR PLATE IS GOUGEDSDR SWIA2026032777755Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 195BB. BLENDED AND EVALUATED, FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW REO 601R-53-00-943, REV -, & SRM 53-00-31 PAR 4 B, FIG 101, & FIG 102. COMPLIED WITH TASK CARD 51-900-10SDR SWIA2026032777751Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 192BB. EVALUATED AND REPAIRED THE AREAS IAW REO 601R-53-31-1372, REV --, & REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, PRESSURIZATSDR SWIA2026032777750Floor Panel · crackedLEFT TRU BAY FLOOR PANEL WAS CRACKED AT BS 193, LBL 30. PERFORMED A REPAIR ON THE TRU BAY FLOOR PANEL IAW REO 601R-53-11-4067, REV-, TASK CARD 51-900-1003-SKY COMPLIED WITH.SDR SWIA2026032777749Skin · corrodedNUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 191BB. EVALUATED & REPAIRED AREAS AS REQUIRED IAW REO 601R-53-31-1372, REV --, REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, NO WEIGSDR SWIA2026032777748Floor Panel · crackedRIGHT TRU BAY FLOOR PANEL WAS CRACKED AT BS 193, RBL 30. PERFORMED A REPAIR ON THE ELECTRICAL BAY FLOOR PANEL IAW REO 601R-53-11-245, REV C, REPAIR TYPE II, VIEW II, SHEET 6.SDR HNAA2026070900588Shear Tie · crackedSHEAR TIE CRACKED AT FR 25 BTW STR 15-16L. R & R SHEAR TIE IAW SRM 51-40-02SDR SWIA2026062676317Floor Support · corrodedFLOOR SUPPORT HAD MULTIPLE SPOTS OF CORROSION AT LBL 27 BETWEEN BS 574 - 621. REPLACEMENT OF FLOOR SUPPORT AT LBL 27 BETWEEN BS 574 AND BS 606.5 PERFORMED ON JOB HN00307254, CAMP 32083421. REPAIRED END FITTING AT LBL 27 BETWEEN BS 606.5 AND BS 621 IAW REO 60SDR SWIA2026032776278Lug · damagedPASSENGER DOORS DOOR SIDE OF THE HINGE LUG 27 ROLL PIN HOLE IS ELONGATED. DRILLED AND LOCATED NEW PAX DOOR PIANO HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01, STEPS E, F, G, H, I AND SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG 601R31702, REV N.SDR SWIA2026032776274Skin · scratchedMULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO BS 1051.30 BETWEEN S27R AND S24R. REPAIRED MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO 1051.30 BETWEEN S27R AND S24R. IAW REO 670-53-61-2715 REV -.SDR VNAA202606120024Shim · corrodedCORROSION ON SHIMS AND NUTS OF HINGE SUPPORT OF ACCESS PANEL 182BR. SHIMS AND NUTS OF HINGE SUPPORT OF ACCESS PANEL 182BR WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-SDR IPXA2026041403483Flap · cracked*** MAJOR REPAIR *** FAULT: 1EA CRACKS FOUND AT R/H RIB 15 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96975-REQ1 AND VT-MAE EA 300-5753-27-A4410, REV. -.SDR IPXA2026033103502Skin · crackedMAJOR RPAIR, 1EA CRACKS FOUND AT RT RIB 26 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. ACCOMPLISHED PERMANTENT REPAIR IN ACCORDANCE WITH EO-96969-REQ1 AND VT-MAE EA 300-5753-27-A4408, REV. -.SDR IPXA2026042710419Skin · crackedLEFT WING I/B FLAP UPPER SURFACE I/B RUB STRIP HAS A CRACK AND ARROUN IT SKIN TOO, ALSO NEEDS A INPECTION UNDER IT TO RULE OUT DAMAGE TO THE RIB DOT 31-015 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97032-REQ1 AND VT-MAE EA 300-5752-27-A4416, REV. _.SDR HNAA2026050500379Retainer · damagedRIGHT THRUST REVERSER HAS DAMAGED OB SEAL RETAINER AND CRACKED OB SEAL RETAINER. R & R SEAL RETAINERS IAWSRM 51-40-02SDR SWAA2026050483868Stiffener · crackedCRACKED VERTICAL STIFFENER. BS 540 AND LBL 24.75 UPPER POSITION AT FWD CARGO BAY. REPLACED VERTICAL STIFFENER & FASTENERS IAW; SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DRAWING 111A2001 SHEET 79, REV -.SDR SWAA2026050483937Web · corrodedCORRODED SHIELD WEB LOCATED BETWEEN STA 492.4 TO STA 500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS AND RBL21 WL156 AT FWD CARGO<BR>COMPARTMENT IAW SRM 51-10-02-0G-0 AND SRM 51-40-02-0G AND DWG: 143A0080; REV:-; .SDR SWAA2026050495348Shield · corrodedCORROSION SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS 492.4 TO 500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT IAW SRM 51-10-02-0G-0 AND SRM 51-40-02-0G AND DWG: 1SDR SWAA2026050483938Angle · crackedCRACKED ANGLE, STA500G AND STR26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP AND FASTENERS LOCATED STA 500G AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40 -02 AND DWG 143A7505 SHEET 137 REV-.SDR SWAA2026050495349Angle · crackedCRACKED ANGLE, STA500G AND STR26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP AND FASTENERS LOCATED STA 500G AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40 -02 AND DWG 143A7505 SHEET 137 REV-.SDR SWAA2026050483933Tie Clip · crackedCRACK TIE CLIP LOCATED BS 500I AND STR26R FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED STA500I AND STR26R FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A1215; SHEET: 157 TO 158; REV - .SDR SWAA2026050483940Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAYS. REPLACED SUPPORT BRACKET LOCATED BS 540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAYS IAW SRM 51-10-02 AND DWG 212A1101 REV -.SDR SWAA2026050483935Support · crackedCRACK SUPPORT ZEE LOCATED BETWEEN STA500C TO STA500D AND LBL21 WL156 AT FWD CARGO COMPARTMENT. THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.SDR SWAA2026043083934Tie Clip · crackedCRACKED TIE CLIP, BS 500I, S26L IN THE FWD CARGO BAY. REPLACED TIE CLIP LOCATED BS 500I, S26L IAW SRM 51-40-02, & DWG 143A1215, SHEET 157 - 158, REV - .SDR SWAA2026043083936Support · corrodedCORRODED SUPPORT ZEE, BTWN BS 500A - 500C, RBL 21, WL 156 IN THE FWD CARGO BAY. REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, & EA M-22-153-01550.SDR SWAA2026043083952Stringer · crackedCRACKED STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING. REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING IAW EA 26-157-00896-WIP1.