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 SWAA2026031668573Nut · corrodedCORROSION ON RAIL NUT LOCATED OSS 126.72 BETWEEN OSS 140.92 AT LH WING. REPLACED NEW RAIL NUT IAW SRM 51-40-02-0G.SDR SWAA2026031668579Nut Plate · corrodedCORROSION ON RAIL NUT LOC OSS 93.30 BETWEEN OSS 106.65, LT WING. REPLACED NEW RAIL NUT LOC APROX OSS 93.30 BETWEEN OSS 106.65 ON LH WING SEE TTG8Q01A8AB5 STEP 5 ITEM 9. IAW SRM 51-40-02-0G.SDR SWAA2026031668580Nut Plate · corrodedCORROSION ON RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LT WING. REPLACED NEW RAIL NUT LOCATED OSS113.18 BETWEEN OSS 118.65 AT LH. WING SEE TTG8Q01A8AB5.SDR SWAA2026031668753Web · crackedCRACK ON WEB INBD FAN COWL ON ENGINE 1 2026-112370<[01] REPLACED WEB ON INBD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30, REV 32, PAGE 10092.SDR SWAA2026031368844Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661BB, RT WING[01] STEP 12. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IPXA2026022786894Skin · delaminatedMAJOR REPAIR, APU COMPT LOWER SKIN BELOW THE EXHAUST DUCT INNER SURFACE DELAMINATED AT BS 1992. THE PROTECTIVE COATING WAS RESTORED IAW AMM 51-21-15-370-802.SDR VNAA202603130009Bulkhead Web · corrodedCORROSION ON LWR WEB OF BULKHEAD FS 280.0 LBL 12 (BEHIND CAP ANGLE) AT COCKPIT. CORROSION ON LWR WEB OF BULKHEAD FS 280.0 LBL 12 (BEHIND CAP ANGLE) AT COCKPIT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPAIRED CRJ-900 SRM 53SDR VNAA202603130008Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBLSDR VNAA202603130007Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBSDR VNAA202603130006Web · crackedCRACK IN THE WEB UNDER THE ADG PUMP FROM STA FS193 (FWD EQUIPMENT COMPARTMENT) CRACK IN THE WEB UNDER THE ADG PUMP FROM STA FS193 (FWD EQUIPMENT COMPARTMENT) WAS REPAIRED PER REO 690-53-11-2148REV. - -SDR SWAA2026031268587Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE, IN THE AFT CARGO BAY. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026031268586Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE LOC AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.SDR SWAA2026031168722Angle · crackedWEB ANGLE CRACKED ON BACK SIDE JUST INBD OF DEFLECTION RIB. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02.SDR ASAA2026020764720Floorbeam · corrodedRIGHT FRAME 947 HAS CORROSION UPPER SURFACE NEAR LAV MOUNT BRACKET. GROUNDED - YES. REPAIRED FLOORBEAM STA 947 IAW BOEING SRM 53-70-51-2R-5 REPAIR 5 & EA 900ER-53EA-29930 REV 00W= .850" O= .180 R= .108 L= .950" D= .072".SDR IPXA2026022486878Skin · delaminatedMAJOR REPAIR APU COMPT LH WALL INNER SKIN DELAMINATED IN AREA ABOVE THE OIL COOLER AIR EXIT DUCT. PREPARED AREA AND FABRICATED REPAIR PARTS IAW B757-200PF SRM 51-70-10-2R-4.SDR CALA2026030514368Stiffener · crackedCRACK FOUND ON RT STABILIZER INSPAR RIB, HSS 92.7, ON INBD SIDE, NEAR BOTTOM OF VERTICAL STIFFINER NR 4. REPAIRED DAMAGE IAW SRM 55-10-09-2R-4, AND SRM 55-10-01-2R-11. TSDR IPXA2026022186459Longeron Fitting · crackedDURING PERFORM UPS EO-281410-JIC017 FOUND LOWER LONGERON SPLICE FITTING AFT SIDE CRACK AT STA 2598 S-11R. ACCOMPLISHED REPAIR I.A.W EO-96692-REQ1 REV1 AND EGAT EI F2026A53M-361 REV.2.SDR IPXA2026022186495Longeron Fitting · crackedCRACK - FITTING - DURING PERFORM UPS EO-28141-JIC017 FOUND LOWER LONGERON SPLICE FITTING AFT SIDE CRACK AT STA 2598 S-11L (REPLACE) RII COMPLETED STEP 19 PERFORM E.I. NO.F2026A53M-361 SEQUENCE:B PAGE 2 OF 10 STEP:12. VERIFY THE SERVICE DIFFICULTY REPORT ( SDR)SDR SWAA2026030368539Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663, LBL 40. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026030368540Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663, LBL 40. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026030368541Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663, LBL 40. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IPXA2026030387426Bracket · crackedLEFT MLG WW INBD SEAL RETAINER SUPPORT STRUCTURE BRACKET 6EA, FOUND CRACKED AFTER REMOVAL OF SEAL RETAINER BS 1060. INSTALLED NEW BRACKETS IAW SRM 51-40-02.SDR IPXA2026030286480Longeron Splice · crackedCRACKED FITTING, DURING PERFORMANCE OF EO-28141-JIC017, FOUND THE UPPER LONGERON SPLICE FITTING AFT SIDE CRACKED AT BS 2598, S11L. REMOVED THE DAMAGE LONGERON SPLICE IAW SRM 51-40-02-0G-0, REV 106, AND INSTALLED A NEW LONGERON SPLICE IAW SRM 51-40-02-0G-0, RESDR IPXA2026030287293Fitting · brokenBROKEN FITTING, LT WING INBD TE CAVITY UPPER RIB SUPPORT FITTING, WBL 432. REMOVED THE DAMAGED FITTING IAW SRM 51-40-02-0G, REV 106, & INSTALLED A NEW FITTING IAW SRM 51-40-02-0G, REV 106, & DWG 65B10865, SHT 2, REV N.SDR IPXA2026030291662Strap · corrodedSTR ACCESS DOOR313AL LOWER STRAP HAS CORROSION BETWEEN RBL 9 AND LBL 12. REMOVED COVER STRAP FOR ACCESS AND STRAP CORRODED IAW SRM 51-40-02-0G-0 INSTALLED AND PAINTED LOWER STRAP ACCESS DOOR 313AL BETWEEN RBL 9 AND LBL 12 IAW SRM 51-40-02SDR IPXA2026022593920Support Angle · corrodedFWD CARGO AT STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19 HAS CORROSION DOT 5842-11 REMOVED CORROSION AT THE STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19. I.A.W SRM 51-10-02. AFTER FURTHER EVALUATION IT WAS FOUND OUT OF LIMITS. I.A.W SRM 51-10-SDR AALA202602263178Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM BS 500 TO BS 500I, AT LBL 24. REPLACED TRANSITION PANEL PER SRM 51-40-02.SDR SWIA2026022575329Skin · corrodedFOUND MINOR CORROSION AROUND 3 SCREW HOLES OF VHF-1 ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION AROUND 3 SCREW HOLES VHF-1 ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPER FUSELAGE SKIN PANSDR SWIA2026022575324Skin · scratchedSURFACE SCRATCHES ON FUSALAGE SKIN UNDER UPPER VHF-1 ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER UPPER VHF-1 ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPER SDR SWIA2026022575323Skin · scratchedSURFACE SCRATCHES ON FUSALAGE SKIN UNDER LH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER LH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPSDR SWIA2026025775318Skin · corrodedFOUND CORROSION AROUND 3 SCREW HOLES UNDER RH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION DAMAGE AROUND 3 SCREW HOLES UNDER RH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2810 REV "A" DATED 2026-02-08 "REPAIR FOR ELONGATED HOLE AND TOSDR SWIA2026020775317Antenna · corrodedFOUND CORROSION AROUND 3 SCREW HOLES UNDER LH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED CORROSION AROUND 3 SCREW HOLES UNDER LH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2811 REV "--" DATED 2026-02-08 "DISPOSITION FOR BLENDED DAMAGE TO UPPESDR SWIA2026022575313Skin · scratchedSURFACE SCRATCHES ON FUSALAGE SKIN UNDER RH ATC L-BAND ANTENNA (C-CHECK RO 02/22/2026)REPAIRED SURFACE SCRATCHES ON FUSELAGE SKIN UNDER RH ATC L-BAND ANTENNA WITH REFERENCE TO REO 670-53-21-2810 REV "A" DATED 2026-02-08 "REPAIR FOR ELONGATED HOLE AND TOOLINSDR SWAA2026022468868Stub Frame · crackedCRACK FOUND R1 DOOR STUB FRAME, .1 INCH ABOVE SEAL DEPRESSOR, BS 291.5 +10, L: .3 INCHES. REMOVED AND REPLACED THE R1 DOOR STUB FRAME IAW SRM 51-40-02.SDR IPXA2026021691664Transition Panel · dentedFWD CARGO TRANSITION PANEL AT STA 630 RBL 22 HAS A GOUGE. REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALLED REPAIR PART ON SIDE PANEL AT STA 630 RBL22. IAW B757-200 WITH SREO-3220-REQ003, SRM 51-70-13 FRSDR DALA2026022301267Battery Pack · inoperativeDURING SVC FOUND SEATS 51FG-56FG EMERGENCY EXIT LIGHTS OUT. R/R EMERGENCY EXIT LIGHT BATTERY (M734) PER B767-400 AMM 33-51. (8564135)SDR REXA2026022300063Crossbeam · corrodedLEFT BS 280 CROSSBEAM CORRODED FROM BL0 - LBL9. REMOVED DAMAGE IAW SRM 51-21-06-001-001-A01, NO ALLOWABLE LIMITS GIVEN. 50% MATERIAL LOSS REQUIRES REPLACEMENT INSTALLED CROSSBEAM , IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-00SDR REXA2026022300062Crossbeam · corrodedRIGHT BS 280 CROSSBEAM CORRODED FROM BL0 - RBL9. CROSSBEAM CORRODED FROM BL0 - RBL9, REMOVED DAMAGE & STOPPED AT 50% MATERIAL LOSS. NO ALLOWABLE DAMAGE GIVEN . REQUIRES REPLACEMENT REMOVED DAMAGE IAW SRM 51-21-06-001-001-A01. REMOVED SPLICE FROM LBL9 - RBL9 SDR FDEA202602070226Safety Wire · wrong partREF WRI 25-60 /7566,WHILE ACCOMPLISHING FEA G-2560-F0386294A, FOUND R/H EMERGENCY EVACUATION SLIDE WITH THE WRONG SAFETY WIRE ON THE PACKBOARD ATTACH CABLE. AMM: 25-66-01-4. INSTALLED RH DOOR SLIDE IN REF TO 777 AMM. OPS CHECKED GOOD.SDR CALA2026021813866Skin · dentedRT EXTERIOR FUSELAGE SKIN DENTED JUST FWD OF FR63 BTWN STR 37-38R. PERFORMED DOUBLER REPAIR IAW SRM 53-41-11-300-109.SDR JJBA20260217049Frame · corrodedAFT WET AREA 1EA FRAME SUPPORT AT FR 59, STR 21L, HAS CORROSION. REMOVED AND REPLACED FRAME SUPPORT AT FR59 STR 21L-21RSDR JJBA20260217040Frame Angle · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY IB FWD FRAME CLIP AT FR 60 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY INBD FWD FRAME CLIP AT FR60SDR JJBA20260217039Pulley Bracket · corrodedAFT WET AREA 1EA RUDDER CABLE PULLEY OB FWD FRAME CLIP AT FR 60 HAS CORROSION. REMOVED AND REPLACED AFT WET AREA 1 EACH RUDDER CABLE PULLEY OUTBD FWD FRAME CLIP AT FR60SDR KCSA2026020706Handle · unsecureDOOR F/D OVHD ADVISORY. SECURED HANDLE IAW KA B747-400 AMM 52-21-00. OPS CHECK GOOD.SDR AALA202602121939Warning Message · false activationAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED A DOOR LEFT OVER WING EXIT ECAM MESSAGE. MAINTENANCE PERFORMED TEST OF DOOR PER TSM 52-22-00-810-835-A AND NO FAULT WAS NOTED. NOTE MAINTENANCE DID NOT IDENTIFY A SPECIFIC PART THAT WOULD HAVE CAUSED THE ECAM MESDR SWAA2026021168736Battery Pack · inoperativeTHREE EMERGENCY AISLE LIGHTS ARE INOPERATIVE, BETWEEN R1 & RT OVERWING EXIT. R & R ONE EMERGENCY BATTERY PACK M1676, OPS CHECKED GOOD IAW AMM 33-51-06-960-805.SDR SWAA2026021168872Battery Pack · inoperativeON AN OPS CHECK, FOUND AFT COS BOX TRIM PANELS; COVE PANELS; AND AFT RT EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK AND TESTED GOOD IAW AMM 33-51-06-960-802.SDR SWAA2026021168871Battery Pack · inoperativeAFT R2 DOOR EMERGENCY SIGN INOPERATIVE. R & R THE BATTERY PACK, AND TESTED GOOD IAW AMM 33-51-06-960-802.SDR DALA2026021101002Sensor · contaminatedR2 DOOR SLIDE INDICATION. FOUND SENSORS COVERED IN LUBE & HAVING A BUILDUP OF DEBRIS, REMOVED DEBRIS. BOTH SENSORS WITHIN PROXIMITY IAW AMM 25- 66, CYCLED DOOR ARM LEVER MULTIPLE TIMES ARMED LIGHT INDICATION OPERATES NORMALLY. (1440864)SDR AALA202602111939Warning Message · illuminatedAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED A DOOR LEFT OVER WING EXIT ECAM MESSAGE. (OPEN)