Service difficulty reports

1,770,704 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.

SDR SWAA2026101970924Support Plate · corrodedCORROSION ON THE AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAD MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED THE RT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, AND DWG 146A7500, REV-.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101993008Support Plate · corrodedCORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0, AND DWG 146A7500, REV-.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101975908Floor Support · corrodedCORROSION FOUND ON FWD WET AREA FLOOR STRUCTURE AT BS 328+11 LBL 45 WL 208. REMOVED AND INSTALLED REPLACEMENT INTERCOSTAL AT BS 328-BS 344 LBL 45 IAW SRM 51-40-02-0G-0 AND DWG 141A5730 REV:A.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101975411Floorbeam · corrodedCORROSION FOUND ON FWD WET AREA FLOORBEAMS AT BS 344, RBL 9, & BS 344, RBL 17, WL 208. CORROSION EVALUATED AND REMOVED FLOORBEAM UPPER FLANGE RBL9 WL208 AND RBL17 1"X1" AREA ORIGINAL MATERIAL THICKNESS IS 0.175" LOWEST MATERIAL THICKNESS IS 0.170" CORROSIONSep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026101921248Baffle Angle · crackedFWD CARGO BAY BAFFLE ANGLES WERE CRACKED, AFT SIDE OF FRAMES BS 500G & BS 500H, RBL 25, WL 156. REMOVED AND REPLACED THE FWD CARGO BAFFLE ANGLES IAW SRM 51-40-02-0G-0, & DWG 145A7505, REV B .Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101920953Attach Bracket · crackedAFT ENTRY DOOR PANEL 834DZ AFT ATTACH BRACKET WAS CRACKED. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02-0G-0, & AIPC 52-13-21-10.Sep 9, 2026 · N8657B · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026101992331Floor Support · corrodedCORROSION FOUND ON AFT WET AREA FLOOR SUPPORT, BS 947+1, RBL 52, WL 208. LOCATED AND DRILLED A NEW FLOOR SUPPORT BS 947 - 967, RBL 52 WL 208 IAW SRM 51-40-05-0G-0, & DWG 147A5650, REV A INSTALLED ON CCN TTG8Q01E78KV, STEP 8.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101984460Baffle Angle · crackedFWD CARGO BAY BAFFLE ANGLES WERE CRACKED, FWD SIDE OF FRAMES BS 500G AND BS 500H, RBL 25, WL 156. REMOVED AND REPLACED FWD CARGO BAY BAFFLE ANGLES IAW SRM 51-40-02-0G-0, AND DWG 145A7505, REV B .Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101916199Floor Panel · debondedFLOOR PANEL 231JF UPPER SKIN HAS A LARGE DEBOND NEAR THE FWD EDGE. REPLACED THE FLOOR PANEL 231JF IAW SRM 51-10-02-0G-0, PARA 9, AND AIPC 53-21-51-58B, ITEM 205.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101970639Floor Panel · debondedFLOOR PANEL 232HF UPPER SKIN HAD A LARGE DISBONDED AREA NEAR FWD EDGE. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101934106Shield · corrodedCORROSION ON THE AFT CARGO BAY SHIELD, FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES, BS 767+3 - 794, RBL 22, WL 156. THE SHIELD WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A0081, REV A.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101993415Shield · corrodedCORROSION ON THE FWD CARGO BAY AFT SHIELD, BS 500+1 - 500+19, RBL 22, WL 156 HAD MULTIPLE AREAS AROUND NUT PLATE HOLES. THE FWD CARGO AFT SHIELD WAS REMOVED AND REPLACED BS 494 - 500A, RBL 22, WL 156 IAW SRM 51-40-02-0G-0, AND DWG 143A0080, REV-.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101988789Floorbeam · corrodedCORROSION FOUND ON AFT WET AREA FLOORBEAM AT BS 987, RBL 42, WL 208. REPAIRED THE UPPER TEE ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026101971602Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101909350Floor Panel · pulledFLOOR PANEL 232EF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101693391Nut Plate · corrodedCORROSION RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 449 LT WING. REPLACED THE RAIL NUT PLATES IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.Sep 9, 2026 · N8656B · Boeing 7378H4 · Wing, Attach FittingsSDR REXA2026101601940Intercostal · corrodedCORRODED INTERCOSTAL, BTWN BS 310 - 319, STR 20R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-00-00-101-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601912Bracket · corrodedCORRODED BRACKETS (6EA) IN THE FWD CARGO BAY, PAINT ON BRACKETS (5EAS) WERE REMOVED & NO DAMAGE FOUND IAW SRM 51-26-01-001-001-A01, DUE TO EXCESSIVE DAMAGE ON BRACKET WAS REPLACED IAW SRM 51-10-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-00Sep 9, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR HNAA2026101601005Floor Support · cracked53-2175 LH OMEGA BEAM CRACKED AT FR24. REPAIRED IAW ETD 2026-145-015894Sep 9, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101600996Shear Tie · cracked53-2166 SHEAR CLIP CRACKED AT FR28 BTW STR21R-21L. RAR SHEAR CLIP IAW SRM 51-40-02Sep 9, 2026 · N650AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026101500984Frame · crackedFR 59 CRACKED BTW STR 15-16L. REPAIRED IAW ETD2026-145-015641Sep 9, 2026 · N650AE · Emb EMB145LR · Fuselage Main, FrameSDR SWAA2026101422704Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380 - 400, RBL 41. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 184, REV -.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101433688Floor Support · crackedCRACK FLOOR SUPPORT, BS 380 - 400, RBL 10. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 139, REV-.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101493681Floor Support · crackedCRACKED FLOOR SUPORT, BS 500I - 520, BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 115, REV A.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101433588Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380 - 400, LBL 50. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHEET 183, REV -.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101411223Access Panel · crackedCRACKED BLADE ACCESS PANEL 333 OF LT HORIZONTAL STAB. REPLACED THE BLADE ON ACCESS PANEL 333 IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9.Sep 9, 2026 · N8656B · Boeing 7378H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026101433592Frame · crackedCRACKED FRAME, BS 312, STR 5L - 6L. REPAIRED THE FRAME IAW EA M-22-153-01244.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2026101453540Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380 - 400 BL 0. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 201, REV -Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101486080Channel · corrodedCORRODED RAIL NUT PLATES INTERNAL CAVITY LT WING L/E OFSS 580 +12 INCHES, REMOVED AND REPLACED GANG CHANNEL IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02.Sep 9, 2026 · N8656B · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026101488795Floor Support · crackedCRACKED FLOOR SUPPORT BTWN BS 380 - 400, LBL 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHT 140, REV -.Sep 9, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101466562Rail · crackedCRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 491 LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 491 LT WING IAW SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0 DWG:112A4402 SHEET: 40 REV: A.Sep 9, 2026 · N8656B · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026101424077Access Panel · damagedELONGATED HOLES ON LEADING EDGE SKIN ACCESS PANEL 341B LOCATED UPPER AREA LE STA 69.93 AT RT HORIZONTAL STABILIZER 2026-558811. PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN ACCESS PANEL 341B LOCATED UPPER AREA LE STA 69.93 AT RT HORIZONTAL STABILIZER I.A.Sep 9, 2026 · N8656B · Boeing 7378H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026101395444Mount · corrodedAFT PASSENGER COMPARTMENT: FOUND CORROSION UNDER LAV MOUNT AT STA 947 LBL 52 BLENDING ACCOMPLISHED ON EA 26-153-02451-WIP1 (TTG8Q01E7B8L) STEP 5. REMOVED .033" OF MATERIAL. REMAINING THICKNESS IS .147". DAMAGE LOCATION AT A HARD MOUNT AND REMOVAL IS OUT OF LIMSep 9, 2026 · N8711Q · Boeing 7378 · Fuselage, Equipment Attach FittingsSDR SWAA2026101329574Angle · corrodedAFT SERVICE DOOR THRESHOLD CORRODED ON Z ANGLE AT BS 957. BLENDED CORROSION, ORIGINAL MATERIAL THICKNESS IS 0.080 MATERIAL LOSS IS 0.013 MAX ALLOWED IS 0.008 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. WILL BE REPLACED ON TASK CARD TTG8Q01E72SG.Sep 9, 2026 · N8711Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026101314302Angle · corrodedAFT SERVICE DOOR THRESHOLD: CORROSION FOUND ON Z ANGLE AT BS 984 - 995. BLENDED CORROSION ON AFT SERVICE DOOR Z ANGLE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED FASTENERS IN ANGLE IAW SRM 51-40-02. WILL BE REPLACED ON TASK CARD TTG8Q01E72SSep 9, 2026 · N8711Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026101371705Angle · corrodedAFT SERVICE DOOR THRESHOLD: CORROSION FOUND ON Z ANGLE AT BS 950. BLENDED CORROSION ORIGINAL MATERIAL THICKNESS IS 0.080 MATERIAL LOSS IS 0.013 MAX ALLOWED IS 0.008 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. WITH MULTIPLE SPOTS OF CORROSION OUT OF LIMITSep 9, 2026 · N8711Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026101389752Angle · corrodedAFT SERVICE DOOR THRESHOLD CORRODED, FOUND ON Z ANGLE IN MULTIPLE AREAS FROM BS 967-986.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-7-15-1A-1. REMOVED THE ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-40-02 AND DWG 147A8501. COUNTERSUNK ALL FASTENER HOSep 9, 2026 · N8711Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026101304403Cam Roller · frozenAFT SERVICE DOOR HANDLE CAM ROLLER IS FROZEN. BENCH CHECK OF BEARING IS GOOD PER SOPM 20-50-03.Sep 9, 2026 · N8711Q · Boeing 7378 · Service DoorsSDR SWAA2026101312388Mount · corrodedAFT PASSENGER CABIN, FOUND CORROSION UNDER LAV MOUNT AT BS 947, RBL 52, BLENDING ACCOMPLISHED ON EA 26-153-02451-WIP1, STEP 5. REMOVED .033" OF MATERIAL. REMAINING THICKNESS IS .147". DAMAGE LOCATION AT A HARD MOUNT AND REMOVAL IS OUT OF LIMITS IAW SRM 53-70Sep 9, 2026 · N8711Q · Boeing 7378 · Fuselage, Equipment Attach FittingsSDR HNAA2026100900975Floor Support · crackedLT OMEGA BEAM CRACKED AT FR 23. REPAIRED IAW ETD 2026-145-015902 AND EO 1-53-26-0485Sep 9, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026100872963Floorbeam · corrodedCORROSION FOUND ON AFT WET AREA FLOORBEAM, BS 947, RBL 52, WL 208. REMOVED DAMAGED UPPER FLANGE ON THE FLOORBEAM FROM RBL 30 - RBL 58, WL 208 AND REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5, ALTERNATIVE 2.Sep 9, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR IPXA2026100251661Crossbeam · corrodedAFT CARGO COMPT. FRAME 54, Y953 - Y1959. CEILING SUPPORT WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR54 CROSSBEAM Y953 TO Y1959. IAW A300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-73-11.Sep 9, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100252048Crossbeam · corrodedAFT CARGO BAY CEILING SUPPORT AT FR 56 - 57.2, BTWN Y 450 - Y953 WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR 56 TO FR 57.2 BETWEEN Y450 TO Y953 IAW A300 SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW A300 SRM 51-73-11.Sep 9, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100252060Crossbeam · corrodedAFT CARGO BAY, FR 57, Y0 - Y953, CEILING SUPPORT WAS CORRODED. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR57, Y0 TO Y953. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS IS .002 REMAINING MATERIAL IS .061 T98828.FOUND TO BE NEGLIGIBLSep 9, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100653507Crossbeam · corrodedAFT CARGO BAY AT FR 62 BTWN Y 0 - Y 1959, CEILING SUPPORT HAS CORROSION. VERIFIED REMOVAL OF CORROSION FROM CEILING AT SUPPORT PANEL FR62, Y0 TO Y1959. IAW SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW SRM 51-73-11.Sep 9, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR HNAA2026100800958Channel · corrodedU CHANNEL FOR SERVICE DOOR, CORRODED BTWN FR 20-22. R & R THE CHANNEL IAW SRM 51-40-02.Sep 9, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026100741321Skin · crackedCRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 3, NOSE SKIN AT THE ACTUATOR AROUND FASTENERS LT WING. REPAIRED LOWER SURFACE OF LEADING-EDGE SLAT 3 NOSE SKIN IAW SRM 57-42-01-2R-8.Sep 9, 2026 · N208WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026100509361Skin · crackedPOSSIBLE CRACK AT BS 780, STR 1. C\W 26-153-02475. REPAIRED THE FUSELAGE SKIN, BTW BS 767 & 787, BELOW S-1.Sep 9, 2026 · N7844A · Boeing 737752 · Fuselage Main, Plate/SkinSDR AALA202610057404Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON 2EA T-ANGLES ON FWD KEEL BEAM LATERAL WEB AT STA 867 LBL-6 AND RBL-6. ACCOMPLISHED PERMANENT REPAIR AT 2EA T-ANGLES ON FWD KEEL BEAM LATERAL WEB AT STA 867 LBL-6 AND RBL-6 IAW EA 379425.Sep 9, 2026 · N832AA · Boeing 7879 · Fuselage Miscellaneous StructureSDR AALA202610057767Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SURFACE OF FWD KEEL BEAM LATERAL WEB BETWEEN STA 866 AND 871 LBL-10 TO RBL-10. ACCOMPLISHED PERMANENT REPAIR AT FWD KEEL BEAM WEB IAW EA 379425.Sep 9, 2026 · N832AA · Boeing 7879 · Fuselage Miscellaneous Structure