Service difficulty reports

1,771,154 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 IPXA2026091019366Stiffener · crackedMAJOR REPAIR, CWB FR40 -Y450 STIFFENER HAS A CRACK INSTALLED PARTS ON STIFFENER IAW SRM 57-10-21-201, PARAGRAPH 5.2.Q AND SRM 51-40-21-001.Jul 23, 2026 · N136UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026091019452Stiffener · crackedMAJOR REPAIR, CWB FR40 Y0 STIFFENER HAS A CRACK INSTALLED PARTS ON STIFFENER IAW SRM 57-10-21-201, PARAGRAPH 5.2.Q AND SRM 51-40-21-001.Jul 23, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR HNAA2026090100818Support · corrodedTOILET WASTE VALVE SUPPORT EXTERNAL STRUCTURE HAS CORROSION. REMOVED AND REPLACED WITH A NEW TOILET WASTE VALVE SUPPORT EXTERNAL STRUCTURE IAW SRM 51-40-02-PR.Jul 23, 2026 · N664MS · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026090100813Skin · corrodedFUSELAGE EXTERNAL SKIN AT FR 61, STRINGER 19L HAD CORROSION. REMOVED CORROSION BY BLENDING ON SKIN AT FR 61, STR 19L. FOUND TO BE WITHIN LIMITS. IAW SRM 53-21-01-AD, PG 121.Jul 23, 2026 · N664MS · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026083164633Skin · delaminatedLEFT OUTBOARD AFT FLAP HAS A 4 INCH DELAMINATION ON LOWER SURFACE(MARKED) RII - OK TO INSTALL LEFT OUTBOARD AFT FLAP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22. RII: VERIFIED REPLACEMENT AND INSTALLATION OF THE L/H O/B AFT FLAP PER AMM 27-51-22. RJul 23, 2026 · N8546V · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026083187376Skin · delaminatedRIGHT OUTBOARD AFT FLAP HAS A LARGE DELAMINATION ON UPPER SURFACE. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22.Jul 23, 2026 · N8546V · Boeing 7378H4 · Trailing Edge FlapsSDR VNAA202608310018Seat Track · corrodedCORROSION ON SEAT TRACKS, RBL 9, BS 485 - 581, BS 582 - 669, BS 708 - 847+16 - 977. DUE TO EXCESSIVE DAMAGE ON SEAT TRACKS (7 EAS) WERE REPLACED IAW SRM 53-31-49-101-001-A02, AND AMM 53-00-49-400-801 (CONFIG A12).Jul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608310017Seat Track · corrodedCORROSION ON SEAT TRACK LBL 27, BS 485 - 533. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACK WAS REPLACED IAW SRM 53-31-49-101-001-A02, & AMM 53-00-49-400-801 (CONFIG A04).Jul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608310016Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9 BTWN BS 485 - 581, 582 - 669, 708 - 847+16 - 977. THE SEAT TRACK EVALUATED WITH EXCESSIVE DAMAGE IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, & REPLACED IAW AMM 5Jul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608310015Seat Track · corrodedCORROSION ON LT SEAT TRACK, BS 744 - 762, BS 847 - 852, BS 853 - 913. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACKS WERE REPLACED IAW SRM 53-41-49-101-001-A02, & AMM 53-00-49-400-801, (CONFIG A12).Jul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608310014Seat Track · corrodedCORROSION ON RT SIDE SEAT TRACK BTWN BS 744 - 762, BS 847 - 852, BS 853 - 977. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACK (6 EA) MUST BE REPLACED.Jul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608310013Door Sill · corrodedCORROSION ON LOWER SILL BTW FS1000.00 AND FS1047.00 AT AFT BAGGAGE DOOR CUTOUT. CORROSION ON LOWER SILL BTW BS 1000 AND 1047 AT AFT CARGO DOOR CUTOUT WAS REMOVED IAW SRM 51-21-06-001-001-A01, & EVALUATED OUT OF LIMITS IAW SRM 53-61-23-201-001-A01, & REPLACEDJul 23, 2026 · N551NN · Cndair CL6002D24 · Fuselage Main, StructureSDR SIMA20260723002Shear Panel · corrodedSSI 53-23-005 AFT GALLEY, RH SHEAR PANEL BETWEEN FR 87/88 CORRODED. (LVL 2 CORR) REMOVED AND REPLACED AFT GALLEY RH SHEAR PANEL BETWEEN FR 87/88 IAW ERJ 170 SRM 51-40-08.Jul 23, 2026 · N769KW · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR SIMA20260723003Floor Support · corrodedSSI 53-23-005 AFT GALLEY LT FLOOR SUPPORT BETWEEN FR 87-88 CORRODED. (LVL 2 CORR). REMOVED AND REPLACED AFT GALLEY LH FLOOR SUPPORT BETWEEN FR 87/88 IAW SRM 51-40-08.Jul 23, 2026 · N769KW · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR SIMA20260723004Shear Panel · corrodedAFT GALLEY, CENTER SHEAR PANEL BETWEEN FR 87/88 CORRODED. (LVL 2 CORR). REMOVED AND REPLACED AFT GALLEY CENTER SHEAR PANEL BETWEEN FR 87/88 IAW SRM 51-40-08.Jul 23, 2026 · N769KW · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR SWAA2026082796842Skid Shoe · damaged#2 ENGINE INLET COWL LIP SKIN HAS 4 FASTENERS PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2026082758386Skin · damaged#2 ENGINE INLET COWL LIP SKIN HAS 2 FASTENERS PULLING AT 9 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2026082780829Skin · damaged#1 ENGINE INLET COWL LIP SKIN HAS 1 FASTENER PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01.Jul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Plate/SkinSDR SWAA2026082746627Mount Bracket · cracked#1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET IS CRACKED AT ATTACH POINT. REMOVED AND REPLACED #1 ENGINE HIGH STAGE REGULATOR MOUNT BRACKET PER AMM 70-20-02. INSPECTED WORK PERFORMEDJul 23, 2026 · N8546V · Boeing 7378H4 · Nacelle/Pylon, Main FrameSDR SWAA2026082591739Support Angle · corrodedCORROSION FOUND IN TWO FASTENER HOLES IN LT AFT CABIN FLOORBEAM, WL 208.1, BS 992.8, FROM LBL 37 - 43. R & R SUPPORT ANGLE IAW SRM 51-10-02, PARA 9.C.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026082533026Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL. REPLACEMENT ACCOMPLISHED IAW SRM 53-00-50-2R-0.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082595278Floorbeam · corrodedCORROSION FOUND ON RT AFT CABIN FLOORBEAM ANGLE AT WL 208.1, BS 992.8, RBL 41. R & R THE FLOORBEAM ANGLE AT BS 992.8 RBL 37 - 43 IAW SRM 51-10-02, PARA 9.C.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026082555230Floor Panel · pulledFWD FLOOR PANEL 221EF 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, DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082594553Floorbeam · corrodedCORROSION FOUND IN ONE FASTENER HOLE IN THE AFT CABIN FLOORBEAM, WL 208.1, BS 986.5, LBL 43. THE FLOORBEAM FASTENER HOLE WAS REPAIRED IAW SRM 53-70-51-2R-6.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026082594600Floorbeam · corrodedCORROSION FOUND ON RT AFT FLOORBEAM AT WL 208.1, BS 947, RBL 52. PERFORMED A REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-5, REPAIR 5.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026082574640Intercostal · crackedFWD CARGO BAY INTERCOSTAL ANGLE CRACKED AT STR 25R, FWD SIDE OF BS 500G WL 156. R & R THE INTERCOSTAL ANGLE IAW SRM 51-40-02, & DWG 143A7505, REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082596920Intercostal · crackedFWD CARGO BAY INTERCOSTAL ANGLE CRACKED AT STR 25L, FWD SIDE OF BS 500H. R & R THE INTERCOSTAL ANGLE, FWD SIDE OF FS500H LBL25 WL156 IAW SRM 51-40-02 DWG: 143A7505 ID:0137 REV: - VERIFIED ITEM 1Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082534542Floor Panel · pulledFLOOR PANEL 231EF, 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, DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082561590Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED THE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9, & AIPC 53-21-00-42A, ITEM 165.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082547147Floor Panel · pulledFLOOR PANEL 231DF, 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, DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082546027Sidewall Support · corrodedCORROSION FOUND ALONG RT SIDE OF FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT, WL 156, BS 500A+7 - 500D+2. R & R THE SIDEWALL SUPPORT BTWN BS 500A TO BS 500I IAW SRM 51-40-02, & DWG 143A7500 REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082525793Floor Panel · pulledFLOOR PANEL 231FF 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. DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082593458Floor Panel · pulledFLOOR PANEL 242CF 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. DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082534550Shield · corrodedCORROSION FOUND ALONG RT FWD CARGO BAY, AFT SHIELD AT WL 156, BS 500+2 - 500+14. R & R THE SHIELD BTWN BS 492 - 500A, RBL 25, WL 156 IAW SRM 51-40-02, & DWG 143A0080 REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082514695Intercostal · crackedFWD CARGO BAY INTERCOSTAL ANGLE CRACKED AT STR 25R AFT SIDE OF BS 440 WL 156. R & R THE INTERCOASTAL ANGLE IAW SRM 51-40-02 & DWG 143A7505, REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082573350Floor Panel · pulledFWD FLOOR PANEL 221GF 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. DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082555707Intercostal · crackedFWD CARGO BAY INTERCOASTAL ANGLE CRACKED AT STR 25R FWD SIDE OF BS 500F. R & R THE INTERCOSTAL ANGLE IAW SRM 51-40-02, & DWG 143A7505, REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082574525Attach Angle · crackedCRACKED COMPOSITE BULKHEAD ATTACH ANGLE AT BS 663, RBL 35, WL 166. R & R THE UPPER ATTACH ANGLE BS 663, RBL 6 - 63, WL 166 IAW SRM 51-40-02, & DWG 111A1000 REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026082513775Support · corrodedCORROSION FOUND ALONG FWD CARGO BAY, END WALL SUPPORT AT WL 156, RBL 25, BS 500I. R & R THE RT BULKHEAD SUPPORT ANGLE IAW SRM 51-40-02, & DWG 143A9481, REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082513307Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAD AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL, REPLACEMENT ACCOMPLISHED IAW SRM 53-00-50-2R-0.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082514145Floor Support · corrodedCORROSION FOUND ON LT FLOOR SUPPORT, BS 947+2, LBL 52, WL 208. R & R FLOOR SUPPORT BTWN BS 947 - 967, LBL 52, WL 208 IAW SRM 51-40-02, & DWG 147A5650, REV A.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082573053Intercostal · crackedFCB INTERCOSTAL WEB CRACKED IN TWO PLACES AT STR 25L, BTWN BS 500 - 500A, WL 156. R & R THE INTERCOSTAL WEB IAW SRM 51-40-02, & DWG 143A7505 REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082556444Floor Panel · pulledFLOOR PANEL 231GF 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, DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082591911Floor Panel · pulledFWD FLOOR PANEL 231AF 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, DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082593043Web · corrodedCORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 796 - 842, RBL18 -28, WL 160. R & R THE SUB-THRESHOLD WEB IAW SRM 51-40-02-OG-0, AND DWG 146A8120, REV A.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082532311Sidewall Support · corrodedCORROSION FOUND ALONG LT SIDE OF FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT, WL 156, BS 500D+9 - 520. R & R THE FLOOR TO SIDEWALL SUPPORT, BS 396 - 500I & SPLICES, LBL 23, WL 153 IAW SRM 51-40-02, DWG 143A7501, REV -, SRM 53-00-53-2R-6, REPAIR 6, & TASK M-22-Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082532496Support · corrodedCORROSION FOUND ALONG FWD CARGO BAY END WALL SUPPORT AT WL 156, RBL 18 - 19, BS 500I. REMOVED AND REPLACED BULKHEAD SUPPORT AT WL 156 RBL 18 -19, BS 500I IAW SRM 51-40-02 AND DWG 143A9481 REV -.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026082589829Floor Panel · pulledFLOOR PANEL 242HF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242HF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9,.A.1. DUE TO AMOUNT OF DAMAGE.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082553413Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED AFT FLOOR PANEL 242UF IAW SRM 51-10-02-0G-0, PARA 9, & AIPC 53-21-51-46, ITEM 250.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026082512308Floor Panel · pulledFWD FLOOR PANEL 222DF 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.Jul 23, 2026 · N8644C · Boeing 7378H4 · Fuselage Floor Panel