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.

SDR AALA202606248842Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S43L. REPAIRED STRINGER IAW EA 375970.Apr 24, 2026 · N9010R · Airbus A319115 · Fuselage Main, Longeron/StringerSDR AALA202606242330Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S42L. REPAIRED STRINGER PER EA 375970.Apr 24, 2026 · N9010R · Airbus A319115 · Fuselage Main, Longeron/StringerSDR IPXA2026061768095Door Frame · dented(MAIN CARGO DOOR FRAME INSTALLATION (STA 600+12.9 & 600+17.25) DAMAGE - TEMPORARY REPAIR) [T3F18E008QANF]Apr 24, 2026 · N413UP · Boeing 75724APF · Fuselage Main, StructureSDR AALA202606164739Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 66 AND S11R AT THE #7 DOOR STOP AREA. REPAIRED FRAME PER SRM 53-41-12-300-011.Apr 24, 2026 · N9010R · Airbus A319115 · Fuselage Main, FrameSDR CALA2026061116997Bracket · crackedONE POWER FEEDER CABLE ATTACH BRACKET IS CRACKED IN MAIN CABIN AT STA 867, BETWEEN S2R AND S3R. REMOVED AND REPLACED ATTACH BRACKET AT STA 867 S2R-S3R IAW BOEING DWG 146A7901 REV- AND B737 SRM 51-40-02.Apr 24, 2026 · N45440 · Boeing 737924ER · Fuselage Main, Attach FittingsSDR VNAA202606060014Acoustic Liner · crackedAFTER Z STIFFENER REMOVAL ON LOWER RH TRANSCOWL CRACK WAS FOUND ON ACOUSTIC PANEL. LOWER RH TRANSCOWL ON ACOUSTIC PANEL WAS REPAIRED PER REO NUMBER 690-54-21-635 REV - -Apr 24, 2026 · N606NN · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR VNAA202606060013Bracket · corrodedCORROSION ON BRACKET MACHINED (10 EAS) BTW FS=517.00 TO FS=661.00+16 AT FWD/CENTER BAGGAGE BAY. PAINT ON BRACKET MACHINED BTW FS=517.00 TO FS=661.00+16 AT FWD/CENTER BAGGAGE BAY WAS REMOVED PER SRM 51-26-01-001-001-A01, GVI WAS PERFORMED PER NDTM TASK 51-20Apr 24, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202606060012Seat Track · corrodedCORROSION AND WEAR ON SEAT RAIL BTW FS349 TO FS 669 3EA LBL 27, 2EA LBL9, 4EA RBL9 AT FLOOR PASSENGER CABIN. WERE EVALUATED,DUE EXCESIVE DAMAGE ON SEAT RAIL BTW FS349 TO FS 669 3EA LBL 27, 2EA LBL 9, 4EA RBL 9 AT FLOOR PASSENGER CABIN PER CRJ-900 SRM 53-21-49Apr 24, 2026 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606060009Channel · crackedCRACK AT INNER STRAP ,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL. CRACK AT INNER STRAP ,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL WAS REPLACED PER CRJ-900 NIEO 34 REV. 2009-01.Apr 24, 2026 · N606NN · Cndair CL6002D24 · Aerodynamic FairingsSDR AALA202606031913Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 59 AND +Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606038539Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 47 AND FR 64 AT -Y1292. REPAIRED SEAT TRACK PER SRM 53-41-15-300-003Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606034071Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 24 AND -Y1292. REPAIRED SEAT TRACK PER SRM 53-21-15-300-009.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606035196Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R AT THE #1 DOORSTOP FITTING. REPAIRED FRAME PER SRM 53-41-12-300-011.Apr 24, 2026 · N9010R · Airbus A319115 · Fuselage Main, StructureSDR AALA202606039743Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 34 AND +Y765. REPAIRED SEAT TRACK PER SRM 53-21-15-300-009.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606032966Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK AT FR 29 AND +Y1292. REPAIRED SEAT TRACK PER 53-21-15-300-009.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026060200451Door Sill · corrodedF122826 CORROSION ON CARGO DOOR CUT-OUT FLOOR SILL. REMOVED AND REPLACE CARGO DOOR CUT OUT FLOOR SILL IAW EMB 145 SRM 51-40-02.Apr 24, 2026 · N902BC · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026060200450Frame · corrodedF122812 CORROSION IN CARGO COMPARTMENT ON FRAME 61 WEBBING AT STRINGER 16R. REMOVED AND REPLACED WEBBING PANEL AT FRAME 61 (BANANA PANEL) IAW EMB 145 SRM 51-40-02Apr 24, 2026 · N902BC · Emb EMB145LR · Fuselage Main, FrameSDR HNAA2026060200449Floor Support · corrodedCORROSION IN CARGO COMPARTMENT ON LH FWD FLOOR SILL. REMOVED AND REPLACED LH FWD CARGO COMPARTMENT FLOOR SILL IAW SRM 51-40-02.Apr 24, 2026 · N902BC · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026060192697Support Web · crackedCRACK SUPPORT WEB LOCATED INBOARD FAN COWL ON ENGINE 1. REPLACED SUPPORT WEB LOCATED INBD FAN COWL ON ENGINE 1 IAW SRM 51-10-020-G-0 STEP 9; SRM 51-40-02-0G-0 AND CMM 71-13-30 FIG 3 SHEET 10092.Apr 24, 2026 · N8635F · Boeing 7378H4 · Nacelle/Pylon Miscellaneous StructureSDR REXA2026060100894Fitting · crackedLEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06.Apr 24, 2026 · N691CA · Cndair CL6002D24 · Emergency ExitsSDR REXA2026052900893Web · crackedCRACK FLOOR WEB LEFT SIDE WL=79.5 AND FS193.00 (NEAR TO BRAKE ACCUMULATOR INDICATION SUPPORT) ON FWD EQUIPMENT COMPARTMENT. FLOOR WEB LEFT SIDE WL=79.5 AND FS193.00 (NEAR TO BRAKE ACCUMULATOR INDICATION SUPPORT) ON FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900891Angle · corrodedAFTER REMOVAL MID CAP ANGLE, WAS FOUND CORRSION ON KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER SRM SRM 53-21-23-101-001-A02 AND WAS REPLACEDApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900887Angle · corrodedCORROSION ON MID CAP ANGLE ON LOWER SIDE OF PASSENGER SURROUND STRUCTURE. CORROSION ON MID CAP ANGLE ON LOWER SIDE OF PASSENGER SURROUND STRUCTURE. WAS EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WAS REPLACED PER SRM 51-41-02-001-001-A01Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900886Floorbeam · corrodedCORROSION ON FLOORBEAM FS333 BTW LBL9 AND LBL27 AT PASSENGER FLOOR STRUCTURE. CORROSION ON FLOOR BEAM FS333 BTW LBL9 AND LBL27 AT PASSENGER FLOOR STRUCTURE WAS REPAIRED PER EA NO: CRJ953-22088 REV IRApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026052900885Support · corrodedCORROSION ON RT/LT MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL AREA CORROSION ON RT MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (2 EAS) RBL 45 ON WHEEL WELL AREApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900884Support Plate · corrodedCORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL AREA CORROSION ON RHMLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (2 EAS) RBL 45 ON WHEEL WELL AREAApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900883Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACEApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900882Support Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LT/RT MAIN WHEEL WELL CORROSION ON CONNECTORS SUPPORT PLATES (PX33, PX17, PX34, PX19) AT LH/RH MAIN WHEEL WELL WERE EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WERE REPLACED PER SApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900881Web · crackedCRACK ON RT MLG BINS SUPPORT STRUCTURE RETAINER ANGLE BS 797.00 AND RBL 34 AT RH WHEEL WELL AREA RT MLG BINS SUPPORT STRUCTURE RETAINER ANGLE BS 797 AND RBL 34 AT RH WHEEL WELL AREA WAS REPLACED PER SRM 51-41-02-001-001-A01 AND SRM 51-42-10-001-001-A01.Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900880Bracket · corrodedCORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 AND STGR 23R TO 24R AT AFT WASTE SERVICE PANEL CORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 AND STGR 23R TO 24R AT AFT WASTE SERVICE PANEL WAS REMOVED AND EVALUApr 24, 2026 · N933XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052900877Support Angle · crackedCRACKED SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE. SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01.Apr 24, 2026 · N933XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026052900874Angle · crackedCRACK ON LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD - AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPApr 24, 2026 · N933XJ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR CALA2026052916614Stub Beam · gougedR2 DOOR UPPER STUB BEAM HAS LIGHT SCRATCHES. REMOVED DAMAGE, ORIGINAL THICKNESS .060, REMOVED .026, REMAINING IS .034, FOUND OUT OF LIMITS IAW SRM 52-10-02-1A-4 DETAIL E. REMOVED AND REPLACED STUB BEAM IAW DWG 147A6149 REV E AND 147A6502 REV F.Apr 24, 2026 · N37255 · Boeing 737824 · Service DoorsSDR SWAA2026052792720Floor Support · crackedCRACK ON INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 46 REV A.Apr 24, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026052792721Web · crackedCRACKED WEB LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9 AND DWG 141A5410 SHEET 126 REV-.Apr 24, 2026 · N8645A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202605269202Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN SEAT TRACK AT FR 44 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202605225013Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR SEAT TRACK AT FR 45 PLUS 13 INCHES, AND AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202605228873Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK BETWEEN FR 36 AND FR 42 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.Apr 24, 2026 · N9011P · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202605217353Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER 21R BETWEEN STA 950 AND STA 967. REPAIRED STRINGER PER SRM 53-70-15.Apr 24, 2026 · N954NN · Boeing 737823 · Fuselage Main, Longeron/StringerSDR SWAA2026052092608Support · corrodedCORROSION SUPPORT ZEE BETWEEN BS 727 TO 767, RBL 21, WL 156. REPLACED SUPPORT ZEE IAW SRM 51-40-02, AND DWG 146A7500, SHEET 85, REV A.Apr 24, 2026 · N250WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052092609Intercostal · crackedCRACKED INTERCOSTAL, BTW BS 500D - 520, S28R IN THE FWD CARGO BAY. REPLACED INTERCOSTAL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.Apr 24, 2026 · N250WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052092610Support · corrodedCORRODED SUPPORT ZEE BTWN BS 727 - 847, LBL 21, WL 156. REPLACED SUPPORT ZEE AND CLIP SECTION IAW SRM 51-40-02-0G, DWG 146A7500, SHEET 86, REV A, & DWG 146A7502 SHEET 27 REV-. EVALUATED REEWORK AREAS LOC ON SUPPORT ZEE, AND FOUND WITHIN LIMITS IAW SRM 53-Apr 24, 2026 · N250WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052092611Stringer · crackedCRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED REPAIR STRINGER 23L LOCATED BETWEEN BS 500D MORE 10 INCHES TO BS 540 AT FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1. REPAIR 1, AND DRAWING 143A3210, SHEET 74, REV B.Apr 24, 2026 · N250WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026051992753Skin · crackedCRACKED RH LOWER HORIZONTAL STAB SKIN. AT STAB STA 193.90; 18' FROM FWD EDGE; .6' IN LENGTH. REMOVED THE DAMAGED PART ON RH HORIZONTAL STAB LOWER SKIN HSS 193.90 18' FROM FWD EDGE; CUT OUT DIMENSIONS 1.7' X 1.0' AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-Apr 24, 2026 · N258WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026051992505Support Angle · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT BS 500A+14.5, WL 156, RBL 25. REMOVED AND REPLACED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE RT SIDE IAW SRM 51-40-02-0G-0, AND DWG 143A7500 0058, REV -.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992501Support · corrodedCORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT BS 400+3, 400+7, 440+14, 440+18, 500+5, AND 500A+18, LBL 25, WL 156. REMOVED AND REPLACED FCB L/H SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A7500 0058, REV -.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992757Support · corrodedACB LT FLOOR TO SIDEWALL SUPPORT, BS 727 - 847 HAS AREAS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT BS 727 TO 847, LBL 24, WL 158 IAW SRM 51-40-02-0G-0 AND DWG 146A7502, REV -.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992502Threshold Web · corrodedCORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT SUB-THRESHOLD WEB FROM BS 440+8 TO 480+7, RBL 27 - RBL 29, WL 155. REMOEVED AND REPLACED FWD CARGO DOOR CUT-OUT SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A8330 0006, REV B.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992755Sidewall Support · corrodedACB FLOOR TO SIDEWALL SUPPORT R/H BS 727-767 HAS AREAS OF CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT BS 727 TO 767, RBL 24, WL 158 IAW SRM 51-40-02-0G-0 AND DWG 146A7502, REV -. REJECTION OF STEP 6 ITEM 3: FLOOR TO SIDEWALL SUPPORT AT RBL 24 HAS 1EA BAApr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051992503Shield · corrodedCORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM BS 420 TO 440, RBL 24, WL 156. REMOVED AND REPLACED ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD BS420 TO BS440 RBL24 IAW SRM 51-40-02 AND DWG 143A0080 0010, REV A.Apr 24, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous Structure