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 REXA2026050500461Retainer · crackedCRACK AND WEAR ON RETEINER SEAL AT FWD/CTR BAGGAGE BAY DOORS COMPARTMENT (LOWER SIDE) NEW RETEINER SEAL AT FWD/CTR BAGGAGE BAY DOORS COMPARTMENT (LOWER SIDE) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-A01, LEAK TEST AT FORWARD AND CENTER DOOR WAS PERFORMED PERMar 10, 2026 · N279PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR U2RA202605000011Fastener · brokenLOCK FASTENER HEAD BROKEN AT TENSION TIE ATTACH FRAME LOCATED AT BS 1220 RT AND STRINGER 10RMar 10, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous StructureSDR REXA2026050400421Stringer · corrodedCORROSION ON STRINGER 18R AND STRINGER 19R BTW STA=453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW STA= 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPHMar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026050400419Stringer · corrodedCORROSION ON STRINGER 19R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400418Stringer · corrodedCORROSION ON STRINGER 18R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR BAGA2026043000009Doubler · corrodedHVY CHECK SUBMISSION - CORROSION FOUND ON WASTE DOUBLER CUTOUT AT REAR BARREL FRAME 75-76. REPAIRED IAW AIRBUS REO.Mar 10, 2026 · N227BZ · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR 2026FA0000302Coil · arcedENGINE CYLINDER NR 4 WAS EXPERIENCING INTERMITTENT MISFIRING. FOUND L/H COIL WAS GROUNDING TO ITS MOUNT THROUGH A SMALL PINHOLE IN BOTTOM OF THE COIL CASE.THE COIL WAS RETURNED TO ELECTROAIR FOR EVALUATION. ELECTROAIR STATED THAT IT WAS TESTED AND "THERE WAS NMar 10, 2026 · N9140X · Mooney M20J · Low Tension CoilSDR SWIA2026031075903Skin · damagedSIGNS OF LIGHTENING DAMAGE BETWEEN RIVET AND SKIN FWD OF BS 453 ABOVE STR 2L. REPAIRED DAMAGE ON EXTERIOR FUSELAGE SKIN BS 453, STR 2L IAW REO 690-53-21-2117, REV - (P1), AND SRM 51-42-06, 53-00-00, 51-12-00, 51-25-01, AMM 21-31-00. NDT PERFORMED.Mar 10, 2026 · N816SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SIMA20260310011Shear Tie · corrodedSHEAR CLIP ON FRAME 86 BETWEEN STRINGERS 28R AND 27R IS CORRODED (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP (SHEAR CLIP PN 170-66033-001, P.O.# 349163) AT FR 86 BETWEEN STR 27R - 28R REF EMB 175 SRM 51-40-08. (MS14218AD5-5 PO# 321413, MS2047AD5-5 PO3Mar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SIMA20260310010Seat Track · corrodedRH FLOOR BEAM CORRODED @ Y+276 AFT OF FRAME FR90 (LEVEL 2 CORROSION) REMOVED AND REPLACED INTERCOSTAL (RH FLOOR BEAM) PART# 170-61041-402 PO# 349163 AND ANGLE SUPPORT PART# 170-60287- 002 PO# 349163) IAW E-175 SRM 51-40-08. SEE WIPS AND TASK FOR ALL WORK ACCMar 10, 2026 · N261NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026042100323Shear Tie · crackedF111743 CARGO SHEAR CLIP CRACKED AT FR 67 BTWN STGRS 6L-7L. REMOVED AND REPLACED CARGO SHEAR CLIP AT FR 67 BTWN STGRS 6L-7L IAW EMB 145 SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026042100322Door Sill · corrodedCARGO DOOR CUTOUT LWR SILL CORRODED IN NUMEROUS AREAS. RAR CARGO DOOR CUTOUT LWR SILL IAW EMB 145 SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026042100315Floor Support · corrodedLH CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 70-72. R & R LT CARGO FLOOR SILL BTWEEN FR 70-72 IAW EMB 145 SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026042100314Door Sill · corrodedF111689 CARGO DOOR CUTOUT LWR SILL CORRODED IN NUMEROUS AREAS. RAR CARGO DOOR CUTOUT LWR SILL IAW EMB 145 SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026042100292Floor Support · corrodedRIGHT CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 71-73. RAR R/H CARGO FLOOR SILL #4 IAW SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026042100291Floor Support · corrodedRIGHT CARGO FLOOR SILL CORRODED IN NUMEROUS AREAS BTWN FR 65-68. RAR RH CARGO FLOOR SILL BTWN FR 65-68 IAW EMB 145 SRM 51-40-02.Mar 10, 2026 · N905JH · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026042078330Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078333Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV-.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078328Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7505, SHEET 138, REV -.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078329Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042091107Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078331Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042091108Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE CLIP AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV-.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078334Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 143A7505, SHEET 138, REV- .Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078567Angle · crackedCRACKED ANGLE, BS 440, STR 26L. REPLACED THE ANGLE IAW SRM 51-40-02; 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078327Angle · crackedCRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 256, REV B.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078568Support · corrodedCORRODED LOWER SILL LOCATED BTW BS 440 TO BS 492. 4 RBL 29 WL 208.1. REPLACED LOWER SILL LOCATED BTW BS 440 TO BS 492. 4 RBL 29 WL 208.1 IAW SRM 51-10-02 ITEM 9; AND DWG 143A8330; SHEET 61; REV -.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078339Web · crackedCRACKED FLOOR WEB BTW BS 270 TO BS 294.5 AT BL 0. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02 AND DWG 141A5400, SHEET 20, REV-.Mar 10, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042091109Web · crackedCRACKED FLOOR WEB BTW BS 270 TO BS 294.5 AT BL 0. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02 AND DWG 141A5400, SHEET 20, REV-.Mar 10, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078340Web · crackedCRACKED FLOOR WEB BTW BS 312 TO BS 328 AT LBL 46. REPLACED FLOOR WEB BTW BS 312 TO BS 328 AT LBL 46 AT FWD GALLEY AREA IAW SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV. -.Mar 10, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042078581Access Panel · crackedCRACK SEAL BLADE ASSY ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED SEAL BLADE ASSY ACCESS PANEL 333AB AT LT HORIZONTAL; IAW SRM-51-20-01-0G-0; CRACK LENGTH: 0.319 INCHESMar 10, 2026 · N8630B · Boeing 7378H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026041778570Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801.Mar 10, 2026 · N8638A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026041778571Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801.Mar 10, 2026 · N8638A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026041778572Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.Mar 10, 2026 · N8638A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026041778573Bracket · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS SERVICE DOOR AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.Mar 10, 2026 · N8638A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026041778580Lens · missingSIDEWALL PANEL 242ZAW EMERGENCY COVER LENS OVER WING HATCH MISSING. INSTALLED LENS IAW AMM 33-51-01-960-801, STEP 2, C, (1), (A), AND 2, C, (4).Mar 10, 2026 · N8630B · Boeing 7378H4 · Emergency LightingSDR SWAA2026041678332Scuff Plate · crackedCRACKED SCUFF PLATE, AFT ENTRY DOOR. REPAIRED THE SCUFF PLATE IAW SRM 53-70-15-2R-1, REPAIR 1, PARAGRAPH 4. B, FIGURE 203.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041678566Angle · crackedCRACKED ANGLE, LOCATED AFT FACE BS 400 AT LEVEL STR 26L FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7505, SHEET 137, REV -.Mar 10, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041678337Floor Support · corrodedCORROSION FLOOR SUPPORT BTW BS 328 TO BS 344 AT LBL 22 AND WL 208.1 AT FWD GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-10-02 ITEM 9 AND DWG 141A5730, SHEET 30, REV A, DWG 141A5730, SHEET 37, REV C.Mar 10, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 8LFA202603100002Nut · looseDURING FLIGHT IT WAS NOTED AN ABNORMAL METALLIC NOISE EMANATING FROM THE TAIL BOOM AREA. IT WAS DECIDED TO PERFORM A PRECAUTIONARY LANDING DUE TO THE NOISE HEARD. UPON INSPECTION OF THE AIRCRAFT THE TAIL ROTOR MAST NUT WAS FOUND IN A LOOSE CONDITION. SAFETYMar 10, 2026 · N463LF · Bell 407 · Tail Rotor HeadSDR SWAA2026041578541Rib · crackedCRACK INSPAR RIB 120.30 AT 27 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 27 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5. REPAIR 5 STEP 4 ITEM N TO S.Mar 10, 2026 · N7729A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2026041578540Rib · crackedCRACK INSPAR RIB 120.30 AT 19 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR LOCATED INSPAR RIB 120.30 AT 19 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.Mar 10, 2026 · N7729A · Boeing 73776N · Horizontal Stabilizer, Spar/RibSDR SWAA2026041578535Window Frame · crackedCRACK INDICATION ON WINDOW FRAME RT SIDE . CRACK LENGTH= 0.115 INCH APPROX. 2026-186433 .<[01] ON STEP 5. REPAIRED THE RT WINDOW FRAME C-D POST IAW EA 26-153-00723-WIP1; 26-153-00723-WIP2; 26-153-00723-WIP3; 26-153-00723-WIP4; 26-153-00723-WIP5 AND 26-153-0072Mar 10, 2026 · N7729A · Boeing 73776N · Fuselage Main, StructureSDR REXA2026041500287Floorbeam · corrodedLH FS 280.00 CROSSBEAM IS CORRODED FROM LBL0 TO LBL9. LOCATED AND DRILLED NEW LH FS 280.00 CROSSBEAM P/N:CC670-34094JP-1S IAW SRM 51-40-11-001-001-A01. INSTALLED NEW LH FS 280.00 CROSSBEAM P/N :CC670-34094JP-1S IAW CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SMar 10, 2026 · N920XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWAA2026041378518Stringer Clip · crackedSTRINGER CLIP BS 500I RBL25 IS CRACK (MARKED).<[01] REPAIRED BY REPLACEMENT STRINGER CLIP AT BS 500I; STR 26R PER SRM 51-10-02 PARAGRAPH 9.C. INSTALLED PER 51-40-02 AND DWG 143A1234 REV: A;[02] VERIFIED CORRECTIVE ACTION 1Mar 10, 2026 · N8631A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026041378519Floor Support · crackedINTERCOSTAL FROM BS277-BS294.5 BL0; WL208 IS CRACKED<[01] REMOVED AND REPLACED PASSENGER CABIN INTERCOSTAL BS277-BS294.5 BL0; WL208 IAW SRM 51-40-02 AND DWG# 141A5400 REV : -;[02] VERIFIED CORRECTIE ACTION 1Mar 10, 2026 · N8631A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041378521Floorbeam · corrodedCORROSION ON BS328 FLOOR BEAM UPPER FLANGE RBL44; WL208. CORROSION ON BS328 FLOOR BEAM UPPER FLANGE RBL44; WL208WILL BE REPAIRED ON CUSTOMER CARD TTG8Q01AXDK2.;[02] VERIFIED CORRECTIVE ACTIONMar 10, 2026 · N8631A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR VNAA202604110024Cowling · crackedCRACK OUTER SKIN OF RH AFT CORE COWL, PYLON INTERFACE AREA. SKIN OF RH AFT CORE COWL, PYLON INTERFACE AREA WAS REPAIRED PER REO 690-54-13-254 REV. - -Mar 10, 2026 · N603NN · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR SWAA2026040978517Intercostal · crackedFCB; FWD INTERCOSTAL ANGLE BS 500G RBL 25 IS CRACK (MARKED).<[01] REMOVED AND REPLACED FWD INTERCOSTAL ANGLE AT BS 500G; RBL 25 PER SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED CORRECTIVE ACTION 1Mar 10, 2026 · N8631A · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2026040978525Angle · crackedFCB; FWD INTERCOSTAL ANGLE BS 500H RBL 25 IS CRACK (MARKED).<[01] REMOVED AND REPLACED FWD INTERCOSTAL ANGLE AT BS 500H; RBL 25 PER SRM 51-10-02 PARAGRAPH 9.C.;[02] VERIFIED CORRECTIVE ACTIONMar 10, 2026 · N8631A · Boeing 7378H4 · Cargo Compartments