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 COEA2026072328803Spar · corrodedUPPER WING AFT SPAR UPPER FLANGE LOWER SURFACE RIBS 0-4R HAS CHAFE DAMAGE AND LEVEL 2 CORROSION. REPAIRED PER SRAS-00026285-01 ISSUE B, DATED 6/17/2026.Mar 5, 2026 · N803FX · Aerosp ATR72212 · Wing SparSDR SWIA2026030576627Door Frame · gougedNLG AFT DOOR CUTOUT ON LH SIDE EDGE IS GOUGED. REMOVED, EVALUATED AND REPAIRED DAMAGE ON LT SIDE EDGE AT NLG AFT DOOR CUTOUT IAW REO 670-53-11-2318 REV -- AND SRM 53-00-00.Mar 5, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, StructureSDR COEA2026070716803Landing · corrodedWO 273091 NR 600048 HEAVY CHECK COE/MAJOR REPAIR: R/H WING 622CT PANEL LANDING HAS FRETTING DAMAGE. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS 00026533-01 ISSUE A, DATED 6/3/2026.Mar 5, 2026 · N803FX · Aerosp ATR72212 · Wing Main, Frame StructureSDR COEA2026070715803Landing · corrodedWO 273091 NR 500061 HEAVY CHECK COE/MAJOR REPAIR: L/H WING PANEL 521DT LANDING HAS FRETTING. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS 00026533-01 ISSUE A, DATED 6/3/2026.Mar 5, 2026 · N803FX · Aerosp ATR72212 · Wing Main, Frame StructureSDR COEA2026070714803Landing · corrodedDURING HEAVY CHECK, LT WING PANEL 522CT WING LANDING FRETTING. LEVEL 2. REPAIRED IAW SRAS 00026533-01 ISSUE A, DATED 6/3/2026.Mar 5, 2026 · N803FX · Aerosp ATR72212 · Wing Main, Frame StructureSDR IPXA2026031834297Strap · corrodedAFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 45.50, ID STICKER NUM. (085-073). ATA 53-20 INSTALLED CEILING STABILIZATION STRAP, REPLACEMENT SECTION AND 2EA REPAIR SPLICES IN AFT CARGO COMPARTMENT BETWEEN STA Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026030934060Strap · corrodedAFT CARGO COMP. CEILING STABILIZATION STRAP HAS CORROSION, APPROX BTW BS 1400 AND BS 1420, RBL 24.75, ID STICKER NUM. (085-078). ATA 53-20 INSTALLED NEW STABILIZATION STRAP P/N STESAA7003349028-2 FOR AFT CARGO CEILING COMP BETWEEN STA 1360 AND STA 1440 IAW B7Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR AALA202606034430Idg · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BWI DUE TO THE FLIGHT CREW REPORTING DURING CLIMB THE #1 AND #2 GENERATORS FAILED AT FL 230. THE RAT DEPLOYED AND THE FLIGHT CREW WAS ABLE TO RESTORE #1 GENERATOR. THE AIRCRAFT LANDEMar 5, 2026 · N556UW · Airbus A321231 · AC Generator-AlternatorSDR 2026FA0000439Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMar 5, 2026 · N73MH · Cessna 172S · Fuselage Main, Longeron/StringerSDR REXA2026050400425Doubler · wornWEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV FMar 5, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2026030575963Floor Support · corrodedRIGHT PRESSURE FLOOR STRAP AT BS 559 AND RBL 36.0 TO RBL 45.0 CORRODED. REMOVED AND REPLACED RT PRESSURE FLOOR STRAP AT BS 559 & RBL 36 - RBL 45 IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 5, 2026 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026030575962Floor Support · corrodedRIGHT PRESSURE FLOOR SUPPORT, BLENDED CORROSION DAMAGE SURROUNDING TWO SCREW HOLES BETWEEN BS 529 - 554. FWD SCREW HOLE FOUND TO HAVE CRACK AND AFT BLEND FOUND BEYOND LIMITS OF REO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-3413 REV--. REPAIR TO PRESSURMar 5, 2026 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026030575961Hinge · damagedRIGHT AILERON HINGE NR 3 INBD BUSHING HOUSING BORE IS DAMAGED. REMOVED AND REPLACED RT AILERON NR 3 HINGE ASSY IAW SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 5, 2026 · N915SW · Cndair CL6002B19 · AileronsSDR SWIA2026030575960Hinge · damagedRIGHT AILERON HINGE NR2 IB BUSHING HOUSING BORE IS DAMAGED. REAMED THE TRAILING EDGE RT NR 2 AILERON HINGE LUGS TO FOURTH OVERSIZE AND INSTALLED THE BUSHINGS IN REFERENCE TO REO 601R-57-51-015, REV NC, COMPLIED WITH TASK CARD 51-900-1003-SKY.Mar 5, 2026 · N915SW · Cndair CL6002B19 · AileronsSDR BAGA2026043000010Hinge · corrodedLH WING TE PANEL SUKPPORT STRUTURE BETWEEN RIB 22-23 HAS CORROSION. REMOVED AND REPLACED HINGE AT RIBMar 5, 2026 · N175BZ · Airbus BD5001A11 · Wing Main, Frame StructureSDR SWIA2026030575928Bulkhead Web · damagedLEFT BS 280 LOWER INBD WEB SHOWS SIGNS OF EXFOLIATION. REMOVED AND INSTALLED NEW FABRICATED REPAIR LT LOWER BULKHEAD WEB IAW SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 5, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026030575918Channel · corrodedCHANNEL ASSY BETWEEN BS 1031 - 1051.30, STR 26 - 27R CORRODED. REMOVED AND INSTALLED A NEW CHANNEL ASSY IAW SRM 51-42-06-001-001-A01 AND DWG MM670-43200, REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.Mar 5, 2026 · N732SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026030575882Floorbeam · crackedBS 280 FORWARD FLOORBEAM ANGLE, REF DWG 600-34017, SRM 53-11-19, BETWEEN RBL 9.0 AND LBL 9.0 CRACKED. REMOVED AND REPLACED THE BS 280 FORWARD FLOORBEAM ANGLE, RBL 9 AND LBL 9 IAW SRM 51-42-06, & SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. . REF 318Mar 5, 2026 · N916SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026030575873Stop Fitting · wrong partDURING THE REPLACEMENT OF THE PAX DOOR FS310.00 STOP DROP DOWN DOOR FITTING, IT WAS FOUND THAT INCORRECT HARDWARE WAS INSTALLED IN THE FWD SUPPORT BRACKET STOP DURING A PREVIOUS REPAIR. REMOVED AND INSTALLED NEW PAX DOOR FS 310 FWD SUPPORT BRACKET STOP. IAW SMar 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026030575871Door Frame · damagedUPON REMOVAL OF PAX DOOR FWD UPPER STOP BRACKET, FOUND 4EA ELONGATED HOLES AND GOUGES AROUND HOLES ON F.S 310.00 PAX DOOR SURROUND FRAME STRUCTURE BETWEEN STR 3L AND 4L, COMMON TO UPPER STOP BRACKET. PERFORMED EVAL. TO DAMAGE HOLES #1 DAMAGE AROUND THE HOLE EMar 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026030575866Door Frame · chafedPAX DOOR CUTOUT FRAME FS310 FITTING CAM CHAFED AFTER CLEANED AREA FOUND CORROSION ON CHAFFED AREA, NO ALLOW. LIMIT FOUND ON SRM. REQ. REPLACEMENT. ORDER NEW FITTING CAM FS310.00 P/N 600-31688-17. PERFORMED LOCATE AND DRILL NEW PAX DOOR FS310 FITTING CAM. IMar 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Main, StructureSDR HNAA2026042100341Skin · damagedFWD FUSELAGE, THERE ARE 9 LIGHTNING STRIKES ON EXTERIOR SKIN FROM FR1A-9, STGR 14R-17R. INSTALLED DOUBLER REPAIR ON FORWARD FUSELAGE - SKIN BETWEEN FR.1A-2 AND STRG. 14R -17R. IAW EMB 145 ETD-2026-145-005225 AND PIEDMONT EO1-53-26-0159.Mar 5, 2026 · N905JH · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026042076912Angle · crackedCRACKED ANGLE, BS T500H, STR 26L. REPLACED ANGLE-CLIP AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042076904Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 138, REV -.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042076913Support Angle · crackedCRACKED ANGLE, BS 400, STR 26L. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV -.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042076902Angle · crackedCRACKED ANGLE, BS 500H, STR 26R FWD CARGO COMPARTMENT. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7505, SHEET 137, REV -.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042091112Angle · crackedCRACKED ANGLE, BS 500H, STR26R FWD CARGO COMPARTMENT. THE ANGLE WAS REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2. CRACK LENGTH IS:0.864 INCHES.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041777111Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN IAW AMM 33-51-15-960-801.Mar 5, 2026 · N8630B · Boeing 7378H4 · Emergency LightingSDR SWAA2026041776898Battery Pack · inoperativeINOPERATIVE BATTERY PACK, EMERGENCY EXIT LIGHT, FWD LOWERED CEILING IN THE PASSENGER CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.Mar 5, 2026 · N8638A · Boeing 7378H4 · Emergency LightingSDR SWAA2026041777101Battery Pack · inoperativeINOPERATIVE BATTERY PACK, EMERGENCY EXIT LIGHT, ON AFT LOWERED CEILING, LT PASSENGER CABIN. REPLACED BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.Mar 5, 2026 · N8638A · Boeing 7378H4 · Emergency LightingSDR SWAA2026041776911Gusset · crackedCRACK GUSSET ANGLE LOCATED BS 500I, STR 19R AT FWD CARGO BAY. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 257, REV B.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041776903Gusset · crackedCRACK GUSSET ANGLE LOCATED BS 500I, STR 21L AT FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 257, REV B.Mar 5, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWIA2026030575737Rib · corrodedCAPTURE MAJOR REPAIR/RII REQUIREMENTS FOR CORROSION DISCOVERED ON LT WING BATTERY RIB AT WS 48.3 DURING REPLACEMENT OF UPPER ANGLE ON HN00281977 CAMP 31329618. 5720COMPLIED WITH ALL THE STEPS OF REO 601R-57-21-4030 REV-- DATED 2026-03-06, INSTALLED -1 REPAIRMar 5, 2026 · N952SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWAA2026041676901Scuff Plate · crackedCRACK FWD CORNER OF SCUFF PLATE. REPAIRED THE SCUFF PLATE IN THE AFT CARGO BAY IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.Mar 5, 2026 · N8638A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026041676899Floor Panel · delaminatedDELAMINATED FLOOR PANEL 232RF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 232RF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-7 REPAIR 7.Mar 5, 2026 · N8638A · Boeing 7378H4 · Fuselage Floor PanelSDR AALA202604159522Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: HORIZONTAL SUPPORT ANGLE CRACKED AT BS 663 24" OUTBOARD OF RIGHT HAND SIDE OF KEEL BEAM. REPLACED THE ENTIRE CRACKED CHORD ANGLE. PER NR 248.Mar 5, 2026 · N951NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202604154745Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: HORIZONTAL SUPPORT ANGLE CRACKED AT BS. 663 24" OUTBOARD OF LEFT HAND SIDE OF KEEL BEAM. REPLACED THE ENTIRE CRACKED CHORD ANGLE. PER NR 244.Mar 5, 2026 · N951NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR VNAA202604110020Canister · crackedCRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -Mar 5, 2026 · N603NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR VNAA202604110019Canister · crackedCRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -Mar 5, 2026 · N603NN · Cndair CL6002D24 · Wing Main, Frame StructureSDR IPXA2026040633932Frame · dentedMAJOR REPAIR. AFT CARGO BAY FRAME UPPER ANGLE DENTED, APPROX AT BS 1220, BTW STGR 26L AND STGR 27 L, REPAIR WAS ACCOMPLISHED IAW EO-96988-REQ1 AND VT-SAA EA 757-5360-01-B0699 REV IR PRIOR TO FURTHER FLIGHT.Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR AALA202604062088Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK CROWN AT STA 1440 AND RBL 74. REPLACED SEAT TRACK PER AARD 51-00-05-1.Mar 5, 2026 · N772AN · Boeing 777223 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026040233747Frame · dentedMAJOR REPAIR, AFT CARGO COMP. FRAME UPPER CHORD HAS 3 EA DENT, APPROX AT BS 1360, BTW STGR 25R AND STGR 27 R, ID STICKER NUM. (085-068). ATA 53-10. REMOVED (3EA) SOLID RIVETS FROM DISCREPANT AREAS AT FS 1360 INBD OF STR 26R FOR ACCESS IAW B757-200PF SRM 51-40-Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2026040133784Intercostal · dentedAFT CARGO COMP. INTERCOSTAL HAS A DEFORMATION APPROX BTW BS 1360 AND BS 1380, BTW STGR 24R AND STGR 25 R, ID STICKER NUM. (085-069). ATA 53-10 INSTALLED 1EA. SHIM AND NEW INTERCOSTAL IAW B757-200PF SRM 51-40-02-0G-0.Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026040176893Angle · crackedLEFT WING TRANSVERSE ANGLE, JUST ABOVE AFT PYLON WAS CRACKED IN RADIUS. REMOVED AND REPLACED THE LT WING TRANSVERSE ANGLE IAW SRM 51-40-02 AND DWG 115A2512, REV B.Mar 5, 2026 · N249WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026033176736Rail · corrodedCORROSION ON THE BULKHEAD, BS 489, STRINGERS 26R - 26L, WL 152. REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD LOWER RAIL, BS 500D, RBL 24 - LBL 24, WL 152 IAW SRM 51-40-02, & DWG 143A7902, REV C.Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026033134415Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1400, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-074). ATA 53-10. REMOVED CORROSION AT MAIN CARGO COMP. FLOOR BEAM LWR CHORD APPROX. AT BS 1400, BTW RBL 24.75 AND RBLMar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026033134469Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO COMP. FLOOR BEAM LWR CHORD HAS CORROSION, APPROX AT BS 1420, BTW RBL 24.75 AND RBL 45.50, ID STICKER NUM. (085-075). ATA 53-10. REMOVED 5EA ANGLES FROM AFT CARGO COMP. FRAME UPPER CHORD APPROX AT BS 1360, BTW STGR 25R AND STGR 27Mar 5, 2026 · N451UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR SWAA2026033076892Stiffener · crackedLEFT STABILIZER RIB NR 3, STFFENER NR 3 CRACKED. FOUND DURING AN INSPECTION. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.Mar 5, 2026 · N249WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026033076735Intercostal · corrodedAFT CARGO INTERCOSTAL BETWEEN BS 767 & 787, RBL 25 CORRODED, TWO LOCATIONS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-05-0G-0, DWG 146A0081, REV-.Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026033076895Floor Support · corrodedCORROSION ON ACB FLOOR SUPPORT SPLICE AT BS 767+5 WL157. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02 AND DWG 146A7500 REV -.Mar 5, 2026 · N249WN · Boeing 7377H4 · Fuselage Miscellaneous Structure