N685SK

Service difficulty reports · 45

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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'
  WHERE n_number = 'N685SK' AND registry_match = 'registration'
  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 SWIA2026042276025Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FApr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026042276024Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLAApr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026042276023Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO Apr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026042276022Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATEDApr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026020475192Skin · corrodedCORROSION ON RIGHT EXTERIOR FUSELAGE AROUND BS 630 FOR PANEL 192BB. REMVOED CORROSION ON RT EXTERIOR FUSELAGE AROUND BS 629 TO BS 708 IAW SRM 51-21-06-001-001-A01, AND REPAIRED BY COMPLYING WITH ALL STEPS OF REO 670-53-00-806, REV -. COMPLIED WITH TASK CARD Dec 22, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026020475181Skin · corrodedCORROSION ON LEFT EXTERIOR FUSELAGE AROUND BS 630 FOR PANEL 191BB. REMOVED CORROSION ON THE LT EXTERIOR FUSELAGE, BS 629 TO 693 IAW SRM 51-21-06-001-001-A01 AND REPAIRED DAMAGE BY COMPLYING WITH ALL STEPS OF REO 670-53-00-804, REV -. COMPLIED WITH TASK CARD Dec 22, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2025091775180Rib · corrodedLEFT WING, TRAILING EDGE RIB AT WS 398, WAS CORRODED AROUND 13 FASTENER HOLES. REMOVED AND REPLACED THE LT WING, T/E RIB IAW SRM 51-42-21-001-001-A01 AND DWG CC670-15010 REV: B. COMPLIED WITH 51-900-1002-SKYSep 17, 2025 · N685SK · Cndair CL6002C10 · Wing, Rib/BulkheadSDR SWIA2025090875191Angle · crackedANGLE COMMON TO LANDING LATCH CUT OUT FOR PANEL 212AR AT APPROXIMATELY BS 173 CRACKED. REMOVED AND REPLACED THE ANGLE COMMON TO LANDING LATCH CUT OUT FOR PANEL 212AR AT APPROXIMATELY BS 173 IAW SRM 51-42-06-001-001-A01, AND DWG CC670-33040, REV G, COMPLIED WISep 8, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025082375209Roller · wornFOUR LT SLAT TRACK SIDE ROLLERS AT 3-2 ARE WORN. REMOVED AND REPLACED FOUR LT WING SLAT TRACK SIDE ROLLERS AT 3-2, IAW AMM:27-81-44-400-803-A01. OPS TESTED GOOD.Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025082375208Roller · wornFOUR LT WING SLAT TRACK SIDE ROLLERS AT 2-2 ARE WORN. REMOVED AND REPLACED THE LT WING FOUR SIDE ROLLERS AT 2-2, IAW AMM:27-81-44-400-802-A01. OPS TESTED GOOD.Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025082375207Roller · wornFOUR LT WING SIDE TRACK ROLLERS AT 1-2 ARE WORN. REMOVED AND REPLACED LT WING FOUR SIDE ROLLERS AT 1-2, IAW AMM:27-81-44-400-801-A01. EXTENSION & RETRACTION OF SLATS GOOD.Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025082275206Roller · wornFOUR RT SLAT TRACK SIDE ROLLERS AT 3-2 ARE WORN REMOVED AND REPLACED FOUR RT WING SLAT TRACK SIDE ROLLERS AT 3-2, IAW AMM:27-81-44-400-803-A01. EXTENSION AND RETRACTION OF SLATS GOOD AND OPERATING SMOOTHLY.Aug 22, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025082275205Roller · wornALL FOUR RT WING SLAT TRACK SIDE ROLLERS AT 2-2 ARE WORN. REMOVED AND REPLACED FOUR RT WING SLAT TRACK SIDE ROLLERS AT 2-2, IAW AMM:27-81-44-400-802-A01. OPS TESTED GOOD.Aug 22, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026020475200Fitting · chafedPAX DOOR FLOOR AFT CLOSING FITTING EXFOLIATED. REPLACED PAX DOOR FLOOR AFT CLOSING FITTING IAW DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 22, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2025082175210Roller · wornFOUR RT SIDE SLAT TRACK ROLLERS AT THE 1-2 ARE WORN. REMOVED AND REPLACED THE FOUR RT WING SLAT TRACK SIDE ROLLERS AT 1-2, IAW AMM:27-81-44-400-801-A01. OPS TESTED GOOD.Aug 21, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026020475179Angle · corrodedPAX DOOR FLOOR MID CAP ANGLE IS CORRODED. INSTALLED NEW PAX DOOR FLOOR MID CAP ANGLE IAW DWG SH670-31810 REV AE AND SRM 51-41-02-001-001-A01. COMPLIED WITH 51-900-1002-SKY. OP TEST GOOD..Aug 21, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026020475199Stringer · corrodedSTRINGER 26R HAS CORROSION IN MULTIPLE AREAS BETWEEN BS 469 AND 485. REPLACED THE STRINGER IAW DWG SH670-30006, REV A, SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 12, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2025081075198Former · crackedPAX DOOR FORMER BS 320.163 SUSPECTED CRACKED. INSTALLED NEW PAX DOOR FORMER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. PRESSURIZATION LEAK CHECK OF THE REPAIR AREA PASSED IAW AMM 21-31-00-Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026020475190Intercostal · crackedPAX DOOR INTERCOSTAL DD1A AFT CRACKED. INSTALLED A NEW PAX DOOR AFT DD1A INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2025081075189Door Frame · crackedPAX DOOR FRAME BS 320 CRACKED. INSTALLED A NEW DOOR FRAME IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.Aug 10, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026020475188Intercostal · dentedPAX DOOR AFT DD1 INTERCOSTAL DENTED AT THE BEND RADIUS. INSTALLED A NEW PAX DOOR AFT DD1 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026020475197Angle · corrodedDOOR FLOOR ANGLE IS CORRODED. FLAGGED. REMOVED CORRODED AND INSTALLED NEW PAX DOOR FLOOR ANGLE IAW DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01, REV 38. OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 9, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026020475196Former · crackedPAX DOOR AFT FORMER IS CRACKED. INSTALLED NEW PAX DOOR AFT FORMER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY900080.Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2025080975187Intercostal · crackedPAX DOOR AFT DD7 INTERCOSTAL IS CRACKED. INSTALLED NEW PAX DOOR AFT DD7 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2025080975186Intercostal · corrodedPAX DOOR MID DD6 INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR MID DD6 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2025080875178Floor Support · damagedFLOOR SUPPORT LBL27 IS PITTED AND CORRODED FROM BS 985 - 1098.2. REPAIRED THE LT FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Aug 8, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2025080775185Landing · crackedSUSPECTED CRACK IN THE AFT A-BAY LANDING LATCH CUT OUT FOR PANEL 212AR. REMOVED AND REPLACED CRACKED LANDING LATCH CUT OUT FOR PANEL 212AR IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, DWG CC670-33040 REV -G, & REO 670-53-11-2178 REV-, COMPLIED WITAug 7, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026020475177Hinge · damagedPAX DOOR PIANO HINGE DOOR SIDE AFT LUG ROLL PIN HOLE IS ELONGATED. INSTALLED NEW PAX DOOR HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01 STEPS R AND T AND DWG 601R31702 REV. N AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. COMPLIEDAug 7, 2025 · N685SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2025080675195Skin · gougedEXTERNAL LOWER SKIN GOUGED FROM WING-TO-BODY FAIRING AT STRG27, BS 977 - BS 985. BLENDED OUT DAMAGE ON EXTERNAL LOWER SKIN AT STGR27, BS 977 - 985 IAW SRM 51-12-00-001-001-A01 AND COMPLIED WITH NOTES A., B., AND C. OF GREO 670-53-00-290, REV F. LEAK CHECKED GAug 6, 2025 · N685SK · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA2025080675194Rivet · looseRIGHT OTBD FLAP OUTER SKIN HAD SMOKING RIVETS. FOUND AT NUMEROUS LOCATIONS ALONG FLAP. REMOVED 10 SMOKING RIVETS AT RT OTBD FLAP OUTER SKIN AT NUMEROUS LOCATIONS ALONG FLAP IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-13-001-001-A01. INSTALLED 10 EACH FASTENEAug 6, 2025 · N685SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2025073075193Stand Off · crackedLEFT UPPER TRANSCOWL INBD -A- BRACKET STAND OFF CRACKED. REMOVED CRACKED STAND OFF FROM LT UPPER TRANSCOWL AND INSTALLED ONE NEW STAND OFF ON LT UPPER TRANSCOWL IAW GREO 670-54-21-971, REV B, STEPS 1-3. COMPLIED WITH SKY CARD 51-900-1002-SKY.Jul 30, 2025 · N685SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2025073075184Stand Off · crackedLEFT LOWER TRANSCOWL INBD -A- BRACKET STAND OFF IS CRACKED. STAND OFF REPAIRED IAW REO 670-54-21-971, REV B. COMPLIED WIT 51-900-1002-SKY.Jul 30, 2025 · N685SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2025072575183Helicoil · damagedLEFT WING JACKING POINT HELI-COIL IS DAMAGED. INSTALLED NEW LEFT WING JACK FITTING IAW SRM 51-42-21-001-001-A01, DWG CC670-10126, REV NC, AND DWG CC670-10038, REV NC. .COMPLIED WITH 51-900-1002-SKY.Jul 25, 2025 · N685SK · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWIA2025061975204Roller · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 RT - DISCARD THE RT SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3. REMOVE AND REPLACE IAW TASK CARD 27-630-824. COMPLIED WITH SCHEDULED MAINTENANCE ON TRACK ROLLER SLAT 3-3 700Jun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025061975203Roller · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 RT - DISCARD THE RT SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 . REMOVE AND REPLACE IAW TASK CARD 27-630-809 (MRB 27-81-43-717), COMPLIED WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SJun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025061975202Roller · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 LH - DISCARD THE LH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-530-824 (MRB 27-81-43-713), COMPLIEDJun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025061975201Roller · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 LH - DISCARD THE LH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 (P/N CC670-12272-1. REMOVE AND REPLACE IAW TASK CARD 27-530-809 (MRB 27-81-43-717), COMPLIED WITH SCHEDULED MAINTENANCE CJun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026020475182Skin · scratchedPERFORMED TEMPORARY REPAIR TO SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP STN. 235.84 - FLAP STN. 254.96. COMPLETE PERMANENT REPAIR 650 HOURS FROM THE TIME OF INCORPERATION. , REPAIRD SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP Jun 19, 2025 · N685SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202163029None · out of toleranceMOUNTING HOLES IN GALLEY AREA ABOVE GALLEY SERVICE DOOR ON RH FRAME AT FS333.00 AND FS349.00 BETWEEN STRINGERS 5R AND 6R DUE TO EA7RJ3519-25 BRACKET REMOVAL (8 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948264 FOR INITIAL DISCREPANCY. THDec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163028None · out of toleranceMOUNTING HOLES IN FLIGHT DECK ON RH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (4 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948260 FOR INITIAL DISCREPANCY. THIS IS A €ŒMAJDec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163027None · out of toleranceMOUNTING HOLES IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (4 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948257 FOR INITIAL DISCREPANCY. THIS IS A €ŒMAJDec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, FrameSDR SWIA202165167None · damagedDAMAGE/HOLES FOUND OUT OF LIMITS IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (FILED - CLOSED) MOUNTING HOLES IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243Dec 4, 2021 · N685SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202165168None · crackedFOUND CRACKED SUPPORT ANGLE CLEAT ON FORWARD SIDE OF FS 349 FLOOR CROSS BEAM AT LBL27.00 (FILED - CLOSED) REMOVED AND REPLACED SUPPORT ANGLE CLEAT ON FORWARD SIDE OF FS 349 FLOOR CROSS BEAM AT LBL27.00, REF CRJ 700 SRM 51-42-06 AND 53-21-43.Dec 2, 2021 · N685SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202165166None · damagedRIGHT EMERGENCY EXIT DOOR WINDOW SCUFFED. (FILED - CLOSED) REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT DOOR IAW TASK CARD 56-200-1000-SKY. LEAK CHECK GOOD. OLD DATE:08-02Nov 17, 2021 · N685SK · Cndair CL6002C10 · DoorsSDR SWIA202165165None · damagedLEFT EMERGENCY EXIT DOOR WINDOW SCUFFED. (FILED - CLOSED) REMOVED AND REPLACED LH OVERWING EMERGENCY EXIT DOOR IAW TASK CARD 56-200-1000-SKY. LEAK CHECK GOOD. OLD DATE:08-02Nov 17, 2021 · N685SK · Cndair CL6002C10 · Doors
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