N611SK

Service difficulty reports · 414

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 = 'N611SK' 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 SWIA2026071477503Slat Track · corrodedREMOVE AND REPLACE RIGHT SLAT TRACK 3-2. REMOVED AND INSTALLED NEW SERVICEABLE RT SLAT TRACK 3-2 IAW AMM27-81-41-000-802-A01, AND AMM27-81-41-400-802-A01.Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071477502Slat Track · corrodedREMOVE AND REPLACE RIGHT SLAT TRACK 3-1. REMOVED AND INSTALLED NEW SERVICEABLE RT SLAT TRACK 3-1 IAW AMM27-81-41-000-801-A01 AND AMM 27-81-41-400-801-A01.Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071477501Slat Track · corrodedREMOVE AND REPLACE RIGHT SLAT TRACK 2-3 . REMOVED AND INSTALLED SERVICEABLE, RT SLAT TRACK 2-3 USING NEW COTTER PINS IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01OPS TEST GOOD.Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377500Slat Track · corrodedREMOVE AND REPLACE RIGHT SLAT TRACK 2-2. REMOVED AND INSTALLED SERVICEABLE, RT SLAT TRACK 2-2 USING NEW COTTER PINS AND SAFETY CABLES IAW AMM 27-81-41-000-802 A01 AND AMM 27-81-41-400-802 A01.Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377499Slat Track · corrodedREMOVE AND REPLACE RIGHT HAND SLAT TRACK 2-1. REMOVED AND INSTALLED SERVICEABLE SLAT TRACK 2-1 USING NEW COTTER PINS AND SAFETY CABLE IAW AMM 27-81-41-000-801 A01, AND AMM 27-81-41-400-801 A01.Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377496Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 3-2. REMOVED AND INSTALLED A NEW SLAT TRACK 3-2 IAW AMM 27-81-41-400-802-A01.Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377495Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 2-3. INSTALLED A NEW LT SLAT TRACK 2-3, IAW AMM 27-81-41-400-801-A01.Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377494Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 2-2. REMOVED AND INSTALLED A NEW LT SLAT TRACK 2-2 IAW AMM 27-81-41-400-802-A01.Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071377436Slat Track · not reportedREMOVE AND REPLACE LH SLAT TRACK 3-3. REMOVED AND INSTALLED THE LH SLAT TRACK 3-3 AT LT WING, IAW AMM27-81-41-000-803-A01 AND AMM27-81-41-400-803-A01Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071277504Slat Track · corrodedREMOVED AND REPLACED LH SLAT TRACK 1-2. REMOVED AND INSTALLED NEW SLAT TRACK 1-2 IAW AMM 27-81-41-400-802-A01.Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071277498Slat Track · corrodedREMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-3 . REMOVED AND INSTALLED SERVICEABLE, PN , RH SLAT TRACK 1-3 USING NEW COTTER PINS IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071277497Slat Track · corrodedREMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-1. REMOVED AND INSTALLED A NEW, , RT WING SLAT TRACK 1-1 IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026071277492Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 1-3. INSTALLED A NEW LT SLAT TRACK 1-3 IAW AMM 27-81-41-400-801-A01.Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026050777454Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN FS310 AND FS319 , STR25L TO STR26L. REPAIRED INNER SKIN IAW REO 670-53-21-2887 REV-.May 7, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026050677414Support · damagedFOUR ELONGATED HOLES FOUND IN BACKUP SILL ON STGR21L FROM FS333 TO FS349. REPLACED BACKUP SILL ON STGR21 AT FS333 TO FS349 WITH NEW PART REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV AEMay 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026050277509Angle · damagedDURING INSTALLATION OF FASTENERS EDGE DAMAGE CREATED ON REINFORCEMENT ANGLE BS 333, BETWEEN STR 21R TO 22R. REPAIRED REINFORCEMENT ANGLE IAW REO 670-53-21-2883, REV -.May 2, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026042477437Skin · dentedPROTRUDING DENT FOUND ON FUSELAGE SKIN BETWEEN FS 333 AND FS 349, AND BETWEEN STR23L AND STR24L. PERFORMED CUTOUT OF DENT AND APPLIED DOUBLER AT FUSELAGE SKIN BETWEEN FS333 - FS349, STGR 23L - 24L REF REO 670-53-21-2876 REV --.Apr 24, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026042077463Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 22L, BS 477. REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, & DWG SH670-30006, REV A.Apr 20, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026041677346Stringer Splice · corrodedCORROSION FOUND ON STRG 21 RT SPLICE AT CIRCUMFERENTIAL JOINT AT FS 477.4. REPLACED STRINGER SPLICE AT STGR21R, FS477 REF SRM 51-42-06-001-001-A01 AND DWG SH670-30006 REV A .Apr 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026041377369Fitting · chafedLEFT MLG SIDE STAY FITTING HAS A MULTIPLES CHAFES AND GOUGES. REMOVED THE CHAFED AREAS ON LT MLG SIDE STAY FITTING IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS 1-5 REF REO 670-57-11-261, REV --.Apr 13, 2026 · N611SK · Cndair CL6002C10 · Main Landing GearSDR SWIA2026040977419Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN BS 280 & 295, STR 24R -25R. PERFORMED A CUT OUT OF THE CORRODED FUSELAGE SKIN BTWN BS 280 - 310, STR 24R - 26R AND APPLIED DOUBLER IAW REO 670-53-21-2866, REV -.Apr 9, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040877489Seat Track · corrodedRIGHT SIDE SEAT TRACK, BS 847 - 879, SCRATCHED AND CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.Apr 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026040877440Frame · fomREMOVE AND SPLICE FRAME FS 485, STR20R FROM STR26R TO FOM. PERFORMED SPLICE REPAIR OF FRAME AT FS485, STGR26R - STGR20R REF REO 670-53-31-1193 REV -, SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-33200 REV G.Apr 8, 2026 · N611SK · Cndair CL6002C10 · Standard Practices/StructuresSDR SWIA2026040877435Frame · fomREMOVE AND SPLICE FRAME FS 469, STR20L FROM STR23L TO FOM C-CHECK RO 09302026REMOVED AND SPLICED FRAME FS469, FROM STR20L TO STR23L BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2857 REV -, SRM 53-00-06-201-001-A03 , SRM 51-42-21-001-001-A01, 51-42-06-001-001Apr 8, 2026 · N611SK · Cndair CL6002C10 · Standard Practices/StructuresSDR SWIA2026040677472Angle · damagedTWO ELONGATED HOLES FOUND IN REINFORCEMENT ANGLE AT BS 333, STR 21L. REPLACED REINFORCEMENT ANGLE AT BS 333, STRINGER 21L IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31810, REV AE.Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026040677464Support · damagedTWO ELONGATED HOLES FOUND IN BACKUP SILL ON STR 21L FROM BS 295 - 333. REPLACED THE BACKUP SILL ON STR 21L BTWN BS 295 - 333 IAW SRM 51-42-06-001-001-A01, REV 38, & DWG SH670-31810, REV AE.Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026040677434Frame · damagedTWO ELONGATED HOLES FOUND IN FRAME AT FS 333 STR 21L. REPLACED FRAME AT BS 333, STR 21L IAW SRM 51-42-21-001-001-A01, & DWG SH670-31810, REV AE.Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026040677376Frame Splice · damagedTWO ELONGATED HOLES FOUND IN FRAME SPLICE AT BS 333, STR 21L. REPLACED THE FRAME SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31810, REV AE.Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026040677351Stringer Splice · damagedTWO ELONGATED HOLES FOUND UPPER STRINGER SPLICE 21L, BS 333. REPLACED UPPER STRINGER SPLICE 21L, BS 333 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026040477396Floor Support · corrodedON REMOVAL OF THE LT FLOOR SUPPORT, BS 533 - 581 FOUND TO BE CORRODED. REPAIRED THE FLOOR SUPPORT, BTWN BS 333 - 581, IAW REO 670-53-21-2855, REV -. AND DWG SH670-32170, REV V.Apr 4, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026040377388Cleat · corrodedCORROSION FOUND ON 3EA CLEATS ON STR20L AT FS 453, FS 364, FS 379 . REMOVED AND REPLACED WITH NEW CLEATS 3EA ON STGR20L AT FS364, FS379 AND FS453 PER CRJ700 SRM 51-42-06-001-001-A01, DWG SH670-32050 REV J AND DWG SH670-31401 REV A COMPLIED WITH TASK CARD 51-9Apr 3, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026040377370Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 20L, BS 477. REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-30006, REV A.Apr 3, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026040277412Bulkhead · corrodedFS280 BULKHEAD RH DOOR POST AT WL795 RBL9 HAS CORROSION. PERFORMED REPAIR ON FS280 BULKHEAD RH DOOR POST AT WL795 RBL9 IAW REF 53-11-10-201-006-A01 REV 38, SRM 51-42-10-001-001-A01 REV 38 AND SRM 51-42-13-001-001-A01 REV 38Apr 2, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026033177474Bracket · damagedREAR SPAR LARTERAL BEAM, LT & RT AFT OTBD HOLE IN FITTING HAVE TWO DEFECTS IN EACH LT AFT OTBD HOLE IN SPAR HAS ONE DEFECT. REAMED DEFECTS IN LT & RT SIDE STAY BRACKETS FRAME SECTOR BETWEEN LBL45, RBL 45 UNTIL NO DEFECTS NOTED. INSTALLED OVERSIZE FASTENERSMar 31, 2026 · N611SK · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWIA2026032677457Angle · crackedDURING AUDIT OF TASK CARD 32-710-125 IT WAS FOUND THAT THE NLG WHEEL WELL, AFT BULKHEAD FS 235, CANTED BULK HEAD BACK UP ANGLE SHOWING SIGNS OF A CRACK. REPLACED REF CRJ-700 SRM 51-42-21-001-001-A01, DWG PLCC670-32106 REV A, DWG CC670-32030 REV H COMPLIED WIMar 26, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026032677360Stringer Splice · corrodedCORROSION FOUND AT STR19R SPLICE BS 477. REMOVED AND REPLACED STRINGER SPLICE WITH A NEW STR19R, BS 477 IAW SRM 51-42-06-001-001-A01, & DWG SH670-30006, REV A.Mar 26, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026032577425Stringer · corrodedCORROSION FOUND ON STRINGER 21R, BS 394 - 477. REPLACED THE STRINGER IAW DWG SH670-31350, REV A, AND SRM 51-42-06-001-001-A01.Mar 25, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026032577382Stringer Splice · corrodedCORROSION FOUND ON STRINGER 18L SPLICE, BTWN BS 469 - 485. REMOVED AND REPLACED WITH A NEW SPLICE ON STRINGER 18L, BS 469 - 485 PER SRM 51-42-06-001-001-A01, AND DWG SH670-30006, REV A.Mar 25, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026032477423Bulkhead · corrodedCORROSION FOUND ON BS 280 BULKHEAD AT STR 26L UNDER CRAWL WAY SUPPORT ANGLE. REMOVED CORROSION ON THE BS 280 BULKHEAD IAW SRM 51-21-06-001-001-A01,COMPLIED WITH ALL STEPS 1-9 OF REO 670-53-11-2298, REV -.Mar 24, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026032377354Floor Support · crackedFLOOR SUPPORT COCKPIT AT APPROX BS 202.75 - 280, RBL12 WAS CRACKED. REMOVED NEW COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND DWG CC670-34010, REV -K.Mar 23, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026032077407Web · corrodedLH LOWER WEB AT FS 280 HAS CORROSION 31921541 C-CHECK RO 09302026REPAIRED LH LOWER WEB AT FS 280 REF CRJ700 SRM 53-11-10-201-003-A01 REPAIR BMar 20, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026031877381Frame · corrodedLOWER FRAME SECTOR AT BS 863, STR 25L - 25R WAS CORRODED OUT OF SCOPE. REPLACED LOWER FRAME SECTOR AT BS 863, STR 20R - 20L IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND DWG SH670-37060, REV F.Mar 18, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026031877350Bulkhead Web · corrodedRIGHT LOWER WEB AT FS 280 HAS CORROSION. REPAIRED RT LOWER WEB AT FS 280 IAW SRM 53-11-10-201-003-A01 REPAIR B.Mar 18, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026031777458Angle · corrodedGALLEY SERVICE DOOR SURROUND STRUCTURE LOWER SILL ANGLE, MOUNTING HAS CORROSION ON BOTH SIDES. REMOVED AND REPLACED LOWER SILL ANGLE MOUNTING REF SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y.Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026031777402Floorbeam · crackedCOCKPIT FLOORBEAM AT APPROX FS 28000 LBL12 HAS CRACK TRANS 31900501 C-CHECK RO 09302026REPARED COCKPIT FLOORBEAM AT LBL1200 REF CRJ700 SRM 53-11-43-201-003-A01 AND COMPLIED WITH FORM M337 AND TASK CARD 51-900-1002-SKY,SEE CONTINUE CARD FORE MORE DETAILSMar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026031777387Floorbeam · crackedCOCKPIT FLOORBEAM AT APPROX FS 28000 RBL12 HAS CRACK. INSTALLED REPAIR PARTS FOR COCKPIT FLOORBEAM AT RBL1200 REF SRM 53-11-43-201-003-A01Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026031777357Attach Angle · crackedATTACH ANGLE AT BS 280, RBL12 HAS CRACK. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21-001-001-A1 AND DWG CC670-34010 REV -K ,Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026031677470Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 24R AT BS 333. REPLACED STRINGER SPLICE AT FS333 , STGR24R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677447Floorbeam · corrodedLEFT CROSSBEAM AT BS 280 HAS CORROSION. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV -K.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026031677444Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR25R. REPLACED STRINGER SPLICE AT FS333 STGR25R IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
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