N631SK

Service difficulty reports · 86

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 = 'N631SK' 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 SWIA2026040375640Hinge · gougedPAX DOOR HINGE (FUSELAGE SIDE) IS GOUGED AT AFT SIDE FROM CONTACT WITH SPRING PIN. BLENDED DAMAGE REMOVING 0.030"D MATERIAL WITHIN ALLOWABLE LIMITS IAW SRM 53-21-23-201-010-A01 REPAIR TYPE IV.Feb 24, 2026 · N631SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026021675634Stringer Splice · not reportedFABRICATION REQUIRED FOR STRINGER 26R, SPLICE, AFT OF FRAME STATION 969 PN BA670-35119-2. COMPLIED WITH SNIEO BA670-35119.Feb 16, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026011775651Skin · corrodedUPON REMOVAL OF AFT DRAIN MAST, FOUND CORROSION ON EXTERNAL SKIN BETWEEN BS 1031 - BS 1047 AND STR 27 - STR 26R. COMPLIED WITH REO 670-53-61-2664 REV -.Jan 17, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375638Hinge · gougedPASSENGER DOOR PIANO HINGE #6 LUG (FROM FWD TO AFT) IS GOUGED ON DOOR SIDE. BLENDED DAMAGE IAW SRM 51-11-01-201-007-A01 TYPE 1 ON NR 6 LUG OF PIANO HINGE FROM ORIGINAL DEPTH OF .0007' TO .0023"TAKING OUT .0016" TOTAL. REMAINING LUG THICKNESS IS .1285" TOOLS UJan 15, 2026 · N631SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026011475657Skin · corrodedUPON REMOVAL OF RAD ALT ANTENNA (E19) , FOUND CORROSION ON INTERNAL SKIN BETWEEN FS 1031 - FS 1047. CUT AWAY IDENTIFIED AREA OF FUSELAGE SKIN, FABRICATED NEW DOUBLER AND INSTALLED AT FS 1031-FS1047 UNDER RAD ALT ANTENNA BETWEEN STGR27 AND 26L IAW REO 670-53-6Jan 14, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026011475643Intercostal · crackedPAX DOOR AFT INTERCOSTAL DD1 FOUND BE CRACKED REQUIRE REPLACEMENT. REMOVED UNSERVICEABLE PAX DOOR AFT INTERCOSTAL DD1 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD1 IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SJan 14, 2026 · N631SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026040375632Former · corrodedPAX DOOR FWD FORMER FS.320 FOUND BE CORRODED REQUIRE REPLACEMENT. REMOVED AND REPLACED PAX DOOR FORMER BS 320 IAW SRM 51-42-06-001-001-A01 AND REO 670-52-11-1555 REV -.Jan 14, 2026 · N631SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026011275660Doubler · corrodedDRAIN MAST DOUBLER, AFT OF FRAME STATION 1031 - CORRODED. (C-CHECK RO 04/01/2026)PERFORMED MAJOR REPAIR BY REPLACING AFT DRAIN MAST DOUBLER PN: MM670-43255-001 IAW CRJ700 SRM 51-42-06-001-001-A01 REV DATE 10 JAN 25 WEIGHT AND BALANCE NOT AFFECTED REFERENCE CJan 12, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026011275656Doubler · corrodedRAD ALT ANTENNA DOUBLER, FORWARD OF FRAME STATION 1015 - CORRODED. INSTALLED NEW SERVICEABLE SHIM ASSY AT RAD ALT ANTENNA FWD OF F.S. 1015 IAW SRM 51-42-06-001-001-A01 REV 38D. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Jan 12, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375654Doubler · corrodedRAD ALT ANTENNA DOUBLER, AFT OF FRAME BS 1031 CORRODED. PERFORMED MAJOR REPAIR BY INSTALLING NEW SERVICEABLE RAD ALT ANTENNA SPACER AND 2EA. SHIM ASSY'S IAW SRM 51-42-06-001-001-A01, REV 38D.Jan 12, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375642Striker · corrodedSERVICE DOOR SURROUND - LOWER SEAL STRIKER CORRODED AND GOUGED. REMOVED AND REPLACED SERVICE DOOR SURROUND SEAL STRIKER WITH A NEW SERVICEABLE STRIKER IAW SRM 51-42-06-001-001-A01.Jan 12, 2026 · N631SK · Cndair CL6002C10 · Service DoorsSDR SWIA2026011275636Doubler · corrodedRAD ALT ANTENNA DOUBLER, AFT OF FRAME STATION 1069 - CORRODED. COMPLIED WITH REPLACEMENT OF RAD ALT ANTENNA DOUBLER AFT OF FS 1069 IAW SRM 51-42-06-001-001-A01, REV 38D.Jan 12, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375659Cleat · crackedFRAME STATION 847, STRINGER 20R - CLEAT CRACKED. (C-CHECK RO 04/01/2026)FABRICATED NEW SERVICEABLE REPLACEMENT CLEAT IAW MHIRJ SNIEO SH670-35950. REMOVED CRACKED CLEAT AT FS847, STGR 20R AND INSTALLED NEWLY FABRICATED CLEAT IAW CRJ700 SRM 51-42-21-001-001-A01Jan 11, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026040375658Stringer Splice · crackedSTRINGER 26R, SPLICE, AFT OF FRAME STATION 969 - CRACKED. (C-CHECK RO 04/01/2026)INSTALLED NEW SERVICEABLE FABRICATED SPLICE AT STR26R FS977 IAW CRJ700 SRM 51-42-21-001-001-A01. REFERENCE CONTINUATION FOR WORK PERFORMED.Jan 11, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026011075649Skin · chafedFUSELAGE SKIN BELOW FORWARD POTABLE WATER SERVICE DOOR - SKIN CHAFED. REPAIRED FUSELAGE SKIN IAW MHIRJ REO 670-53-21-2790 REV --.Jan 10, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375648Skin · corrodedFUSELAGE SKIN BELOW TCAS OMNIDIRECTIONAL ANTENNA - CORRODED. CUT AWAY DAMAGE FROM FUSELAGE SKIN, FABRICATED DOUBLER AND INSTALLED IAW REO 670-53-21-2794 REV -- .Jan 10, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375641Skin · gougedSKIN BELOW FORWARD DRAIN MAST GOUGED IN MULTIPLE LOCATIONS. BLENDED OUT GOUGES IAW 51-12-00-001-001-A01. PERFORMED UT THICKNESS MEASUREMENTS OF REWORKED AREAS IAW NDTM, PART 1, 51-20-004-270-A01, REV-37. FOUND LOWEST REMAINING THICKNESS OF .057 OR GREATER. Jan 10, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026040375655Intercostal · corrodedFWD JACK MOUNT (FWD OF FS 280 AT STR 27) LH AND RH SUPPORTS HAVE CORROSION ON LOWER ANGLES. PERFORMED MAJOR REPAIR BY REPAIRING LH INTERCOSTAL (CC670-32179-3) IAW REO 670-53-11-2256 REV -- DATED 2026-01-20 AND REPLACING THE RH INTERCOSTAL (CC670-32179-4) IAJan 9, 2026 · N631SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026010975653Longeron · corrodedLEFT OVERWING LONGERON CORRODED SEVERAL LOCATIONS ON INTERIOR SURFACE BETWEEN BS 752.5 AND 785.15. BLENEDED AREA, PERFORMED LPI, REPLACED FASTENERS AND PAINTED AT OVERWING LONGERON BETWEEN BS 752.5 AND 785.15 IAW REO 670-53-41-804 REV--.Jan 9, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026010675650Frame · corrodedFRAME AT FRAME STATION 379, FORWARD SIDE AT 23R - CORRODED. INSTALLED NEW FRAME P/N: SH670-32118-3A AT FS379 BETWEEN STR20R-STR25R, IAW SRM 51-42-06-001-001-A01.Jan 6, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026040375646Floorbeam · corrodedBS 280 FLOORBEAM AT LBL 9 CORRODED IN MULTIPLE LOCATIONS. REMOVED FINISH FROM BS 280 FLOORBEAM UPPER FLANGE IAW SRM 51-26-01-001-001-A0. MEASURED CORROSION, CORROSION MEASURED 0.042" DEEP. NOMINAL THICKNESS MEASURED 0.080", 53% MATERIAL LOSS. OUT OF LIMITS Jan 6, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026040375645Stringer Splice · corroded23R STRINGER SPLICE AT FRAME STATION 333 CORRODED, FORWARD SIDE. REMOVED 4EA SKIN FASTENERS FROM FWD SIDE OF STRINGER 23R SPLICE AT BS 333 IAW SRM 51-42-06-001-001-A01, LOCATED AND DRILLED STRINGER SPLICE CLEAT AT STR 23R FS 333 IAW SRM 51-40-11-001-001-A01.Jan 6, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026040375639Floorbeam · corrodedBS 280 FLOORBEAM AT RBL 6 CORRODED ON AFT EDGE BELOW CORROSION CAP. INSTALLED RH BS 280 FLOORBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-20-11-001-001-A01, AND SRM 53-00-00-101-001-A0Jan 6, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026040375637Frame · corrodedFRAME STATION 310 - FRAME CORRODED, FORWARD SIDE, BETWEEN 18R AND 19R. (C-CHECK RO 04/01/2026)REMOVED CORROSION FROM FS310 FRAME SKIN FLANGE BETWEEN STR18R AND STR19R IAW SRM 51-21-06-001-001-A01. FOUND THE FRAME AT FS310 BETWEEN STGR18R - STGR19R TO HAVE A Jan 6, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026040375635Intercostal · corrodedAVIONICS BAY DOOR INTERCOSTAL, FORWARD OF FRAME STATION 364, LEFT OF STRINGER 27 - CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL AT BS 349 - 364 LEFT OF STGR 27 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jan 6, 2026 · N631SK · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR SWIA2026010475661Bulkhead Web · corrodedRIGHT BS 280 WEB AND ASSOCIATED FASTENERS CORRODED. LOWER FS280 WEB FOUND TO BE HEAVILY CORRODED AND OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED RT BS 280 CAP ANGLE TO FOM IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-13-001-001-A01. REMOVED AJan 4, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026040375647Bulkhead · corrodedLEFT BS 280 WEB & ASSOCIATED FASTENERS CORRODED. REMOVED AFFECTED FASTENERS FROM THE CAP ANGLE. REMOVED 5 SOLID RIVET, 1 CHERRYMAX, AND 1 VISU-LOK IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-22-001-001-A01. REMOVE CORROSION FROM LTJan 4, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026040375652Roller · chafedRIGHT HAND OUTBOARD FLAP VANE ROLLER GUIDES, CHAFED, MULTIPLE LOCATIONS. REPAIRED RIGHT HAND OUTBOARD FLAP VANE ROLLER GUIDES IAW REO 670-57-53-452 REV -.Dec 30, 2025 · N631SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2026040375644Former · corrodedWHILE ACCESSING PAX DOOR WED FOUND FWD PAX DOOR FORMER TO BE CORRODED REQUIRES REPLACEMENT. REMOVED AND REPLACED PAX DOOR FWD FORMER IAW SRM 51-42-06-001-00-A01 REV 38D, AND SRM 51-42-21-001-001-A01 REV 38D, SRM 51-40-11-001-001-A01, REV 38D.Dec 30, 2025 · N631SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026040375664Roller · out of limitsUPON REMOVAL OF THE LT SLAT TRACK 3-2 SIDE ROLLERS FOUND 3 ROLLERS IN NEED OF REPLACEMENT. REMOVED AND INSTALLED NEW SERVICEABLE LT WING SLAT TRACK 2-2 SIDE ROLLERS 3EA INTO BRACKETS IAW SRM 51-42-07-001-001-A01 AND AMM SKY WEST SUPPLEMENT SW1636DATED 5 MAY 2Dec 29, 2025 · N631SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026040375663Roller · out of limitsUPON REMOVAL OF THE LT SLAT TRACK 2-2 SIDE ROLLERS FOUND ALL FOUR ROLLERS TO BE IN NEED OF REPLACEMENT REMOVED AND INSTALLED NEW SERVICEABLE SLAT TRACK 2-2 SIDE ROLLERS 2EA INTO BRACKETS IAW SRM 51-42-07-001-001-A01 AND AMM SKYWEST SUPPLEMENT SW1636 DATED 5Dec 29, 2025 · N631SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026040375662Roller · out of limitsUPON REMOVAL OF THE LT SLAT TRACK 1-2 SIDE ROLLERS, FOUND THREE ROLLERS TO BE IN NEED OF REPLACEMENT. REMOVED AND INSTALLED NEW SERVICEABLE LT 1-2 SIDE ROLLERS INTO BRACKET IAW SRM 51-42-07-001-001-A01, AMM SW1631, AND RIL 2631 REV A.Dec 29, 2025 · N631SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025121575633Skin Panel · gougedPANEL 631BZ FOUND TO BE GOUGED. REMOVED GOUGE DAMAGE FROM PANEL 631BZ. NOMINAL THICKNESS OF 0.071", AT 2 LOCATIONS MARKED A AND B, IN THE NON CHEM MILLED AREA OF THE PANEL IAW SRM 51-12-00-001-001-A01, STEPS 7B (1-3). PERFORMED UT THICKNESS OF PANEL 631BZ REDec 15, 2025 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026030475631Doubler · unknownCOMPLY WITH SCHEDULED MAINTENANCE WIFI PCS/TIMING ANTENNA SDI 700 - COMPLY WITH INSPECTION OF THE PCS/TIMING ANTENNA SDI & DI IAW STC ST02541CH ICA DOCUMENT D12454-20110 SEC 4 (LATEST REVISION) 1. INTERNAL A/C SKIN - DOUBLER OUTER EDGE FASTENER HOLES - SDI2.Jul 3, 2025 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2025F00853Windshield · crackedL WINDSHIELD INSIDE CRACKED (FLIGHT 6516 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30361298 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH CRJ700 TASK CARD 56-220-1000-SKY (COCKPIT WINDSHIELD INSTALLATION). PRESSURIZATION CHECK GOOD."Jun 22, 2025 · N631SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2025062300022Windshield · crackedL WINDSHIELD INSIDE CRACKED (FLIGHT 6516 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJun 22, 2025 · N631SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA202266510None · odorD: AS SOON AS WE PARKED AT THE GATE FAINT SMELL OF SMOKE IN CABIN AND COCKPIT AND PACK 1 WENT TO 99 DEG C. / C: MEL 21-51-1E / CAT C EXP 9-29-22 / SMELL OF SMOKE WAS DUE TO LEFT PACK SEIZED PACK TEMP WENT TO 99C AND NO AIR COMING OUT FROM THE LEFT PACK EXHAUSep 20, 2022 · N631SK · Cndair CL6002C10 · Air Conditioning SystemSDR SWIA202265431None · leakingDURING PRESSURIZATION CHECK FOUND LEFT SIDE WINDOW TO BE LEAKING ALL AROUND WINDOW (FILED - CLOSED) REMOVED AND REPLACED LH FLIGHT COMPARTMENT WINDOW IN REFERENCE TO CRJ 900 AMM 56-12-01 AND COMPLIED WITH TASK CARD 56-220-100-SKY.Apr 18, 2022 · N631SK · Cndair CL6002C10 · Window/Windshield SystemSDR SWIA202053446Panel · crackedFWD CARGO DOOR SURROUND PANEL 151FLW CRACKED. C-CHECK RO 10/17/2020. LOCATED AND DRILLED NEW PANEL SURROUND 151FLW PN 9846201-502, REF CRJ700 SRM.Oct 11, 2020 · N631SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202053445Stiffener · crackedSTIFFENER WAS CRACKED AT FWD OF FS 280.00 RT LOWER WEB, MARKED. C-CHECK RO 10/17/2020. REMOVED, REPLACED, AND INSTALLED NEW STIFFENER AT FS 280 RT SIDE LOWER WEB, REF CRJ 700 SRM.Sep 30, 2020 · N631SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202053441Lintel · damagedCOMPLY WITH REO 670-53-21-493 REV-D DATED 2015-07-10 FOR SB 670BA-53-040. SEE JOB-71032965 OP-74 MXTRANS-21556987. C-CHECK RO 10/17/2020. COMPLIED WITH REO REPAIR TO PAX DOOR LINTEL (STG 3L) BETWEEN FS 280 AND FS 295 FOR SB SEE JOB-71032965 OP-74 MX TRANS-2Sep 30, 2020 · N631SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202053440Frame · corrodedTHERE IS EVIDENCE OF CORROSION AT FS 319.70 FRAME BETWEEN STR 18L AND STR 21L. C-CHECK RO 10/17/2020. REMOVED AND REPLACED THE CORRODED FRAME AT FS 319.70 BETWEEN STGR 18L AND STGR 21L WITH NEW FRAME (P/N SH670-31891-3S), PER BOMBARDIER DWG AND CRJ700 SRM. Sep 27, 2020 · N631SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202053439Door · crackedLT OVERWING EMERGENCY EXIT DOOR IS CRACKED, MARKED. C-CHECK RO 10/17/2020. REPAIRED LT OVERWING EMERGENCY EXIT DOOR BY CUTTING AWAY DAMAGE AND INSTALLING REPAIR PARTS, REF REO. ALL STEPS OF REO COMPLIED WITH. NO LEAKS NOTED. OPERATIONS CHECKS GOOD. COMPSep 26, 2020 · N631SK · Cndair CL6002C10 · Emergency ExitsSDR SWIA202053438Floor Support · corrodedCORROSION FOUND ON LT FLOOR SILL MACHINED ANGLE BETWEEN FS 761.85 AND FS 785.15. C-CHECK RO 10/17/2020. REPAIRED CORROSION FOUND ON LT FLOOR SILL MACHINED ANGLE BETWEEN FS 761.85 AND FS 785.15, REF CRJ700 SRM AND MHI RJ REO. ALL STEPS OF REO COMPLIED WITH ISep 22, 2020 · N631SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202053465Seat Track · corrodedCORROSION ON RT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 570.00 TO 661.00, AREAS MARKED. C-CHECK RO 10/17/2020. REPLACED RT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 573-FS 661, REF CRJ700 AMM.Sep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053464Seat Track · corrodedCORROSION ON RT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 570.00 TO 549.00, AREAS MARKED. C-CHECK RO 10/17/2020. REPLACED RT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 570.00 TO FS 549.00, REF CRJ700 AMM.Sep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053463Seat Track · corrodedCORROSION ON RT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 379.00 TO 485.00, AREAS MARKED. C-CHECK RO 10/17/2020. REMOVED UNSERVICEABLE RT SIDE SEAT RAILS AND INSTALLED NEW REPLACEMENT RT SIDE SEAT RAILS FS 349.00 TO FS 469.00 AND FS 483.00, REF CRJ700 AMM. TOSep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053462Seat Track · corrodedCORROSION ON LT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 570.00 TO 677.00, AREAS MARKED. C-CHECK RO 10/17/2020. REPLACED LT SEAT RAIL BETWEEN FS 570.00-FS 677.00, IAW CRJ700 AMM.Sep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053461Seat Track · corrodedCORROSION ON LT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 565.00 TO 570.00, AREAS MARKED. C-CHECK RO 10/17/2020. INSTALLED NEW REPLACEMENT LT SIDE SEAT RAIL, FS 483.00 TO FS 573.00, REF CRJ700 AMM. TOOL NR TUC8604, CAL: 01-JUN-20 DUE: 30-JUN-21.Sep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053460Seat Track · corrodedCORROSION ON LT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 379.00 TO 485.00, AREAS MARKED. C-CHECK RO 10/17/2020. REPLACED LT SIDE SEAT RAIL BETWEEN APPROXIMATELY FS 349.00-FS 483.00, REF CRJ700 AMM. TORQUE WRENCH TUC8612 CAL DUE 31-OCT-20.Sep 21, 2020 · N631SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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