# Service difficulty reports: N594SW, cancelled Feb 16, 2023 A list on [N594SW, cancelled Feb 16, 2023](https://openairdocs.org/deregistered/N594SW-2023-02-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 115 reports - [SDR SWIA202156492](https://openairdocs.org/sdr/SWIA202156492.md): Sensor · out of rig · Mar 1, 2021 · N594SW · Cndair CL6002B19 · Landing Gear Position and Warning > D:ON TAKE OFF RETRACTED LANDING GEAR. AFTER 10 SECONDS RECEIVED NOSE DOOR OPEN WARNING MSG FOLLOWED BY GEAR DISAGREE WARNING MSG. MAIN GEAR WERE INDICATING UP AND WHITE. NOSE INDICATING DOWN AND RED. FOLLOWED QRH PROCEDURES. MANUAL RELEASE HANDLE WAS PULLED AN - [SDR SWIA202154936](https://openairdocs.org/sdr/SWIA202154936.md): Unknown · smoke · Jan 4, 2021 · N594SW · Cndair CL6002B19 · Air Distribution System > ON THE LANDING ROLLOUT WITH THRUST REVERSERS AT IDLE, SMOKE OBSERVED OUTSIDE OF AIRCRAFT COMING FORWARD AND WITH THE SMELL OF BURNING RUBBER IN THE FLIGHT DECK. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22074262 WITH THE FOLLOWING CORRECTIVE ACTION: "INSP - [SDR SWIA2020082451970](https://openairdocs.org/sdr/SWIA2020082451970.md): Support Bracket · cracked · Aug 24, 2020 · N594SW · Cndair CL6002B19 · Cargo/Baggage Doors > CARGO DOOR FWD RAIL TOP SUPPORT BRACKET CRACKED. REPLACED CARGO DOOR FWD RAIL TOP SUPPORT BRACKET IN REFERENCE TO CRJ 200 SRM. - [SDR SWIA2019092546336](https://openairdocs.org/sdr/SWIA2019092546336.md): Warning System · false activation · Sep 23, 2019 · N594SW · Cndair CL6002B19 · Landing Gear Position and Warning > GEAR DISAGREE WARNING MESSAGE DURING GEAR EXTENSION ON LANDING. COMPLIED WITH QRH. MANUAL GEAR EXTENSION REQUIRED. (FLT#3134) CLOSED PERFORMED FUNCTION CHECK OF MLG EXTENSION AND RETRACTION, AND PERFORMED GEAR DISAGREE OPS CHECK IAW AMM. FUNCTION AND OPS CHECK - [SDR SWIA2019051745898](https://openairdocs.org/sdr/SWIA2019051745898.md): Bulkhead · damaged · May 4, 2019 · N594SW · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621.00 BULKHEAD DAMAGED. (C-CHECK) RO: 05/16/2019 REPAIRED DAMAGE IAW REO. LEAK CHECK GOOD. - [SDR SWIA2019051745897](https://openairdocs.org/sdr/SWIA2019051745897.md): Angle · cracked · Apr 28, 2019 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CRACK LOCATED AT FS621.00 BETWEEN LBL 36 TO LBL 42. (C-CHECK) RO: 05/16/2019 REMOVED AND INSTALLED NEW ANGLE P/N 601R-53-61-117-1 AT FS621 BETWEEN LBL36 - LBL42 IAW REO. - [SDR SWIA2019051745896](https://openairdocs.org/sdr/SWIA2019051745896.md): Support Angle · corroded · Apr 21, 2019 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE CORREDED. (C-CHECK) RO: 05/16/2019 REMOVED AND INSTALLED NEW PAX DOOR SILL LOWER FLOOR SUPPORT ANGLE ASSY. P/N: 601R31527-221 IAW SRM. - [SDR SWIA2019051745895](https://openairdocs.org/sdr/SWIA2019051745895.md): Drag Angle · damaged · Apr 15, 2019 · N594SW · Cndair CL6002B19 · Aerodynamic Fairings > TAILCONE DRAG ANGLE HAS 5 ELONGATED FASTENER HOLES. (C-CHECK) RO: 05/16/2019 REPAIRED TAILCONE DRAG ANGLE 5 ELONGATED FASTENER HOLES IAW REO. - [SDR SWIA2019051745894](https://openairdocs.org/sdr/SWIA2019051745894.md): Bulkhead · damaged · Apr 14, 2019 · N594SW · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS621 PRESSURE BULKHEAD HAS DAMAGE. (C-CHECK) RO: 05/16/2019 REPAIRED THE FS621 PRESSURE BULKHEAD IAW REO. LEAK CHECK GOOD. - [SDR SWIA2019051745901](https://openairdocs.org/sdr/SWIA2019051745901.md): Door Sill · corroded · Apr 13, 2019 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LEFT HAND FLOOR SILL IN AFT CARGO COMPARTMENT HAS CORROSION AROUND SCREW HOLE FROM APPROX FS 559+80 TO FS 621. (C-CHECK) RO: 05/16/2019 REPLACED LT FLOOR SILL IAW SRM. - [SDR SWIA2019051745900](https://openairdocs.org/sdr/SWIA2019051745900.md): Door Sill · corroded · Apr 13, 2019 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RIGHT HAND FLOOR SILL IN AFT CARGO COMPARTMENT HAS CORROSION AROUND SCREW HOLE FROM APPROX FS 589 TO FS 621. (C-CHECK) RO: 05/16/2019 REMOVED AND REPLACED THE RT CARGO FLOOR SILL IAW REO. ALL CHECKS GOOD - [SDR SWIA2019051745899](https://openairdocs.org/sdr/SWIA2019051745899.md): Frame · corroded · Apr 11, 2019 · N594SW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 349.00 UPPER AND LOWER FLANGES ARE CORRODED BETWEEN STGR25L - 26R. (C-CHECK) RO: 05/16/2019 REMOVED CORROSION ON FRAME 349.00 UPPER AND LOWER FLANGES BETWEEN STGR25L - 26R IAW REO AND SRM. - [SDR SWIA2019051745893](https://openairdocs.org/sdr/SWIA2019051745893.md): Skin · dented · Apr 1, 2019 · N594SW · Cndair CL6002B19 · Passenger/Crew Doors > 2 DENTS LOCATED ON MCD SKIN 4.830" AFT OF FWD LEADING EDGE AND 8.480" FROM TOP EDGE AND 14.5" FWD OF MCD AFT EDGE AND 26.2" FROM MCD TOP EDGE. (C-CHECK) RO: 05/16/2019 COMPLIED WITH REO REPAIR FOR TWO EACH DENTS ON THE PAX DOOR OUTER SKIN. LEAK CHECK GOOD. - [SDR SWIA201743229](https://openairdocs.org/sdr/SWIA201743229.md): Mount · corroded · Apr 5, 2017 · N594SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > EVIDENCE OF CORROSION ON FWD CLOSET MOUNT UNDER FLOOR PANEL 231CLF. REMOVED AND REPLACED THE MOUNT IAW SRM. - [SDR SWIA201743228](https://openairdocs.org/sdr/SWIA201743228.md): Mount · corroded · Apr 5, 2017 · N594SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > CLOSET MOUNT CORRODED UNDER 231BLF FLOOR PANEL. REMOVED AND REPLACED THE MOUNT IAW SRM. - [SDR SWIA201743227](https://openairdocs.org/sdr/SWIA201743227.md): Doubler · corroded · Apr 1, 2017 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SSUPPORT LIPPED DOUBLER PLATE FROM BS 559+96 TO 559+112 HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED A NEW THE FLOOR SUPPORT LIPPED DOUBLER PLATE IAW SRM. - [SDR SWIA201743226](https://openairdocs.org/sdr/SWIA201743226.md): Floor Support · corroded · Apr 1, 2017 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SSUPPORT JUST AFT AF BS 559 IS CORRODED. REPAIRED IAW REO AND SRM. - [SDR SWIA201743225](https://openairdocs.org/sdr/SWIA201743225.md): Skin · chafed · Mar 29, 2017 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBOARD FLAP VANE L/E SKIN CHAFED AT CENTER SECTION. REMOVED AND REPLACED THE LT INBOARD FLAP VANE CENTER VANE CAP IAW SRM AND AMM. - [SDR SWIA201743224](https://openairdocs.org/sdr/SWIA201743224.md): Frame · corroded · Mar 28, 2017 · N594SW · Cndair CL6002B19 · Fuselage Main, Frame > AFT FUSELAGE INTERNAL FRAME BS 559+112 BETWEEN STRINGERS 26L AND 26R HAS CORROSION. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM. - [SDR SWIA201743223](https://openairdocs.org/sdr/SWIA201743223.md): Panel · corroded · Mar 27, 2017 · N594SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > GALLEY FLOOR PROTECTOR PANEL UNDER THE SERVICE DOOR HAS CORROSION. INSTALLED NEW GALLEY FLOOR PROTECTOR PLATE IAW SRM. - [SDR SWIA201743222](https://openairdocs.org/sdr/SWIA201743222.md): Structure · dented · Mar 25, 2017 · N594SW · Cndair CL6002B19 · Fuselage Main, Structure > SMALL DENT APROXIMATELY 2 INCHES AFT OF BS 589+29, BELOW CARGO DOOR. COMPLIED WITH ALL STEPS OF REPAIR IAW REO. - [SDR SWIA201642270](https://openairdocs.org/sdr/SWIA201642270.md): Unknown · failed · Jun 27, 2016 · N594SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > GEAR DISAGREE, ON TAKEOFF. RIGHT GEAR WAS YELLOW, THEN RED, WHEN NOSE AND LT SHOWED UP AND WHITE. REMOVED AND REPLACED THE RT MLG WHEEL BIN IAW AMM. OPS CHECK GOOD. - [SDR SWIA201541650](https://openairdocs.org/sdr/SWIA201541650.md): Hydraulic System · malfunctioned · Nov 30, 2015 · N594SW · Cndair CL6002B19 · Hydraulic System, Main > HYD SYS 3 LOW CAUTION MESSAGE ON GEAR RETRACTION, HAD GEAR DISAGREE, THEN STARTING SHOWING 100 PERCENT QUANTITY AND 3200 PSI. RETURNED TO FIELD. BLED NR 3 HYDRAULICS SYSTEM, PERFORMED MULTIPLE EXTENSION/RETRACTION AND MANUAL EXTENSION OPS CHECK OF THE GEAR G - [SDR SWIA201439773](https://openairdocs.org/sdr/SWIA201439773.md): Bulkhead · corroded · Oct 27, 2014 · N594SW · Cndair CL6002B19 · Fuselage Main, Bulkhead > BULKHEAD FOUND CORRODED. C-CHECK, REMOVED CORRODED MATERIAL AND REPAIRED LAV 9G BULKHEAD IAW EA. - [SDR SWIA201439769](https://openairdocs.org/sdr/SWIA201439769.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. C-CHECK BLENDED OUT CHAFING ON RT WING INBD FLAP VANE OTBD L/E SKIN IAW REO. - [SDR SWIA201439768](https://openairdocs.org/sdr/SWIA201439768.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E CHAFED AT INBD POSITION. C-CHECK, BLENDED OUT CHAFING ON RT INBD FLAP VANE INBD L/E SKIN IAW REO. - [SDR SWIA201439767](https://openairdocs.org/sdr/SWIA201439767.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E CHAFED AT CTR POSITION. C-CHECK, BLENDED OUT CHAFING ON RT WING INBD FLAP VANE MID OTBD L/E SKIN IAW REO. - [SDR SWIA201439754](https://openairdocs.org/sdr/SWIA201439754.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP VANE L/E CHAFED AT OTBD POSITION. C-CHECK, BLENDED OUT CHAFING ON LT WING INBD FLAP VANE OTBD L/E SKIN. ORIGINAL MATERIAL THICKNESS AT REWORKED AREA IS 0.050" IAW SRM AND REO. - [SDR SWIA201439753](https://openairdocs.org/sdr/SWIA201439753.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > LT INBD FLAP VANE L/E CHAFED AT INBD POSITION. C-CHECK, BLENDED OUT CHAFING ON LT WING INBD FLAP VANE INBD L/E SKIN IAW SRM AND REO. - [SDR SWIA201439752](https://openairdocs.org/sdr/SWIA201439752.md): Vane · chafed · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Trailing Edge Flaps > LT INBD FLAP VANE L/E CHAFED AT CENTER POSITION. C-CHECK BLENDED OUT CHAFING ON LT WING INBD FLAP VANE MID OTBD L/E SKIN IAW REO. - [SDR SWIA201439751](https://openairdocs.org/sdr/SWIA201439751.md): Access Panel · damaged · Oct 25, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > FUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTED, INBD & OTBD ENDS. C-CHECK, FUEL TANK ACCESS PANEL 540BB CLAMP RING FRETTING REPAIRED IAW REO. - [SDR SWIA201439772](https://openairdocs.org/sdr/SWIA201439772.md): Panel · out of tolerance · Oct 23, 2014 · N594SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin > THE UPPER RT HORIZONTAL STABILIZER VISOR PANEL 326AR FAILED ITS GAP CHECK. C-CHECK, R & R NEW VISOR PANEL 326AR IAW REO C. - [SDR SWIA201439771](https://openairdocs.org/sdr/SWIA201439771.md): Panel · failed · Oct 23, 2014 · N594SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin > THE LOWER RT HORIZONTAL STABILIZER VISOR PANEL 326BR FAILED ITS GAP CHECK. C-CHECK, R & R NEW VISOR PANEL 326BR IAW REO. - [SDR SWIA201439770](https://openairdocs.org/sdr/SWIA201439770.md): Panel · out of tolerance · Oct 23, 2014 · N594SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin > THE LOWER LT HORIZONTAL STABILIZER VISOR PANEL 326BL FAILED ITS GAP CHECK. C-CHECK, RECONTOURED VISOR PANEL 326BL IAW REO. - [SDR SWIA201439757](https://openairdocs.org/sdr/SWIA201439757.md): Structure · damaged · Oct 23, 2014 · N594SW · Cndair CL6002B19 · Wing Main, Frame Structure > LEFT WING TIP EXTENSION HAS COMPOSITE DAMAGE ON UPPER T/E. C-CHECK, REPAIRED LT WING TIP EXTENSION AT UPPER T/E IAW REO AND SRM. - [SDR SWIA201439765](https://openairdocs.org/sdr/SWIA201439765.md): Skin · damaged · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640CT HAS FRETTING. C-CHECK, FRETTING TO RT UPPER WING SKIN AT PANEL 640CT REPAIRED IAW EA. - [SDR SWIA201439764](https://openairdocs.org/sdr/SWIA201439764.md): Skin · damaged · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640BT HAS FRETTING. C-CHECK FRETTING TO RT UPPER WING SKIN AT PANEL 640BT REPAIRED IAW EA. - [SDR SWIA201439763](https://openairdocs.org/sdr/SWIA201439763.md): Skin · damaged · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING UPPER SKIN MATING SURFACE FOR PANEL 640AT HAS FRETTING. C-CHECK, FRETTING TO RT UPPER WING SKIN AT PANEL 640AT REPAIRED IAW EA. - [SDR SWIA201439762](https://openairdocs.org/sdr/SWIA201439762.md): Panel · damaged · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING LOWER SURFACE HAS FRETTING ON MATING SURFACE FOR PANEL 650KB. C-CHECK, BLENDED OUT DAMAGED AREAS TO A SMOOTH CONTOUR ON LANDINGS OF PANEL 650KB, RT SIDE IAW REO. - [SDR SWIA201439761](https://openairdocs.org/sdr/SWIA201439761.md): Panel · chafed · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > LT WING PANEL 699CB IS CHAFED. C-CHECK, LT WING PANEL 699CB CHAFED REPAIRED IAW REO. - [SDR SWIA201439760](https://openairdocs.org/sdr/SWIA201439760.md): Panel · chafed · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > LT WING PANEL 699BB CHAFED. C-CHECK, LT WING PANEL 699BB CHAFED, REPAIRED IAW REO. - [SDR SWIA201439759](https://openairdocs.org/sdr/SWIA201439759.md): Panel · chafed · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > LT WING PANEL 699AB CHAFED. C-CHECK, LT WING PANEL 699AB CHAFED, REPAIRED IAW REO. - [SDR SWIA201439758](https://openairdocs.org/sdr/SWIA201439758.md): Panel · damaged · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > RT WING PANEL 640CT HAS FRETTING ON MATING SURFACE. C-CHECK, REPLACED PANEL 640CT WITH FABRICATED PANEL, PN 600-10003-37 IAW STS EA. - [SDR SWIA201439756](https://openairdocs.org/sdr/SWIA201439756.md): Panel · chafed · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > LEFT WING PANEL 599CB IS CHAFED. C-CHECK LT WING PANEL 599CB CHAFES REPAIRED IAW REO. - [SDR SWIA201439755](https://openairdocs.org/sdr/SWIA201439755.md): Panel · chafed · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Wing, Plate/Skin > LEFT WING PANEL 599BB IS CHAFED. C-CHECK LT WING PANEL 599BB CHAFES REPAIRED IAW REO. - [SDR SWIA201439750](https://openairdocs.org/sdr/SWIA201439750.md): Drain Mast · cracked · Oct 22, 2014 · N594SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame > CORE COWL 445AB DRAIN MAST CRACKED. C-CHECK, REPAIRED CRACK IN DRAIN MAST ON PANEL 445AB IAW EA. - [SDR SWIA201439766](https://openairdocs.org/sdr/SWIA201439766.md): Tube · damaged · Oct 21, 2014 · N594SW · Cndair CL6002B19 · Service Doors > SERVICE DOOR HARNESS CONVOLEX TUBING DAMAGED. C-CHECK, REPLACED THE SERVICE DOOR HARNESS CONVOLEX TUBING IAW REO. - [SDR SWIA201437651](https://openairdocs.org/sdr/SWIA201437651.md): Charger · inoperative · May 20, 2014 · N594SW · Cndair CL6002B19 · Emergency Lighting > FLOOR EMERGENCY LIGHTS AFT OF ROW 8 DO NOT ILLUMINATE. REPLACED BATTERY CHARGER ASSEMBLY IAW AMM. - [SDR SWIA201435932](https://openairdocs.org/sdr/SWIA201435932.md): Light · inoperative · Jan 9, 2014 · N594SW · Cndair CL6002B19 · Emergency Lighting > MAIN CABIN DOOR LOWER EMERGENCY LIGHT SINGLE BULB IS BURNED OUT. FLT 6481 RELAMPED. - [SDR SWIA201335509](https://openairdocs.org/sdr/SWIA201335509.md): Light · malfunctioned · Dec 6, 2013 · N594SW · Cndair CL6002B19 · Passenger Compartment Lighting > SMOKE COMING FROM SIDE WALL LIGHTS AT 7A. FLT 3475 REPLACED LIGHT FIXTURE AT SEAT 7A, IAW AMM. PN BC1-0065-003 Next page: https://openairdocs.org/deregistered/N594SW-2023-02-16/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N594SW' AND deregistration_id = 'N594SW-2023-02-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N594SW-2023-02-16/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.