# Service difficulty reports: N457SW

A list on [N457SW](https://openairdocs.org/aircraft/N457SW.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 · 147 reports

- [SDR SWIA2026042076115](https://openairdocs.org/sdr/SWIA2026042076115.md): Skin · corroded · Apr 20, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION FOUND AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96. PERFORMED BLEND REPAIR AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96 IAW REO 601R-53-51-740 REV--
- [SDR SWIA2026042076113](https://openairdocs.org/sdr/SWIA2026042076113.md): Skin · corroded · Apr 20, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN CORRODED BETWEEN FS 559+80 AND FS559+96 AT STRINGERS 21R AND 23R. COMPLIED WITH BLEND REPAIR TO EXTERIOR SKIN BETWEEN FS559+80 - FS559+96 AT STGR 21R AND 23R IAW REO 601R-53-51-740 REV--. COMPLETE TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026030676134](https://openairdocs.org/sdr/SWIA2026030676134.md): Window Frame · cracked · Mar 6, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Structure
  > COPILOT WINDSHIELD UPPER SILL AFT WEB HAS A CRACK LOCATED I/B OF THE RH WINDSHIELD SIDE POST. REPAIRED COPILOT WINDSHIELD UPPER SILL AFT WEB BY CUTTING AWAY DAMAGE AND REPAIRING AREA IAW REO 601R-53-11-4062 REV--. COMPLETED TASK CARD 51--900-1003-SKY.
- [SDR SWIA2026022876125](https://openairdocs.org/sdr/SWIA2026022876125.md): Intercostal · chafed · Feb 28, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT OVERWING EMERGENCY EXIT CUTOUT SURROUND INTERCOSTAL CHAFED BETWEEN FS439 TO FS449.85, STGR 9L AND STGR 10L. REMOVED AND REPLACED INTERCOSTAL LOCATED AT LH OVERWING EE CUTOUT SURROUND BETWEEN FS439-449.85 STGR9L AND 10L IAW SRM 51-42-06.
- [SDR SWIA2026022776133](https://openairdocs.org/sdr/SWIA2026022776133.md): Landing · corroded · Feb 27, 2026 · N457SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING FUEL PANEL CUTOUT LANDING UNDER 510AB CORRODED. REPAIRED CORROSION ON LH WING FUEL PANEL 510AB CUTOUT LANDING IAW REO 601R-57-21-030- REV L DATED 2014-02-05
- [SDR SWIA2026022776118](https://openairdocs.org/sdr/SWIA2026022776118.md): Landing · corroded · Feb 27, 2026 · N457SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > RH WING FUEL PANEL CUTOUT LANDING UNDER 650CB CORRODED. REPAIRED CORROSION ON RH WING FUEL PANEL 650CB LANDING IAW REO 601R-57-21-030- REV L DATED 2014-02-05. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA2026022676129](https://openairdocs.org/sdr/SWIA2026022676129.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS500 RBL 45. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT BS 500, RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11.
- [SDR SWIA2026022676128](https://openairdocs.org/sdr/SWIA2026022676128.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CABIN PRESSURE FLOOR SILL IS CORRODED AT LBL43 FS 476. REMOVED CORROSION BY BLENDING LH CABIN PRESSURE FLOOR SILL AT LBL43 FS 476 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06.
- [SDR SWIA2026022676124](https://openairdocs.org/sdr/SWIA2026022676124.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AROUND SCREW HOLE AT \RBL 45 FS520. REPAIRED RH CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 520 RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA2026022676122](https://openairdocs.org/sdr/SWIA2026022676122.md): Floorbeam · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH CABIN PRESSURE FLOOR ANGLE IS CORRODED AT FS 501 LBL 42. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 501 LBL 42 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026022676117](https://openairdocs.org/sdr/SWIA2026022676117.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH CABIN PRESSURE FLOOR SILL IS CORRODED AT FS 449.87 LBL 45. PERFORMED A MAJOR REPAIR TO THE LH PRESSURE FLOOR SILL AT FS 449.87 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06
- [SDR SWIA2026022676116](https://openairdocs.org/sdr/SWIA2026022676116.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS518 LBL 45. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 518 LBL 45 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06.
- [SDR SWIA2026022676112](https://openairdocs.org/sdr/SWIA2026022676112.md): Floor Support · corroded · Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS506 RBL 42. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 506 RBL 42 IAW MHIRJ REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED
- [SDR SWIA2026022476135](https://openairdocs.org/sdr/SWIA2026022476135.md): Frame · corroded · Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME IS CORRODED AT STGR 23R. INSTALLED NEW SERVICEABLE RH LOWER FRAME SEGMENT OF BS 333 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026022476131](https://openairdocs.org/sdr/SWIA2026022476131.md): Frame · corroded · Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 319 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 25R. REPLACED FS 319 FRAME SECTOR FROM STGR 23L-23R IAW SRM 51-42-06 AND 51-42-21.
- [SDR SWIA2026022476130](https://openairdocs.org/sdr/SWIA2026022476130.md): Intercostal · corroded · Feb 24, 2026 · N457SW · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26R. REPLACED AVI DOOR INTERCOSTAL PN:601R31049-10 IAW SRM 51-42-06 AND 51-42-21.
- [SDR SWIA2026022476119](https://openairdocs.org/sdr/SWIA2026022476119.md): Frame · corroded · Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 333 FRAME IS CORRODED BETWEEN STGR 20L TO STGR 21L. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FS 333 LH SIDE FRAME SEGMENT IAW SRM 51-40-11, 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026022476114](https://openairdocs.org/sdr/SWIA2026022476114.md): Stringer · corroded · Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR 23R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. UPON FURTHER INVESTIGATION FOUND CORROSION TO BE ON FS333 SPLICE STRAP AND STGR23R LAP JOINT. COMPLIED WITH BLEND REPAIR TO FS333 SPLICE STRAP AND STGR23R LAP JOINT IAW MHIRJ REO 601R-53-21-3803 REV --. COM
- [SDR SWIA2026022376138](https://openairdocs.org/sdr/SWIA2026022376138.md): Skin · corroded · Feb 23, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN CORRODED IN SEVERAL AREAS FS559+80 TO FS559+112 STRINGER 26L TO 26R. PERFORMED REPAIR BY BLENDING CORROSION IAW REO 601R-53-51-734 REV-A DATED 2026-04-23.
- [SDR SWIA2026022376132](https://openairdocs.org/sdr/SWIA2026022376132.md): Skin · chafed · Feb 23, 2026 · N457SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT LOWER WING PLANK IS CHAFED AT RBL45. COMPLIED WITH REPAIR TO LOWER WING PLANK CHAFE AT RBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.
- [SDR SWIA2026022376121](https://openairdocs.org/sdr/SWIA2026022376121.md): Skin · chafed · Feb 23, 2026 · N457SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK IS CHAFED AT LBL45. COMPLIED WITH BLEND REPAIR TO LOWER WING PLANK CHAFE AT LBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.
- [SDR SWIA2026021776126](https://openairdocs.org/sdr/SWIA2026021776126.md): Hinge Fitting · gouged · Feb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON THE FUSELAGE SIDE 11TH, 13TH, 14TH LUGS FROM FWD SIDE OF HINGE ARE GOUGED. REPLACED PAX DOOR HINGE ON THE FUSELAGE SIDE IAW SRM 53-21-23 AND REO 601R-53-21-656 REV--DATED 2024-03-15. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026021776123](https://openairdocs.org/sdr/SWIA2026021776123.md): Pan · corroded · Feb 17, 2026 · N457SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR LOWER PAN IS CORRODED. INSTALLED NEW SERVICEABLE SERVICE DOOR PAN P/N:601R38437-2 IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026021776120](https://openairdocs.org/sdr/SWIA2026021776120.md): Hinge · gouged · Feb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON THE DOOR SIDE 11TH, 12TH, 13TH, 16TH LUG LANDINGS FROM FWD SIDE OF HINGE ARE GOUGED. REMOVED UNSERVICEABLE PAX DOOR HINGE ON THE DOOR SIDE AND REPLACED WITH A SERVICEABLE HINGE IAW SRM 52-10-31. C
- [SDR SWIA2026020176127](https://openairdocs.org/sdr/SWIA2026020176127.md): Post · failed insp · Feb 1, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS409+128 BL0 VERTICAL POST RH & LH SIDES HAVE INDICATIONS: LH IS 60% FSH.3? LONG, AND RH IS 50% FSH.3? LONG IN THE AFT RADIUS OF POST @ WL69. FAILED NDT INSPECTION. INSTALLED NEW SERVICEABLE BL0 VERTICAL POST LH AND RH ANGLES AND LH/RH STIFFENERS AT FS 40
- [SDR SWIA2026012476136](https://openairdocs.org/sdr/SWIA2026012476136.md): Skin · chafed · Jan 24, 2026 · N457SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STAB UPPER SURFACE RBL 6.0 APPROXIMATELY 4 INCHES FROM FWD EDGE THERE ARE 2 CHAFES, ONE ON SUPPORT ANGLE FOR FAIRING AND ONE ON SPLICE DOUBLER. PERFORMED BLEND OUT AND DOUBLER REPAIR TO HORIZONTAL STAB UPPER SURFACE RBL6.0 IAW MHIRJ REO 601R-55-822
- [SDR SWIA2025092476137](https://openairdocs.org/sdr/SWIA2025092476137.md): Floor Panel · corroded · Sep 24, 2025 · N457SW · Cndair CL6002B19 · Fuselage Floor Panel
  > THE LH PRESSURE FLOOR PANEL BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION. REPAIRED LT PRESSURE FLOOR PANEL BETWEEN FS 409+128 AND FS 559 REF REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH 51-900-1003-SKY DETAILED VISUAL INSPECT BLEN
- [SDR SWIA2025F01361](https://openairdocs.org/sdr/SWIA2025F01361.md): Attach Fitting · gouged · Aug 1, 2025 · N457SW · Cndair CL6002B19 · Wing, Fuselage Attach Fittings
  > L/H WING AFT ATTACHMENT FITTING AT WS264.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00603) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON L/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS264.0 AT I/B AND O/B CENTER LUGS. REF. CRJ200 S
- [SDR SWIA202266947](https://openairdocs.org/sdr/SWIA202266947.md): Skin · damaged · Nov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REMOVE AND REPLACE LEFTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-51S (C-CHECK) REMOVED AND REPLACED LH INBD FLAP VANE SKIN PANEL P/N 601R14303-51S REF DWG #PL601R14302 REV.E AND CRJ 200 SRM 51-42-13 REV.39 DATED MAR-10-2021. COMPLIED WITH TASK CA
- [SDR SWIA202266946](https://openairdocs.org/sdr/SWIA202266946.md): Skin · damaged · Nov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-54S (C-CHECK) REMOVED AND INSTALLED NEW SKIN PANEL P/N: 601R14303-54S AT RIGHTHAND INBOARD FLAP VANE REF CRJ200 SRM 51-42-13 AND DWG# PL601R14302 REV E, COMPLIED WITH TASKCARD 51-
- [SDR SWIA202266945](https://openairdocs.org/sdr/SWIA202266945.md): Skin · worn · Nov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-52S (C-CHECK RO 12/1/2022) REMOVED WORN LEADING EDGE VANE CAP AND INSTALLED NEW R/H MID FLAP VANE SKIN P/N: 601R14303-52. REF: CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV. E. COMPLI
- [SDR SWIA202266944](https://openairdocs.org/sdr/SWIA202266944.md): Support Bracket · cracked · Nov 6, 2022 · N457SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET IS CRACKED (C-CHECK RO 12/1/2022) REMOVED AND INSTALLED NEW AFT CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET ASSY REF DWG # 601R35050 REV AC, REF CRJ200 SRM 51-42-06, SRM 51-41-02. COMPLIED WITH 51-900-1003-S
- [SDR SWIA202265258](https://openairdocs.org/sdr/SWIA202265258.md): None · failed · Mar 31, 2022 · N457SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > L MAIN AND R MAIN DID NOT COME DOWN WHEN LANDING GEAR WERE LOWERED ON APPROACH. THE F/A HEARD A BANG OR POP FOLLOWED BY A GRINDING SOUND ON TAKEOFF/DEPARTURE. SHE INFORMED US OF THIS AT 10,000 FEET OUT OF STERILE COCKPIT. WITH NO ABNORMAL MESSAGES OR PRESSURIZ
- [SDR SWIA202265257](https://openairdocs.org/sdr/SWIA202265257.md): None · failed · Mar 31, 2022 · N457SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > L MAIN AND R MAIN DID NOT COME DOWN WHEN LANDING GEAR WERE LOWERED ON APPROACH. THE F/A HEARD A BANG OR POP FOLLOWED BY A GRINDING SOUND ON TAKEOFF/DEPARTURE. SHE INFORMED US OF THIS AT 10,000 FEET OUT OF STERILE COCKPIT. WITH NO ABNORMAL MESSAGES OR PRESSURIZ
- [SDR SWIA202161607](https://openairdocs.org/sdr/SWIA202161607.md): Sensor · obstructed · Oct 5, 2021 · N457SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > PERFROM FULL FLAP FAIL AD 2009-06-12 WITH IN 10 FC DUE TO FLAPS FAILED AT 20 ON ARRIVAL. C:MCI / DUE TAC 34821, FLAPS FAILED AT 20 ON ARRIVAL. CLOSED RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SER
- [SDR SWIA2019102346557](https://openairdocs.org/sdr/SWIA2019102346557.md): Frame · corroded · Oct 22, 2019 · N457SW · Cndair CL6002B19 · Fuselage Main, Frame
  > L/H FUSELAGE FRAME HAS CORROSION ON UPPER SURFACE, JUST ABOVE FLOOR LEVEL. (C-CHECK) RO: 10/20. COMPLIED WITH STRUCTURAL MAJOR REPAIR.
- [SDR SWIA2018091845080](https://openairdocs.org/sdr/SWIA2018091845080.md): Actuator · failed · Sep 18, 2018 · N457SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > GEAR DISAGREE WARNING AFTER PUTTING GEAR DOWN FOR LANDING. (FLT 7438) CLOSED REMOVED AND REPLACED NLG DOOR ACTUATOR IAW AMM. PERFORMED GEAR SWINGS AND EMERGENCY EXTENSION CHECK IAW AMM. OPS CHECK GOOD.
- [SDR SWIA2018061544781](https://openairdocs.org/sdr/SWIA2018061544781.md): Engine · failed · Jun 15, 2018 · N457SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LOST RIGHT ENGINE RESPONSE JUST OUTSIDE OF THE FINAL APPROACH FIX WHEN RIGHT THRUST LEVER WAS ADVANCED. RIGHT ENGINE SPOOLED DOWN AND ITT WENT RED. ACCOMPLISHED ENGINE SHUTDOWN IN FLIGHT. (FLT 7423) 06/15/2018 CLOSED REMOVED AND REPLACED RT ENGINE. OPS AND LEA
- [SDR SWIA2017100243806](https://openairdocs.org/sdr/SWIA2017100243806.md): Pressure Deck · corroded · Aug 27, 2017 · N457SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT PRESSURE FLOOR BS 520 HAS CORROSION. REMOVED THE CORROSION IAW REO AND SRM.
- [SDR SWIA2017100243805](https://openairdocs.org/sdr/SWIA2017100243805.md): Skin · chafed · Aug 24, 2017 · N457SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LOWER LEADING EDGE SKIN CHAFED INBD OF CENTER HINGES. REMOVED AND REPLACED THE AILERON LOWER LEADING EDGE SKIN PANEL IAW SRM.
- [SDR SWIA2017100243804](https://openairdocs.org/sdr/SWIA2017100243804.md): Vane · chafed · Aug 23, 2017 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE SKIN LEADING EDGE CHAFED. REMOVED AND REPLACED THE RT INBD FLAP LEADING EDGE VANE IAW SRM.
- [SDR SWIA2017100243803](https://openairdocs.org/sdr/SWIA2017100243803.md): Vane · chafed · Aug 23, 2017 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE SKIN LEADING EDGE HAS TWO CHAFED AREAS. REMOVED AND REPLACED THE LT INBD FLAP, OTBD SIDE LEADING EDGE VANES IAW SRM.
- [SDR SWIA201439675](https://openairdocs.org/sdr/SWIA201439675.md): Adg · unwanted deploy · Oct 26, 2014 · N457SW · Cndair CL6002B19 · AC Generation System
  > ADG DEPLOYED ON WEIGHT OFF WHEELS. ALL OTHER SYSTEMS NORMAL. COMPLIED WITH INSPECTION AFTER ADG - INFLIGHT DEPLOYMENT IAW AMM. INSPECTION CK GOOD. ADG AUTO DEPLOYMENT PANEL FAILED OPS CK. R & R ADG AUTO DEPLOYMENT CONTROL PANEL IAW AMM. OPS CK OF ADG AUT
- [SDR SWIA201439484](https://openairdocs.org/sdr/SWIA201439484.md): Element · broken · Oct 12, 2014 · N457SW · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI-ICE DUCT WARNING 1000' AFTER T/O. RAN QRH, MSG PERSISTED FOR 15 MIN THEN WENT OUT. RETURN TO FIELD. SHUTDOWN LT ENGINE TAXIING IN, LT FUSELAGE ANTI-ICE DUCT MSG RETURNED. R & R BROKEN SENSING ELEMENT IN THE LT WHEEL WELL IAW AMM, PN 35548-3-255.
- [SDR SWIA201439239](https://openairdocs.org/sdr/SWIA201439239.md): Smoke Detector · no test · Sep 1, 2014 · N457SW · Cndair CL6002B19 · Smoke Detection
  > CARGO BOTTLE, TEST 2 INOPERATIVE. NO MASTER WARNING, RED "SMOKE CARGO" EICAS ANNUNCIATION, OR CARGO SMOKE PUSH BUTTON LIGHTS ON FIRE EXTINGUISHER CONTROL PANEL. SQUIB CHECKS GOOD. R & R CARGO SMOKE DETECTOR 2 IAW AMM. CARGO SMOKE DETECTION SYSTEM, OPS CHECK
- [SDR SWIA201438459](https://openairdocs.org/sdr/SWIA201438459.md): Window · cracked · Jun 27, 2014 · N457SW · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN'S SIDE WINDOW CRACKED CLIMBING OUT OF 7,000-8,000'. R & R SIDE WINDOW IAW AMM. PN ON: NP-139322-11, SN ON:13213H4868, PN OFF: NP-139322-001, SN OFF: 02329H1945.
- [SDR SWIA201436640](https://openairdocs.org/sdr/SWIA201436640.md): Battery · discharged · Mar 7, 2014 · N457SW · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT BY EXIT DOES NOT ILLUMINATE. SERVICE REPLACED THE NR 2 EMERGENCY BATTERY ASSEMBLY, PN AD-2013-1A, SN ON 69013 & SN OFF 50481.
- [SDR SWIA201435846](https://openairdocs.org/sdr/SWIA201435846.md): Uplock · failed · Jan 4, 2014 · N457SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE AFTER RETRACTING THE GEAR. AFTER QRH PROCEDURE, GEAR INDICATED DOWN, 3 GREEN. FLT 4760 REPLACED LT MLG UPLOCK ASSEMBLY IAW AMM. SWUNG GEAR, PERFORMED EMERGENCY EXTENSION & CONSECUTIVE SWINGS, OPERATIONS CHECKED GOOD.
- [SDR SWIA201335152](https://openairdocs.org/sdr/SWIA201335152.md): Door · chafed · Oct 26, 2013 · N457SW · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG DOOR CHAFED ON LE CORNER. C-CHECK REPAIRED MLG DOOR RT IAW REO.
- [SDR SWIA201335153](https://openairdocs.org/sdr/SWIA201335153.md): Flap · dented · Oct 21, 2013 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP DENTED APPROXIMATELY 11 INCHES FROM OTBD EDGE ON THE TE. C-CHECK REPAIRED LT INBD FLAP BY REPLACING TE STRIP IAW SHORTS DRAWING.

Next page: https://openairdocs.org/aircraft/N457SW/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 = 'N457SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N457SW/reports

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