# Service difficulty reports: N487CA A list on [N487CA](https://openairdocs.org/aircraft/N487CA.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 5 · 219 reports - [SDR SWIA2026092977284](https://openairdocs.org/sdr/SWIA2026092977284.md): Windshield · cracked · Sep 29, 2026 · N487CA · Cndair CL6002B19 · Flight Compartment Windows > RIGHT WINDSHIELD DEVELOPED A CRACK AT FL 220 AFTER A RT WINDSHIELD HEAT MESSAGE. FLIGHT 5128. REMOVED AND REPLACED THE FO WINDSHIELD IAW AMM 56-11-01 AND COMPLIED WITH STEPS 1-10 OF MIP TASK CARD 56-220-1000-SKY. - [SDR SWI2025F00183](https://openairdocs.org/sdr/SWI2025F00183.md): Hinge Fitting · damaged · Jan 9, 2025 · N487CA · Cndair CL6002B19 · Rudder Structure > AFTER RUDDER LOWER CENTER HINGE REMOVAL, FOUND PREVIOUS DAMAGE AROUND FASTENERS HOLES (2EA) ON FITTING ONLY. (C-CHECK RO 2/27/2025) REPLACED WITH NEW RUDDER LOWER CENTER HINGE FITTING PER RIL # 0602 REV J TYPE IV DATE 21-SEP-2019 AND REO 601R-55-31-471 - [SDR SWI2025F00182](https://openairdocs.org/sdr/SWI2025F00182.md): Floor Support · corroded · Jan 9, 2025 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION NOTED AT R/H FLOOR SILL AT APPROX. FS310-FS319 NEXT TO FWD GALLEY MOUNTING ANGLE (NUTPLATE HOLE) MX# 29445766 (C-CHECK RO 2/27/2025) REPLACED RH FLOOR SILL P/N: 601R31148-79 AT APPROX. FS310 - FS319 REF CRJ200 SRM 51-42-06,CRJ 200 SRM 51-42-1 - [SDR SWI2025F00184](https://openairdocs.org/sdr/SWI2025F00184.md): Stringer · cracked · Jan 8, 2025 · N487CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FS379.00 STRG 3LH, STRINGER CRACKED AT THE LINTEL ATTACH (MARKED) (C-CHECK RO 2/27/2025) REPAIRED CRACK IN STGR 3L AT F.S. 379.00 WITH A STRINGER SPLICE REPAIR PER MHIRJ REO 601R-53-21-3716 REV -- DATED 2025-01-14 AND CRJ 200 SRM 53-00-03. COMPLIED WITH - [SDR SWIA20250228108](https://openairdocs.org/sdr/SWIA20250228108.md): Stringer · cracked · Jan 8, 2025 · N487CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FS280.00 STRG 3LH, STRINGER CRACKED AT THE LINTEL ATTACH (MARKED) (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW STRINGER LINTEL ATTACH ANGLE AT FS280.00 STGR3L PER CRJ200SRM 51-42-06, CRJ200SRM 51-42-21, AND DWG 600-31057 REV P. LEAK CHECK GOOD. - [SDR SWI2025F00187](https://openairdocs.org/sdr/SWI2025F00187.md): Frame · cracked · Jan 6, 2025 · N487CA · Cndair CL6002B19 · Fuselage Main, Frame > FS333.00 FRAME CRACKED NEXT TO STR 2L (C-CHECK RO 2/27/2025) REPAIRED FS333.00 FRAME NEXT TO STR 2L REF REO 601R-53-21-3715 REV --(P1) DATE 2025-01-13, AND REO 601R-53-21-3715 REV -- DATED 2025-01-17. PRESSURE LEAK CHECK GOOD. SEE CONTINUATION FOR WORK - [SDR SWI2025F00186](https://openairdocs.org/sdr/SWI2025F00186.md): Cleat · corroded · Jan 6, 2025 · N487CA · Cndair CL6002B19 · Emergency Exits > 2 EA CLEATS BETWEEN FS338.00 AND FS335.76 HAVE INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND REPLACED 2 EA. PAX DOOR CLEATS BETWEEN FS338.00 AND FS335.76. CRJ-200 SRM 51-42-06 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-10 - [SDR SWI2025F00185](https://openairdocs.org/sdr/SWI2025F00185.md): Intercostal · corroded · Jan 6, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD7A FS320.00 - FS327.763 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD7A FS320.00 - FS327.763. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7A FS320 - [SDR SWIA20250228106](https://openairdocs.org/sdr/SWIA20250228106.md): Intercostal · corroded · Jan 6, 2025 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CLIP ON INTERCOSTAL DD7 @ FS311.75 IS CORRODED (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR CLIP ON INTERCOSTAL DD7 @ FS311.75. REF: CRJ-200 SRM 51-42-06 CORRECTIVE ACTION: INSTALLED NEW PAX DOOR CLIP ON INTERCOSTAL DD7 @ FS311.75. CR - [SDR SWI2025F00270](https://openairdocs.org/sdr/SWI2025F00270.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD3 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD3 FS338.00 - FS347.25. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 FS338.00 - - [SDR SWI2025F00269](https://openairdocs.org/sdr/SWI2025F00269.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX DOOR INTERCOSTAL DD2 FS320.00 - FS338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD2 FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AND INSTALLED NEW PAX DOOR IN - [SDR SWI2025F00268](https://openairdocs.org/sdr/SWI2025F00268.md): Cleat · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR CLEAT @ DD4 AND FRAME FS313.56 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND REPLACED PAX DOOR CLEAT @ DD4 AND FRAME FS313.56. CRJ-200 SRM 51-42-06 AND DRAWING 601R31702 REV N.COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWI2025F00267](https://openairdocs.org/sdr/SWI2025F00267.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD5 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD5 FS338.00 - FS347.25. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD5 FS338.00 - - [SDR SWI2025F00266](https://openairdocs.org/sdr/SWI2025F00266.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD4 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD4 FS338.00 - FS347.25. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS338.00 - - [SDR SWI2025F00265](https://openairdocs.org/sdr/SWI2025F00265.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD1 FS338.00 - FS347.25. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1 FS338.00 - - [SDR SWI2025F00264](https://openairdocs.org/sdr/SWI2025F00264.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 FS320.00 - FS338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD6 FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AND INSTALLED NEW PAX DOOR I - [SDR SWI2025F00263](https://openairdocs.org/sdr/SWI2025F00263.md): Former · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FORMER FS329.41 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR FORMER FS329.41. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AND INSTALLED NEW PAX DOOR FORMER FS329.41. CRJ-200 SRM 51-42-06, C - [SDR SWI2025F00262](https://openairdocs.org/sdr/SWI2025F00262.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD3 FS320.00 - FS338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD3 FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AND INSTALLED NEW PAX DOOR IN - [SDR SWI2025F00261](https://openairdocs.org/sdr/SWI2025F00261.md): Intercostal · corroded · Jan 2, 2025 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1A FS320.00 - FS338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR INTERCOSTAL DD1A FS320.00 - FS338.00. REF: CRJ-200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS320.00 - [SDR SWIA2025022841231](https://openairdocs.org/sdr/SWIA2025022841231.md): Former · corroded · Dec 31, 2024 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR AFT FORMER FS347.25 IS CORRODED (C-CHECK RO 2/27/2025) INSTALLED NEW PAX DOOR AFT FORMER FS347.25. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N. COMPLIED WITH SKY WEST TC 51-900-1003-SKY. LEAK CHECKED GOOD. - [SDR SWIA2025022841230](https://openairdocs.org/sdr/SWIA2025022841230.md): Former · corroded · Dec 30, 2024 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FWD FORMER FS311.75 IS CORRODED (C-CHECK RO 2/27/2025) REMOVED AND DISCARDED CORRODED PAX DOOR FWD FORMER FS311.75. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AND INSTALLED NEW PAX DOOR FWD FORMER FS311.75. REF: CRJ-200 SRM 51-42-06, CR - [SDR SWI2025F00260](https://openairdocs.org/sdr/SWI2025F00260.md): Window Post · cracked · Dec 28, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > WINDSHIELD CENTER POST LOWER LH CLIP CRACKED (C-CHECK RO 2/27/2025) INSTALLED 1EA NEW LOWER LH CLIP TO WINDSHIELD CENTER POST REF CRJ200 SRM 51-42-21, DWG 601R33007 REV -U. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWI2025F00258](https://openairdocs.org/sdr/SWI2025F00258.md): Stringer · dented · Dec 20, 2024 · N487CA · Cndair CL6002B19 · Vertical Stabilizer > STGR SECTION 18R BETWEEN F.S. 755.00 AND V.S. 67.50 FOUND DAMAGED WHILE ADDRESSING SKIN DENT BETWEEN F.S. 755.00 AND V.S. 67.50 (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW STGR18R BETWEEN FS755.00 AND V.S.67.50 PER CRJ200SRM 51-42-06 AND DWG 60 - [SDR SWI2025F00257](https://openairdocs.org/sdr/SWI2025F00257.md): Stringer · dented · Dec 20, 2024 · N487CA · Cndair CL6002B19 · Vertical Stabilizer > STGR 17R BETWEEN F.S. 755 AND V.S. 67.50 FOUND DAMAGED WHEN ADDRESSING FUSELAGE SKIN DENT BETWEEN F.S. 755.00 AND V.S. 67.50 (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW STGR17R BETWEEN FS755.00 AND V.S.67.50 PER CRJ200SRM 51-42-06 AND DWG 600-2 - [SDR SWI2025F00255](https://openairdocs.org/sdr/SWI2025F00255.md): Skin · corroded · Dec 19, 2024 · N487CA · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING UPPER SURFACE, MATING SURFACE FOR PANEL 640AT HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 2/27/2025) REMOVED CORROSION FROM THE MATING SURFACE FOR PANEL 640AT ON THE R/H UPR WING SURFACE PER CRJ200SRM 51-21-06 AND REPAIRED PER REO 6 - [SDR SWIA2025022841218](https://openairdocs.org/sdr/SWIA2025022841218.md): Stop Fitting · worn · Dec 18, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > AFT SERVICE DOOR STOPS WORN(5EACH) MARKED. CAMP # 29339521. (C-CHECK RO 2/27/2025) COMPLIED WITH BLEND REPAIR TO THE SERVICE DOOR SUROUND STOP FITTING AT FS349 REF REO 601R-53-21-3712 REV -A 2025-02-25. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-10 - [SDR SWI2025F00226](https://openairdocs.org/sdr/SWI2025F00226.md): Skin · chafed · Dec 17, 2024 · N487CA · Cndair CL6002B19 · Wing, Plate/Skin > LH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS (C-CHECK RO 2/27/2025) BLENDED AND REMOVED CHAFE FOUND TO BE ACCEPTABLE REF REO NO. 601R-57-21-880 REV -D DATE 2017/03/06. COMPLIED WITH TASK CARD 51-900-1003-SK - [SDR SWI2025F00225](https://openairdocs.org/sdr/SWI2025F00225.md): Skin · chafed · Dec 17, 2024 · N487CA · Cndair CL6002B19 · Wing, Plate/Skin > RH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS (C-CHECK RO 2/27/2025) PERFORMED REPAIR OF RH LOWER WING PLANK CHAFFED ON TRAILING EDGE WHERE MLG BAY FORWARD FAIRING (193AB) MOUNTS REF REO NO. 601R-57-21-880 REV - [SDR SWIA2025022841216](https://openairdocs.org/sdr/SWIA2025022841216.md): Pressure Blkhd · cracked · Dec 16, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Bulkhead > AFT PRESSURE BULKHEAD FS621.00 TO FS625.30 FRAME RH INTERCOSTAL (P/N 601-35012-52) IS CRACKED (C-CHECK RO 2/27/2025) REMOVED AND REPLACED INTERCOSTAL 601-35012-52 REF. CRJ 200 SRM 51-42-06, 51-42-21, AND DWG 601-35012 REV. D.COMP;LIED WITH 51-900-1003-S - [SDR SWI2025F00224](https://openairdocs.org/sdr/SWI2025F00224.md): Skin · corroded · Dec 15, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin > THE EXTERIOR SKIN AROUND APU EXHAUST HAS FRETTING CORROSION WHERE THE APU EXHAUST SHIELD IS INSTALLED. (C-CHECK RO 2/27/2025) PERFORMED REPAIR OF EXTERIOR SKIN AROUND APU EXHAUST FRETTING CORROSION WHERE THE APU EXHAUST SHIELD IS INSTALLED REF REO 601R - [SDR SWIA2025022841214](https://openairdocs.org/sdr/SWIA2025022841214.md): Skin · chafed · Dec 14, 2024 · N487CA · Cndair CL6002B19 · Ailerons > RH AILERON UPPR LEADING EDGE IS CHAFFED (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW R/H AILERON UPR L/E SKIN ASSY. PER CRJ200SRM 51-42-06, CRJ200SRM 51-42-13, DWG 601R13031 REV K, AND REO 601R-57-61-872 REV -- DATE 2025-01-16. SEE CONTINUATION - [SDR SWI2025F00253](https://openairdocs.org/sdr/SWI2025F00253.md): Skin · chafed · Dec 13, 2024 · N487CA · Cndair CL6002B19 · Wing, Plate/Skin > S/N 0295CENTER LH WING PLANK APPROX. (WS47.61), CHAFES FOUND FROM OUTBD CORNER PANEL 193AB. FLAGGED (C-CHECK RO 2/27/2025) BLENDED AND REMOVED DAMAGED FOUND TO BE ACCEPTABLE WITHIN THE MAX ALLOWABLE DAMAGE AT NON PAD UP IS 0.040" ( ZONE A) AND PAD UP - [SDR SWI2025F00251](https://openairdocs.org/sdr/SWI2025F00251.md): Floor Panel · dented · Dec 11, 2024 · N487CA · Cndair CL6002B19 · Fuselage Floor Panel > MULTIPLE DENTS NOTED AT FLIGHT COMPARTMENT FLOOR PANEL BETWEEN FS261-268 AND RBL19-RBL24 (MARKED) (C-CHECK RO 2/27/2025) RH COCKPIT FLOOR REPAIRED AS PER REO 601R-53-11-3972 REV --, DATED 2025-01-13, SEE CONTINUATION CARD FURTHER DETAILS COMPLIED WITH S - [SDR SWI2025F00250](https://openairdocs.org/sdr/SWI2025F00250.md): Floor Panel · dented · Dec 11, 2024 · N487CA · Cndair CL6002B19 · Fuselage Floor Panel > DENT NOTED AT FLIGHT COMPARTMENT FLOOR PANEL AT APPROX LBL19 AND FS263.00 (MARKED) (C-CHECK RO 2/27/2025) LH COCKPIT FLOOR REPAIRED AS PER REO 601R-53-11-3972 REV --, DATED 2025-01-13, SEE CONTINUATION CARD FURTHER DETAILS. COMPLIED WITH SKYWEST TASK CA - [SDR SWI2025F00249](https://openairdocs.org/sdr/SWI2025F00249.md): Window Frame · cracked · Dec 11, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > L/H WINDSHIELD SIDE POST SUPPORT CHANNEL BELOW WL110 IS CRACKED (MARKED) (C-CHECK RO 2/27/2025) REMOVED L/H WINDSHIELD SIDE POST ANGLE BETWEEN WL97.80 - WL110.00 AT FS230 & INSTALLED NEW L/H WINDSHIELD SIDE POST ANGLE BETWEEN WL97.80 - WL110.00 AT FS230 - [SDR SWI2025F00248](https://openairdocs.org/sdr/SWI2025F00248.md): Floorbeam · corroded · Dec 11, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Floor Beam > FS621.00 LBL 9 FLOOR BEAM - TO PRESSURE BULKHEAD - UPPER ATTACH FITTING CORRODED (MARKED) (C-CHECK RO 2/27/2025) REMOVED AND INSTALLED 1EA NEW FLOOR RAIL FITTING AT FS621.00 LBL9 (P/N 601-35017-5) PER CRJ200SRM 51-41-02, DWG 601R35031 REV AG, AND REO 60 - [SDR SWI2025F00217](https://openairdocs.org/sdr/SWI2025F00217.md): Fitting · gouged · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > THE PAX DOOR SURROUND AFT UPPER CAM FITTING IS GOUGED. (C-CHECK RO 2/27/2025) REPLACED PAX DOOR SURROUND AFT UPPER CAM FITTING IAW CRJ200 SRM 51-42-21 AND DWG 600-31900 REV K. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWI2025F00216](https://openairdocs.org/sdr/SWI2025F00216.md): Door Sill · corroded · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE PAX DOOR SURROUND LOWER SILL BY FWD AND AFT DRAINS HAVE CORROSION. (C-CHECK RO 2/27/2025) REMOVED CORROSION AND FOUND TO BE ACCEPTABLE REF REO NO. 601R-53-21-3711 REV -- DATE 2024-12-25. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19) MAJOR RE - [SDR SWI2025F00215](https://openairdocs.org/sdr/SWI2025F00215.md): Floor Support · corroded · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > AREAS OF CORROSION ON LH PRESSURE FLOOR SILL (C-CHECK RO 2/27/2025) LH FLOOR SILL REPAIRED AS PER REO 601R-53-41-666 REV -C, DATED 2012-11-06. SEE CONTINUATION CARD FOR FURTHER DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWI2025F00214](https://openairdocs.org/sdr/SWI2025F00214.md): Floor Support · corroded · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure > AREAS OF CORROSION ON RH PRESSURE FLOOR SILL (C-CHECK RO 2/27/2025) RH FLOOR SILL REPAIRED AS PER REO 601R-53-41-666 REV -C, DATED 2012-11-06. SEE CONTINUATION CARD FOR FURTHER DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWI2025F00213](https://openairdocs.org/sdr/SWI2025F00213.md): Pressure Deck · cracked · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > CLIP CRACKED FOR PRESSURE FLOOR INTERCOSTAL AT FS484 LBL36 (C-CHECK RO 2/27/2025) PERFORMED REPAIR OF CRACKED CLIP ON PRESSURE FLOOR INTERCOSTAL AT FS484 LBL36 BY COMPLYING WITH ALL STEPS OF REO 601R-53-41-059 REV-C REV 2020-03-11, REFERENCED CRJ 200 SR - [SDR SWI2025F00239](https://openairdocs.org/sdr/SWI2025F00239.md): Cam · gouged · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Passenger/Crew Doors > THE PAX DOOR SURROUND FWD UPPER CAM FITTING IS GOUGED. (C-CHECK RO 2/27/2025) REPLACED PAX DOOR SURROUND FWD UPPER CAM FITTING REF CRJ 200 SRM 51-42-21 AND DWG#600-31900 REV K.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJO - [SDR SWI2025F00238](https://openairdocs.org/sdr/SWI2025F00238.md): Door Frame · gouged · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > THE PAX DOOR SURROUND UPPER SILL IS GOUGED BEHIND 4EA NUTPLATES BETWEEN FS310 AND FS349. (C-CHECK RO 2/27/2025) BLENDED AND REMOVED DAMAGE FOUND TO BE ACCEPTABLE REF REO NO. 601R-53-21-3710 REV -- DATE 2024-12-25. COMPLIED WITH TASK CARD 51-900-1003-S - [SDR SWI2025F00237](https://openairdocs.org/sdr/SWI2025F00237.md): Floorbeam · cracked · Dec 10, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Floor Beam > FLOOR BEAM FITTING AT FS461 RBL9 CRACKED (C-CHECK RO 2/27/2025) INSTALLED NEW FITTING FLOOR SUPPORT TO FLOOR BEAM AT FS461 RBL9 REF CRJ200 SRM 51-42-21 AND DWG 601R31145 REV P. COMPLIED WITH TASK CARD 51-900-1003-SKY - [SDR SWIA2025022841127](https://openairdocs.org/sdr/SWIA2025022841127.md): Skin · gouged · Nov 27, 2024 · N487CA · Cndair CL6002B19 · Cargo/Baggage Doors > ADM# N487CA-8983 CARGO DOOR OUTER UPPER SKIN. TWO GOUGES ON UPPER SKIN OF CARGO DOOR. ONE GOUGE MEASURING 13" FROM THE FRONT OF THE DOOR. THE SECOND GOUGE MEASURING 23" INCHES FROM THE FRONT OF THE DOOR. ONE GOUGE MEASURING.76" W X 1.25" L X.012" D. THE S - [SDR SWIA20240829](https://openairdocs.org/sdr/SWIA20240829.md): Pressure Deck · cracked · Aug 29, 2024 · N487CA · Cndair CL6002B19 · Fuselage Main, Structure > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA55667-601R-53-41-2669-N487CA MXCODEID50804-PR - THE PRESS FLOOR SKIN HAS 2-OFF CRACKS AT FS461 BTWN LBL9-RBL9. REMOVED DAMAGE AND APPLIED TEMP DBLR REPAIRS IN REF TO REO 601R-53-41-2669 REV--, DTD 01/14/2020. PERFOR - [SDR SWIA20231200007](https://openairdocs.org/sdr/SWIA20231200007.md): Unknown · chafed · Dec 7, 2023 · N487CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin > WHILE REMOVING AFT DRAIN MAST, FOUND FUSELAGE CHAFFED AND CORRODED DIRECTLY UNDER DRAIN MAST FLANGE. (FILED CLOSED)PERMANENTLY REPAIRED FUSELAGE SKIN BETWEEN FS605.00 - FS621.00 & STR25R - STR26R IN REFERENCE TO REO 601R-53-61-8125 REV-- DATED 2023-12-10. - [SDR SWIA20230302](https://openairdocs.org/sdr/SWIA20230302.md): Unknown · corroded · Mar 2, 2023 · N487CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin > *R/H WING LOWER PLANK HOLE FOR PANEL 640DB HAS FRETTING CORROSION (MARKED) (C-CHECK RO 3/23/2023) REMOVED FRETTING CORROSION ON R/H WING LOWER PLANK HOLE FOR PANEL 640DB ( LANDING) FROM 270 DEGREES TO 345 DEGREES WITH-IN LIMITS REF REO 601R-57-21-030 R - [SDR SWIA202303011](https://openairdocs.org/sdr/SWIA202303011.md): Unknown · corroded · Mar 1, 2023 · N487CA · Cndair CL6002B19 · Fuselage Structure (General) > *APPROX FS559.00+8 - FS409.00+128 LBL9 ENTIRE STICK OF FLOOR SEAT TRACK CORRODED/GOUGED (OUT OF SCOPE, MARKED) (C-CHECK RO 3/23/2023) REPLACED SEAT TRACK FROM APPROXIMATELY FS559.00+8 - FS409.00+128, LBL9,WITH NEW SEAT TRACK. REF. CRJ200 A.M.M. 53-01-1 - [SDR SWIA202303012](https://openairdocs.org/sdr/SWIA202303012.md): Unknown · corroded · Mar 1, 2023 · N487CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings > *APPROX FS559.00+8 - FS409.00+128 RBL9 ENTIRE STICK OF FLOOR SEAT TRACK CORRODED/GOUGED (OUT OF SCOPE, MARKED) (C-CHECK RO 3/23/2023) REPLACED SEAT TRACK FROM APPROXIMATELY FS559.00+8 - FS409.00+128 RBL9 WITH NEW SEAT TRACK. REF. CRJ200 A.M.M. 53-01-11- Next page: https://openairdocs.org/aircraft/N487CA/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 = 'N487CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N487CA/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.