# Service difficulty reports: N498CA

A list on [N498CA](https://openairdocs.org/aircraft/N498CA.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 · 149 reports

- [SDR SWIA202266509](https://openairdocs.org/sdr/SWIA202266509.md): None · corroded · Sep 20, 2022 · N498CA · Cndair CL6002B19 · Doors
  > FOUND CARGO DOOR STOP (TOP) SHIMS CORRODED AND WORN TO LIMITS (FILED CLOSED) REMOVED AND REPLACED THE CARGO DOORS STOP(TOP) SHIMS IAW CRJ 200 AMM 52-31-00.
- [SDR SWIA202155734](https://openairdocs.org/sdr/SWIA202155734.md): Skin · dented · Jan 12, 2021 · N498CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP LOWER SKIN HAS 3 DENTS INBOARD OF THE INBOARD HINGE ARM. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED SKIN PANEL 601R-14028-45 AND INSTALLED NEW SERVICEABLE SKIN SECTION 601R-14028-45 IAW CRJ-200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202155761](https://openairdocs.org/sdr/SWIA202155761.md): Angle · cracked · Jan 9, 2021 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AND SUPPORT CLIP CORRODED AT FS280 AND STGR2L (C-CHECK) RO 2/1/2021 REMOVED CLIP, REMOVED DOUBLER, REMOVED BRAACKET IAW CRJ SRM 51-42-06. REMOVED CORROSION IAW CRJ 200 SRM 51-21-06. NO CRACKS FOUND. INSTALLED DOUBLER, BRACKET AND CLIP IAW CR
- [SDR SWIA202155760](https://openairdocs.org/sdr/SWIA202155760.md): Angle · cracked · Jan 3, 2021 · N498CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > ANGLE CRACKED AT STR 16L BETWEEN FS 621 AND FS 625 (C-CHECK) RO 2/1/2021 REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11
- [SDR SWIA202155773](https://openairdocs.org/sdr/SWIA202155773.md): Bolt · corroded · Jan 1, 2021 · N498CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > WHILE PERFORMING INSPECTION ON 57-590-600 AND 57-690-6000 FOUND THAT L/H AND R/H HINGE BOX BOLTS ON W.S. 178, 220, 264 WERE ALL CORRODED AND NEED TO BE REPLACED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED HARDWARE ON L/H AND R/H W.S 178-.00, 220.00, AND 26
- [SDR SWIA202055731](https://openairdocs.org/sdr/SWIA202055731.md): Skin · chafed · Dec 31, 2020 · N498CA · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H CENTER WING, LOWER SKIN IS CHAFED AT B.L. 45.00 AT AFT SPAR. (C-CHECK) RO 2/1/2021 REPAIRED LH CENTER WING LOWER SKIN AT BL 45 AT REAR SPAR IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 ZONE A REFERENCE SKYCARD 51-900-1003-SKY (CL-600-2B19)
- [SDR SWIA202055730](https://openairdocs.org/sdr/SWIA202055730.md): Skin · chafed · Dec 31, 2020 · N498CA · Cndair CL6002B19 · Wing, Plate/Skin
  > R/H CENTER WING, LOWER SKIN IS CHAFED AT B.L. 45.00 AT REAR SPAR. (C-CHECK) RO 2/1/2021 REPAIRED RH CENTER WING LOWER SKIN AT BL 45 AT REAR SPAR IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 ZONE A REFERENCE SKYCARD 51-900-1003-SKY (CL-600-2B19)
- [SDR SWIA202055772](https://openairdocs.org/sdr/SWIA202055772.md): Web · corroded · Dec 28, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB IS CORRODED. (C-CHECK) RO 2/1/2021 REPLACED PAX DOOR AFT WEB P/N 601R317071-11 IAW CRJ 200 SRM 51-40-11, 51-42-06 REV 38 7-1019
- [SDR SWIA202055733](https://openairdocs.org/sdr/SWIA202055733.md): Hinge · gouged · Dec 21, 2020 · N498CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON THE FUSELAGE SIDE IS GOUGED ON THE 11TH, 12TH, 13TH, 14TH, 15, 16TH, 17TH, 18TH, 23RD, 24TH, 25TH AND 27TH LUG VALLEYS FROM FWD SIDE OF THE HINGE. (C-CHECK) RO 2/1/2021 REPAIRED PAX DOOR HINGE FUSELAGE SIDE IAW BOMBARDIER REO 601R-53-21-8
- [SDR SWIA202055759](https://openairdocs.org/sdr/SWIA202055759.md): Skin · cracked · Dec 19, 2020 · N498CA · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H WING STATION 200 HAS 2 CRACKS IN THE TRAILING EDGE OF THE PANEL WHERE THE SKIN IS COVERED BY THE I/B FLIGHT SPOILER (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING TRAILING EDGE IAW CRJ 200 SRM 51-42-06 & 51-42-21
- [SDR SWIA202055755](https://openairdocs.org/sdr/SWIA202055755.md): Frame · damaged · Dec 18, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND DAMAGED AREA AT FS 605 BETWEEN STRINGERS 20R AND 21R. (C-CHECK) RO 2/1/2021 COMPLIED WITH REPAIR DAMAGED AREA AT FS 605 BETWEEN STRINGERS 20R AND 21R IAW MHIRJ REO 601R-53-61-7515 REV -- DATED 2021-01-04 BY CUTTING AWAY DAMAGE, REMOVEING BURRS,VISU
- [SDR SWIA202055777](https://openairdocs.org/sdr/SWIA202055777.md): Bearing · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR TORQUE TUBE SHAFT BEARINGS(QTY 2) RUSTED AND HAVE SIDE TO SIDE PLAY BEYOND ALLOWABLE LIMITS. REPLACE P/N'S 600-31320-73. (C-CHECK) RO 2/1/2021 LOCATED AND DRILLED 2EA NEW BEARING ASSYS P/N 600-31320-73 IAW CRJ200 SRM 51-40-11 REV38 DATED JUL 10/1
- [SDR SWIA202055754](https://openairdocs.org/sdr/SWIA202055754.md): Intercostal · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTALS 3RD AND 4TH FROM HINGE AFT SIDE CORRODED BEYOND LIMITS. P/N'S 601R31902-317 (QTY 2). (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 200 SRM 51-40-11 AND 51-42-06. SEE CONTINUATION C
- [SDR SWIA202055753](https://openairdocs.org/sdr/SWIA202055753.md): Intercostal · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 CORRODED BEYOND LIMITS. P/N 601R318081-1 (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM 51-40-11 AND 51-42-06. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. AND C
- [SDR SWIA202055752](https://openairdocs.org/sdr/SWIA202055752.md): Intercostal · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 CORRODED BEYOND LIMITS. P/N 601R318056-1 (C-CHECK) RO 2/1/2021 REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM 51-40-11 AND 51-42-06 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIG
- [SDR SWIA202055751](https://openairdocs.org/sdr/SWIA202055751.md): Frame · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER AT FS347.27 CORRODED BEYOND LIMITS. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FORMER AND INSTALLED NEW SERVICEABLE FORMER IAW CRJ 200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIGHT CHANGE. REFE
- [SDR SWIA202055750](https://openairdocs.org/sdr/SWIA202055750.md): Frame · corroded · Dec 16, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER AT FS311.75 CORRODED BEYOND LIMITS. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FORMER AND INSTALLED NEW SERVICEABLE FORMER IAW CRJ 200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND SKYWEST CARD 51-900-1003-SKY, 337 ATTACHED, AND NO WEIGHT CHANGE.REFER
- [SDR SWIA202055771](https://openairdocs.org/sdr/SWIA202055771.md): Floorbeam · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LEFT FLOOR SILL ASSY LBL41 TO LBL45 LFS560 HAS CORROSION (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH TENSION STRAP IAW CRJ 200 SRM 51-42-06
- [SDR SWIA202055749](https://openairdocs.org/sdr/SWIA202055749.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL ASSY LBL45 LFS491 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 RERV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA202055748](https://openairdocs.org/sdr/SWIA202055748.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL ASSY LBL45 LFS499 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM 337. WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA202055747](https://openairdocs.org/sdr/SWIA202055747.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL ASSY LBL45 LFS513 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKY CARD 51-900-1003-SKY AND FORM M-337. WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA202055746](https://openairdocs.org/sdr/SWIA202055746.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL ASSY LBL45 LFS529 HAS CORROSION (C-CHECK) RO 2/1/2021 REPAIRED AREA IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AND FORM M -337. WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA202055745](https://openairdocs.org/sdr/SWIA202055745.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL ASSY LBL45 LFS535 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/30
- [SDR SWIA202055744](https://openairdocs.org/sdr/SWIA202055744.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL ASSY RBL45 RFS505 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/3
- [SDR SWIA202055743](https://openairdocs.org/sdr/SWIA202055743.md): Floor Support · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL ASSY RBL45 RFS499 HAS CORROSION (C-CHECK) RO 2/1/2021 COMPLIED WITH BMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 DISPOSITION 1.2 AND SKYCARD 51-900-1003-SKY (CL600-2B19). CAL TOOLING USED WVACT3099 CAL DATE 06/15/2020 CAL DUE 06/3
- [SDR SWIA202055742](https://openairdocs.org/sdr/SWIA202055742.md): Frame · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 605 FRAME IS CORRODED IN TWO LOCATIONS. FIRST LOCATION IS BETWEEN STRG 20R TO 21R. SECOND LOCATION IS BETWEEN 26R TO 27. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AT FS605 AND INSTALLED NEW SERVICEABLE FRAME IAW CRJ-200 SRM 51-42-06 AND 51-42-21. SE
- [SDR SWIA202055729](https://openairdocs.org/sdr/SWIA202055729.md): Frame · corroded · Dec 14, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 589 FRAME IS CORRODED IN TWO LOCATIONS. FIRST LOCATION IS BETWEEN STRG 20R TO 21R. SECOND IS AT STRG 23R AT THE TOP AND AFT SIDE. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME IAW CRJ-200 SRM 51-42-06, 51-42-21 AND 51
- [SDR SWIA202055741](https://openairdocs.org/sdr/SWIA202055741.md): Intercostal · corroded · Dec 11, 2020 · N498CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRG20L CORRODED BETWEEN FS333 AND FS349. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED INTERCOSTALAT STR21L BETWEEN FS333 AND FS349 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. REFER TO CONTINUATION CARD FOR ALL MAINTAINENCE PERFORMED. AND COMPLIED
- [SDR SWIA202055740](https://openairdocs.org/sdr/SWIA202055740.md): Frame · corroded · Dec 11, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS310 CORRODED BETWEEN STGR26L AND STGR26R. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED FRAME SECTOR IAW CRJ 200 SRM 51-42-06 & 51-42-21. REFER TO CONTINUATION CARD FOR ALL WORK PERFORMED, AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHE
- [SDR SWIA202055735](https://openairdocs.org/sdr/SWIA202055735.md): Frame · corroded · Dec 11, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS333 CORRODED BETWEEN STGR21L AND STGR23L. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME AT FS 333 IAW CRJ-200 SRM 51-42-06, 51-40-11 AND 51-42-21 AND COMPLIED WITH SKYWEST CARD 51-900-1003-SKY. 337 ATTACHED.PART
- [SDR SWIA202055732](https://openairdocs.org/sdr/SWIA202055732.md): Frame · corroded · Dec 11, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS310 CORRODED BETWEEN STGR20R AND STGR21R. (C-CHECK) RO 2/1/2021 REMOVED DAMAGED FRAME AND INSTALLED NEW SERVICEABLE FRAME AT FS 310 BETWEEN STGR20R AND STGR21R IAW CRJ-200 SRM 51-42-06, 51-40-11 AND 51-42-21 REV 38 DATED 10 JULY 2019 AND COMPLIE
- [SDR SWIA202055776](https://openairdocs.org/sdr/SWIA202055776.md): Fitting · chafed · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ARRESTER FITTING CHAFED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED NEW SERVICEABLE PN 601R31722-1 IAW CRJ 200 AMM 20-21-00-910--801
- [SDR SWIA202055770](https://openairdocs.org/sdr/SWIA202055770.md): Tension Tie · corroded · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT TENSION TIE BAR HARDWARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED FWD AND AFT TENSION TIE BAR HARDWARE IAW CRJ200 AMM 52-11-19-400-803 REV62 DATED DEC10/20. INSTALLATION OF TENSION TIES TO BE ACCOMPLISHED ON MX TR
- [SDR SWIA202055758](https://openairdocs.org/sdr/SWIA202055758.md): Bracket · cracked · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF AFT BULKHEAD, LH SIDE @ FS625.30 STR 14, @ THREE INCHES FROM OUTBOARD SKIN, CRACKED BRACKET (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED BRACKET AFT SIDE AFT PRESSURE BULKHEAD LH SIDE @FS625.30 STR14 IAW CRJ200 SRM 51-42-21 AND 51-40-11
- [SDR SWIA202055757](https://openairdocs.org/sdr/SWIA202055757.md): Angle · cracked · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT BULKHEAD, AFT SIDE, RH CLIP CRACKED @ FS 621 STR 14 (C-CHECK) RO 2/1/2021 REMOVED AND LOCATED AND DRILLED, INSTALLED AND PAINTED NEW CLIP IAW CRJ 200 SRM 51-40-11,51-42-21, AND 51-25-21.
- [SDR SWIA202055739](https://openairdocs.org/sdr/SWIA202055739.md): Intercostal · corroded · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD3 INTERCOSTAL CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND INSTALLED SERVICABLE INTERCOSTAL IAW CRJ200 SRM 51-42-06 REEV 38 DATED JUL10/19 AND SKY CARD 51-900-1003-SKY (CL600-2B19). 337 COMPLETED PART FOR PART REPLACEMENT, NO WEIGHT CHANGE. REFE
- [SDR SWIA202055738](https://openairdocs.org/sdr/SWIA202055738.md): Intercostal · corroded · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD6 INTERCOSTAL CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND INSTALLED SERVICABLE DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 REV 38 DATED JUL 10/19 AND SKYCARD 51-900-1003-SKY (CL600-2B19). FORM 337 COMPLETED. PART FOR PART REPLACEMENT, NO WEIGHT CH
- [SDR SWIA202055736](https://openairdocs.org/sdr/SWIA202055736.md): Skin · gouged · Dec 10, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS GOUGED 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. (C-CHECK) RO 2/1/2021 COMPLIED WITH REPAIR OF FUSELAGE SKIN IS GOUGES 4 PLACES JUST AFT OF PASSENGER DOOR HINGE BETWEEN STR 17L AND 18L. IAW MHIRJ REO 601R-53-21-3
- [SDR SWIA202055756](https://openairdocs.org/sdr/SWIA202055756.md): Fitting · cracked · Dec 5, 2020 · N498CA · Cndair CL6002B19 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST LOWER O/B ANGLE IS CRACKED. (C-CHECK) RO 2/1/2021 REMOVED OLD UNSERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE. DRILLED, LOCATED, AND INSTALLED NEW SERVICEABLE RH WINDSHIELD SIDE POST LOWER O/B ANGLE, P/N 601R33235-4S IAW CRJ 2
- [SDR SWIA202055769](https://openairdocs.org/sdr/SWIA202055769.md): Washer · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > R/H WING FLIGHT SPOILER O/B ACTUATOR ATTACHMNET THROUGH BOLT HARWARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED R/H WING FLIGHT SPOILER O/B ACTUATOR ATTACHMNET THROUGH BOLT HARWARE IAW CRJ 200 AMM 27-62-01-943-003.
- [SDR SWIA202055768](https://openairdocs.org/sdr/SWIA202055768.md): Nut · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > R/H WING O/B GROUND SPOILER ACTUATOR ATTACHMNET NUT HARDWARE (QTY 2) IS CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 27-63-01-400-801 STEP 2 B. 1(D,E,F)
- [SDR SWIA202055767](https://openairdocs.org/sdr/SWIA202055767.md): Pcu · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING FLIGHT SPOILER PCU'S ( I/B AND O/B) MOUNTNG ATTACHMENT HARDWARE NUTS ARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING FLIGHT SPOILER PCU'S ( I/B AND O/B) MOUNTNG ATTACHMENT HARDWARE NUTS IAW CRJ 200 AMM 27-62-01-910-004.
- [SDR SWIA202055766](https://openairdocs.org/sdr/SWIA202055766.md): Rod End · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING I/B GROUND SPOILER ACTUATOR ROD END ATTACHMENT HARDWARE CORRODED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH WING IB GROUND SPOILER ACTUATOR ROD END ATTACHMENT HARDWARE IAW CRJ 200 AMM 27-63-01-000/400-801
- [SDR SWIA202055765](https://openairdocs.org/sdr/SWIA202055765.md): Angle · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING SPOILERON I/B HINGE BOLT STOP ANGLE HARDWARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED L/H WING SPOILERON I/B HINGE BOLT STOP ANGLE HARDWARE IAW CRJ 200 AMM 27-64-01-420-001.
- [SDR SWIA202055764](https://openairdocs.org/sdr/SWIA202055764.md): Nut · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING SPOILERON I/B HINGE NUT HARDWARE CORRODED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED L/H WING SPOILERON I/B HINGE NUT HARDWARE IAW CRJ 200 AMM 27-64-01-869-001
- [SDR SWIA202055763](https://openairdocs.org/sdr/SWIA202055763.md): Nut · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING FLIGHT SPOILER BOTH I/B HINGE ATTACH PIONT HARDWARE NUTS ARE CORRORDED. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED CORRODED L/H WING FLIGHT SPOILER BOTH I/B HINGE ATTACH PIONT HARDWARE NUTS IAW CRJ 200 AMM 27-64-01-946-004,
- [SDR SWIA202055762](https://openairdocs.org/sdr/SWIA202055762.md): Angle · corroded · Dec 3, 2020 · N498CA · Cndair CL6002B19 · Spoilers
  > L/H WING FLIGHT SPOILER I/B HINGE BOLT STOP ANGLE HAS CORRODED HARDWARE BOLTS. ( QTY 2) (C-CHECK) RO 2/1/2021 REMOVED AND REPLACE CORRODED HARDWARE ON L/H WING FLIGHT SPOLIER BOLT STOP ANGLE IAW CRJ 200 AMM 27-64-01-869-001.
- [SDR SWIA202055775](https://openairdocs.org/sdr/SWIA202055775.md): Skin · chafed · Dec 1, 2020 · N498CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED CHAFED DAMAGED R/H FLAP VANE LEADING EDGE SKINS. LOCATED, DRILLED, INSTALLED,ALODINED,PRIMED, AND TOPCOATED 3 NEW SERVICEABLE R/H I/B FLAP VANE LEADING EDGE SKINS
- [SDR SWIA202055774](https://openairdocs.org/sdr/SWIA202055774.md): Skin · chafed · Dec 1, 2020 · N498CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LH IB FLAP VANE LEADING EDGE IS CHAFED AT ALL 3 CONTACT POINTS (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED LH IB FLAP VANE LEADING EDGE AT 3 CHAFED CONTACT POINTS IAW CRJ 200 SRM 51-42-10. REFER TO CONTINUATION CARD FOR DETAILED WORK PERFORMED.
- [SDR SWIA202055737](https://openairdocs.org/sdr/SWIA202055737.md): Bushing · damaged · Nov 19, 2020 · N498CA · Cndair CL6002B19 · Ailerons
  > REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK) RO 2/1/2021 REMOVED R/H AILERON AFT SPAR BUSHING AND HARDWARE ANDD INSTALLED NEW SERVICEABLE BUSHINGS AND HARDWARE AT AFT SPAR IAW CRJ-200 AMM 2

Next page: https://openairdocs.org/aircraft/N498CA/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 = 'N498CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N498CA/reports

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