# Service difficulty reports: N494CA

A list on [N494CA](https://openairdocs.org/aircraft/N494CA.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 · 209 reports

- [SDR SWI2025F01517](https://openairdocs.org/sdr/SWI2025F01517.md): Trunnion · damaged · Oct 20, 2025 · N494CA · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > DURING REPLACEMENT OF THE LH MLGTRUNNION AN UNDOCUMENTED FREEZE PLUG REPAIR WAS FOUND AT 1-OFF FASTENER LOCATION ON UPPER AFT WING PLANK. (FILED CLOSED)FABRICATED 1 EA. CSK FREEZE PLUG USING 7075-T7351, PO #20153681. REF. REO 601R-57-21-3981 REV --(P1) DATED
- [SDR SWI2025F01524](https://openairdocs.org/sdr/SWI2025F01524.md): Rib · cracked · Oct 10, 2025 · N494CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT BATTERU RIB CAP ANGLE CRACKED AT W/S 48.30 (FILED CLOSED)REMOVE AND REPLACED LH BATT RIB CAP ANGLE AT W/S 48.30 REF DWG600-10389 REV E AND CRJ200 SRM 51-42-21.COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA20251110001](https://openairdocs.org/sdr/SWIA20251110001.md): Skin · chafed · Oct 10, 2025 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFTER REMOVAL OF L/H WING AUX SPAR FOUND FUSELAGE APRON SKIN CHAFED. REPAIRED THE LH APRON SKIN PANEL ASSY PER REO 601R-53-41-115 REV A.
- [SDR SWIA2025111000911](https://openairdocs.org/sdr/SWIA2025111000911.md): Trunnion · cracked · Sep 11, 2025 · N494CA · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > REPAIRED 3 EACH CRACKED HOLES FOR LH TRUNION REF REO 601R-57-21-1748 REV. --, THIS IS A SAFE LIFE REPAIR. LIFE LIMIT/DISCARD TIME IS 20,475 CYCLES FROM INCORPERATION OF REPAIR DUE BY TAC 41408., PART NUMBER: -, SERIAL NUMBER: 7765, POSITION: (FILED CLOSE
- [SDR SWIA2024092572002](https://openairdocs.org/sdr/SWIA2024092572002.md): Floorbeam · corroded · Jul 22, 2024 · N494CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BEAM FLOOR RBL9 IN FS559.00+80 WITH FRETLING CORROSION (C-CHECK RO 9/24/2024) BEAM FLOOR RBL9 IN FS 559.00+80 WAS REPLACED IAW CRJ200 SRM53.00.43 REPAIR #2
- [SDR SWIA20240925068](https://openairdocs.org/sdr/SWIA20240925068.md): Intercostal · corroded · Jul 16, 2024 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > LOWER MID INTERCOSTAL ON PAX DOOR HAS CORROSION. (C-CHECK RO 9/24/2024) REMOVED AND REPLACED INTERCOSTAL P/N 601R 318056-1 ON LOWER SIDE OF PAX DOOR IAW CRJ200 SRM 51-42-06
- [SDR SWIA20240925712](https://openairdocs.org/sdr/SWIA20240925712.md): Intercostal · corroded · Jul 12, 2024 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > 4TH INTERCOSTAL FROM THE BOTTOM OF THE PAX DOOR IS CORRODED. (C-CHECK RO 9/24/2024) REMOVED AND REPLACED 4TH INTERCOSTAL FROM THE BOTTOM OF THE PAX DOOR IAW CRJ200 SRM 51-42-06
- [SDR SWIA202409250808](https://openairdocs.org/sdr/SWIA202409250808.md): Riser · cracked · Jul 8, 2024 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT RISER IS CRACKED. (C-CHECK RO 9/24/2024) PAX DOOR AFT RAISER WAS REPAIRED IAW REO #601R-52-11-702
- [SDR SWIA202409250798](https://openairdocs.org/sdr/SWIA202409250798.md): Riser · cracked · Jul 8, 2024 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD RISER IS CRACKED. (C-CHECK RO 9/24/2024) ON PAX DOOR FWD RAISER WAS REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 AND SRM 51-42-10
- [SDR SWIA2024092570008](https://openairdocs.org/sdr/SWIA2024092570008.md): Intercostal · corroded · Jul 8, 2024 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > CENTER MID INTERCOSTAL HAS AREAS OF CORROSION INNER PAX DOOR. (C-CHECK RO 9/24/2024) REMOVED AN REPLACED INTERCOSTAL P/N 601R318081-1 ON CENTER MID OF THE PAX DOOR IAW CRJ200 SRM 51-42-06
- [SDR SWIA20240925606](https://openairdocs.org/sdr/SWIA20240925606.md): Radome · dented · Jun 6, 2024 · N494CA · Cndair CL6002B19 · Aerodynamic Fairings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA81072-601R-53-11-3808 N494CA MXCODEID64640-PR - 2 DENT'S BETWEEN FS169 AND FS 173 AT RIGHT SIDE FORWARD EQUIPMENT COMPARTMENT DOOR AND NOSE RADOME. PERFORMED TEMPORARY REPAIR/DRESSBACK OF DENTS ACCEPTABLE FOR 2950 FHS
- [SDR SWIA202264094](https://openairdocs.org/sdr/SWIA202264094.md): None · arced · Jan 25, 2022 · N494CA · Cndair CL6002B19 · Window/Windshield System
  > D:L WINDOW HEAT CAUTION MESSAGE DURING CLIMB. RAN QRH MESSAGE CLEARED. RECEIVED MESSAGE AGAIN ON APPROACH / C: MEL 30-41-2 / CAT A DUE WITHIN 1 FLIGHT DAY / NOTE: MX ACTION C/W / L WINDOW HEAT CAUTION MESSAGE DURING CLIMB. RAN QRH MESSAGE CLEARED. RECEIVED MES
- [SDR SWIA2021071959594](https://openairdocs.org/sdr/SWIA2021071959594.md): Wire Harness · failed · Jul 17, 2021 · N494CA · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE WARNING MESSAGE IN FLIGHT. RAN QRH AND PROBLEM RESOLVED. (FLIGHT 5140 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23140060 WITH THE FOLLOWING CORRECTIVE ACTION: "REF CP 23140668 FOR TROUBLESHOOTING OF GEAR DISAGREE WARNIN
- [SDR SWIA202157461](https://openairdocs.org/sdr/SWIA202157461.md): Skin · dented · Mar 27, 2021 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 604995: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 604978, FOUND DENT AT 8.5" AFT OF FUSE STA 589, 2"ABOVE STR 25 MEASURING.066 DEEP. (FLIGHT 5300 - FILED CLOSED) COMPLIED WITHREO 601R-53-61-7619 REV:-- DATED 2021-04-05
- [SDR SWIA202053335](https://openairdocs.org/sdr/SWIA202053335.md): Bracket · cracked · Sep 30, 2020 · N494CA · Cndair CL6002B19 · Wing, Attach Fittings
  > LT WING LEADING EDGE INBOARD BRACKET, BETWEEN INBOARD AND CENTER LEADING EDGE, IS CRACKED, FLAGGED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED NEW LT WING LEADING EDGE INBOARD BRACKET, BETWEEN INBOARD AND CENTER LEADING EDGE, REF CRJ 200 SRM.
- [SDR SWIA202053334](https://openairdocs.org/sdr/SWIA202053334.md): Bracket · cracked · Sep 30, 2020 · N494CA · Cndair CL6002B19 · Wing, Attach Fittings
  > RT WING LEADING EDGE BRACKETS CRACKED (2 EA) IN BETWEEN INBOARD AND CENTER LEADING EDGE, FLAGGED. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW RT WING LEADING EDGE BRACKETS (2 EA) LOCATED BETWEEN INBOARD AND CENTER LEADING EDGE, REF CRJ 200 SRM. SEE CON
- [SDR SWIA202053330](https://openairdocs.org/sdr/SWIA202053330.md): Intercostal · cracked · Sep 23, 2020 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DD7 INTERCOSTAL HAS CRACK ON TOP FLANGE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED CRACKED DD7 INTERCOSTAL P/N 601R318825-1, REF DWG AND CRJ200 SRM. PERFORMED PRESSURE CHECK OF FASTENERS, ALL CHECKS GOOD.
- [SDR SWIA202053328](https://openairdocs.org/sdr/SWIA202053328.md): Former · cracked · Sep 21, 2020 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT FORMER HAS CRACK AT POWER ASSIST PULLY BRACKET FASTENER HOLE. C-CHECK RO 10/13/2020. REMOVED AFT FORMER FROM PASSENGER DOOR, REF CRJ200 SRM. INSTALLED NEW AFT FORMER P/N 601R318034-5, REF DWG AND CRJ200 SRM. RESTORED FINISH ALL FASTENERS
- [SDR SWIA202053344](https://openairdocs.org/sdr/SWIA202053344.md): Bracket · corroded · Sep 19, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Structure
  > LT WINDSCREEN INBOARD FLOOR MOUNT CORROSION W/100% MATERIAL LOSS. C-CHECK RO 10/13/2020. REPLACED CORRODED INBOARD FLOOR MOUNT WITH NEW MOUNT ON LEFT WINDSCEEN, REF C&D CMM.
- [SDR SWIA202053343](https://openairdocs.org/sdr/SWIA202053343.md): Seat Track · corroded · Sep 16, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 409.00+128 TO FS 559.00 FLOOR SEAT TRACK RBL 9 CORRODED ON SIDES/CENTER/TOP, MARKED. C-CHECK RO 10/13/2020. REPLACED FS 409.00+128-FS 559.00 FLOOR SEAT TRACK AT RBL 9 WITH NEW FABRICATED SEAT TRACK, REF REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053342](https://openairdocs.org/sdr/SWIA202053342.md): Seat Track · corroded · Sep 16, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 409.00+128 TO FS 559.00 FLOOR SEAT TRACK LBL 9 CORRODED ON SIDES/CENTER/TOP, MARKED. C-CHECK RO 10/13/2020. REPLACED FS 409.00+128-FS 559.00 FLOOR SEAT TRACK LBL 9 WITH A NEW FABRICATED PART, REF REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053327](https://openairdocs.org/sdr/SWIA202053327.md): Pressure Deck · cracked · Sep 16, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 461.00 AND BL 0-RBL 9, POSSIBLE CRACK ON THE PRESSURE FLOOR SKIN, MARKED. C-CHECK RO 10/13/2020. REPAIRED CRACK AT FS 461.00 AND BL 0-RBL 9 ON THE PRESSURE FLOOR SKIN BY COMPLYING WITH MHIRJ REO. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053341](https://openairdocs.org/sdr/SWIA202053341.md): Hinge Fitting · corroded · Sep 15, 2020 · N494CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LT AND RT OUTBOARD FLAP HINGE BOXES HAVE SEVERAL CORRODED MOUNTING HARDWARE NUTS. LT CENTER HINGE BOX, AFT INBOARD AND OUTBOARD NUTS, LT INBOARD HINGE BOX, AFT OUTBOARD NUT, RT CENTER HINGE BOX, AFT INBOARD NUT, RT INBOARD HINGE BOX, AFT INBOARD NUT. C-CHECK
- [SDR SWIA202053340](https://openairdocs.org/sdr/SWIA202053340.md): Skin · corroded · Sep 15, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 559.00+80-FS 559.00+112 STRG 22RH TO 23RH, CORROSION ON EXTERIOR SKIN IN SEVERAL PLACES AROUND LAV SERVICE AREA, MARKED. C-CHECK RO 10/13/2020. CORROSION DAMAGE BLENDED/REMOVED FROM EXTERNAL FUSELAGE SKIN, AS MARKED. FS 559.0+112 STR 22R-23R, REF CRJ 200
- [SDR SWIA202053326](https://openairdocs.org/sdr/SWIA202053326.md): Skin · chafed · Sep 15, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LOWER CENTER WING PLANK EXTERIOR, APPROXIMATELY WS 45.0 LT AFT EDGE CHAFED, MARKED. C-CHECK RO 10/13/2020. REPAIRED LOWER WING PLANK AT LBL 45, AS MARKED REF REO. BLENDED AREA LOCATED WITHIN.150" OF A FASTENER. COMPLIED WITH TASK CARD.
- [SDR SWIA202053339](https://openairdocs.org/sdr/SWIA202053339.md): Anchor Fitting · corroded · Sep 14, 2020 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT ANCHOR FITTING HAS MULTIPLE CORRODED SCREWS AND NUTS. C-CHECK RO 10/13/2020. REMOVED CORRODED SCREWS AND NUTS AFT PASSENGER DOOR ANCHOR FITTING, REF CRJ 200 AMM AND INSTALLED NEW HARDWARE (6 EA SCREWS AND NUTS) REF CRJ 200 AMM. TORQUE WRE
- [SDR SWIA202053338](https://openairdocs.org/sdr/SWIA202053338.md): Plate · corroded · Sep 14, 2020 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE HAS CORROSION. C-CHECK RO 10/13/2020. REMOVED AND REPLACED CORRODED PASSENGER DOOR AFT ANCHOR FITTING SERRATED PLATE, REF CRJ 200 AMM TASK. OPERATIONS CHECK GOOD.
- [SDR SWIA202053325](https://openairdocs.org/sdr/SWIA202053325.md): Striker · chafed · Sep 14, 2020 · N494CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR OPENING FWD SEAL STRIKER CHAFED NEAR UPPER PIN FITTING. C-CHECK RO 10/13/2020. TRIMMED OUT DAMAGED PART OF SEAL STRIKER. FABRICATED REPAIR STRAP FROM 2024T-3.050". INSTALLED NEW REPAIR PARTS TO REWORK AREA, REF REO. LEAK CHECKS GOOD.
- [SDR SWIA202053324](https://openairdocs.org/sdr/SWIA202053324.md): Bulkhead Web · chafed · Sep 14, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF THE FS 280.00 BULKHEAD RT CENTER NEAR DOOR POST AREA WEB PATCH CHAFED, MARKED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED AFT SIDE OF THE FS 280.00 BULKHEAD RT CENTER NEAR DOOR POST AREA WEB DOUBLER, REF REO.
- [SDR SWIA202053323](https://openairdocs.org/sdr/SWIA202053323.md): Rib · cracked · Sep 13, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WS 53.60 RT BATTERY RIB ASSEMBLY IN MLG GEAR WELL IS CRACKED ON THE FWD OUTBOARD SIDE, MARKED. C-CHECK RO 10/13/2020. INSTALLED ANGLE P/N: 601R10203-26 AT WS 53.60 RT, REF CRJ-200 SRM AND BOMBARDIER REO. DOUBLER P/N: 601R10203-32 WAS DISCARDED AND REPLACED
- [SDR SWIA202053322](https://openairdocs.org/sdr/SWIA202053322.md): Rib · cracked · Sep 13, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > WS 53.60 LT BATTERY RIB ASSEMBLY IN MLG GEAR WELL IS CRACKED ON THE FWD OUTBOARD SIDE, MARKED. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW WS 53.60 LT BATTERY RIB ASSEMBLY IN MLG GEAR WELL, REF REO CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA202053321](https://openairdocs.org/sdr/SWIA202053321.md): Attach Angle · cracked · Sep 13, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT MLG WHEEL WELL HAS ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT APPROXIMATELY WS 48.00 CRACKED, FLAGGED. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW LT MLG WHEEL WELL ANGLE (BATT RIB) ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT APPROXIMATELY W
- [SDR SWIA202053320](https://openairdocs.org/sdr/SWIA202053320.md): Bulkhead Web · damaged · Sep 13, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PERFORM REPAIR OF FS 280 BULKHEAD WEB LBL 20.75-RBL 20.75, REF REO. C-CHECK RO 10/13/2020. PERFORMED REPAIR OF FS 280 BULKHEAD WEB LBL 20.75-RBL 20.75, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202053333](https://openairdocs.org/sdr/SWIA202053333.md): Attach Angle · cracked · Sep 12, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIP BAY RT ACM SUPPORT STRUCTURE LATERAL CROSS BRACE ATTACH ANGLE AT APPROXIMATELY FS 711.0 AND BL 23 RT IS CRACKED THROUGH IN RADIUS. C-CHECK RO 10/13/2020. REPLACED CRACKED SUPPORT ANGLE CLIP ON RT ACM SUPPORT STRUCTURES WITH NEW PN 601R95159-43 PO T
- [SDR SWIA202053332](https://openairdocs.org/sdr/SWIA202053332.md): Bypass Valve · cracked · Sep 12, 2020 · N494CA · Cndair CL6002B19 · Cabin Cooling System
  > AFT EQUIPMENT BAY RT ACM SUPPORT STRUCTURE PLATE ASSEMBLY AT APPROXIMATELY FS 708.0 AND BL 18 RT HAS CRACKS AT INBOARD AFT MOUNT BOLT. C-CHECK RO 10/13/2020. REPLACED CRACKED PLATE ASSEMBLY ON RT ACM SUPPORT STRUCTURES WITH NEW PN 601R95222-1 PO T- 56457, RE
- [SDR SWIA202053331](https://openairdocs.org/sdr/SWIA202053331.md): Crossbeam · cracked · Sep 12, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT EQUIP BAY RT ACM SUPPORT STRUCTURE LATERAL CROSS BRACE AT APPROXIMATELY FS 711.0 AND BL 13 RT HAS EVIDENCE OF CRACK. C-CHECK RO 10/13/2020. REPLACED CRACKED SUPPORT CROSS BEAM ON RT ACM SUPPORT STRUCTURES WITH NEW PN 601R95159-35 PO T- 56457, REF CRJ 200
- [SDR SWIA202053319](https://openairdocs.org/sdr/SWIA202053319.md): Angle · cracked · Sep 12, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY CLIP BETWEEN FS 621 INTERCOSTAL AT STR 14 RT AND FRAME FS 625.30 HAS EVIDENCE OF CRACK. C-CHECK RO 10/13/2020. REPLACED AFT EQUIPMENT BAY CLIP BETWEEN FS 621 INTERCOSTAL AT STGR 14R AND FRAME FS 625.30, REF CRJ 200 SRM AND REO, SEE CONTINUA
- [SDR SWIA202053337](https://openairdocs.org/sdr/SWIA202053337.md): Seat Track · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT RAIL HAS CORROSION AT FS 473. C-CHECK RO 10/13/2020. REPLACED LT SIDE SEAT RAIL AT FS 473 WITH A NEW FABRICATED SEAT RAIL, REF MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053336](https://openairdocs.org/sdr/SWIA202053336.md): Seat Track · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 HAS TOOLING MARKS AT FS 559+16 AND CORROSION AT FS 559+64 FS 559+80. C-CHECK RO 10/13/2020. REPLACED SEAT TRACK AT RBL 9 FS 559+16-FS 559+80 WITH NEW FABRICATED PART, REF REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053318](https://openairdocs.org/sdr/SWIA202053318.md): Frame · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 333 IS CORRODED ON AFT SIDE AT STR 21L. C-CHECK RO 10/13/2020. REMOVED CORROSION AT FS 333 FRAME AT STGR 21L, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FRAME SECTION AT FS 333.00 FROM STGR 18L TO STGR 23L, REF CRJ200 SRM AND DWG. OPS
- [SDR SWIA202053317](https://openairdocs.org/sdr/SWIA202053317.md): Intercostal · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STR 21L BETWEEN FS 333 AND FS 349 IS CORRODED. C-CHECK RO 10/13/2020. PART IS OUT OF LIMITS, PART CONTAINS ROLLING CORROSION OVER TWO OR MORE ELEMENTS. INTERCOSTAL HAS MORE THAN 30% OF ITS LENGTH UNDER CORROSION, REF CRJ200 SRM. REMOVED THE
- [SDR SWIA202053316](https://openairdocs.org/sdr/SWIA202053316.md): Frame · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 605 IS CORRODED BETWEEN STR 24L AND 27. C-CHECK RO 10/13/2020. BLENDED OUT CORROSION ON FS 605.00 FRAME FROM STGR 27 TO 24L, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LOWER FRAME SECTOR AT FS 605 FROM STR 20L TO STR 20R,
- [SDR SWIA202053315](https://openairdocs.org/sdr/SWIA202053315.md): Strap · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON TRANSVERSE FLOOR BEAM UPPER STRAP OUTBOARD OF LBL 27 AT FS 349. C-CHECK RO 10/13/2020. REMOVED AND REPLACED TRANSVERSE FLOOR BEAM UPPER STRAP OUTBOARD OF LBL 27 AT FS 349, REF BOMBARDIER DWG STS EA, CRJ-200 SRM.
- [SDR SWIA202053314](https://openairdocs.org/sdr/SWIA202053314.md): Strap · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF RBL 27 IS CORRODED. C-CHECK RO 10/13/2020. BLENDED CORROSION ON SUPPORT STRAP AT RBL 27 FS 559, REF CRJ200 SRM. ORIGINAL MATERIAL.050, IAW CRJ 200 SRM AFTER REWORK.043 MATERIAL LOSS.007, MAXIMUM ALLOWED.005 AREA
- [SDR SWIA202053313](https://openairdocs.org/sdr/SWIA202053313.md): Strap · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP AT FS 559 OUTBOARD OF LBL 27 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED OUT OF LIMITS STRAP AND INSTALLED NEW SUPPORT STRAP AT LBL 27 FS 559, REF CRJ200 SRM AND DWG.
- [SDR SWIA202053312](https://openairdocs.org/sdr/SWIA202053312.md): Angle · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD OF SERVICE DOOR SURROUND FLOOR SILL HAS CORROSION APPROXIMATELY FS 319.70 TO FS 310.00, MARKED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT ATTACHING ANGLE AT FS 310.00 TO APPROXIMATELY FS 318.00, REF CRJ200 SRM AND DWG. BLENDED OUT CORROSION, WITHIN
- [SDR SWIA202053311](https://openairdocs.org/sdr/SWIA202053311.md): Door Sill · corroded · Sep 11, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SURROUND LOWER SILL HAS CORROSION, MARKED. C-CHECK RO 10/13/2020. SERVICE DOOR LOWER SILL FOUND TO BE OUT OF LIMITS, REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS. REMOVED AND REPLACED WITH NEW SERVICE DOOR LOWER SILL, REF CRJ200 SRM AND
- [SDR SWIA202053310](https://openairdocs.org/sdr/SWIA202053310.md): Support Bracket · cracked · Sep 10, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RADAR LOWER SUPPORT BRACKET STIFFNER AT FS 169 HAS A SUSPECTED CRACK ON THE RT SIDE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RADAR LOWER SUPPORT BRACKET P/N: 601-34010-39, REF BOMBARDIER DWG CRJ-200 SRM. OPERATIONAL CHECKS GOOD, REFERENCE THE CONTINUE C
- [SDR SWIA202053309](https://openairdocs.org/sdr/SWIA202053309.md): Floor Support · corroded · Sep 9, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE RT FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 409+128 AND FS 559, MARKED WITH RED GREASE PENCIL. C-CHECK RO 10/13/2020. REPAIRED THE RT FLOOR SILL PANEL MULTIPLE SPOTS OF CORROSION BETWEEN FS 409+128 AND FS 559, REF REO. SEE CONTINUATIO
- [SDR SWIA202053308](https://openairdocs.org/sdr/SWIA202053308.md): Floor Support · corroded · Sep 9, 2020 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE LT FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 409+128 AND FS 559. MARKED WITH RED GREASE PENCIL. C-CHECK RO 10/13/2020. REPAIRED CORROSION DAMAGE ON LT PRESSURE FLOOR SILL PANEL, REF REO. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/aircraft/N494CA/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 = 'N494CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N494CA/reports

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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.