# Service difficulty reports: N496CA

A list on [N496CA](https://openairdocs.org/aircraft/N496CA.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 4 · 163 reports

- [SDR SWIA2026032576216](https://openairdocs.org/sdr/SWIA2026032576216.md): Frame · corroded · Mar 25, 2026 · N496CA · Cndair CL6002B19 · Fuselage Main, Frame
  > POSSIBLE CORROSION BELOW WL STA 605.30 BTW STR 24L AND STR 24R. REMOVED AND REPLACED FRAME AT FS 605.30 IAW SRM 51-42-06 AND 51-40-11.
- [SDR SWI2025F01086](https://openairdocs.org/sdr/SWI2025F01086.md): Acm · smoke · Aug 16, 2025 · N496CA · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK STARTED HEATING UP AND SMELLING HOT, SHUT PACK OFF, RESTARTED PACK 1 MINUTE LATER AND SMOKE STARTED BLOWING OUT OF THE FLIGHT DECK AIR VENTS, SHUT PACK OFF. (FLIGHT 5861 - FILED CLOSED)FOUND LEFT PACK TO BE SEIZED AND CAUSING HOT PACK TEMPS AND SM
- [SDR SWIA2025071100009](https://openairdocs.org/sdr/SWIA2025071100009.md): Acm · smoke · Jul 9, 2025 · N496CA · Cndair CL6002B19 · Cabin Cooling System
  > COCKPIT FILLED WITH SMOKE DURING TAXI. SHORTLY AFTER, L PACK FAULT MESSAGE. QRH STOPPED SMOKE FROM CONTINUING. (FLIGHT 5306 - FILED CLOSED)PILOT REPORTED SMOKE IN COCKPIT WITH LITTLE SMOKE IN CABIN. COMPLIED WITH FIM FOR ABNORMAL SMELL REF FIM 21-21-00. ISOL
- [SDR SWI2025F00768](https://openairdocs.org/sdr/SWI2025F00768.md): Engine · smoke · Jun 26, 2025 · N496CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AFTER STARTING ENGINE 2 (FOR SINGLE ENGINE TAXI) TURNED PACKS ON AND STARTED TO HEAR A WHIRRING NOISE. SUBSEQUENTLY, SECONDS LATER WHAT WOULD APPEAR TO BE SMOKE WAS ENTERING THE COCKPIT WITH A BAD AROMA.IMMEDIATELY TURNED PACKS OFF.STARTED ENGINE 1 AND PULLED
- [SDR SWIA202404250018](https://openairdocs.org/sdr/SWIA202404250018.md): Skin · gouged · Apr 18, 2024 · N496CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND GOUGES AND TOOLING MARKS BETWEEN TWO LOCK FASTENERS AT RBL45 AT WING REAR SPAR DATUM/TRAILING EDGE OF WING PLANK INSIDE OF THE FUEL CELL. (C-CHECK RO 4/24/2024) COMPLIED WITH REO 601R-57-21-3837 REV: (--) DATED: 2024-04-20 STEPS 1-8 FOR REPAIRING THE
- [SDR SWIA202404250292](https://openairdocs.org/sdr/SWIA202404250292.md): Bracket · cracked · Apr 10, 2024 · N496CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF AFT PRESSURE BUILKHEAD AT FS621.00 JUST OUTBOARD OF LBL 36.20 AND IN LINE WITH STRINGER 15L, INTERCOSTAL/CLEAT CRACKED. (C-CHECK RO 4/24/2024) REMOVED AND REPLACED INTERCOSTAL/CLEAT ON AFT SIDE OF AFT PRESSURE BUILKHEAD AT FS621.00 JUST OUTBOAR
- [SDR SWIA202404250010](https://openairdocs.org/sdr/SWIA202404250010.md): Fairing · damaged · Apr 10, 2024 · N496CA · Cndair CL6002B19 · Aerodynamic Fairings
  > CHAFING DAMAGE FROM MLG FAIRING ON WING LWR AFT SKIN PLANK LBL45 AND RBL45 AT WING REAR SPAR DATUM/TRAILING EDGE OF WING PLANK. (C-CHECK RO 4/24/2024) REPAIRED CHAFING DAMAGE FROM MLG FAIRING ON WING LWR AFT SKIN PLANK LBL45 AND RBL45 AT WING REAR SPAR DAT
- [SDR SWIA202404250004](https://openairdocs.org/sdr/SWIA202404250004.md): Skin · dented · Apr 4, 2024 · N496CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE FUSELAGE SKIN DENTS BETWEEN FS605.00 - FS589.00 AND STRINGERS 23R - 26R. (C-CHECK RO 4/24/2024) PERFORMED TEMPORARY REPAIR OF 3 FUSELAGE SKIN DENTS BETWEEN FS605.00 - FS589.00 AND STRINGERS 24R - 26R IN REF TO REO 601R-53-61-8184, REV--, DATED 202
- [SDR SWIA202404250291](https://openairdocs.org/sdr/SWIA202404250291.md): Floor Support · corroded · Apr 1, 2024 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL AT RBL 36.00 HAS 4 SPOTS OF CORROSION BETWEEN FS 409.00+128 AND FS 559.00. (C-CHECK RO 4/24/2024) BLENDED AND TREATED 4 SPOTS OF CORROSION ON RH PRESSURE FLOOR SILL AT RBL 36.00 BETWEEN FS 409.00+128 AND FS 559.00 IN REF TO REO 601R-
- [SDR SWIA2024042500001](https://openairdocs.org/sdr/SWIA2024042500001.md): Floor Support · corroded · Apr 1, 2024 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL AT LBL 36.00 HAS 8 SPOTS OF CORROSION BETWEEN FS 409.00+128 AND FS 559.00. (C-CHECK RO 4/24/2024) BLENDED AND TREATED 8 SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL AT LBL 36.00 BETWEEN FS 409.00+128 AND FS 559.00 IN REF TO REO 601R-
- [SDR SWIA202156467](https://openairdocs.org/sdr/SWIA202156467.md): Flap · corroded · Feb 21, 2021 · N496CA · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE CORRODED L/H WING OUTBD FLAP INBD BUTE DOOR SERRATED STOP ASSY P/N 601R10353-1 (C-CHECK) RO 2/25/2021. RECIEVED L/H WING OUTBD FLAP INBD BUTE DOOR SERRATED STOP ASSY P/N 601R10353-1 REF CRJ 200 SRM 51-77-00.
- [SDR SWIA202156466](https://openairdocs.org/sdr/SWIA202156466.md): Bulkhead · corroded · Feb 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 9G BULKHEAD HAS 2 CORRODED MOUNT BOLTS AND 1 MOUNT FITTING THAT NEEDS TO BE REPLACED (C-CHECK) RO 2/25/2021. RECEIVED AND REPLACED 2 MOUNT BOLTS AND 1 MOUNT FITTING FOR THE 9G BULKHEAD REF CRJ 200 SRM 51-41-02.
- [SDR SWIA202156452](https://openairdocs.org/sdr/SWIA202156452.md): Web · elongated · Feb 3, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Frame
  > L/H BATT RIB WEB AT WS 48.30 HAS EXISTING ELONGATED HOLE IN TOP FWD CORNER. (C-CHECK) RO 2/25/2021. L/H BATT RIB WEB AT WS 48.30 REMOVED AND REPLACED WITH NEW PART REF DWG 601R10204 REV-J AND REO 601R-57-21-3419 REV -- DATED 2021-02-08. COMPLETED SKYWEST TA
- [SDR SWIA202156451](https://openairdocs.org/sdr/SWIA202156451.md): Frame · elongated · Feb 2, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND ELONGATED HOLE, IN FWD LOWER FLANGE ON FS589 FRAME, INBD SIDE OF STRG L26 (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED FRAME FS589 FWD LWR FLANGE INBE SIDE OF STRG 26L REF CRJ 200 SRM 53-00-15 AND CRJ 200 SRM 51-42-06 / PERFORMED PRESSURIZATION CHECK OF
- [SDR SWIA202156455](https://openairdocs.org/sdr/SWIA202156455.md): Stiffener · cracked · Jan 30, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STIFFENER FOR PAX DOOR MOTOR IS CRACKED (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED 1 EA STIFFENER ON PAX DOOR AFT WEB P/N 601R317745-7. REF: CRJ-200 SRM 51-42-06 AND DRAWING 601R31707 REV -E.
- [SDR SWIA202156450](https://openairdocs.org/sdr/SWIA202156450.md): Intercostal · corroded · Jan 29, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PAX DOOR INTERCOSTAL DD3 BETWEEN FS32.00 AND FS338.00 IS CORRODED. (C-CHECK) RO 2/25/2021. INSTALLED NEW INTERCOSTAL DD3 P/N 601R318056-1S. REF: CRJ-200 SRM 51-42-21 AND DWG601R31702, REV-N. C/W 51-900-1003-SKY. LEAK CHECK GOOD.
- [SDR SWIA202156449](https://openairdocs.org/sdr/SWIA202156449.md): Former · corroded · Jan 29, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT FORMER FS347.25 IS CORRODED (C-CHECK) RO 2/25/2021. INSTALLED NEW PAX DOOR FORMER FS347.25 P/N 601R318034-5. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N LEAK CHECK GOOD. C/W 51-900-1003-SKY.
- [SDR SWIA202156448](https://openairdocs.org/sdr/SWIA202156448.md): Former · corroded · Jan 29, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Frame
  > PAX FWD FORMER FS311.75 IS CORRODED. (C-CHECK) RO 2/25/2021. REMOVED AND INSTALLED NEW PAX DOOR FORMER FS311.75. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N / COMPLIED WITH TASK CARD 51-900-1003-SKY / PERFORMED PRESSURIZATION
- [SDR SWIA202156447](https://openairdocs.org/sdr/SWIA202156447.md): Angle · cracked · Jan 28, 2021 · N496CA · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > L/H BATT RIB WS48.30 FWD UPPER ANGLE CRACKED. (C-CHECK) RO 2/25/2021. REPLACED LH BATT RIB WS48.30 FWD UPPER ANGLE PER REO 601R-57-21-3416 REV -- DATED 2021-02-01 AND DRAWING 601R10204 REV J AND DRAWING 601R10212 REV A AND CRJ200SRM 51-42-21 REV 38 DATED 10
- [SDR SWIA202156454](https://openairdocs.org/sdr/SWIA202156454.md): Intercostal · cracked · Jan 25, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > INTERCOSTAL BETWEEN FS621 AND FS625 AT APPROX STR13R, IS CRACKED. (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS621 AND FS625 AT STGR 13R P/N 601-35012-52 REF CRJ200 SRM51-42-21.
- [SDR SWIA202156446](https://openairdocs.org/sdr/SWIA202156446.md): Doubler · elongated · Jan 23, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES FOUND ON DOUBLER AT FS621 LBL9 ATTACHED TO LH OUTBOARD END ATTACH ANGLE. (C-CHECK) RO 2/25/2021. INSTALLED NEW DOUBLER AT FS621, LBL9, REF CRJ 200 SRM 51-42-21, & BOMBARDIER REO 601R-53-61-117, REV -E, DATE 2018-01-15 / COMPLIED WITH TASK
- [SDR SWIA202156468](https://openairdocs.org/sdr/SWIA202156468.md): Fitting · chafed · Jan 22, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PASSENGER DOOR FORWARD UPPER PIN STOP FITTING ON FUSELAGE HAS CHAFES/SCRATCHES (MARKED). (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED PAX DOOR FWD UPPER PIN STOP FITTING ON FUSELAGE SIDE REF CRJ 200 SRM 51-41-02 PERFORMED OPERATIONAL CHECK GOOD. ?
- [SDR SWIA202156445](https://openairdocs.org/sdr/SWIA202156445.md): Bracket · broken · Jan 21, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Frame
  > UPON INSPECTION OF TASK CARD 53-900-511 AUDIT FOUND T BRACKET AT FS 499 ON R/H SIDE BROKEN. (C-CHECK) RO 2/25/2021 INSTALLED NEW CLEAT P/N 601R38605-3 I.A.W. DRW 601R38605 REV. NC REF. CRJ200 SRM 51-42-21 / COMPLIED WITH TASK CARD 51-900-1003-SKY / PERFORMED P
- [SDR SWIA202156444](https://openairdocs.org/sdr/SWIA202156444.md): Spar · cracked · Jan 21, 2021 · N496CA · Cndair CL6002B19 · Elevator, Spar/Rib
  > LH ELEVATOR HAS CRACKED SPAR LIP AT LOWER INBOARD NUTPLATE NEAR RIB 1. (C-CHECK) RO 2/25/2021 COMPLIED WITH REO 601R-55-21-539 REV -- DATED 2021-01-26 FOR REPAIR CRACK ON LH ELEVATOR SPAR AT LOWER LIP INBOARD NEAR RIB 1. COMPLIED WITH SKY CARD 51-900-1003
- [SDR SWIA202156470](https://openairdocs.org/sdr/SWIA202156470.md): Spoiler · dented · Jan 20, 2021 · N496CA · Cndair CL6002B19 · Spoilers
  > RH INBD GROUND SPOILER HAS 2EA SMALL DENTS IN THE LWR SKIN (C-CHECK) RO 2/25/2021. FOUND DENTS ON RH INBOARD GROUND SPOILER TO BE OUT OF LIMITS CRJ200 SRM 57-71-00. REMOVED AND INSTALLED SERVICEABLE RH INBOARD GROUND SPOILER REF CRJ200 AMM 27-65-01-000-801 A
- [SDR SWIA202156443](https://openairdocs.org/sdr/SWIA202156443.md): Intercostal · corroded · Jan 20, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PAX DOOR DD4 INTERCOSTAL HAS EVIDENCE OF CORROSION AT THE FS 329.76 FORMER. (C-CHECK) RO 2/25/2021 REMOVED AND INSTALLED NEW PAX DOOR FORMER FS311.75. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31702 REV N / COMPLIED WITH TASK CARD 5
- [SDR SWIA202156442](https://openairdocs.org/sdr/SWIA202156442.md): Floor Support · corroded · Jan 20, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON FLOOR BEAM CAP AT RBL.9 FROM FS.409 TO FS.409+128. (C-CHECK) RO 2/25/2021 FLOOR BEAM CAP AT RBL 9 BETWEEN FS 409.00+5 AND FS 409.00+118 REMOVED AND REPLACED WITH NEW FABRICATED PART REF DWG 601R31117 REV E AND REO 601R-53-
- [SDR SWIA202156441](https://openairdocs.org/sdr/SWIA202156441.md): Stringer · cracked · Jan 20, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 310 - STGR 9R - STRINGER CRACKED AS MARKED (C-CHECK) RO 2/25/2021 FABRICATED AND INSTALLED REPAIR SPLICE TO STRINGER 9R FS310 REF REO 601R-53-21-3393 REV.-- DATED 2021-02-08 / COMPLIED WITH TASK CARD 51-900-1003-SKY / PERFORMED PRESSURIZATION CHECK OF R
- [SDR SWIA202156440](https://openairdocs.org/sdr/SWIA202156440.md): Pressure Deck · corroded · Jan 18, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H PRESSURE FLOOR SILL ANGLEL IS CORRODED AT MULTIPLE SPOTS MARKED IN BLACK. (C-CHECK) RO 2/25/2021 REPAIRED THE R/H PRESSURE FLOOR SILL ANGLE BETWEEN FS499 AND FS559 REF BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ 601R-53-41-2862 REV -
- [SDR SWIA202156439](https://openairdocs.org/sdr/SWIA202156439.md): Pressure Deck · corroded · Jan 18, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H PRESSURE FLOOR SILL PANEL IS CORRODED AT MULTIPLE SPOTS MARKED IN BLACK. (C-CHECK) RO 2/25/2021 REPAIRED R/H PRESSURE FLOOR SILL PANEL CORROSION AT MULTIPLE SPOTS REF REO 601R-53-41-666 REV C DATE 2012-11-06 C/W 51-900-1003 SKY
- [SDR SWIA202156438](https://openairdocs.org/sdr/SWIA202156438.md): Pressure Deck · corroded · Jan 18, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H PRESSURE FLOOR SILL PANEL IS CORRODED AT MULTIPLE SPOTS MARKED IN BLACK. (C-CHECK) RO 2/25/2021 BLENDED AND NDT INSPECTED ALL LOCATIONS FOR THICKNESS AND CRACKS, EVALUATED AND REPAIRED LH FLOOR SILL PANEL BETWEEN FS409+128 AND FS559. REF BOMBARDIER RE
- [SDR SWIA202156437](https://openairdocs.org/sdr/SWIA202156437.md): Hydraulic Line · chafed · Jan 18, 2021 · N496CA · Cndair CL6002B19 · Hydraulic System, Main
  > L/H MLG BAY RETRACT ACTUATOR HYDRAULIC LINE IS CHAFING AGAINST THE ATTACH BRACKET. (C-CHECK) RO 2/25/2021 REMOVED EDGE DAMAGE FROM L/H MLG BAY RETRACT ACTUATOR FITTING, ENSURED DAMAGE HAS A SMOOTH CONTOUR, BLENDED AREA DID NOT EXCEED REPORTED DEPTH NO FURT
- [SDR SWIA202156436](https://openairdocs.org/sdr/SWIA202156436.md): Bracket · cracked · Jan 18, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > R/H MLG BAY HYDRAULIC FUSE BRACKET IS CRACKED. (C-CHECK) RO 2/25/2021 REMOVED AND INSTALLED 1EA NEW HYDRAULIC FUSE BRACKET P/N 601R75278-11 ON R/H MLG BAY. REF CRJ 200 SRM 51-42-06 AND DWG: 601R75278 REV NC. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-
- [SDR SWIA202156465](https://openairdocs.org/sdr/SWIA202156465.md): Seat Track · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL27 SEAT TRACK BETWEEN FS559+80 AND FS559+94 HAS CORROSION (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED NEW FLOOR SEAT TRACK P/N 601R38779-9 AT LBL 27 BETWEEN FS559+80 AND FS559+94 REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202156464](https://openairdocs.org/sdr/SWIA202156464.md): Seat Track · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK HAS CORROSION BETWEEN FS559+16 AND FS559+80 (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED NEW RBL9 SEAT TRACK P/N 601R31032-9 REF REO 601R-53-00-485, REV-D, DATED 2018-01-29. SEE CONTINUE CARD FOR DETAILS ON WORK PERFORMED. ORDERED NEW HARDWARE
- [SDR SWIA202156463](https://openairdocs.org/sdr/SWIA202156463.md): Seat Track · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK HAS CORROSION BETWEEN FS559+16 AND FS559+80 (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED. NEW FLOOR SEAT TRACK P/N 601R31032-9 FROM LBL9 AT FS559-16 AND FS 559+80. REF REO 601R-53-00-485 REV -D, DATED 2018-01-29 AND CRJ200 AMM 53-01-11-400-80
- [SDR SWIA202156435](https://openairdocs.org/sdr/SWIA202156435.md): Bracket · cracked · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Landing Gear Brake System
  > L/H MAIN LANDING GEAR WHEEL WELL, BRAKE PRESSURE TRANSDUCER BRACKET ON BOTTOM OF PRESSURE FLOOR PANEL IS CRACKED. (C-CHECK) RO 2/25/2021 REMOVED AND INSTALLED NEW BRAKE PRESSURE TRANSDUCER BRACKET (P/N 601R75262-159) ON BOTTOM OF PRESSURE FLOOR PANEL FROM
- [SDR SWIA202156434](https://openairdocs.org/sdr/SWIA202156434.md): Skin · dented · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL SKIN IS DENTED JUST ABOVE HANDLE HOUSING, MARKED. (C-CHECK) RO 2/25/2021 REPAIRED CARGO DOOR INTERNAL SKIN JUST ABOVE HANDLE HOUSING REF REO 601R-52-31-338 REV.-- DATED 2021-02-05 AND COMPLIED WITH SKY CARD 51-900-1003-SKY
- [SDR SWIA202156433](https://openairdocs.org/sdr/SWIA202156433.md): Support Beam · cracked · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > * CARGO - DOOR TRACK SUPPORT BEAM AFT LOWER ATTACH ANGLE AT FS621 IS CRACKED (C-CHECK) RO 2/25/2021 INSTALLED NEW LOWER ATTACH ANGLE ON CARGO DOOR SUPPORT BEAM AT FS621 REF. CRJ200 SRM 51-42-21 REV 38, DATED JUL 10/19, AND DWG 601R35050 REV. AC. / PERFORME
- [SDR SWIA202156432](https://openairdocs.org/sdr/SWIA202156432.md): Cargo Track · cracked · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * CARGO - FWD TRACK SUPPORT AT FS574 LOWER AFT "C" CHANNEL CRACKED AT RIVET LOCATION. (C-CHECK) RO 2/25/2021 RREMOVED AND REPLACED THE FWD TRACK SUPPORT AT FS574 LOWER AFT "C" CHANNEL WITH NEW PART AND FASTENERS REF. CRJ200 SRM 51-41-02 & DWG 601R35050 REV
- [SDR SWIA202156431](https://openairdocs.org/sdr/SWIA202156431.md): Door Sill · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR FLOOR SILL HAS CORROSION BETWEEN FS576 AND FS605 AND CRACKED AT FS605 RIVET LOCATION (C-CHECK) RO 2/25/2021 REMOVED AND REPLACED CARGO DOOR FLOOR SILL (P/N: 601R35011-63) REF CRJ 200 SRM 51-42-06, & BOMBARDIER DWG 601R35011 REV -R. PRESSURE CHEC
- [SDR SWIA202156430](https://openairdocs.org/sdr/SWIA202156430.md): Floor Support · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR BEAM CAP HAS CORROSION BETWEEN FS589 AND FS605 (C-CHECK) RO 2/25/2021 REMOVED AND REPLACED LBL9 FLOOR BEAM CAP BETWEEN FS589 AND FS605 P/N 601R35031-263 REF REO NO. 601R-53-61-3780 REV -A DATED 2011-07-05. C/W 51-900-1003-SKY
- [SDR SWIA202156429](https://openairdocs.org/sdr/SWIA202156429.md): Floorbeam · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL27 FLOOR BEAM CAP HAS CORROSION BETWEEN FS559+109 AND FS559+118 (C-CHECK) RO 2/25/2021 REMOVED AND REPLACED LBL27 FLOOR BEAM CAP FROM FS559+10 TO 559+118, REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-34, CRJ200 SRM 51-45-00, CRJ200 SRM 51-42-22, DWG 601R31
- [SDR SWIA202156428](https://openairdocs.org/sdr/SWIA202156428.md): Floorbeam · corroded · Jan 16, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * RBL9 FLOOR BEAM CAP HAS CORROSION MULTIPLE PLACES STARTING AT APPROXIMATELY FS559+10 TO FS559+80 (C-CHECK) RO 2/25/2021 REMOVED AND REPLACED RBL9 FLOOR BEAM CAP FROM FS559+10 TO 559+80. REF DWG 601R31119, REV-H, CRJ200 SRM'S 51-42-21, 51-42-22, 51-42-34,
- [SDR SWIA202156462](https://openairdocs.org/sdr/SWIA202156462.md): Seat Track · corroded · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CORROSION ON LBL9 SEAT TRACK AT MULTIPLE LOCATIONS BETWEEN FS399 AND FS 409+124 (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED NEW FLOOR SEAT TRACK P/N 601R31032-21 FROM LBL9 AT FS399.00+16 TO FS 409.00+124. REF REO 601R-53-00-485 REV -D, DATED 2018-01-29 AND
- [SDR SWIA202156427](https://openairdocs.org/sdr/SWIA202156427.md): Stiffener · cracked · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Wing Miscellaneous Structure
  > *R/H BATT RIB AT WING STATION 48.30 IS CRACKED. (C-CHECK) RO 2/25/2021 REMOVED AND REPLACED BATT RIB ANGLE(P/N: 600-10389-2) AT R/H WING STATION 48.30 REF. CRJ200SRM 51-42-21, DWG 601R10204 REV -J, AND DWG 601R10212 REV A. / COMPLETED SKYWEST TASK CARD 51-
- [SDR SWIA202156426](https://openairdocs.org/sdr/SWIA202156426.md): Isolator · damaged · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > (3EA) REAR PRESSURE BULKHEAD F.S. 621.00, WALL PANEL ATTACHMENT NUT ISOLATOR (ATTACHMENT/ANGLES) FOUND DAMAGED. (1EA) ANGLE "CRACKED" FAR R/H SIDE OF BULKHEAD @ APROX STGR 14 LEVEL, (1EA) ANGLE BENT/DISTORTED AT RBL 9.00 @APROX STGR 8 LEVEL, AND (1EA) ANGLE BE
- [SDR SWIA202156425](https://openairdocs.org/sdr/SWIA202156425.md): Angle · cracked · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE ATTACHED TO FS621 AT FLOOR LEVEL €“ CRACKED ON LH OUTBOARD END (MARKED). (C-CHECK) RO 2/25/2021 REMOVED AND AND INSTALLED NEW ANGLE ATTACHED TO FS621 AT FLOOR LEVEL LH OUTBOARD END REF CRJ200 SRM 51-42-06, 51-42-21, AND REO 601R-53-61-117 REV-E, DAT
- [SDR SWIA202156424](https://openairdocs.org/sdr/SWIA202156424.md): Strap · corroded · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP OUTBOARD OF RBL 27 AT FS559. (C-CHECK) RO 2/25/2021 RBL27 O/B STARP AT FS559 IS OUT OF LIMITS DUE TO OVER 30% OF THE LENGTH, REF CRJ 200 SRM 53-00-00, REMOVED AND REPLACED PART WITH NEW, REF CRJ 200 SRM 51-42-06, & BOMBARDIER DWG# 601R3
- [SDR SWIA202156423](https://openairdocs.org/sdr/SWIA202156423.md): Strap · corroded · Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP OUTBOARD OF LBL 27 AT FS559. (C-CHECK) RO 2/25/2021 REMOVED CORROSION ON STRAP O/B OF LBL27 AT FS559, REF: CRJ 200, SRM 51-21-06, STRAP FOUND TO BE OUT OF LIMITS, REF: SRM 53-00-00, REMOVED AND REPLACED PART WITH NEW, REF: CRJ 200, BOMB

Next page: https://openairdocs.org/aircraft/N496CA/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 = 'N496CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N496CA/reports

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