# Service difficulty reports: N479CA

A list on [N479CA](https://openairdocs.org/aircraft/N479CA.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 · 187 reports

- [SDR SWIA2026040275665](https://openairdocs.org/sdr/SWIA2026040275665.md): Windshield · cracked · Apr 2, 2026 · N479CA · Cndair CL6002B19 · Flight Compartment Windows
  > CA SIDE WINDSHIELD CRACKED IN CRUISE (FLIGHT 5852) REMOVED AND REPLACED CA WINDSHIELD AND PERFORMED OPERATIONAL CHECKS IN REF WITH AMM 56-11-01. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2026031875544](https://openairdocs.org/sdr/SWIA2026031875544.md): Mount · cracked · Feb 15, 2026 · N479CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR, FWD AND AFT BALANCE SPRING BOXES MOUNTING PLATES CRACKED AROUND BALANCE SPRING BOX MOUNTING BOLTS. REMOVED AND INSTALLED NEW AFT CARGO DOOR BALANCE SPRING BOX FWD AND AFT MOUNTING PLATE IAW DWG 601R35055, REV T AND SRM 51-42-06. OPS TEST GOOD.
- [SDR SWIA2026031875548](https://openairdocs.org/sdr/SWIA2026031875548.md): Intercostal · corroded · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED. REPAIRED THE INTERCOSTAL BY REMOVING AND REPLACING IAW SRM 51-42-0, AND DWG 601R31702, REV N.
- [SDR SWIA2026031875546](https://openairdocs.org/sdr/SWIA2026031875546.md): Doubler · cracked · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR FWD PULL, IN CAM DOUBLER. REMOVED AND INSTALLED A NEW PAX DOOR FWD PULL IN CAM DOUBLER IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702 REV N.
- [SDR SWIA2026011175542](https://openairdocs.org/sdr/SWIA2026011175542.md): Intercostal · cracked · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR AFT DD1 INTERCOSTAL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, & DWG 601R31702, REV N. LEAK CHECK GOOD.
- [SDR SWIA2026031875531](https://openairdocs.org/sdr/SWIA2026031875531.md): Angle · gouged · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL FWD PULL IN LEVER FOUND PAX DOOR ANGLE SUPPORT DEEP GOUGE. REPAIRED FWD PULL IN LEVER PAX DOOR ANGLE SUPPORT DAMAGE BY REMOVING AND REPLACING WITH A NEW SERVICEABLE SUPPORT ANGLE IAW SRM 51-42-06, 51-42-21, & DWG 601R31702, REV N.
- [SDR SWIA2026031875528](https://openairdocs.org/sdr/SWIA2026031875528.md): Cleat · corroded · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AT DD1A LOCATION BETWEEN MID AND AFT INTERCOSTAL CLEATS ARE CORRODED. REMOVED AND INSTALLED 2 NEW CLEATS ON PAX DOOR AT DD1A LOCATION BETWEEN MID AND AFT INTERCOSTAL IAW SRM 51-42-06, AND DWG 601R31702, REV N.
- [SDR SWIA2026031875524](https://openairdocs.org/sdr/SWIA2026031875524.md): Bracket · misrepaired · Jan 11, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER AT BS 347.25 UNAUTHORIZED PLUG REPAIR AT PULLEY MOUNTING BRACKET LOCATION. REPAIRED PAX DOOR AFT FORMER AT BS 347.25 BY REMOVING AND REPLACING PAX DOOR AFT FORMER. IAW SRM 51-42-21, SRM 51-42-06, AND DWG 601R31702, REV N.
- [SDR SWIA2026031875537](https://openairdocs.org/sdr/SWIA2026031875537.md): Intercostal · corroded · Jan 10, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD2 INTERCOSTAL IS CORRODED. THE INTERCOSTAL WAS REMOVED & REPLACED WITH NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702 REV N.
- [SDR SWIA2026031875532](https://openairdocs.org/sdr/SWIA2026031875532.md): Intercostal · corroded · Jan 10, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD3 INTERCOSTAL IKS CORRODED. REMOVED AND REPLACED WITH NEW PAX DOOR MID DD3 INTERCOSTAL IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R31702, REV N. RESTORED FINISH ALL FASTENERS AND APPLIED CIC AT REPAIR LOCATION IAW SRM 51-25-16, & SRM 51-21-11. A
- [SDR SWIA2026011075529](https://openairdocs.org/sdr/SWIA2026011075529.md): Former · corroded · Jan 10, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER, FS329.41 BETWEEN DD5 AND DD6 INTERCOSTAL IS CORRODED. REPAIRED PAX DOOR FORMER FS329.41 BETWEEN DD5 AND DD6 INTERCOSTAL BY REMOVING AND REPLACING WITH A NEW SERVICEABLE FORMER. IAW SRM 51-42-06 AND DWG 601R31702, REV N. MAJOR REPAIR, LEAK C
- [SDR SWIA2026031875543](https://openairdocs.org/sdr/SWIA2026031875543.md): Intercostal · corroded · Jan 8, 2026 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MID DD6 INTERCOSTAL IS CORRODED ( MX 31504355). REPAIRED THE INTERCOSTAL BY REMOVING AND REPLACING WITH A NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R31702, REV N.
- [SDR SWIA2026031875539](https://openairdocs.org/sdr/SWIA2026031875539.md): Angle · corroded · Dec 30, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ON FRAME REINFORCING ANGLE AT BS 589 BETWEEN S20R - 20L. EVALUATED CORROSION ON REINFORCING ANGLE AS OUT-OF-LIMITS. REMOVED CORRODED REINFORCING ANGLE AND INSTALLED A NEW REINFORCING ANGLE IAW SRM 51-42-06, AND DWG 601R36025, REV P, SHEET 1.
- [SDR SWIA2026031875547](https://openairdocs.org/sdr/SWIA2026031875547.md): Floor Support · corroded · Dec 16, 2025 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION NOTED ON FLOOR SUPPORT LBL 9 FROM BS 409 TO 409+128 IN MULTIPLE LOCATIONS. REPAIRED THE FLOOR SUPPORT BY REPLACING IAW REO 601R-53-31-1362, REV -, AND SRM 53-00-43.
- [SDR SWIA2026031875525](https://openairdocs.org/sdr/SWIA2026031875525.md): Frame · corroded · Nov 24, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 589 FWD SIDE FROM STR 26R TO STR 25L HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED FRAME BS 589 BETWEEN STGR 20R AND 20L (PN 601R36025-61) IAW SRM 51-42-06, AND DRAWING 601R35005, REV AG, SHEET 1.
- [SDR SWIA2026031875536](https://openairdocs.org/sdr/SWIA2026031875536.md): Skin · chafed · Nov 22, 2025 · N479CA · Cndair CL6002B19 · Aerodynamic Fairings
  > THE APRON SKIN UNDER THE LT STUB FAIRING IS CHAFED. REPAIRED THE APRON SKIN UNDER THE LT STUB FAIRING BY CUTTING OUT THE DAMAGED PORTION AND REPLACING WITH NEW SKIN PANEL IAW REO 601R-53-41-115, REV -A.
- [SDR SWIA2026031875526](https://openairdocs.org/sdr/SWIA2026031875526.md): Window Frame · cracked · Nov 22, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Structure
  > THE LH WINDSHIELD SIDE POST LOWER INBD ATTACH ANGLE HAS A POSSIBLE CRACK. REMOVED AND REPLACED WITH NEW LT WINDSHIELD SIDE POST INBD FITTING IAW SRM 51-42-21 AND DWG 601R33007, REV U.
- [SDR SWIA2026031875535](https://openairdocs.org/sdr/SWIA2026031875535.md): Lug · damaged · Nov 20, 2025 · N479CA · Cndair CL6002B19 · Ailerons
  > EVALUATE RT AILERON NR 1 OTBD HINGE LUG FOR DAMAGE. REPAIRED THE RT AILERON NR 1 HINGE OTBD HINGE LUG BY BLENDING OUT DAMAGE IAW REO 601R-57-51-1092, REV-.
- [SDR SWIA2026031875530](https://openairdocs.org/sdr/SWIA2026031875530.md): Angle · cracked · Nov 12, 2025 · N479CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT BATT CAP ANGLE AT WS48.3 IS CRACKED. REMOVED AND REPLACED WITH NEW LT BATT CAP ANGLE IAW SRM 51-40-11, SRM 51-42-21, & DWG 600-10389, REV -.
- [SDR SWIA2026031875523](https://openairdocs.org/sdr/SWIA2026031875523.md): Angle · cracked · Nov 12, 2025 · N479CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT BATT CAP ANGLE AT WS 48.3 IS CRACKED. REMOVED CRACKED RT BATT CAP ANGLE AT WS48.3 AND INSTALLED NEW REPLACEMENT IAW DWG 600-10204, REV M, DWG 601R10212, REV A, & SRM 51-42-21.
- [SDR SWIA2026031875533](https://openairdocs.org/sdr/SWIA2026031875533.md): Crossbeam · corroded · Nov 11, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Structure
  > BS 349 CROSSBEAM AFT SUPPORT ANGLE IS CORRODED LOCATED BETWEEN LBL36 AND LBL27. REMOVED AND REPLACED THE CROSSBEAM AFT SUPPORT ANGLE IAW SRM 51-42-06, & DWG 601R38673, REV D.
- [SDR SWIA2026031875540](https://openairdocs.org/sdr/SWIA2026031875540.md): Stringer Clip · corroded · Nov 8, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER CLIP 22L JUST AFT OF FRAME 559+112 CORRODED. R & R STRINGER CLIP IAW DWG 601R31057, REV J, SRM 51-42-06, & 51-42-21.
- [SDR SWIA2026031875538](https://openairdocs.org/sdr/SWIA2026031875538.md): Floor Support · corroded · Nov 8, 2025 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE PRESSURE FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION FROM BS 409+128 - 559. REPAIRED THE DAMAGE ON LT SIDE PRESSURE FLOOR SUPPORT BY BLENDING OUT DAMAGE. EVALUATED BLEND-OUT, FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666, REV C.
- [SDR SWIA2026031875534](https://openairdocs.org/sdr/SWIA2026031875534.md): Shear Tie · corroded · Nov 8, 2025 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION ON FRAME, BS 310, AFT WEB STR 26 - 27 AND TWO AREAS ON THE LOWER FLANGE STR 25 - 27. REMOVED AND INSTALLED NEW BS 310 FRAME LOWER SECTION BETWEEN STGR23L AND STGR 23R IAW SRM 51-42-06 AND 51-42-21 AND DWG 601R32002, REV AD. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2026031875527](https://openairdocs.org/sdr/SWIA2026031875527.md): Floor Support · corroded · Nov 8, 2025 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE PRESSURE FLOOR SILL HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559. REPAIRED RH PRESSURE FLOOR SILL FROM FS409+128 TO FS559.0 BY BLENDING OUT THE CORROSION. EVALUATED, EVALUATION GOOD, FOUND TO BE WITHIN LIMITS. IAW REO 601R-53-41-666, R
- [SDR SWIA2026031875545](https://openairdocs.org/sdr/SWIA2026031875545.md): Skin · chafed · Nov 2, 2025 · N479CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING SKIN CHAFED UNDER PANEL 686AB. REPAIRED THE RIGHT LOWER WING SKIN CHAFED UNDER PANEL 686AB IAW REO 601R-57-21-4005, REV-.
- [SDR SWIA2025030775541](https://openairdocs.org/sdr/SWIA2025030775541.md): Skin · dented · Mar 7, 2025 · N479CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BIRD STRIKE ON FINAL APPROACH AT 400 AGL, STRUCK NOSE BELOW FO WINDSCREEN.. DENT FOUND UNDER FO WINDSHIELD RT FUSELAGE SKIN PANEL BTWN BS 185 - 193, BL 0 - RBL 6.10. REPIARED THE DENT BETWEEN BS 185 - 193, IAW SRM 51-42-06, & DWG 600-33010, REV AD, SHEET 1.
- [SDR SWIA20250109042](https://openairdocs.org/sdr/SWIA20250109042.md): Unknown · smoke · Jan 8, 2025 · N479CA · Cndair CL6002B19 · Air Distribution System
  > A FEW MINUTES AFTER POWER UP USING THE APU WE GOT A SMOKE CARGO WARNING MESSAGE. SMOKE WAS OBSERVED COMING OUT OF THE CARGO COMPARTMENT. SHUT THE AIRCRAFT DOWN AND SMOKE DISSIPATED. FIREX BOTTLES WERE NOT USED.PERFORMED INSPECTION OF THE CARGO COMPARTMENT A
- [SDR SWIA202405310001](https://openairdocs.org/sdr/SWIA202405310001.md): Windshield · cracked · May 30, 2024 · N479CA · Cndair CL6002B19 · Flight Compartment Windows
  > FO SIDE WINDSHIELD CRACKED ONCE HE TAPPED IT TO KILL A MOSQUITO (FLIGHT 5635 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28311221 WITH THE FOLLOWING CORRECTIVE ACTION: "R/R RH WINDSHIELD IAW TASK CARD 56-200-1000-SKY.OPS CHECK AND LEAK CHECK GO
- [SDR SWIA20240118](https://openairdocs.org/sdr/SWIA20240118.md): Flap System · warning message · Jan 18, 2024 · N479CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > D:DUE TO FLAP FAIL CAUTION AT FLAPS 20 ON APPROACH, DID A GO AROUND, RAN QRH, LANDED FLAPS 20.COMPLY WITH FULL FLAP EVAULATION IN REF TO FIM CH 27 AND AD 2009-06-12C:MCICAT A DUE BY TAC 40952****SMOD APPROVAL REQUIRED FOR RTS****FLAP FAIL CAUTION AT FLAPS 20 O
- [SDR SWIA202307170004](https://openairdocs.org/sdr/SWIA202307170004.md): Unknown · warning message · Jul 14, 2023 · N479CA · Cndair CL6002B19 · Landing Gear System
  > ON TAKEOFF CLIMB, RECEIVED €ŒGEAR DISAGREE€? WARNING. NOSE AND RIGHT GEAR NORMAL AND UP, LEFT GEAR RED. LEVELED AT 10K AND REMAINED BELOW 200KIAS. NO ADVERSE CHARACTERISTICS OR UNUSUAL NOISE NOTED, BELIEVED GEAR TO BE IN UP POSITION. RAN QRH FOR UP DISAGREE,
- [SDR SWIA202265427](https://openairdocs.org/sdr/SWIA202265427.md): None · cracked · Mar 16, 2022 · N479CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND OTBD LBL 9 TO F.S. 280 CROSSBEAM ATTACH ANGLE CRACKED. (C-CHECK RO 4/20/2022) REMOVED DAMAGED CROSSBEAM ATTACH ANGLE, FABRICATED AND INSTALLED AT FS 280 TO LBL9 IAW CRJ-200 SRM 51-42-06, 51-42-21, (REFERENCED REO 601R-53-11-171 REV -D DATED 13
- [SDR SWIA202265426](https://openairdocs.org/sdr/SWIA202265426.md): None · cracked · Mar 16, 2022 · N479CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND OTBD RBL 9 TO F.S. 280 CROSSBEAM ATTACH ANGLE CRACKED. (C-CHECK RO 4/20/2022) REMOVED DAMAGED CROSSBEAM ATTACH ANGLE, FABRICATED AND INSTALLED AT FS 280 TO RBL9 IAW CRJ-200 SRM 51-42-06, 51-42-21, 51-24-36, AND 51-40-11 (REFERENCED REO 601R-53-
- [SDR SWIA202265425](https://openairdocs.org/sdr/SWIA202265425.md): None · damaged · Mar 15, 2022 · N479CA · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR LOWER AFT PAN REQUIRES REPLACEMENT. (C-CHECK RO 4/20/2022) REMOVED AND REPLACED SERVICE DOOR LOWER AFT PAN IAW MHIRJ REO# 601R-52-41-481 REV -- DATED 2022-03-15 AND SKYCARD 51-900-1003-SKY AND ATTACHED FORM337. NO WEIGHT CHANGE NOTED. REF C
- [SDR SWIA202265424](https://openairdocs.org/sdr/SWIA202265424.md): None · damaged · Mar 15, 2022 · N479CA · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR LOWER FWD PAN REQUIRES REPLACEMENT. (C-CHECK RO 4/20/2022) REMOVED AND REPLACED SERVICE DOOR LOWER FWD PAN IAW REO 601R-52-41-482 REV -- DATED 2022-03-15. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO
- [SDR SWIA202265423](https://openairdocs.org/sdr/SWIA202265423.md): None · corroded · Mar 15, 2022 · N479CA · Cndair CL6002B19 · Doors
  > FOUND INTERCOSTAL ON PAX DOOR AT DD4 CORRODED. (C-CHECK RO 4/20/2022) REMOVED AND REPLACED INTERCOSTAL ON PAX DOOR AT DD4 IAW CRJ-200-SRM-51-42-06 AND 51-42-21 REV 38B DATED 11/25/2020. SKYCARD 51-900-1003-SKY AND M-337 COMPLETED AND ATTACHED. NO WEIGH
- [SDR SWIA202265422](https://openairdocs.org/sdr/SWIA202265422.md): None · corroded · Mar 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > R/H PRESSURE FLOOR SILL BETWEEN FS 449.85 AND FS 461.00 IS CORRODED, (C-CHECK RO 4/20/2022) REMOVED DAMAGE FROM RH PRESSURE FLOOR SILL BETWEEN FS 449.85 AND FS 461 IAW REO 601R-53-41-3022 REV -- DATED 2022-02-18. COMPLETED SKYWEST TASK CARD 51-900-1003
- [SDR SWIA202265421](https://openairdocs.org/sdr/SWIA202265421.md): None · cracked · Mar 13, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FOUND SPLICE CRACKED ON PREVIOUS FLOOR MEMBER BEAM REPAIR AT FS280.00 OTBD OF RBL 9.00. (C-CHECK RO 4/20/2022) REMOVED DAMAGED SPLICE, FABRICATED AND INSTALLED NEW SPLICE AT FS 280 OTBD OF RBL9 IAW CRJ-200 SRM 51-42-06 (REFERENCED REO 601R-53-11-171 RE
- [SDR SWIA202265420](https://openairdocs.org/sdr/SWIA202265420.md): None · corroded · Mar 13, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON TOP OF FLOOR MEMBER BEAM AT FS280.00 (C-CHECK RO 4/20/2022) COMPLIED WITH REO 601R-53-11-136 REV -A, DATED 2007/11/01, REPAIR TO PILOTS BULKHEAD FS 280.00, LBL 9.0-RBL 9.0,. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED F
- [SDR SWIA202265419](https://openairdocs.org/sdr/SWIA202265419.md): None · damaged · Mar 11, 2022 · N479CA · Cndair CL6002B19 · Ailerons
  > R/H WING AFT MOUNT FLAP HINGE BOX ATTACHMENT I/B AND O/B LUG FITTINGS DAMAGED AT WS220 (C-CHECK RO 4/20/2022) COMPLIED WITH REO 601R-57-21-3579 REV - - DATED 2022-03-14 BLENDING GOUGE DAMAGE TO RHS FLAP HINGE BOXES AND FITTINGS. COMPLETED SKYWEST TA
- [SDR SWIA202265418](https://openairdocs.org/sdr/SWIA202265418.md): None · damaged · Mar 11, 2022 · N479CA · Cndair CL6002B19 · Ailerons
  > R/H WING FLAP HINGE BOX LUG FITTINGS I/B AND O/B DAMAGED AT WS264 FLAP HINGE BOX REQUIRES REMOVAL FOR REPAIR. (C-CHECK RO 4/20/2022) REPAIRED R/H WING FLAP HINGE BOX LUG FITTINGS ON I/B AND O/B POSITIONS AT WS. 264 IAW CRJ 200 REO 601R57-21-3529 REV--
- [SDR SWIA202265417](https://openairdocs.org/sdr/SWIA202265417.md): None · damaged · Mar 11, 2022 · N479CA · Cndair CL6002B19 · Ailerons
  > R/H WING FLAP HINGE BOX LUG FITTINGS I/B AND O/B DAMAGED AT WS178 FLAP HINGE BOX REQUIRES REMOVAL FOR REPAIR. (C-CHECK RO 4/20/2022) COMPLIED WITH REO 601R-57-21-3579 REV - - DATED 2022-03-14, BLENDING OF GOUGES ON ON FLAP HINGE BOXES AND LUGS. COMPLE
- [SDR SWIA202265416](https://openairdocs.org/sdr/SWIA202265416.md): None · damaged · Mar 2, 2022 · N479CA · Cndair CL6002B19 · Doors
  > CUSTOMER REQUEST REMOVE AND REPLACE PAX DOOR AFT FORMER DUE TO PREVIOUS REPAIR (C-CHECK RO 4/20/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHA
- [SDR SWIA202265415](https://openairdocs.org/sdr/SWIA202265415.md): Retainer · corroded · Mar 2, 2022 · N479CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED (C-CHECK RO 4/20/2022) REMOVED AND REPLACED PASSENGER DOOR FORMER I.A.W. CRJ200 SRM 51-42-06 AND 51-42-21 REV.38B, DATED 11/25/2020. COMPLIED WITH SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO W
- [SDR SWIA202265414](https://openairdocs.org/sdr/SWIA202265414.md): None · cracked · Feb 18, 2022 · N479CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 280 FWD J ANGLE FOUND CRACKED BETWEEN LBL9 AND RBL9 (C-CHECK RO 4/20/2022) REMOVED AND REPLACED FWD "J" ANGLE AT FS 280 BETWEEN LBL9 AND RBL 9 IAW CRJ-200 SRM 51-42-06. COMPLIED WITH SKY CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE WEIGHT AND BALA
- [SDR SWIA202265413](https://openairdocs.org/sdr/SWIA202265413.md): None · corroded · Feb 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 499 TO F.S. 574. (C-CHECK RO 4/20/2022) REMOVED AND REPLACED LBL 9 PRESSURE FLOOR BEAM CAP FROM FS 409+118 - FS 559+16 IAW REO 601R-53-41-3023 REV -- DATED 2022-02-21. REF CAMP # 24369101 FOR REPAIR OF LBL 9 FLOO
- [SDR SWIA202265412](https://openairdocs.org/sdr/SWIA202265412.md): None · corroded · Feb 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RBL9 FLOOR BEAM IS CORRODED AT F.S. 416. (C-CHECK RO 4/20/2022) REMOVED AND REPLACED PRESSURE FLOOR BEAM CAP IAW REO 601R-53-41-3024 REV -- DATED 2022-02-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE +3.9
- [SDR SWIA202265411](https://openairdocs.org/sdr/SWIA202265411.md): Floor Support · corroded · Feb 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL27 FLOOR BEAM IS CORRODED BETWEEN F.S. 559.0+112 F.S. 574. (C-CHECK RO 4/20/2022) REPAIRED LBL 27.00 FLOORBEAM BETWEEN F.S. 559.00+112 AND F.S. 574.00 I.A.W. BOMBARDIER CRJ200 SRM 53-00-43 REV.38B, DATED 11/25/2020 AND MHIRJ REO 601R-53-51-618 REV.--
- [SDR SWIA202265410](https://openairdocs.org/sdr/SWIA202265410.md): None · corroded · Feb 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LBL9 FLOOR BEAM IS CORRODED BETWEEN F.S. 559.0+16 TO F.S. 559.0+32. (C-CHECK RO 4/20/2022) COMPLIED WITH CRJ 200 SRM 53-00-43 REPAIR 1 ON LBL#9 BETWEEN 559.00+16- 559.00+43. ATTACHED COMPLETED SKYCARD 51-900-1003- SKY, COMPLETED 337 ATTACHED.TOTAL WE
- [SDR SWIA202265409](https://openairdocs.org/sdr/SWIA202265409.md): Floor Support · corroded · Feb 15, 2022 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL9 IS CORRODED BETWEEN F.S. 559.0+64 TO F.S. 559.0+80. (C-CHECK RO 4/20/2022) REPAIRED FLOORBEAM AT RBL 9.00 BETWEEN F.S. 559.00+64 TO F.S. 559.00+80 I.A.W. MHIRJ REO 601R-53-51-617 REV.--, DATED 2022-03-07 AND BOMBARDIER CRJ200 SRM 51-42-06 AND 51-42

Next page: https://openairdocs.org/aircraft/N479CA/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 = 'N479CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N479CA/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.