# Service difficulty reports: N554CA

A list on [N554CA](https://openairdocs.org/aircraft/N554CA.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 · 210 reports

- [SDR SWI2025F00394](https://openairdocs.org/sdr/SWI2025F00394.md): Floor Support · corroded · Feb 5, 2025 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION FOUND ON LBL 27 BETWEEN FS1000.00-FS1070.00 (C-CHECK RO 3/18/2025) REMOVED AND INSTALLED ALL REPAIR PARTS OF FLOOR BEAM SECTION ON LBL 27.0 BETWEEN F/S 1000.00-FS1070.00 IAW CRJ 900 SRM 53-00-41-201-001-A03
- [SDR SWI2025F00393](https://openairdocs.org/sdr/SWI2025F00393.md): Floorbeam · corroded · Feb 5, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON LBL 9 AT FS1031.00 (C-CHECK RO 3/18/2025) REMOVED AND INSTALLED ALL REPAIR PARTS OF FLOOR BEAM SECTION ON LBL 9.0 AT F/S 1031.00 IAW CRJ 900 SRM 53-00-41-201-001-A03. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2025031900205](https://openairdocs.org/sdr/SWIA2025031900205.md): Floorbeam · corroded · Feb 5, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON RBL 9 AT FS1031.00 (C-CHECK RO 3/18/2025) REMOVED AND INSTALLED ALL REPAIR PARTS OF FLOOR BEAM SECTION ON RBL 9.0 BETWEEN F/S 1031 IAW CRJ 900 SRM 53-00-41-201-001-A03, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA2025031900203](https://openairdocs.org/sdr/SWIA2025031900203.md): Frame · corroded · Feb 3, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION NOTED ON FUSELAGE FRAME AT APPROX FS969 AT STGR 27. (S/N 00840) (C-CHECK RO 3/18/2025) REPAIRED FRAME SECTION FS 696.00 BETWEEN STGR 25L - STGR 25R REF CRJ900 SRM 53-00-06-201-001-A03 REV 38 JUL 25/2020 COMPLIED WITH TASK CARD 51-900-1002-SK
- [SDR SWIA2025031900116](https://openairdocs.org/sdr/SWIA2025031900116.md): Doubler · corroded · Jan 16, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON THE RH TCAS ANTENNA DOUBLER AT APPROXIMATELY FS 349, STRINGER 25-26R. SEE ATTACHED PICTURES. (C-CHECK RO 3/18/2025) INSTALLED NEW CHANNEL/DOUBLER P/N SH670-31032-5 FOR ANTENNA AT FS349 BETWEEN STGR 25R-26R REF CRJ 900 SRM 51-42-06-001-001-A
- [SDR SWIA2025031900114](https://openairdocs.org/sdr/SWIA2025031900114.md): Stand Off · cracked · Jan 14, 2025 · N554CA · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/18/2025) INSTALLED NEW I/B "A" BRACKET INTO R/H LWR TRANSCOWL (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.SEE CONTINUAT
- [SDR SWIA2025031900109](https://openairdocs.org/sdr/SWIA2025031900109.md): Door Frame · cracked · Jan 9, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Structure
  > RH OVERWING FWD EMER DOOR HAS POSSIBLE CRACK ON TOP FRAME. MARKED (C-CHECK RO 3/18/2025) REPAIRED RH OVERWING EMERGENCY EXIT DOOR PER MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 ALL STEPS COMPLIED WITH, SEE CONTINUATION FOR WORK PERFORMED. COMPLIED
- [SDR SWI2025F00392](https://openairdocs.org/sdr/SWI2025F00392.md): Floorbeam · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 FLOOR SUPPORT ANGLE AT APPROX LBL9 HAS CORROSION. (C-CHECK RO 3/18/2025) INSTALLED NEW FS280 FLOOR SUPPORT ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-51620 REV -B & DWG670-34010 REV -K. COMPLIED W
- [SDR SWI2025F00391](https://openairdocs.org/sdr/SWI2025F00391.md): Door Frame · damaged · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Structure
  > THE A-BAY DOOR SURROUND FUSELAGE SIDE LANDING HAS FRETTING ALONG ENTIRE CUT-OUT. (C-CHECK RO 3/18/2025) REPAIR A-BAY DOOR SURROUND FUSELAGE SIDE LANDING FRETTING ALONG ENTIRE CUT-OUT. BY COMPLYING WITH REO 690-53-21-032 REV-- DATED 2008-03-07 COMPLIED
- [SDR SWI2025F00390](https://openairdocs.org/sdr/SWI2025F00390.md): Stringer · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FORWARD BAGGAGE BAY STGR 27 AFT BETWEEN FS629.00-FS661.00+16 CORRODED (C-CHECK RO 3/18/2025) PERFORMED REPAIR OF FORWARD BAGGAGE BAY STGR 27 AFT BETWEEN FS629.00-FS661.00+16 CORROSION BY COMPLYING WITH REO 690-53-31-914 REV.-- DATED: 2025-02-07. LEAK CH
- [SDR SWI2025F00389](https://openairdocs.org/sdr/SWI2025F00389.md): Frame · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FORWARD BAGGAGE BAY FS501.00 FRAME BETWEEN STGR24L-25L CORRODED (C-CHECK RO 3/18/2025) REPAIRED FORWARD BAGGAGE BAY FS501.00 FRAME BETWEEN STGR24L-25L REF REO 690-53-31-915 REV. -- DATED 2025-02-07 COMPLIED STEPS 1 -16. COMPLIED WITH 51-900-1002-SKY. L
- [SDR SWI2025F00388](https://openairdocs.org/sdr/SWI2025F00388.md): Channel · bent · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR CUTOUT FS1000.00 AFT LOWER CHANNEL (MM670-35517-003) AND BRACKET ( CC670-38812-1) BENT (C-CHECK RO 3/18/2025) EVALUATED AFT BAGGAGE BAY DOOR CUTOUT FS1000.00 AFT LOWER CHANNEL (MM670-35517-003) AND BRACKET ( CC670-38812-1), NO DAMAG
- [SDR SWI2025F00398](https://openairdocs.org/sdr/SWI2025F00398.md): Strap · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H FRAME STRAP AT FS349.00 AT STGR18L OF PASSENGER DOOR CUTOUT CORRODED (C-CHECK RO 3/18/2025) REMOVED AND REPLACED WITH NEW LH FLOOR BEAM FITTING P/N: SH670-31942-3 AT FS349.00 ON STGR18L REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV. AE
- [SDR SWI2025F00397](https://openairdocs.org/sdr/SWI2025F00397.md): Strap · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME STRAP AT FS319.00 AT STGR18R OF SERVICE DOOR CUTOUT CORRODED (C-CHECK RO 3/18/2025) INSTALLED NEW FRAME STRAP P/N SH670-31990-1 AT FS319.00 AT STGR18R OF SERVICE DOOR CUTOUT. REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31950 REV Y. COMPLIED
- [SDR SWI2025F00396](https://openairdocs.org/sdr/SWI2025F00396.md): Door Frame · cracked · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Main, Structure
  > THE LH TRU BAY LANDING IS CRACKED IN THE RADIUS OF AFT LATCH OPENING. (C-CHECK RO 3/18/2025) REMOVED AND REPLACED THE LH TRU BAY LANDING REF CRJ-900 SRM 51-42-06-001-001-A01, REV-38 DATED JUL 25/2020 CRJ-900 SRM 51-42-22-001-001-A01 REV-38. DATED JUL
- [SDR SWI2025F00395](https://openairdocs.org/sdr/SWI2025F00395.md): Coaming · gouged · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR CUTOUT UPPER COAMING GOUGED/CHAFFED UPPER AFT AND AFT SIDE (C-CHECK RO 3/18/2025) REPLACED AFT CARGO DOOR SURROUND UPPER COAMING. REF CRJ900 SRM 51-41-02-001-001-A01. REF CRJ900 SRM 51-24-36-001-001-A01. REF CRJ900 SRM 51-23-00-001
- [SDR SWIA202503190107](https://openairdocs.org/sdr/SWIA202503190107.md): Floor Support · corroded · Jan 7, 2025 · N554CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED FS310.00 - FS319.00 AS MARKED (C-CHECK RO 3/18/2025) REPAIRED RH FLOOR SILL IS CORRODED FS310.00 - FS319.00 REF REO 690-53-21-1866 REV -- DATED 2025-02-03. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2025031901211](https://openairdocs.org/sdr/SWIA2025031901211.md): Skin · damaged · Dec 11, 2024 · N554CA · Cndair CL6002D24 · Wing, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA73255-690-57-41-248 N554CA MXCODEID59074-PR - TEMPORARY DISPOSITION FOR BLENDED WEAR DAMAGE TO LH WING FIXED LEADING EDGE SKIN. COMPLIED WITH TEMPORARY REPAIR TO LH WING FIXED LEADING EDGE SKIN AT SS144.94, REF REO
- [SDR SWIA20240522427](https://openairdocs.org/sdr/SWIA20240522427.md): Skin · damaged · Apr 27, 2024 · N554CA · Cndair CL6002D24 · Wing, Plate/Skin
  > DAMAGE TO RIGHT WING LOWER SURFACE DURING CROSSWIND LANDING. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28155864 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED DAMAGED PANELS 672AB AND 672BB. SEE CP 2816+3762 FOR REPLACEMENT OF DAMAGED RIB. SE
- [SDR SWIA2023122200016](https://openairdocs.org/sdr/SWIA2023122200016.md): Unknown · warning message · Dec 16, 2023 · N554CA · Cndair CL6002D24 · Central Display
  > ANTI ICE DUCT WARNING MESSAGE. MESSAGE CLEARED WITH QRH AND TURNING OFF WINGS. (FLIGHT 3706 FILED CLOSED)B#349543. LOOP A FS759 22%. LOOP B FS739 @ 17%.UPON FURTHER INVESTIGATION FOUND V-BAND CLAMP LOOSE AND LEAKING AT FS 759. TORQUED V-BAND CLAMP AND PERFORM
- [SDR SWIA20230614](https://openairdocs.org/sdr/SWIA20230614.md): Unknown · damaged · Jun 14, 2023 · N554CA · Cndair CL6002D24 · Air Conditioning System
  > DAMAGE ON RH SIDE OF AIRCRAFT FUSELAGE BETWEEN FS333.00 AND FS349.00, BETWEEN STGR19R AND STGR21RTHIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1156202 AND 1156470 (FILED CLOSED)COMPLIED WITH REPAIR AT RH SIDE OF AIRCRAFT FUSEL
- [SDR SWIA20230615014](https://openairdocs.org/sdr/SWIA20230615014.md): Unknown · smoke · Jun 14, 2023 · N554CA · Cndair CL6002D24 · Humidity Control System
  > *****ODI EVENT******D: WE WERE WAITING ON THE RAMP WITH ONLY OUR APU UP (AS WE HAD A FLOW TIME FOR ABOUT AN HOUR AWAY) WHEN WHITE SMOKE CAME RUSHING INTO THE COCKPIT. FAS REPORTED HAZE ON THEIR END IN THE BACK OF THE CABIN. UPON TROUBLESHOOTING FOUND LH PACK
- [SDR SWIA202266445](https://openairdocs.org/sdr/SWIA202266445.md): None · damaged · Sep 3, 2022 · N554CA · Cndair CL6002D24 · Ailerons
  > FOUND DAMAGE CAUSED BY PROTRUDING SCREW ON LH #1 SLAT LOCATED ROUGHLY AT WS108 ON THE UPPER AFT SIDE. (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR FOR GOUGE DAMAGE TO LH SLAT #1 TRAILING EDGE AND AFT SKIN NEAR SS144.94 PER REO 690-57-42-908 REV "--" DAT
- [SDR SWIA202265831](https://openairdocs.org/sdr/SWIA202265831.md): None · damaged · May 28, 2022 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)
  > STRUCK GEESE ON TAKEOFF AT 1200FT. RETURNED TO FIELD. DO NOT BELIEVE WE INGESTED ANY BIRDS INTO ENGINES. BELIEVE IT WAS TOP OF FUSELAGE ONLY. ( FLIGHT 3647 - FILED CLOSED) COMPLIED WITH COMPLETE BIRD STRIKE INSPECTION PER AMM 05-51-05, FOUND DAMAGE TO UPP
- [SDR SWIA202163232](https://openairdocs.org/sdr/SWIA202163232.md): None · damaged · Dec 20, 2021 · N554CA · Cndair CL6002D24 · Window/Windshield System
  > TRANSFER FROM EAML 807605: R WINDOW HEAT CAUTION MESSAGE IN FLIGHT. RAN QRH. ISSUE RESOLVED. (FLIGHT 4317 - FILED CLOSED)COMPLIED WITH TASK CARD CRJ MIP 56-220-1000-SKY RH WINDOW REPLACEMENT.. OPS AND LEAK CHECK GOOD
- [SDR SWIA202161905](https://openairdocs.org/sdr/SWIA202161905.md): None · corroded · Sep 21, 2021 · N554CA · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > RH FLOOR SILL AFT OF SERVICE DOOR FROM FS349-FS364 HAS CORROSION. (C-CHECK RO 10/22/2021) REPAIRED RH FLOOR SILL AFT OF SERVICE DOOR FROM FS349-FS364 REF REO 690-53-21-1429 REV.-- DATED 2021-09-27. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202161904](https://openairdocs.org/sdr/SWIA202161904.md): None · chafed · Sep 14, 2021 · N554CA · Cndair CL6002D24 · Powerplant System
  > COMPLY WITH REO 690-54-22-027 REV.-- DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO LH LOWER TRANSCOWL HINGE BEAM. (C-CHECK RO 10/22/2021) COMPLIED WITH REO 690-54-22-027 REV.-- DATED 2021-09-06 ALL STEPS COMPLETED FOR BLENDED CHAFE DAMAGE TO THE LH LOWER
- [SDR SWIA202161903](https://openairdocs.org/sdr/SWIA202161903.md): None · damaged · Sep 11, 2021 · N554CA · Cndair CL6002D24 · Powerplant System
  > COMPLY WITH REO 690-54-24-007 REV. -- DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO LH TRANSCOWL FLOATING TIE BAR. (C-CHECK RO 10/22/2021) COMPLIED WITH REO 690-54-24-007 REV --, DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO L/H TRANSCOWL FLOATING TIE BAR
- [SDR SWIA202161902](https://openairdocs.org/sdr/SWIA202161902.md): None · corroded · Sep 11, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > PAX DOOR STRUCTURE INTERCOSTAL, DD4 HAS CORROSION (C-CHECK RO 10/22/2021) REPLACED PAX DOOR STRUCTURE INTERCOSTAL DD4 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK
- [SDR SWIA2021102661901](https://openairdocs.org/sdr/SWIA2021102661901.md): Cleat · corroded · Sep 11, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CLEAT ATTACHING TO FRAME FS313.56 HAS CORROSION (C-CHECK RO 10/22/2021) REMOVED AND REPLACED CLEAT ATTACHING TO FRAME FS313.56. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV. -N / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24
- [SDR SWIA202161940](https://openairdocs.org/sdr/SWIA202161940.md): None · corroded · Sep 9, 2021 · N554CA · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > CORRODED SIDE SEAT TRACK RETAINER IN MID CABIN BETWEEN FS693.00 TO FS720.85 ON RIGHTHAND SIDE (C-CHECK RO 10/22/2021) REMOVED AND REPLACED R/H SIDE SEAT TRACK RETAINER IN MID CABIN BETWEEN FS 693.00 TO FS 720.85 REF CRJ-900 AMM 53-00-49-000-801-A07 AND
- [SDR SWIA202161900](https://openairdocs.org/sdr/SWIA202161900.md): None · corroded · Sep 7, 2021 · N554CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > R/H LOWER BULKHEAD WEB AT FS 280.0 CORRODED (C-CHECK RO 10/22/2021) REPAIRED RH LOWER BULKHEAD WEB AT FS280.0 REF CRJ900 SRM 53-11-10-201-004-A01. COMLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202161899](https://openairdocs.org/sdr/SWIA202161899.md): None · cracked · Sep 7, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CRACK FOUND ON ATTACH CLIP AT FS 280.0 RBL 9.0 OUTBOARD INTERCOSTAL (C-CHECK RO 10/22/2021) REMOVED AND INSTALLED NEW ATTACH CLIP AT FS280.0 RBL 9.0 OUTBOARD INTERCOSTAL REF CRJ-900 SRM 51-42-21-001-001-A01 AND DWG CC670-34099 REV.--. COMPLIED WITH 51-
- [SDR SWIA202161944](https://openairdocs.org/sdr/SWIA202161944.md): None · cracked · Sep 3, 2021 · N554CA · Cndair CL6002D24 · Doors
  > PAX DOOR AFT DRAG ANGLE HAS SUSPECT CRACK (MARKED) (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE REF. CRJ900 SRM 51-42-06-001-001-A01.
- [SDR SWIA202161943](https://openairdocs.org/sdr/SWIA202161943.md): None · cracked · Sep 3, 2021 · N554CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR AFT WEB PANEL TEE FITTING HAS VISIBLE CRACK€”REPLACE TEE FITTING (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PAX DOOR AFT WEB PANEL TEE FITTING REF. CRJ900 SRM 51-42-06-001-001-A01.
- [SDR SWIA202161898](https://openairdocs.org/sdr/SWIA202161898.md): None · dented · Sep 2, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL AT DD7 BETWEEN FS338.963 AND FS347.25 IS DENTED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR INTERCOSTAL DD7 BETWEEN FS338.963 AND FS347.25 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900
- [SDR SWIA202161897](https://openairdocs.org/sdr/SWIA202161897.md): None · dented · Sep 2, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL AT DD7 BETWEEN FS311.75 AND FS320.163 IS DENTED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR INTERCOSTAL AT DD7 BETWEEN FS311.75 AND FS320.163 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-
- [SDR SWIA202161896](https://openairdocs.org/sdr/SWIA202161896.md): None · corroded · Sep 2, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY FS280.00 FLOORBOARD SUPPORT ANGLE CORRODED (C-CHECK RO 10/22/2021) REPLACED MAIN AVIONICS BAY FS280.00 FLOORBOARD SUPPORT ANGLE REF DWG CC670-34010 REV. K AND CRJ900 SRM 51-42-06-001-001-A01, AND CRJ900 SRM 51-42-21-001-001-A01. COMPLI
- [SDR SWIA202161895](https://openairdocs.org/sdr/SWIA202161895.md): None · chafed · Aug 31, 2021 · N554CA · Cndair CL6002D24 · Powerplant System
  > LH LOWER TRANSCOWL OUTBOARD LEADING EDGE CHAFED ON INNER SURFACE (C-CHECK RO 10/22/2021) LH LOWER TRANSCOWL OUTBOARD LEADING EDGE BLENDED AND FINISH RESTORED AND REPLACED COAMING REF REO 670-54-21-1207 REV. A DATED 2015-08-27, REO 690-54-21-394 REV.--
- [SDR SWIA202161894](https://openairdocs.org/sdr/SWIA202161894.md): None · dented · Aug 31, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)
  > PASSENGER DOOR INTERCOSTAL AT DD1, BETWEEN FS311.750 AND FS320.163 IS DENTED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR INTERCOSTAL AT DD1 BETWEEN FS311.750 AND FS320.163 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH
- [SDR SWIA202161893](https://openairdocs.org/sdr/SWIA202161893.md): None · corroded · Aug 31, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)
  > PASSENGER DOOR FORMER AT FS347.250, BETWEEN DD4 AND DD5, IS CORRODED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR AFT FORMER REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202161892](https://openairdocs.org/sdr/SWIA202161892.md): None · corroded · Aug 31, 2021 · N554CA · Cndair CL6002D24 · Fuselage Structure (General)
  > PASSENGER DOOR FORMER AT FS320.163 ON FWD SIDE IS CORRODED BETWEEN DD6 AND DD7. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR FORMER AT FS320.163 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK G
- [SDR SWIA202161891](https://openairdocs.org/sdr/SWIA202161891.md): None · corroded · Aug 31, 2021 · N554CA · Cndair CL6002D24 · Doors
  > PASSENGER DOOR ANGLE AT DD6, ON THE FWD SIDE OF FS320.163 IS CORRODED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR ANGLE (CLIP) AT DD6 ON THE FWD SIDE OF FS320.163 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-10
- [SDR SWIA202161890](https://openairdocs.org/sdr/SWIA202161890.md): None · cracked · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL AT DD1, BETWEEN FS347.250 AND FS338.963 IS CRACKED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR INTERCOSTA AT DD1 BETWEEN FS347.250 AND FS338.963 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH
- [SDR SWIA202161889](https://openairdocs.org/sdr/SWIA202161889.md): None · corroded · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL BETWEEN DD7 AND DD8, BETWEEN FS327.763 AND FS320.163 IS CORRODED. (C-CHECK RO 10/22/2021) REPLACED PASSENGER DOOR INTERCOSTAL BETWEEN DD7 AND DD8 BETWEEN FS327.763 AND FS320.163 REF DWG 601R31702 REV. N AND CRJ900 SRM 51-42-0
- [SDR SWIA2021102661888](https://openairdocs.org/sdr/SWIA2021102661888.md): Angle · corroded · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE AT DD8, ON THE AFT SIDE OF FS320.163 IS CORRODED. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PASSENGER DOOR ANGLE AT DD8, ON THE AFT SIDE OF FS320.163. REF. CRJ900 SRM 51-42-06-001-001-A01, DWG# 601R31702 REV.-N AND DWG# 601R31871
- [SDR SWIA2021102661887](https://openairdocs.org/sdr/SWIA2021102661887.md): Angle · corroded · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE AT DD8, ON THE FWD SIDE OF FS320.163 IS CORRODED. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PASSENGER DOOR ANGLE AT DD8, ON THE FWD SIDE OF FS320.163. REF. CRJ900 SRM 51-42-06-001-001-A01, DWG# 601R31702 REV.-N AND DWG# 601R31871
- [SDR SWIA2021102661886](https://openairdocs.org/sdr/SWIA2021102661886.md): Angle · corroded · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE AT DD8, ON THE AFT SIDE OF FS338.963 CORRODED. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PASSENGER DOOR ANGLE AT DD8, ON THE AFT SIDE OF FS338.963. REF. CRJ900 SRM 51-42-06-001-001-A01, DWG# 601R31702 REV.-N AND DWG# 601R31871 RE
- [SDR SWIA202161885](https://openairdocs.org/sdr/SWIA202161885.md): Angle · corroded · Aug 30, 2021 · N554CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE AT DD8, ON THE FWD SIDE OF FS338.963 CORRODED. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED PASSENGER DOOR ANGLE AT DD8, ON THE FWD SIDE OF FS338.963. REF. CRJ900 SRM 51-42-06-001-001-A01, DWG# 601R31702 REV.-N AND DWG# 601R31871 R
- [SDR SWIA202161884](https://openairdocs.org/sdr/SWIA202161884.md): None · corroded · Aug 28, 2021 · N554CA · Cndair CL6002D24 · Standard Practices/Structures
  > (WIFI) AFT ATG ANTENNA INNER CHANNEL HAS CORROSION. (C-CHECK RO 10/22/2021) REMOVED AND REPLACED WITH NEW AFT ATG ANTENNA INNER CHANNEL REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG P13112-20110 REV H. PRESSURE CHECKS GOOD, NO LEAKS NOTED COMPLIED WIT

Next page: https://openairdocs.org/aircraft/N554CA/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 = 'N554CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N554CA/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.