# Service difficulty reports: N548CA

A list on [N548CA](https://openairdocs.org/aircraft/N548CA.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 · 182 reports

- [SDR SWIA2026042875914](https://openairdocs.org/sdr/SWIA2026042875914.md): Skin · scratched · Apr 26, 2026 · N548CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FOUND SCRATCH ON RH FUSELAGE STARTING AT FS1039.5 TO FS1029.62 LOCATED ON STGR19R MEASURING 11-3/8" LONG; MAX DEPTH:.0022". INSPECTED RH FUSLAGE SKIN AT FS1029.62 - FS1039.5 ON STGR 19R WITH NO DAMAGE FOUND; LOCATED SCRATCH ON RH FUSELAGE FS1029.62 TO FS1039
- [SDR SWI2026F00075](https://openairdocs.org/sdr/SWI2026F00075.md): Diaphragm · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > RIGHT SIDE, LOWER SILL DIAPHRAGM STRUCTURE HAS CORROSION ON INBD EDGE FROM BS 720 TO BS 744. COMPLIED WITH PERMANENT REPAIR REO 690-53-41-566 REV-.
- [SDR SWI2026F00074](https://openairdocs.org/sdr/SWI2026F00074.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND THREE FASTENER HOLES ON LT SILL DECK BETWEEN BS 797 AND BS 813. COMPLIED WITH REO 690-53-41-569 REV-.
- [SDR SWI2026F00073](https://openairdocs.org/sdr/SWI2026F00073.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND ON LT SILL DECK, BS 801 FOR OTBD FASTENER COMMON TO SILL DECK AND DIAPHRAGM. REPAIRED LT SILL DECK AND DIAPHRAGM AT FS 801 IAW MHIRJ REO 690-53-41-565 REV-. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE.
- [SDR SWI2026F00072](https://openairdocs.org/sdr/SWI2026F00072.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND ON LEFT SILL DECK, BS 792 FOR OTBD 3 FASTENERS COMMON TO SILL DECK AND DIAPHRAGM. COMPLIED WITH REO 690-53-41-565 REV-.
- [SDR SWI2026F00071](https://openairdocs.org/sdr/SWI2026F00071.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON LT OTBD SILL DECK AT BS 786. COMPLIED WITH REO 690-53-41-569 REV-.
- [SDR SWI2026F00070](https://openairdocs.org/sdr/SWI2026F00070.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON LT OTBD SILL DECK AT BS 781. COMPLIED WITH REO 690-53-41-569 REV-.
- [SDR SWI2026F00069](https://openairdocs.org/sdr/SWI2026F00069.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON LT OTBD SILL DECK AT BS 768. COMPLIED WITH REO 690-53-41-569 REV-.
- [SDR SWI2026F00068](https://openairdocs.org/sdr/SWI2026F00068.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON LT OTBD SILL DECK AT BS 734. COMPLIED WITH REO 690-53-41-569 REV-.
- [SDR SWI2026F00067](https://openairdocs.org/sdr/SWI2026F00067.md): Diaphragm · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > RIGHT, LOWER SILL DIAPHRAGM STRUCTURE CORRODED ON INBD EDGE BETWEEN BS 761 TO 785. REPAIRED RT LOWER SILL DIAPHRAGM INBD EDGE AT BS 761 - 785 IAW REO 690-53-41-566, REV-. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. RE
- [SDR SWI2026F00066](https://openairdocs.org/sdr/SWI2026F00066.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON RT OTBD SILL DECK AT BS 781. RT SILL DECK AT BS 781 IAW REO 690-53-41-567, REV-. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FORM 337 NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA2026011300002](https://openairdocs.org/sdr/SWIA2026011300002.md): Deck Plate · corroded · Nov 2, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION DISCOVERED AROUND FASTENER HOLE ON RT SILL DECK AT FS801. REPAIRED RT SILL DECK AT BS 801 IAW REO 690-53-41-567, REV-. COMPLETED TASK CARD 51-900-1002-SKY. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA2026011300018](https://openairdocs.org/sdr/SWIA2026011300018.md): Skin · chafed · Oct 18, 2025 · N548CA · Cndair CL6002D24 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP LOWER SKIN HAS CHAFING DAMAGE AT THE INBOARD AND OUTBOARD HINGE ARM LOCATIONS FROM CONTACT WITH THE CANOE FAIRINGS. COMPLIED WITH REPAIR OF FLAP IAW REO 690-57-52-559 REV-- AND SRM 57-52-01-201-005-A01. REMOVED AND INSTALLED INNER HINGE ARM
- [SDR SWIA2026011300017](https://openairdocs.org/sdr/SWIA2026011300017.md): Skin · chafed · Oct 17, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN FS 913-FS 927 STR 27 HAS TWO CHAFES FROM CONTACT WITH SCREWS FROM ATTACHING PANEL. REPAIRED LOWER FUELAGE SKIN AT FS913-FS927 AT STGR 27 IAW MHIRJ REO 690-53-51-529 REV -- DATED 2025-11-18. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED
- [SDR SWIA2026011300009](https://openairdocs.org/sdr/SWIA2026011300009.md): Skin · dented · Oct 9, 2025 · N548CA · Cndair CL6002D24 · Leading Edge Devices
  > ADM N548CA7851 RT SLAT L/E, APPROX WS 70. DENTED, L=1.25" W= 1.0625" D= 0.0145. W/D RATIO= 73PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. VERIFIED MEASURMENTS AT RT SLAT L/E WS7
- [SDR SWIA20260113007](https://openairdocs.org/sdr/SWIA20260113007.md): Structure · damaged · Oct 7, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > WHILE INSPECTING TEMP REPAIR REO 690-53-61-1110 AREA AROUND LOW-PRESSURE GROUND AIR DOOR, WE HAVE DISCOVERED THAT ADDITIONAL DAMAGE HAS OCCURED FROM BS 1000 - 1051 BETWEEN S23 - 27R AFTER INCORPORATION OF TEMP REO. REPAIRED AREA AROUND LOW PRESSURE GROUND AIR
- [SDR SWIA2026011300909](https://openairdocs.org/sdr/SWIA2026011300909.md): Skin · damaged · Sep 9, 2025 · N548CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA18772-690-53-11-149 548CA-DTI - COMPLY WITH DAMAGE TOLERANCE INSPECTION ON RA ID: 18772 REPAIRED LIGHTNING STRIKE DAMAGE IAW REO 690-53-11-049. PERFORM SPECIAL DETAILED INSPECTION OF CUTOUT PERIMETER AND FASTENER HOLE
- [SDR SWIA2025082600024](https://openairdocs.org/sdr/SWIA2025082600024.md): A/C Pack · smoke · Aug 24, 2025 · N548CA · Cndair CL6002D24 · Cabin Cooling System
  > LIGHT SMOKE (WHITE) AND LIGHT BURNING SMELL AFTER TAKEOFF (FLIGHT 3835 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30722258 WITH THE FOLLOWING CORRECTIVE ACTION: "ODI EVENT -TROUBLESHOT PER CRJ 900 FIM 21-22-00 FOUND WHEN LH PACK IS TURNED
- [SDR SWIA202312080002](https://openairdocs.org/sdr/SWIA202312080002.md): Unknown · gouged · Dec 2, 2023 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > UPON REPLACEMENT OF THE RH SIDE WINDOW, FOUND GOUGE DAMAGE AT 3 LOCATIONS ON THE WINDOW SILL (AIRFRAME SIDE). ALL 3 LOCATIONS COINCIDE WITH THE 3 MOUNTING SLING HOLES ON THE WINDOW (1 UPPER, AND 2 LOWR HOLES). SUSPECT DAMAGE WAS CAUSED BY THE SLING DURING PREV
- [SDR SWIA202309080529](https://openairdocs.org/sdr/SWIA202309080529.md): Unknown · fire · May 29, 2023 · N548CA · Cndair CL6002D24 · Flight Compartment Windows
  > LEFT WINDSHIELD STARTED SPARKING AND CAUGHT FIRE ON THE ELECTRICAL ELEMENT MID FLIGHT. WE TURNED OFF WINDSHIELD HEAT AND CONTAINED THE FIRE. (FLT 4113 FILED CLOSED)LEFT WINDSHIELD STARTED SPARKING AND CAUGHT FIRE ON THE ELECTRICAL ELEMENT MID FLIGHT. WE TURNED
- [SDR SWIA20230530029](https://openairdocs.org/sdr/SWIA20230530029.md): Unknown · fire · May 29, 2023 · N548CA · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > LEFT WINDSHIELD STARTED SPARKING AND CAUGHT FIRE ON THE ELECTRICAL ELEMENT MID FLIGHT. WE TURNED OFF WINDSHIELD HEAT AND CONTAINED THE FIRE. (FLT 4113 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202266679](https://openairdocs.org/sdr/SWIA202266679.md): Brake Assy · overheated · Oct 30, 2022 · N548CA · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVERTEMP WITH GEAR STOWED AFTER TAKE OFF. RAN QRH THEN RETURNED TO FIELD KATL. LH IB BRAKE BTMS INDICATED RED AND 22 DEGREES. REMOVED AND REPLACED BRAKE ASSY IN REF TO CRJ900 AMM 32-43-26. OPS CHECK GOOD.
- [SDR SWIA202266600](https://openairdocs.org/sdr/SWIA202266600.md): None · cracked · Oct 9, 2022 · N548CA · Cndair CL6002D24 · Window/Windshield System
  > CLIMBING THROUGH 30000 FEET, CRACKS BEGAN FORMING IN RIGHT WINDSHIELD. R WINDOW HEAT CAUTION IN FLIGHT, FOLLOWED BY R WSHLD HEAT CAUTION. CRACKING IN THE WINDSHIELD, TURNED OFF RIGHT WINDSHIELD HEAT AND CRACKS STOPPED SPREADING. AFTER PERFORMING QRH, WINDSHIEL
- [SDR SWIA202266449](https://openairdocs.org/sdr/SWIA202266449.md): None · cracked · Sep 10, 2022 · N548CA · Cndair CL6002D24 · Window/Windshield System
  > FO SIDE WINDOW DELAMINATING AND CRACKS AND GREW DURING FLIGHT (FLIGHT #3687 FILED CLOSED) R&R RIGHT SIDE WINDOW IN REF TASK CARD 56-220-1000-SKY. OPS CHECK GOOD. A/C OK FOR SERVICE
- [SDR SWIA202264219](https://openairdocs.org/sdr/SWIA202264219.md): None · malfunctioned · Feb 14, 2022 · N548CA · Cndair CL6002D24 · Landing Gear Door Actuator
  > GOT €ŒGEAR DISAGREE€? WHEN EXTENDING THE GEAR ON FINAL, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. PERFORMED MISSED APPROACH PROCEDURE, RAN QRH PROCEDURE, GEAR THEN EXTENDED NORMALLY DURING QRH PROCEDURE. (FLIGHT 3718 - FILED CLOSED) THIS DISCREPANCY WA
- [SDR SWIA202264199](https://openairdocs.org/sdr/SWIA202264199.md): None · malfunctioned · Feb 8, 2022 · N548CA · Cndair CL6002D24 · Landing Gear Door Actuator
  > GEAR DISAGREE ON LANDING IN SYR. NOSE GEAR WAS NOT COMING DOWN. RAN QRH, AFTER CYCLING GEAR 2 TIMES NOSE GEAR DID COME DOWN. NORMAL LANDING CONDUCTED (FLIGHT 4170 - FILED CLOSED) TROUBLESHOT GEAR DISAGREE WITH NO EXTENSION OF NLG PER CRJ900 FIM 32-60-00.
- [SDR SWIA202158558](https://openairdocs.org/sdr/SWIA202158558.md): Retainer · corroded · Apr 9, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT BOTTOM CORNER SEAL RETAINER IS CORRODED (C-CHECK RO 5/25/2021) REPLACED PAX DOOR AFT BOTTOM CORNER SEAL RETAINER PN: 601R318712-1 IAW CRJ900 SRM 51-42-06-001-001-A01 & DWG 601R31871 REV -D, COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHEC
- [SDR SWIA202158557](https://openairdocs.org/sdr/SWIA202158557.md): Intercostal · cracked · Apr 6, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD7 BETWEEN FS338.963 & FS347.25 IS CRACKED AT THE RADIUS ON IB FLANGE (C-CHECK RO 5/25/2021) REPLACED PAX DOOR INTERCOSTAL DD7 BETWEEN FS338 & FS347 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 REV N. COMPLIED WITH TASK
- [SDR SWIA202158556](https://openairdocs.org/sdr/SWIA202158556.md): Intercostal · corroded · Apr 6, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD5 BETWEEN FS338.963 & FS347.25 IS CORRODED (C-CHECK RO 5/25/2021) REPLACED PAX DOOR INTERCOSTAL DD5 BETWEEN FS338.963 & FS347.25 PN: 601R31902-317 CRJ900 IAW SRM 51-42-06-001-001-A01 & DWG 601R31702 REV -N, COMPLIED WITH 337 FORM,
- [SDR SWIA202158555](https://openairdocs.org/sdr/SWIA202158555.md): Stringer · corroded · Apr 6, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STGR18R AT APPROX FS620 - FS645 (C-CHECK RO 5/25/2021) REMOVED DAMAGED SECTION OF STR 18R BETWEEN FS620 AND FS661+53 AND INSTALLED NEW STRINGER SECTION AND SPLICE ANGLES IAW CRJ900 SRM 53-00-03-201-001-A02 REV. 38 DATE: 14 DEC 2020. F
- [SDR SWIA202158554](https://openairdocs.org/sdr/SWIA202158554.md): Cleat · corroded · Apr 5, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLEET ON THE AFT SIDE OF FORMER AT FS338.963 & DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 5/25/2021) REPLACED PAX DOOR CLEAT PN: 600-31902-269 ON THE AFT SIDE OF FORMER AT FS338.963 & DD5 INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01 & DWG 601R3
- [SDR SWIA202158552](https://openairdocs.org/sdr/SWIA202158552.md): Support Fitting · corroded · Apr 4, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WARDROBE FLOOR MOUNT SUPPORT FITTING AT LBL 20, BETWEEN FS 280.00 AND FS 295.00. (C-CHECK RO 5/25/2021) REMOVED CORROSION ON WARDROBE FLOOR MOUNT FITTING AT LBL 20, BETWEEN FS 280.00 AND FS 295.00, CORROSION FOUND TO BE OUT OF LIMITS. REMOV
- [SDR SWIA202158588](https://openairdocs.org/sdr/SWIA202158588.md): Angle · corroded · Apr 1, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew Doors
  > EXFOLIATION CORROSION FOUND ON PAX DOOR CLIP LOCATED APPROX AT FS340 UPPER INBD CORNER AGAINST INBD FORMER (UNDER HINGE) (C-CHECK RO 5/25/2021) REMOVED AND REPLACED PAX DOOR CLIP LOCATED APPRX AT FS340 UPPER INBD CORNER WITH A "NEW" CLIP DUE TO CORROSIO
- [SDR SWIA202158551](https://openairdocs.org/sdr/SWIA202158551.md): Floorbeam · cracked · Mar 28, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > *COCKPIT FLOOR BEAM LBL9 IS CRACKED AT FS 280.00. (C-CHECK RO 5/25/2021) REPAIRED THE CENTER COCKPIT FLOOR BEAM AT LBL9 REF CRJ-900 SRM 53-11-43-201-003-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202158550](https://openairdocs.org/sdr/SWIA202158550.md): Stringer · corroded · Mar 26, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26 LH IS CORRODED BETWEEN FS 333.00 AND FS 364.00 (C-CHECK RO 5/25/2021) REPLACED STRINGER REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG: SH670-31350 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA202158549](https://openairdocs.org/sdr/SWIA202158549.md): Post · corroded · Mar 25, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Structure
  > RH FS280.00 POST AT BL11.128 HAS CORROSION AT LOWER CORNER (C-CHECK RO 5/25/2021) INSTALLED R/H F.S.280.00 POST AT BL11.128 REPAIR IAW CRJ-900 SRM 53-11-10-201-006-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202158589](https://openairdocs.org/sdr/SWIA202158589.md): Angle · corroded · Mar 21, 2021 · N548CA · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION ON ANGLE ON WING TO BODY FAIRING 195DL(MARKED) (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS REF CRJ-900 SRM 53-00-00-101-A01. REPLACED STRAP PN: CC690-39171-7
- [SDR SWIA202158545](https://openairdocs.org/sdr/SWIA202158545.md): Doubler · corroded · Mar 20, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > T-CAS DOUBLER CORRODED AT STR 27 BETWEEN FS 295.00-310.00 (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND T-CAS DOUBLER AT STGR27, FS295 - FS310 TO BE OUT OF LIMITS. REPLACED DOUBLER REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-
- [SDR SWIA202158544](https://openairdocs.org/sdr/SWIA202158544.md): Stringer Splice · corroded · Mar 20, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 26 LH SPLICE AT FS 333.00 CORRODED AROUND RIVET TAILS (C-CHECK RO 5/25/2021) REPLACED STGR 26L SPLICE AT FS333 WITH NEW SPLICE REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202158543](https://openairdocs.org/sdr/SWIA202158543.md): Stringer Splice · corroded · Mar 20, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 26 RH SPLICE CORRODED AT FS 333.00 (C-CHECK RO 5/25/2021) REMOVED AND REPLACED STRG 26R SPLICE AT F.S. 333.00, REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24) STRUCTURAL
- [SDR SWIA202158542](https://openairdocs.org/sdr/SWIA202158542.md): Floor Support · corroded · Mar 19, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > * LH FLOOR SILL BETWEEN FS913 AND FS969 HAS CORROSION (MARKED). (C-CHECK RO 5/25/2021) REPAIRED CORROSION TO LH FLOOR SILL BETWEEN F.S.913 AND F.S. 969 TO MHIRJ REO 690-53-51-283 REV -- DATED 2021-04-16, SEE CONTINUE CARD FOR DETAILS / COMPLIED WITH SKY
- [SDR SWIA202158541](https://openairdocs.org/sdr/SWIA202158541.md): Stringer · corroded · Mar 19, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > * CORROSION DETECTED ON STGR (22L) BETWEEN F.S. 333.00 AND F.S. 349.00, SEVERAL PLACES AROUND FASTENER BUCKTAILS (MARKED). (C-CHECK RO 5/25/2021) REPAIRED STGR 22L SECTION BETWEEN F.S. 333.00 AND F.S. 349.00, REF CRJ 900 SRM 53-00-03-201-001-A02, CRJ 90
- [SDR SWIA202158540](https://openairdocs.org/sdr/SWIA202158540.md): Intercostal · corroded · Mar 19, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED ON A-BAY DOOR SURROUND STRUCTURE, (FWD/LH) INTERCOSTAL, IN LINE WITH STGR (26L) ON L/H VERTICAL "FACE" JUST FWD OF F.S. 364.00 (MARKED). (C-CHECK RO 5/25/2021) REMOVED CORROSION FROM INTERCOSTAL AT STGR26L, FS349 - FS364 AND FOUND R
- [SDR SWIA202158539](https://openairdocs.org/sdr/SWIA202158539.md): Intercostal · corroded · Mar 19, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED ON A-BAY DOOR SURROUND STRUCTURE, (FWD/RH) INTERCOSTAL,TO THE RIGHT OF STGR (27). R/H VERTICAL "FACE" AND "FLANGE", THAT SPANS FROM F.S. 349.00 BACK TO F.S. 364.00 (MARKED). (C-CHECK RO 5/25/2021) REMOVED AND REPLACED INTERCOSTAL T
- [SDR SWIA202158587](https://openairdocs.org/sdr/SWIA202158587.md): Floorbeam · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > * CORROSION DETECTED ON CRAWLWAY FLOOR "SUPPORT" ANGLE, ON AFT SIDE OF F.S. 280.00 BETWEEN STGR 26L AND 26R, AROUND NUT PLATE HOLES (MARKED). (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-11-10-001-003-A01. IN
- [SDR SWIA202158586](https://openairdocs.org/sdr/SWIA202158586.md): Strap · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED "ON" THE (CIRCUMFERENTIAL JOINT STRAP), BELOW FLOOR AT F.S. 333.00, ON BOTH FWD AND AFT SIDES OF THE F.S. AROUND FASTENERS IN SEVERAL PLACES BETWEEN STGR 25L AND STGR 25R (MARKED). (C-CHECK RO 5/25/2021) (CIRCUMFERENTIAL JOINT STRAP
- [SDR SWIA202158585](https://openairdocs.org/sdr/SWIA202158585.md): Floorbeam · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > *CORROSION ON FLOOR BEAM PACKER ON FS 333.00, LBL9. MARKED. (C-CHECK RO 5/25/2021) REMOVED AND REPLACED F.S.333.00 LBL9 PACKER IAW CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR SWIA202158584](https://openairdocs.org/sdr/SWIA202158584.md): Mount · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > *CORROSION ON AFT/INBD WARDROBE FLOOR MOUNT ATTACHED TO FLOOR SUPPORT BEAM FS 310.00 BETWEEN LBL9 €“ LBL27 (C-CHECK RO 5/25/2021) REMOVED AND REPLACED AFT/INBD WARDROBE FLOOR MOUNT ATTACH FITTING IAW CRJ-900 SRM 51-42-21-001-001-A01
- [SDR SWIA202158583](https://openairdocs.org/sdr/SWIA202158583.md): Seat Track · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > * RH SIDE SEAT TRACK HAS CORROSION MULTIPLE PLACES BETWEEN FS785 AND FS847+14. (C-CHECK RO 5/25/2021) REPLACED RH SIDE SEAT TRACK BETWEEN FS 785 - 847+14 REF CRJ-700 AMM 53-00-49-400-801-A07
- [SDR SWIA202158582](https://openairdocs.org/sdr/SWIA202158582.md): Seat Track · corroded · Mar 18, 2021 · N548CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > * RH SIDE SEAT TRACK HAS CORROSION MULTIPLE PLACES BETWEEN FS847+14 AND FS868. (C-CHECK RO 5/25/2021) REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN F.S. 847+14 AND F.S. 868.00. SEE CONTINUE CARD FOR DETAILS

Next page: https://openairdocs.org/aircraft/N548CA/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 = 'N548CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N548CA/reports

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