N549CA

Service difficulty reports · 129

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N549CA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026090801779Fitting · damagedFOUND R/H AILERON SIDE BEARING LUGS LABELED H AND I TO BE OVERSIZED. REPAIRED R/H AILERON LUG LABELED H AND I IAW MHIRJ REO 690-57-61-549 REV -- DATED 2026-08-21.Sep 6, 2026 · N549CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026091401769Bearing · failedRUDDER PCU SYSTEMS NR 1 & 2 FAILED BOTH PCU AND BEARING BACKLASH. SYSTEM NR 1 PCU MEASURED 0.330IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.180IN WITH A MAX OF 0.120IN. SYS NR 2 PCU MEASURED 0.273IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.135IN Aug 24, 2026 · N549CA · Cndair CL6002D24 · Aileron Control SystemSDR REXA2026091001795Door · cracked"RH AFT EMERGENCY EXIT UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF RH AFT EMERGENCY EXIT FORMER AT AFT LUG IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 STEP 1 FOUND FORMER HAS INDICATION NOTED .750 INCHES LONG FAILED NDT AREA MARKED ON FORMER. COMAug 24, 2026 · N549CA · Cndair CL6002D24 · Emergency ExitsSDR REXA2026083101766Web · corroded"RH FS 280 WEB IS CORRODED AT RBL 11. REMOVED CORROSION FROM R/H F.S. 280 WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG. .040"", REMOVED .010"" REMAINING .030"", ALLOWABLE .005"". REQUIRES REPLACAug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2026083101765Web · corroded"LH FS 280 WEB IS CORRODED AT LBL 11. REMOVED CORROSION FROM L/H F.S. 280 WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG. .040"", REMOVED .007"" REMAINING .033"", ALLOWABLE .005"" REQUIRES REPLACEAug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2026082501638Angle · crackedFLOOR STRUCTURE ANGLE P/N CC670-34099-1 AT FS280.00, LBL12.0 IS CRACKED. LOCATED AND DRILLED SERVICEABLE LBL 12 AT FS 280 ATTACH ANGLE P/N CC670-34099-1SB IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE ATTACH ANGLE AT FS 280 LBL 12 P/N CC670-34Aug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026090401774Bushing · abnormalRIGHT AILERON CENTER HINGE FITTING BUSHING LUG MARKED C FOUND TO BE O/S UPON BUSHING REMOVAL. REPAIRED RT AILERON SIDE LUG LABELED C IAW STEP F.(1) - F.(4) OF GREO 670-57-61-237 REV --. LPI PERFORMED ON REAMED BORE IAW STEP F.(5) OF GREO 670-57-61-237 REV --.Aug 20, 2026 · N549CA · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026092101831Floorbeam · corrodedRT BS 280 BEAM HAS CORROSION UNDER UPPER SPLICE STRIP. BLENDED CORROSION ON RT BEAM UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. BEAM REQUIRES REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE RT CROSSBEAM IAW SRM 5Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026092101830Floorbeam · corrodedLT FS280 BEAM HAS CORROSION ON FWD SIDE UNDER J-ANGLE. BLENDED CORROSION ON LH FS280 BEAM UNDER J-ANGLE & UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. LT 280 BEAM REQUIRES REPLACEMEMNT. INSTALLED UPPER SPLICE STRIP Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026091401827Drag Angle · crackedRH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED R/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026091401826Drag Angle · crackedLH VERTICAL STAB AFT DRAG ANGLE IS CRACKED REMOVED CRACKED DRAG ANGLE AND LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE L/H VERT. STAB AFT DRAG ANGLE P/N AV670-21186-003 IAW CRJ-900 SRM 51-40-11-001-001-A01, AND 51-42-13/21/22-001-001-A01.Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026091401825Drag Angle · crackedLH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026090401773Floorbeam · corrodedJ-ANGLE AT BS 280 IS CORRODED AROUND FASTENER HOLES. EVAL CORROSION ON FS280 J-ANGLE. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE 100% MATERIAL LOSS AT CAMLOCK RECEPTACLE. J-ANGLE REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE J-ANGLE FROM FS 280 Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026091101799Door · crackedLH AFT EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH AFT EMERGENCY EXIT FORMER AT AFT LUG IAW REO 670-52-21-103 REV -, STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER. COMPLETED STEPS 2, 3 AAug 4, 2026 · N549CA · Cndair CL6002D24 · Emergency ExitsSDR REXA2026091001794Door · cracked"LH FWD EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH FWD EMERGENCY EXIT FORMER AT AFT LUG IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER.Aug 4, 2026 · N549CA · Cndair CL6002D24 · Emergency ExitsSDR REXA2026042200297Handle · stuckPASSENGER DOOR INNER HANDLE GETTING STUCK MOVING UP TRYING TO OPEN DOOR. COULD NOT OPEN DOOR FROM INSIDE OR FROM THE OUTSIDE. RAMPERS TRIED. HANDLE WAS STUCK BETWEEN BEING FULLY DOWN AND FULLY UP. FELT LIKE LIKE ANY MORE PRESSURE WOULD BREAK OFF HANDLE, IN EIApr 9, 2026 · N549CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2025111700014Windshield · crackedFRONT LEFT WINDSHIELD CRACKED AND STARTED SMOKING. (FLIGHT 3922) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31192916 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED FRONT LEFT WINDSHIELD IN REF TO AMM 56-11-01.Nov 14, 2025 · N549CA · Cndair CL6002D24 · Flight Compartment WindowsSDR SWIA2025010301Bracket · out of adjustGEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. THE GEAR INDICATION SHOWED THE LEFT MAIN GEAR WAS NOT UP. RAN THE QRH AND THE MESSAGE CLEARED AND ALL THREE GEAR SHOWED DOWN AND GREEN. MLG FAULT AND MDC STATUS MESSAGES REMAIN ON AT THE GATE (FLIGHT 4066 - FILEDJan 1, 2025 · N549CA · Cndair CL6002D24 · Main Landing GearSDR SWIA202501020001Landing Gear · warning messageGEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. THE GEAR INDICATION SHOWED THE LEFT MAIN GEAR WAS NOT UP. RAN THE QRH AND THE MESSAGE CLEARED AND ALL THREE GEAR SHOWED DOWN AND GREEN. MLG FAULT AND MDC STATUS MESSAGES REMAIN ON AT THE GATE (FLIGHT 4066 - FILEDJan 1, 2025 · N549CA · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR SWIA20230326Unknown · smokeFA REPORTS ON TAKEOFF AIRCRAFT HAS A SMOKE SMELL, FOLLOWED BY VERY LIGHT GREY SMOKE SETTLING AT FLOOR LEVEL IN FIRST CLASS, FOLLOWED BY A SOLVENT SMELL THAT REMAINED FOR THE DURATION OF THE 20 MINUTE FLIGHT. (FLIGHT 4504 - FILED OPEN) PLEASE REFERENCE AMMar 26, 2023 · N549CA · Cndair CL6002D24 · Air Conditioning SystemSDR SWIA2023030013Unknown · smokeAFTER DEPARTURE F/A'S NOTIFIED CREW OF THIN GRAY SMOKE THROUGHOUT THE CABIN AND AN ODOR MORE PRONOUNCED IN THE FRONT OF THE CABIN. (FLIGHT 3583 FILED CLOSED)PRIOR TO TROUBLESHOOTING, COULD NOT IDENTIFY THE SOURCE AND TYPE OF SMELL. TROUBLESHOT PER FIM 21-22-00Mar 13, 2023 · N549CA · Cndair CL6002D24 · Buffet/GalleysSDR SWIA202265530None · corrodedRH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 HAS CORROSION AROUND SEVERAL FASTENER HOLES (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED RH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF DWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-AMar 14, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202265529None · corrodedLH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 HAS CORROSION AROUND SEVERAL FASTENER HOLES (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED LH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF DWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-AMar 14, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202265528None · elongatedSTRINGER SPLICE AT FS333, STGR 22L HAS ELONGATED HOLES. (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STRINGER SPLICE AT FS333, STGR 22L. REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-32420 REV E. COMPLIED WITH TMar 9, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, KeelSDR SWIA202265527None · elongatedSTRINGER CLEAT AT FS295, STGR 23L HAS ELONGATED HOLES. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED STRINGER CLEAT AT FS295, STGR 23L. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG # SH670-31630 REV. K. / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (Mar 9, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, KeelSDR SWIA202265526None · crackedRH SLAT TRACK 1-3 CANNISTER SUPPORT FITTING INSIDE WING FUEL PANEL 651AB POSSIBLE CRACK (MARKED) (C-CHECK RO 4/25/2022) REMOVED BRACKET (CC670-12942-2) INSIDE WING FUEL PANEL 651AB REF REO 670-57-42--577, REV --, DATED 2016-12-02 AND INSTALLED ALL REPAIMar 8, 2022 · N549CA · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR SWIA202265525None · corrodedMAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 22L BETWEEN FS280.00 TO FS333.00 REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG # SH670-31630 REV. K. COMPLIEDMar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265524None · corrodedMAIN AVIONICS BAY STR 23L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 23L BETWEEN FS280.00 TO FS333.00 REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG # SH670-31630 REV. K. COMPLIEDMar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265523None · corrodedMAIN AVIONICS BAY STR 24L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 24L BETWEEN FS280.00 TO FS333.00 IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG:SH670-31630 REV K. COMPLIMar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265522None · corrodedMAIN AVIONICS BAY STR 25L CORRODED BETWEEN FS295.00 AND FS319.70 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 25L BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. COMPLMar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265521None · corrodedMAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 23R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG:SH670-32420 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEMar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265520None · damagedUPON REMOVAL OF PREVIOUSLY REPAIRED LOCATION ON COCKPIT FLOOR BEAM LOCATED AT FS274 RBL 12.0 FOUND DAMAGE ON COCKPIT FLOOR SKIN. (C-CHECK RO 4/25/2022) REPAIRED COCKPIT FLOORBEAM LOCATED AT FS274 RBL 12.0 REF REO 690-53-11-1407 REV.-- DATED 2022-03-11 AMar 1, 2022 · N549CA · Cndair CL6002D24 · Fuselage Floor PanelSDR SWIA202265519None · gougedINTERCOSTAL IS GOUGED BELOW FWD BAGGAGE BAY TIE DOWN FITTING AT FS517.00/STGR 26L-27 (C-CHECK RO 4/25/2022) REMOVED AND REPLACED INTERCOSTAL FS 517 STGR 26L-27 REF. DWG SH690-33600 REV. AG, CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-06-001-001-Feb 28, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202265518None · corrodedFWD CARGO TIE DOWN FITTING @ FS629.00, STGR 26L-27 (PN SH670-33389-1) REQUIRES REPLACEMENT DUE TO CORROSION. (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW TIE DOWN FITTING P/N SH670-33389-1 AT FS629. REF: DWG SH690-33600, REV: AG, CRJ900 SRM 51-42-21Feb 27, 2022 · N549CA · Cndair CL6002D24 · Cabin Equipment/FurnishingsSDR SWIA202265517None · corrodedFWD CARGO TIE DOWN FITTING @ FS517.00, STGR 26L-27 (PN SH670-33389-1) REQUIRES REPLACEMENT DUE TO CORROSION. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED CARGO TIE DOWN FITTING FS 517 STGR 26L-27 REF. DWG SH690-33600 REV. AG, CRJ 900 SRM 51-42-21-001-001Feb 27, 2022 · N549CA · Cndair CL6002D24 · Cabin Equipment/FurnishingsSDR SWIA202265516None · corrodedMAIN AVIONICS BAY STR 23L CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED STR 23L FROM FS333.00 TO FS357.00 AND STR 23L SPLICE REPAIR AT FS357.00 REF DWG SH690-31350 REV-M, CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265515None · corrodedMAIN AVIONICS BAY STR 22R CLEAT AT FS319.70 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 22R CLEAT AT FS319.70 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV-Y. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FORFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265514None · corrodedMAIN AVIONICS BAY STR 21R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 21R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH690-30006 REV-C. COMPLIED WITH TASK CARD 5Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265513None · corrodedMAIN AVIONICS BAY STR 22R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 22R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG: SH690-30006 REV-C. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265512None · corrodedMAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REPLACED MAIN AVIONICS BAY STR 21R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, ALL STEPS 1-4 OF REO 690-53-21-Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265511None · corrodedMAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STRINGER 22RH FROM FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, AND DWG SH670-31630 REV K. COFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265510None · corrodedMAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 23R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV-K. COMPLFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265509None · corrodedMAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 24R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV-K. ALL SFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)SDR SWIA202265508None · crackedUPON REMOVAL OF DAMAGED RH BEAM AT FS 280 AND APPROX. RBL 26.00 ANGLE P/N CC670-34117-6 IS CRACKED. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED ANGLE AT FS 280 LOWER WEB, RBL 26. REF: CRJ-900 SRM 51-42-06-001-001-A01 AND DWG. CC670-34010 REV K. SEE CONFeb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA202265507None · corrodedFOUND CORROSION ON FRAME STUB P/N: SH670-33260-3 AT FWD BAGGAGE BAY FS501.00. (C-CHECK RO 4/25/2022) REMOVED FRAME P/N: SH670-33260-3 FROM STRG 25L TO STRG 26L, FS 501.00 REF. CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND INSFeb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA202265506None · corrodedIN MAIN CABIN, AT FS549, UNDERR STR17L, BELOW L/H SILL, FRAME HAS AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/25/2022) REPAIRED FRAME AT FS549 STGR 18L-16L REF REO 690-53-31-628 REV.-- DATED 2022-03-01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-Feb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA202265505None · corrodedIN MAIN CABIN, AT FS533, UNDER STR17L, BELOW L/H SILL, FRAME HAS AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/25/2022) REPLACED FRAME SECTOR, FRAME SPLICE ANGLE, STRINGER CLEAT REF REO 690-53-31-628 REV.-- DATED 2022-03-01 AND DWG SH690-33100 REV. N, CRJFeb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA202265504None · corroded* FLOOR BEAM LBL 18 BETWEEN FS 1015.00- FS 1051.00 HAS AREAS OF CORROSION (C-CHECK RO 4/25/2022) REPAIRED FLOOR BEAM LBL 18 BETWEEN FS1005.5 TO FS1037.5 REF CRJ900 SRM 53-00-41-201-001-A03. COMPLIED WITH 51-900-1002-SKY.Feb 20, 2022 · N549CA · Cndair CL6002D24 · Fuselage Internal Mounting StructureSDR SWIA202265503None · corroded* FLOOR BEAM LBL 9 BETWEEN FS 1015.00- FS 1051.00 HAS AREAS OF CORROSION (C-CHECK RO 4/25/2022) REMOVED CORROSION ON LBL9 FLOOR BEAM UPPER SURFACE FS1005-FS1025.5 AND FS1037.5-FS1057 REF. CRJ900 SRM 51-21-06-001-001-A01. REQUESTED ENGINEERING, RECEIVED Feb 20, 2022 · N549CA · Cndair CL6002D24 · Fuselage Internal Mounting StructureSDR SWIA202265502None · out of toleranceREPLACE FS280 RH BEAM DUE TO FOUND OUT OF LIMITS ON CAMP#24366017. (C-CHECK RO 4/25/2022) REPLACED RH FS280 BEAM REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-10-001-001-A01, CRJ900 SRM 53-11-10-201-004-A01 AND DWG CC670-34010 REV. K. COMPLIED WFeb 19, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
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