N548CA

Service difficulty reports · 182

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 = 'N548CA' 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 SWIA202158509Slat Track · worn* LH SLAT TRACK 3-3 HAS MULIPLE NICKS ON THE FWD FACE RAIL AND THE AFT FACE L/E RAILS. (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOT / PITTING FROM THE LH SLAT TRACK 3-3, MATERIAL LOSS FOUND TO BE WITHIN LIMITS REF MHIRJ REO 690-57-42-797 REMar 17, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158508Slat Track · worn* LH SLAT TRACK 3-2 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED) (C-CHECK RO 5/25/2021) .REMOVED FLAT SPOTS / PITTING FROM THE LH SLAT TRACKMar 17, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158507Slat Track · worn* LH SLAT TRACK 3-1 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOT / PITTING FROM THE LH SLAT TRACK 3-1, MATERIAL Mar 17, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158506Slat Track · worn* LH SLAT TRACK 2-3 HAS MULIPLE FLAT SPOTS AND PITTING AND COROSSION ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOTS / PITTING FROM THE Mar 17, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158505Slat Track · worn* LH SLAT TRACK 2-2 HAS MULIPLE FLAT SPOTS AND PITTING AND COROSSION ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOTS / PITTING FROM THE LMar 17, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158504Slat Track · worn* LH SLAT TRACK 2-1 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOT / PITTING FROM THE LH SLAT TRACK 2-Mar 16, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158503Slat Track · worn* LH SLAT TRACK 1-3 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED) (C-CHECK RO 5/25/2021) .REMOVED FLAT SPOTS / PITTING FROM THE LH SLAT TRACK 1Mar 16, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158502Slat Track · worn* LH SLAT TRACK 1-2 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS WITH PITTING AND COROSSION ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOT / PITTING FROM THE LH SLAT TRACK 1-Mar 16, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158501Slat Track · worn* LH SLAT TRACK 1-1 HAS MULIPLE FLAT SPOTS AND PITTING ON THE FWD FACE RAIL, AFT FACE L/E RAILS AND PITTING ON THE LOWER END OF THE AFT FACE RAIL (AREAS MARKED). (C-CHECK RO 5/25/2021) REMOVED FLAT SPOT / PITTING FROM THE LH SLAT TRACK 1-1, MATERIAL LOMar 16, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158500Cleat · corrodedPAX DOOR CLEAT ATTACHED TO FRAME DD4 FS 313.56 IS CORRODED (C-CHECK RO 5/25/2021) REMOVED CORROSION ON CLEAT PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKENESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100 % MATERIAL LOSS CLEAT FMar 15, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA202158499Former · corrodedPAX DOOR FORMER @ FS 320.163 IS CORRODED ON BOTTOM FLANGE (C-CHECK RO 5/25/2021) REPLACED PAX DOOR FORMER FS320.163 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158498Structure · corroded*EVALUATE CHAFE IN RIGHT MLG WHEEL WELL WING STRUCTURE. (MARKED) (C-CHECK RO 5/25/2021) REPAIRED CHAFE IN RIGHT MLG WHEEL WELL WING STRUCTURE AT THE WS14.50 BATT RIB REF REO 690-57-21-387 REV--, DATED 2021-03-26. COMPLIED WITH 51-900-1002-SKY. SEE CONTIMar 15, 2021 · N548CA · Cndair CL6002D24 · Wing Main, Frame StructureSDR SWIA202158497Intercostal · corrodedPAX DOOR INTERCOSTAL IS CORRODED FS 311.125 # 6 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION ON INTERCOSTAL PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOUMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158496Intercostal · corrodedPAX DOOR INTERCOSTAL IS CORRODED FS 311.125 #2 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION FROM INTERCOSTAL PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS INMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158495Intercostal · corrodedPAX DOOR INTERCOSTAL IS CORRODED FS 311.125 #1 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORRPSION FROM INTERCOSTAL PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 51-11-06-01-001-A01, 100% MATERIAL LOSS INTMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158494Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 # 8 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION ON BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNES IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS BRACKMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158493Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 # 7 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROISON ON BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOUNMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158492Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 # 6 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION FROM BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158491Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 # 5 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION FROM BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158490Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 # 4 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION ON BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOUNMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158489Bracket · corrodedBRACKET ON PAX DOOR FOUND CORRODED @ FS 311.125 #3 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION ON BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIAL LOSS FOMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158488Bracket · corrodedCORROSION FOUND ON PAX DOOR BRACKET FS 311.125 #2 FROM THE TOP (C-CHECK RO 5/25/2021) REMOVED CORROSION FROM PAX DOOR BRACKET PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATERIALMar 15, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158487Angle · corrodedCORROSION FOUND ON CLIP INTERCOSTAL DD7 #1 FROM THE TOP OF PAX DOOR (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND CLIP INTERCOSTAL DD7 #1 FROM THE TOP OF PAX DOOR BE OUT OF LIMITS. REPLACED CLIP WITH NEW PER CRJ900 SRM 51-42-06-001-001-A01 & DWG Mar 15, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWIA202158560Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL BETWEEN GS 338.963 AND 347.250 MID SECTION OF DOOR (C-CHECK RO 5/25/2021) CORROSION FOUND TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 REV N. COMPLIED WITH TASKMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158486Post · corrodedL/H F.S.280.00 POST AT BL11.128 HAS CORROSION AT LOWER CORNER. (C-CHECK RO 5/25/2021) INSTALLED L/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-SKYMar 14, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA202158485Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD6 BETWEEN FS 338.963 AND 347.250 (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND INTERCOSTAL DD6 BETWEEN FS 338-963 AND 347.250 TO BE OUT OF LIMITS. REPLACED INTERCOSTAL DD6 WITH PN: 601R31902-323 BETWEEN FSMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158484Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD1 BETWEEN FS 338.963 AND 347.250 (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND INTERCOSTAL DD1 BETWEEN FS338 AND FS347 TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-900 SRM 51-42-06-001-001-A01, DWG: 60Mar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158483Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD4 BETWEEN FS 311.75 AND 320.163 (C-CHECK RO 5/25/2021) REMOVED CORROSION ON PAX DOOR INTERCOSTAL DD4 PER CRJ 900 SRM 51-21- 06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-AMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158482Door Frame · corrodedCORROSION FOUND ON PAX DOOR FRAME DD4 BETWEEN FS 311.75 AND 320.163 (C-CHECK RO 5/25/2021) REMOVED CORROSION ON PAX DOOR FRAME DD4 PER CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100 % MATMar 14, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA202158481Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD7A BETWEEN FS 320.163 AND 327.563 (C-CHECK RO 5/25/2021) REMOVED CORROSION ON INTERCOSTAL DD7A AND FOUND REWORKED AREA OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 Mar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158480Angle · corrodedCORROSION FOUND ON CLIP @ FS 329.563 TOP SIDE OF PAX DOOR (C-CHECK RO 5/25/2021) REPLACED CLIP PN: 601R318058-1, COMMON TO PAX DOOR FRAME AT FS327.763 AND INTERCOSTAL DD7A IAW CRJ900 SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N, COMPLIED WITH 337 FORMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158479Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD3 BETWEEN FS 320.163 AND 338.963 (C-CHECK RO 5/25/2021) REMOVED PAX DOOR INTERCOSTAL DD3 BETWEEN FS320.163 AND FS338.963 IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED NEW PAX DOOR INTERCOSTAL DD3 PN: 601R31805Mar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158478Intercostal · corrodedCORROSION FOUND ON PAX DOOR INTERCOSTAL DD3 BETWEEN FS 311.75 AND 320.163 (C-CHECK RO 5/25/2021) REMOVED CORROSION ON INTERCOSTAL DD3 PER CRJ 900 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS IS .050 PER CRJ 900 SRM 52-11-06-001-001-A01, 100% MATEMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158477Former · corrodedCORROSION FOUND ON PAX DOOR FORMER @ FS 347.25 (C-CHECK RO 5/25/2021) REMOVED AND REPLACED PAX DOOR FORMER P/N 601R318034-1 AT FS 347.25. PRESSURE CHECK GOOD. NO DEFECTS NOTED. REF: CRJ 900 SRM 51-42-06-001-001 (A01), CRJ 900 AMM 51-42-21-001-001 (A01)Mar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158476Structure · corrodedMULTIPLE SPOTS OF CORROSION FOUND ON BOTTOM CORNER OF PAX DOOR AFT SIDE (C-CHECK RO 5/25/2021) REMOVED AFT BOTTOM CORNER FITTING IAW CRJ900 SRM 51-42-21-001-001-A01 & SRM 51-42-21-001-001-A01. INSTALLED NEW PAX DOOR BOTTOM AFT CORNER PN: 601R319983-4 IMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158475Structure · corrodedMULTIPLE SPOTS OF CORROSION FOUND ON BOTTOM CORNER OF PAX DOOR FWD SIDE (C-CHECK RO 5/25/2021) REMOVED AND REPLACED PAX DOOR FWD BOTTOM CORNER PER PN 601R319983-3S PO # 15159-0008 PER CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01 AMar 14, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158474Floor Support · corrodedCOCKPIT FLOOR SUPPORT HAS POSSIBLE CORROSION. (C-CHECK RO 5/25/2021) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT IAW BOMBARDIER DWG CC670-34010 REV.-K CRJ-900 SRM 51-42-06-001-001-A01 REV.38 25JUL2020 CRJ-900 SRM 51-42-21-001-001-A01 REV.38 25JUL2020. COMar 14, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA202158473Slat Track · worn* RH SLAT TRACK 2-2 HAS WEAR MARKS. (C-CHECK RO 5/25/2021) BLENDED THE WEAR DAMAGE ON 2-2 RHS SLAT TRACK AND FOUND TO BE WITHIN LIMITS REF REO 690-57-42-786 REV -A 2021-03-19 STEPS 1-5. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 13, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158559Nut · corroded* CORROSION DETECTED ON L/H-AFT EMER EXIT DOOR, AT (10EA) "NUTS" THAT ATTACH THE LATCH MECHANISM TO THE TOP INTERCOSTAL INSIDE THE DOOR (MARKED). (C-CHECK RO 5/25/2021) REMOVED AND REPLACED L/H-AFT EMER EXIT DOOR NUTS (10EA) THAT ATTACH THE LATCH MECHANMar 12, 2021 · N548CA · Cndair CL6002D24 · Emergency ExitsSDR SWIA202158472Door Sill · corroded*AFT BAGGAGE BAY - DOOR SILL IS HEAVILY CORRODED ACROSS MULTIPLE ELEMENTS. (C-CHECK RO 5/25/2021) REMOVED CORRODED DOOR SILL AND REPLACED WITH NEW DOOR SILL @ AFT BAGGAGE BAY DOOR PER DWG:MM670-35085 REV L & CRJ-900 SRM 51-42-06-001-001-A01 & SRM 51-42-Mar 11, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA202158471Former · corroded*PASSENGER DOOR €“ FORWARD FORMER HAS CORROSION AT THE TOP AND LOWER ENDS. (MARKED) (C-CHECK RO 5/25/2021) REMOVED AND REPLACED FWD FORMER ON PAX DOOR. REF: SRM 51-42-06-001-001 (A01), DWG 601R31702 REV. N, AND CRJ 900 SRMS 51-42-21-001-001 (A01), 51-4Mar 11, 2021 · N548CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA202158470Receptacle · cracked*FWD EQUIPMENT COMPARTMENT DECK HAS CRACK IN FLANGE AT AFT LATCH RECEPTACLE CUT OUT FOR ACCESS DOOR 212AR. (C-CHECK RO 5/25/2021) REPLACED LOWER DOOR LANDING FOR FWD ACCESS DOOR FS173 - FS193 RHS REF REO 690-53-11-1310 REV -- 2021-03-26, SNIEO: CC670-33Mar 11, 2021 · N548CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA202158469Skin · dentedEVALUATE DENT LOCATED ON THE RH SLAT LEADING EDGE AT APPROXIMATELY WS88.00. (C-CHECK RO 5/25/2021) EVALUATED DENT ON RH SLAT LEADING EDGE AT APPROX WS88.00 AND FOUND ACCEPTABLE AT THIS TIME REF REO 690-57-42-787 REV -A 2021-04-05. COMPLIED WITH TASK CARMar 2, 2021 · N548CA · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202158468Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA39771-690-53-11-1035 548CA-PR - DENT FOUND AT FS 192.00 BETWEEN STGR23 & STGR24 FWD OF EXTERNAL POWER RECEPTACLE DOOR. COMPLIED WITH TEMPORARY DISPOSITION PER REO 690-53-11-1035 REV A DATED 2019-05-14. PERMANENT REPAIRFeb 17, 2021 · N548CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2020020348061Unknown · odorON DEPARTURE AT 1000FT AGL, SMOKE AFT LAV MASTER WARNING ILLUMINATED. FAS CALLED AND SMELLED FUMES AS WELL AS HEARD THE AFT LAV FIRE ALARM GOING OFF. QRH PROCEDURE WAS RUN AND THE INDICATION DID NOT PERSIST. DECLARED AN EMERGENCY AND RETURNED TO FIELD WITH EMEFeb 1, 2020 · N548CA · Cndair CL6002D24 · Air Distribution SystemSDR SWIA2019091046262Proximity Sensor · out of adjustGEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. PERFORMED QRH PROCEDURES AND HAD A NORMAL LANDING. (FLT#3755) CLOSED ADJUSTED THE NLG CENTERING PROXIMITY SENSOR IAW AMM. OPS CHECK GOOD AT THIS TIME.Sep 10, 2019 · N548CA · Cndair CL6002D24 · Landing Gear Position and WarningSDR SWIA201743409Floorbeam · corrodedAFT COCKPIT FLOORBEAM ANGLE ATTACHED TO BS 280 HAS CORROSION BETWEEN LBL 9 TO RBL 9. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM.Jun 9, 2017 · N548CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA201541417Stringer · corrodedSTRINGER 26R, BS 280 - 333 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM.Aug 20, 2015 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201541416Stringer · corrodedSTRINGER 25R BETWEEN BS 280 - 333 CORRODED. REPLACED THE STRINGER IAW REO AND SRM.Aug 20, 2015 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA201541419Stringer · damagedSTRINGER 25R BETWEEN BS 333 & 363. REPLACED THE STRINGER IAW SRM.Aug 19, 2015 · N548CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
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