N582CA

Service difficulty reports · 174

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 = 'N582CA' 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 REXA2024101700882Pressure Deck · misalignedWHILE INCORPORATING SB 670SH-53-043 REV C, WE HAVE ENCOUNTERED MISMATCHED FACTORY PILOT HOLES @FS 843 LBL 18 COMMON TO THE LBL18 FLOOR BEAM AND PRESSURE BOX EXISTING HOLES. REPAIRED BY INSTALLING A FREEZE PLUG IAW MHIRJ REO 690-53-41-502 REV -- DATED 2024-10-Oct 6, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024101500871Bracket · noneWHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. FABRICATED AND INSTALLED BRACKETS IAW MHIRJ SNIEOS KSH670-35829-S8Oct 6, 2024 · N582CA · Cndair CL6002D24 · Standard Practices/StructuresSDR REXA2024101800887Fitting · unknownWHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND LH AND RH FITTINGS PN CC670-33562-001SB AND CC670-33563-001SB AT STR12A CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING RIVET PATTERN ON THE AIRCRAFT. TRIMOct 3, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024101800886Beam · failed inspLBL 9 BULKHEAD BEAM, I/B SIDE @ FS 693 HAS A PREVIOUS REPAIR ON TOP FLANGE COMMON TO THE FLOOR BEAM AND FLOORBOARD MOUNTING STRUCTURE. THIS REPAIR WAS DISCOVERED WHILE REMOVING STRUCTURE TO INCORPORATE SB 670SH-53-043 AND WILL REQUIRE A DEVIATION FROM ENGINEEROct 1, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024110101365Door Frame · crackedR/H AFT EMERGENCY EXIT DOOR, UPPER AFT FITTING IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR AIR EA # CRJ952-16440 REV.IR, DATED 04/20/2024.Jun 5, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024102501010Housing · crackedWHILE PERFORMING SDI OF MAIN AVIONICS COMPARTMENT DOOR HANDLE FOUND MULTIPLE INDICATIONS 50%FSH, FAILED NDT INSTALLED AVIONICS BAY DOOR HANDLE HOUSING AND FASTENERS IAW CRJ900 SRM 51-42-06-001-001-A01Jun 5, 2024 · N582CA · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2024110101364Stringer · corrodedSTRINGER 19R FROM F.S.280.00 TO F.S.316.00 IS CORRODED AT MULTIPLE FASTENER LOCATIONS. INSTALLED NEW SERVICEABLE STRG 19R PN SH670-31632-1 FOR FS 280 - FS 316 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01May 31, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024110101363Stringer · corrodedSTRINGER 20R CORRODED BETWEEN FS280 AND FS333. INSTALLED STRG 20R (PN SH670-31208-3) BETWEEN FS 280 - FS 316 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.May 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024103001163Floorbeam · crackedLBL 12.00 COCKPIT FLOOR BEAM IS CRACKED IN RADIUS AT FS280.00. REMOVED CRACKED BEAM AT LBL 12 FS280. FABRICATED AND INSTALLED NEW L/H FLOOR BEAM P/N CC670-33202-21 IAW CRJ 900 SRM 53-11-43-201-003-A01.May 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2024080600621Stringer · corrodedSTRINGER 19RH IS CORRODED BETWEEN FS437-453 REMOVED AND INSTALLED NEW SERVICEABLE STRINGER 19R BETWEEN FS349 TO FS477 (PN# SH670-31103-4S) IAW CRJ900 51-42-06-001-001-A01.May 25, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024070300497Angle · corroded"WATER WASTE SERVICE DOOR SURROUND DIAPHRAGM P/N SH670-32285-13 IS CORRODED ON OUTER SURFACE BETWEEN FS379.00 AND FS394.00, STR 21R. INSTALLED NEW SERVICEABLE SURROUND DIAPHRAGM PN SH670-32285-15 IAW CRJ 900 SRM 51-42-06-001-001-A01.EVALUATE AND BLEND CORROSIMay 23, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024100100750Angle · corrodedPAX DOOR MID SILL ANGLE IS CORRODED. REMOVED PAX DOOR MID SILL PN: SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE PAX DOOR MID SILL PN: SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42May 21, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024110101362Stringer · corrodedAFT CARGO STR 26R HAS CORROSION BETWEEN FS 1031 AND FS 1047. COMPLIED WITH ENDEAVOR EA CRJ953-16613 REV.IR DATED 5-7-2024.May 14, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024052800406Floor Support · corrodedPREVIOUS FLOOR BEAM REPAIR AT L.B.L 27.00 HAS CORROSION ON THE CAP AT F.S. 1025.00 TO F.S. 1037.00. REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ900 SRM 53-00-41-201-001-A03.May 14, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024052800405Drag Angle · crackedVERTICAL STAB., R/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.May 14, 2024 · N582CA · Cndair CL6002D24 · Vertical StabilizerSDR REXA2024052800404Intercostal · corrodedPAX DOOR FORWARD INTERCOSTAL DD5 IS CORRODED. REPLACED INTERCOSTAL I.A.W. CRJ900 SRM 51-40-1-001-001-A01 AND 51-42-06-001-001-A01.May 13, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024052800403Drag Angle · crackedVERTICAL STAB., L/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.May 13, 2024 · N582CA · Cndair CL6002D24 · Vertical StabilizerSDR REXA2024052800407Intercostal · corrodedPAX DOOR INTERCOSTAL DD7A MID CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR INTERCOSTAL DD7 MID C ANGLE P/N 601R317052-1 IAW CRJ 900 SRM 52-42-21-001-001-A01May 10, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024052200394Intercostal · corrodedINTERCOSTAL BETWEEN FS 310 AND FS 319.70 ON STRG 20R IS CORRODED. UPON FURTHER INVESTIGATION FOUND STGR 20R INTERCOSTAL AT FS 310 TO FS 319.70 (PN SH670-32047-1) TO BE CORRODED BEYOND ALLOWABLE LIMITS IAW CRJ 900 SRM 53-21-23-101-002-A02 AND REQUIRES REPLACMay 10, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024080600620Intercostal · corrodedPAX DOOR INTERCOSTAL DD4 FWD CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD4 P/N 601R318093-1 IAW CRJ 900 SRM 51-42-06-001-001-A01May 9, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024052800402Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 FWD CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3 IAW CRJ 900 SRM 51-42-06-001-001Ï¿½A01May 9, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024102100899Door · corrodedL/H AFT OVERWING EMERGENCY EXIT DOOR S/N B1394 TOP FORMER IS CRACKED. RECEIVED ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. COMPLIED WITH STEPS 1,2,4-7 OF ENDEAVOR AIR EA CRJ952-16638 REV IR (P1) DATED 5/12/2024. REMOVED DOOR LINING IAW CRJ900 AMMay 7, 2024 · N582CA · Cndair CL6002D24 · Emergency ExitsSDR REXA2024062400471Stringer Splice · corrodedSTGR 19R SPLICE IS CORRODED BETWEEN F.S. 469 TO F.S. 485. STGR 19R SPLICE IS CORRODED BETWEEN F.S. 469 TO F.S. 485. DAMAGE REQUIRES EVALUATION. FOUND STRINGER SPLICE PN: SH670-33264-1 AT STR 19R AND FS 477.40 TO BE CORRODED OUT OF LIMITS IAW CRJ-900 SRM 53-00-Apr 30, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024092600724Frame · crackedRH FRAME FS333 CRACKED BETWEEN STGR1R AND STGR2R REPAIRED DAMAGE RH FRAME FS333 BETWEEN STGR1R AND STGR2R IAW EA NO. CRJ953-16546 DATED: 5/10/2024 REV IRApr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2024091000687Former · corrodedPAX DOOR FS329.41 FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED FORMER AT FS 329.14 IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED NEW FORMER AT F/S 329.14 BETWEEN DD4 AND DD5 P/N 601R318088-3 IAW CRJ 900 SRM 51-42-06-001-001-A01 Apr 29, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024062400470Floor Support · corrodedRBL 9 FLOOR BEAM CAP CORRODED AROUND NUTPLATE HOLES FROM FS693 TO FS752.50 REPAIRED RBL9 FLOOR BEAM CAP IAW MHIRJ REO 690-53-41-470 REV -- DATED 2024-06-13.Apr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024052800401Frame · corrodedFRAME CORRODED AT FS 847+32 BETWEEN STRINGERS 26L AND 26R. REPAIRED DAMAGE I.A.W. CRJ 900 SRM 53-00-06-201-001-A01.Apr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2024062400469Stringer · corrodedSTRINGER20RH @ FS549-565 IS CORRODED. S20R @ FS 549-565 IS CORRODED REQUIRES EVAL BLENDED OUT DAMAGE IAW CRJ900 SRM 51-21-06-001-001-A01 NO DAMAGE ALLOWED IN AREA PER CRJ900 SRM 53-31-03-101-003-A04 REPAIR REQUIRED STGR 20R FROM FS 477-613 REQUIRES INSTALL INSApr 28, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024062400468Stringer · corrodedAFT CARGO STR 21L HAS CORROSION AFT OF FS 985.00. AFT CARGO STR 21L HAS CORROSION AFT OF FS 985.00. REMOVED CORROSION AFT CARGO STR 21L, AFT OF FS 985.00, IAW CRJ 900 SRM 51-21-06-001-001-A01. REQUIRE UT FOR CHECK THICKNESS (NDT) PERFORMED UT THICKNESS OF STRIApr 26, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024052800400Intercostal · corrodedINTERCOSTAL AT FS865.00-FS881.00 @STGR21R IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL (PN: SH690-37121-1S) AT STRG 21R BETWEEN FS 865 TO FS 881 IAW CRJ900 SRM 51-42-06-001-001-A01Apr 26, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024110101360Bracket · corrodedPAX DOOR BRACKET ON FWD INTERCOSTAL DD5 CORRODED REQUIRES REPLACEMENT PAX DOOR BRACKET ON FWD INTERCOSTAL DD5 INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024110101359Stringer · corrodedAFT CARGO STRINGER 26L HAS CORROSION BETWEEN FS1069-FS1088. REPAIRED DAMAGE I.A.W. CRJ900 SRM 53-00-03-201-001-A02.Apr 21, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2024091100707Door Frame · corrodedPAX DOOR F.S. 320 FRAME IS CORRODED BETWEEN INTERCOSTAL DD4 AND DD5. REMOVED PAX DOOR FS320 FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. RECEIVED NEW F/S 320 FRAME P/N 601R318032-5 , LOCATED AND DRILLED IAW CRJ 900 SRM 51-40-11-001-001Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024052800399Handle · crackedPAX DOOR INNER HANDLE CRACKED. REMOVED AND REPLACED HANDLE I.A.W. 51-40-11-00-001-001-A01 AND 51-43-00-001-001-A01.Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2024103001164Bracket · crackedGALLEY SERVICE DOOR STABILIZER BAR IS CRACKED. GALLEY SERVICE DOOR STABILIZER BAR BRACKET REQUIRES REPLACEMENT. REMOVED GALLEY SERVICE DOOR STABILIZER BAR BRACKET IAW CRJ 900 AMM 52-41-27-400-801-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE BRACKET PN:Apr 17, 2024 · N582CA · Cndair CL6002D24 · Service DoorsSDR REXA2024052200392Angle · corrodedPAX DOOR MID SILL ANGLE IS CORRODED AROUND SCREW HOLES. UPON FURTHER INVESTIGATION, FOUND PAX DOOR MID CAP ANGLE P.N. SH670-31825-7 TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELAMENTS AND IN EXCESS OF OVER 40% OF MATERIAL THICKNESS IAW CRJ900SRM TASK 53Apr 17, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020121600836Battery Pack · inoperativeON PREFLIGHT EMERGENCY LIGHTS IN ROW 13 DO NOT WORK-SIDE WALL & OVERHEAD LIGHTS. R & R NR 2 BATTERY PACK, IAW CRJ 900 AMM 33-51-17. OPERATIONS CHECK GOOD NO FURTHER DEFECTS NOTED.Dec 15, 2020 · N582CA · Cndair CL6002D24 · Emergency LightingSDR REXA2020121500834Battery Pack · inoperativeREAR FACE OF CEILING EMERGENCY EXIT LT AND ROW 13 LOWER EMERGENCY EXIT LIGHTS NOT ILLUMINATED DURING TEST. REMOVED AND REPLACED BATTERY ASSEMBLY PS 37. P/N OFF: AD-2013-1A SN: 71935; P/N ON: 2013-1ASMI SN: 10096. OPERATIONS CHECK GOOD, IAW CRJ-900 33-51-17.Dec 10, 2020 · N582CA · Cndair CL6002D24 · Emergency LightingSDR REXA2019122671775Hinge Fitting · corrodedCORROSION FOUND ON THE LT & RT HINGE FITTINGS AT THE NLG STRUCTURE. THE FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.Dec 17, 2019 · N582CA · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2019122671767Plate · corrodedCORROSION ON PLATE LOWER AT FWD BAGGAGE BAY DOOR, THE PLATE WAS REPLACED IAW AMM 52-35-07-400-802 ( CONFIG. A02 ) FIGURE 410.Dec 17, 2019 · N582CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019122671733Stringer · corrodedCORROSION ON STRINGER 25L, BS 280 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-20-001-001-A01. "Dec 17, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019122611780Receptacle · crackedCRACK FOUND IN RECEPTACLE PLATE AT FUSELAGE. THE RECEPTACLE PLATE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 16, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019122651774Canister · crackedCRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. REPAIRED PER REO 670-57-42-577 REV--. AND FUEL LEAK CHECK WAS PERFORMED PER AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND.Dec 15, 2019 · N582CA · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA201912651773Canister · crackedCRACK FOUND IN CANISTER, WELDED NR 3 AT LWS 148 IN THE LT MAIN FUEL TANK. REPAIRED IAW REO 670-57-42-577 REV--. AND FUEL LEAK CHECK WAS PERFORMED PER CRJ-900 AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND "Dec 15, 2019 · N582CA · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2019126251766Coaming · wornWEAR FOUND ON LOWER COAMING AT THE AFT BAGGAGE DOOR CUT-OUT. THE LOWER COAMING WAS REPLACED IAW SRM 51-41-02-001-001-A01 PAR 6.Dec 15, 2019 · N582CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019122641778Doubler · corrodedCORROSION WAS FOUND ON THE C CHANNEL DOUBLER AT BS 333 TO 349 BETWEEN STRINGERS 24R & 25R IN THE MAIN AVIONICS COMPARTMENT. THE DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR 6.C.Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019122641777Stringer · corrodedCORROSION FOUND ON STRINGER 24R, BS 337 TO 394 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPAIRED RM 53-00-03-201-001-A02, FIG. 53-00-03-995-807.Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019122641768Floor Support · crackedCRACK ON THE LONGITUDUNAL FLOOR SUPPORT RBL 12, BS 279. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-11-43-201-003-A01, AND FIGURE 53-11-43-995-819.Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019122641765Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM ANGLE AT BS 280 BETWEEN LBL 11TO RBL 11. FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-20-001-001-A01.Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019122641763Intercostal · corrodedCORROSION FOUND ON INTERCOSTAL, BS 349 TO 364 NEAR STRINGER 27 IN THE MAIN AVIONICS COMPARTMENT. INTERCOSTAL WAS REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6.C, AND SRM 51-42-20-001-001-A01 PAR. 6.Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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