# Service difficulty reports: N582CA

A list on [N582CA](https://openairdocs.org/aircraft/N582CA.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 · 174 reports

- [SDR REXA2024101700882](https://openairdocs.org/sdr/REXA2024101700882.md): Pressure Deck · misaligned · Oct 6, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Structure
  > WHILE 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-
- [SDR REXA2024101500871](https://openairdocs.org/sdr/REXA2024101500871.md): Bracket · none · Oct 6, 2024 · N582CA · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE 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-S8
- [SDR REXA2024101800887](https://openairdocs.org/sdr/REXA2024101800887.md): Fitting · unknown · Oct 3, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WHILE 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. TRIM
- [SDR REXA2024101800886](https://openairdocs.org/sdr/REXA2024101800886.md): Beam · failed insp · Oct 1, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Structure
  > LBL 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 ENGINEER
- [SDR REXA2024110101365](https://openairdocs.org/sdr/REXA2024110101365.md): Door Frame · cracked · Jun 5, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Structure
  > R/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.
- [SDR REXA2024102501010](https://openairdocs.org/sdr/REXA2024102501010.md): Housing · cracked · Jun 5, 2024 · N582CA · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > WHILE 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-A01
- [SDR REXA2024110101364](https://openairdocs.org/sdr/REXA2024110101364.md): Stringer · corroded · May 31, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 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-A01
- [SDR REXA2024110101363](https://openairdocs.org/sdr/REXA2024110101363.md): Stringer · corroded · May 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR REXA2024103001163](https://openairdocs.org/sdr/REXA2024103001163.md): Floorbeam · cracked · May 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LBL 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.
- [SDR REXA2024080600621](https://openairdocs.org/sdr/REXA2024080600621.md): Stringer · corroded · May 25, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR REXA2024070300497](https://openairdocs.org/sdr/REXA2024070300497.md): Angle · corroded · May 23, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "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 CORROSI
- [SDR REXA2024100100750](https://openairdocs.org/sdr/REXA2024100100750.md): Angle · corroded · May 21, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX 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 51-42
- [SDR REXA2024110101362](https://openairdocs.org/sdr/REXA2024110101362.md): Stringer · corroded · May 14, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STR 26R HAS CORROSION BETWEEN FS 1031 AND FS 1047. COMPLIED WITH ENDEAVOR EA CRJ953-16613 REV.IR DATED 5-7-2024.
- [SDR REXA2024052800406](https://openairdocs.org/sdr/REXA2024052800406.md): Floor Support · corroded · May 14, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PREVIOUS 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.
- [SDR REXA2024052800405](https://openairdocs.org/sdr/REXA2024052800405.md): Drag Angle · cracked · May 14, 2024 · N582CA · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB., R/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.
- [SDR REXA2024052800404](https://openairdocs.org/sdr/REXA2024052800404.md): Intercostal · corroded · May 13, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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.
- [SDR REXA2024052800403](https://openairdocs.org/sdr/REXA2024052800403.md): Drag Angle · cracked · May 13, 2024 · N582CA · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB., L/H FORWARD DRAG ANGLE IS CRACKED. REPAIRED DAMAGE I.A.W. CRJ900 SRM 55-31-00-201-001-A01.
- [SDR REXA2024052800407](https://openairdocs.org/sdr/REXA2024052800407.md): Intercostal · corroded · May 10, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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-A01
- [SDR REXA2024052200394](https://openairdocs.org/sdr/REXA2024052200394.md): Intercostal · corroded · May 10, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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 REPLAC
- [SDR REXA2024080600620](https://openairdocs.org/sdr/REXA2024080600620.md): Intercostal · corroded · May 9, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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-A01
- [SDR REXA2024052800402](https://openairdocs.org/sdr/REXA2024052800402.md): Intercostal · corroded · May 9, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 FWD CORRODED AND REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD3 IAW CRJ 900 SRM 51-42-06-001-001Ï¿½A01
- [SDR REXA2024102100899](https://openairdocs.org/sdr/REXA2024102100899.md): Door · corroded · May 7, 2024 · N582CA · Cndair CL6002D24 · Emergency Exits
  > L/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 AM
- [SDR REXA2024062400471](https://openairdocs.org/sdr/REXA2024062400471.md): Stringer Splice · corroded · Apr 30, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 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-
- [SDR REXA2024092600724](https://openairdocs.org/sdr/REXA2024092600724.md): Frame · cracked · Apr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Frame
  > RH 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 IR
- [SDR REXA2024091000687](https://openairdocs.org/sdr/REXA2024091000687.md): Former · corroded · Apr 29, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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
- [SDR REXA2024062400470](https://openairdocs.org/sdr/REXA2024062400470.md): Floor Support · corroded · Apr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 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.
- [SDR REXA2024052800401](https://openairdocs.org/sdr/REXA2024052800401.md): Frame · corroded · Apr 29, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME CORRODED AT FS 847+32 BETWEEN STRINGERS 26L AND 26R. REPAIRED DAMAGE I.A.W. CRJ 900 SRM 53-00-06-201-001-A01.
- [SDR REXA2024062400469](https://openairdocs.org/sdr/REXA2024062400469.md): Stringer · corroded · Apr 28, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER20RH @ 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 INS
- [SDR REXA2024062400468](https://openairdocs.org/sdr/REXA2024062400468.md): Stringer · corroded · Apr 26, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFT 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 STRI
- [SDR REXA2024052800400](https://openairdocs.org/sdr/REXA2024052800400.md): Intercostal · corroded · Apr 26, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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-A01
- [SDR REXA2024110101360](https://openairdocs.org/sdr/REXA2024110101360.md): Bracket · corroded · Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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-A01
- [SDR REXA2024110101359](https://openairdocs.org/sdr/REXA2024110101359.md): Stringer · corroded · Apr 21, 2024 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 26L HAS CORROSION BETWEEN FS1069-FS1088. REPAIRED DAMAGE I.A.W. CRJ900 SRM 53-00-03-201-001-A02.
- [SDR REXA2024091100707](https://openairdocs.org/sdr/REXA2024091100707.md): Door Frame · corroded · Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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 51-40-11-001-001
- [SDR REXA2024052800399](https://openairdocs.org/sdr/REXA2024052800399.md): Handle · cracked · Apr 21, 2024 · N582CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX 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.
- [SDR REXA2024103001164](https://openairdocs.org/sdr/REXA2024103001164.md): Bracket · cracked · Apr 17, 2024 · N582CA · Cndair CL6002D24 · Service Doors
  > GALLEY 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:
- [SDR REXA2024052200392](https://openairdocs.org/sdr/REXA2024052200392.md): Angle · corroded · Apr 17, 2024 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX 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 53
- [SDR REXA2020121600836](https://openairdocs.org/sdr/REXA2020121600836.md): Battery Pack · inoperative · Dec 15, 2020 · N582CA · Cndair CL6002D24 · Emergency Lighting
  > ON 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.
- [SDR REXA2020121500834](https://openairdocs.org/sdr/REXA2020121500834.md): Battery Pack · inoperative · Dec 10, 2020 · N582CA · Cndair CL6002D24 · Emergency Lighting
  > REAR 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.
- [SDR REXA2019122671775](https://openairdocs.org/sdr/REXA2019122671775.md): Hinge Fitting · corroded · Dec 17, 2019 · N582CA · Cndair CL6002D24 · Landing Gear Doors
  > CORROSION FOUND ON THE LT & RT HINGE FITTINGS AT THE NLG STRUCTURE. THE FITTINGS WERE REPLACED IAW SRM 51-42-20-001-001-A01.
- [SDR REXA2019122671767](https://openairdocs.org/sdr/REXA2019122671767.md): Plate · corroded · Dec 17, 2019 · N582CA · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION ON PLATE LOWER AT FWD BAGGAGE BAY DOOR, THE PLATE WAS REPLACED IAW AMM 52-35-07-400-802 ( CONFIG. A02) FIGURE 410.
- [SDR REXA2019122671733](https://openairdocs.org/sdr/REXA2019122671733.md): Stringer · corroded · Dec 17, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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. "
- [SDR REXA2019122611780](https://openairdocs.org/sdr/REXA2019122611780.md): Receptacle · cracked · Dec 16, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR REXA2019122651774](https://openairdocs.org/sdr/REXA2019122651774.md): Canister · cracked · Dec 15, 2019 · N582CA · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK 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.
- [SDR REXA201912651773](https://openairdocs.org/sdr/REXA201912651773.md): Canister · cracked · Dec 15, 2019 · N582CA · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACK 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 "
- [SDR REXA2019126251766](https://openairdocs.org/sdr/REXA2019126251766.md): Coaming · worn · Dec 15, 2019 · N582CA · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR 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.
- [SDR REXA2019122641778](https://openairdocs.org/sdr/REXA2019122641778.md): Doubler · corroded · Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR REXA2019122641777](https://openairdocs.org/sdr/REXA2019122641777.md): Stringer · corroded · Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR REXA2019122641768](https://openairdocs.org/sdr/REXA2019122641768.md): Floor Support · cracked · Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR REXA2019122641765](https://openairdocs.org/sdr/REXA2019122641765.md): Floorbeam · corroded · Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION 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.
- [SDR REXA2019122641763](https://openairdocs.org/sdr/REXA2019122641763.md): Intercostal · corroded · Dec 14, 2019 · N582CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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.

Next page: https://openairdocs.org/aircraft/N582CA/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 = 'N582CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N582CA/reports

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