# Service difficulty reports: N367CA

A list on [N367CA](https://openairdocs.org/aircraft/N367CA.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 5 · 240 reports

- [SDR REXA202601997](https://openairdocs.org/sdr/REXA202601997.md): Lamp · inoperative · Oct 22, 2026 · N367CA · Cndair CL6002C10 · Emergency Lighting
  > 3 EMERGENCY FLOODLIGHT LAMPS INOP. R+R 3 EMERGENCY FLOODLIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.
- [SDR REXA2026052000602](https://openairdocs.org/sdr/REXA2026052000602.md): Lamp · inoperative · May 19, 2026 · N367CA · Cndair CL6002C10 · Emergency Lighting
  > REAR MOST OVERHEAD EMERGENCY LIGHT INOP R/R BULB IAW AMM 33-51-09, OPS TEST GOOD. P/N OFF/ON: 1317
- [SDR REXA2026041500285](https://openairdocs.org/sdr/REXA2026041500285.md): Bulb · inoperative · Apr 10, 2026 · N367CA · Cndair CL6002C10 · Emergency Lighting
  > FA STATED. MID CEILING INDICATOR LIGHTS ARE NOT WORKING. R & R BULBS IN CEILING EXIT SIGN IAW CRJ AMM 33-51-09 OPS TEST GOOD.
- [SDR REXA2025091600868](https://openairdocs.org/sdr/REXA2025091600868.md): Sensor · faulted · Sep 10, 2025 · N367CA · Cndair CL6002C10 · Landing Gear Brake System
  > DURING CLIMB OUT AT AROUND 8000+ BRAKE OVHT WARNING MSG DISPLAYED FOR THE IB L SIDE BRAKES. FOLLOWED THE QRH. MSG WENT AWAY MOC NOTIFIED DEFERD LH IB BRAKE TEMP. INDACATION. MEL 32-46-1D CAT C MX PROCEDURES C/W. MOC NOTIFIED. 7821 PLACARD. R & R BREAK TEMP S
- [SDR REXA2025020500136](https://openairdocs.org/sdr/REXA2025020500136.md): Hinge · corroded · Nov 24, 2024 · N367CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFT LAV SERVICE POINT DOOR HINGES AND HINGE FITTINGS HAVE CORROSION AFT LAV SERVICE POINT DOOR HINGES AND HINGE FITTINGS WERE REPLACED PER CRJ-700 AMM 52-45-01 (CONFIG A01), SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01
- [SDR REXA2025020500135](https://openairdocs.org/sdr/REXA2025020500135.md): Skin · cracked · Nov 24, 2024 · N367CA · Cndair CL6002C10 · Wing, Plate/Skin
  > CRACK ON SLOT OF TRACK 2 OF SLAT 1 AT FIXED LEADING EDGE LH WING CRACK ON SLOT OF TRACK 2 OF SLAT 1 AT FIXED LEADING EDGE LH WING
- [SDR REXA2025020500134](https://openairdocs.org/sdr/REXA2025020500134.md): Support Plate · corroded · Nov 24, 2024 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45. DUE TO EXCESSIVE DAMAGE RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA, RBL 45/LBL 45 WERE REPLACED PER CRJ 70
- [SDR REXA2025020500133](https://openairdocs.org/sdr/REXA2025020500133.md): Bracket · cracked · Nov 24, 2024 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON FITTING OF PAD FWD UPPER AT FS310.00 PASSENGER DOOR SURROUND STRUCTURE (L1). FITTING OF PAD FWD UPPER AT FS310.00 PASSENGER DOOR SURROUND STRUCTURE (L1) WAS REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01
- [SDR REXA2021050500322](https://openairdocs.org/sdr/REXA2021050500322.md): Floor Support · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500321](https://openairdocs.org/sdr/REXA2021050500321.md): Fitting · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500320](https://openairdocs.org/sdr/REXA2021050500320.md): Fitting · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500319](https://openairdocs.org/sdr/REXA2021050500319.md): Fitting · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500318](https://openairdocs.org/sdr/REXA2021050500318.md): Fitting · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500317](https://openairdocs.org/sdr/REXA2021050500317.md): Floor Support · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500316](https://openairdocs.org/sdr/REXA2021050500316.md): Floor Support · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE.- REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500315](https://openairdocs.org/sdr/REXA2021050500315.md): Floor Support · corroded · Apr 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE AREAS OF CORROSION ON PAX DOOR FLOOR SUPPORT ANGLE. - REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT AFT CAP ANGLE, FWD CAP ANGLE, MID CAP ANGLE, AFT CLOSING FITTING, FWD CLOSING FITTING, AFT HANDRAIL FITTING, FWD HANDRAIL FITTING AND KICKPLATE ANGLE IAW
- [SDR REXA2021050500314](https://openairdocs.org/sdr/REXA2021050500314.md): Intercostal · corroded · Apr 29, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR INTERCOSTAL AT STGR 19R IS CORRODED FROM FS 310 TO FS 349 - REMOVED AND REPLACED INTERCOSTAL P/N SH670-32047-1, FS 310 - FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND INTERCOSTAL P/N SH670-32004-1, FS 319 - FS 349 IAW CRJ 700 SRM 51-40-11-001-00
- [SDR REXA2021050500313](https://openairdocs.org/sdr/REXA2021050500313.md): Intercostal · corroded · Apr 29, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR INTERCOSTAL AT STGR 19R IS CORRODED FROM FS 310 TO FS 349 - REMOVED AND REPLACED INTERCOSTAL P/N SH670-32047-1, FS 310 - FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND INTERCOSTAL P/N SH670-32004-1, FS 319 - FS 349 IAW CRJ 700 SRM 51-40-11-001-00
- [SDR REXA2021050500312](https://openairdocs.org/sdr/REXA2021050500312.md): Floor Support · corroded · Apr 12, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOORBEAM AT RBL 9 FS 581 TO 677 HAS CORROSION ON TOP OF BEAM. - COMPLIED WITH MHIRJ REO #670-53-41-514 REV-- DATED 2021-04-09 FOR REPAIR TO FLOORBEAM @ RBL9 FS 581-FS 677. WVAC EMP STAMP #738 MTC
- [SDR REXA2021050700311](https://openairdocs.org/sdr/REXA2021050700311.md): Floor Support · corroded · Apr 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TOP OF FLOORBEAM AT FS 485.00 TO FS 581.00 LBL 9 IS CORRODED IN MULTIPLE LOCATIONS. - REMOVED CORRODED FLOOR BEAM FROM F.S.485 TO F.S.581, LBL9 AND INSTALLED NEW SERVICABLE FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01.
- [SDR REXA2021050500299](https://openairdocs.org/sdr/REXA2021050500299.md): Seat Track · corroded · Apr 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED & REPLACED SEAT TRACK AT RBL 9 FS 581 PN SH670-33425-3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17-A03.WVAC EMP STAMP #712 MTC
- [SDR REXA2021050500199](https://openairdocs.org/sdr/REXA2021050500199.md): Seat Track · corroded · Apr 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED & REPLACED SEAT TRACK AT RBL 9 FS 485 TO FS 581 PN SH670-33426-1 IAW CRJ 700 AMM 53-00-49-000/400-801-A17-A03. WVAC EMP STAMP #712 MTC
- [SDR REXA2021050500147](https://openairdocs.org/sdr/REXA2021050500147.md): Seat Track · corroded · Mar 31, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING AT APPROX FS 785 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED TRACK IAW CRJ 700 AMM 53-00-49-400-801(A17) WVAC EMP STAMP #711 MTC
- [SDR REXA2021050500148](https://openairdocs.org/sdr/REXA2021050500148.md): Seat Track · corroded · Mar 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK SHORT SEGMENT AND ADJACENT TRACK BEGINNING AT APPROX FS 847.00 CORRODED IN SEVERAL LOCATIONS. - REPLACED TRACK AT FSS 866-969 LH SIDE RAIL IAW CRJ 700 AMM 53-00-49-400-801-A17. CLEANED TRACK AT 847-866 IAW CRJ 700 AMM 51-26-00-120-801-A01. N
- [SDR REXA2021050400135](https://openairdocs.org/sdr/REXA2021050400135.md): Crossbeam · corroded · Mar 30, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H & R/H FS 280 BEAMS ARE CORRODED. - REMOVED AND REPLACED FS 280 L/H AND R/H CROSS BEAMS PT#CC 670-34175-7 AND ""J"" ANGLE PT #CC670-33292-13 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. REMOVED A
- [SDR REXA2021050500150](https://openairdocs.org/sdr/REXA2021050500150.md): Stringer · corroded · Mar 28, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 19L IS CORRODED BETWEEN FS 333 TO FS 349. - REPAIRED STR 19L BETWEEN FS 333 AND 349 IAW ENDEAVOR AIR EA# CRJ 753-11283 DATED 3/2/21. WVAC EMP STAMP #703 MTC
- [SDR REXA2021050400138](https://openairdocs.org/sdr/REXA2021050400138.md): Seat Track · corroded · Mar 24, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BEGINNING AT APPROX FS 830.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED NEW SEAT TRACK PT #SH670-37411-3 AT FS 830.00 TO FS 696+8 RBL9 IAW CRJ 700 AMM 53-00-49-400-801-A17. FIXED 3 EACH SCREWS THAT WERE NOT FULLY ENGAGED AND ATTACHED TECH
- [SDR REXA2021050500310](https://openairdocs.org/sdr/REXA2021050500310.md): Seat Track · corroded · Mar 18, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK BEGINNING AT APPROX. FS 785.00 CORRODED IN SEVERAL LOCATIONS. - LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK RH SIDE FS 785.00 IAW CRJ 700 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01, REO 670-53-00-343 REV-N DATED 2019-07-16 AND CRJ 700
- [SDR REXA2021050400128](https://openairdocs.org/sdr/REXA2021050400128.md): Bulkhead Web · corroded · Mar 18, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > L/H FS 280 WEB IS CORRODED. - REMOVED FABRICATED, LOCATED, DRILLED AND INSTALLED FS280 LOWER WEB AN SPLICE ON LH BULKHEAD IAW CRJ 700 SRM 53-11-10-201-004-A01. 908.1 AND 303.6 ACCEPTABLE AS IS THIS IS NOT A PRESSURE BULKHEAD.
- [SDR REXA2021050500192](https://openairdocs.org/sdr/REXA2021050500192.md): Angle · corroded · Mar 13, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FS 280 L/H LOWER WEB FOUND STIFFENER ANGLE AT LBL 17.46 TO BE DAMAGED. - REMOVED,LOCATED, AND DRILLED AND INSTALLED NEW SERVICEABLE STIFFENER ANGLE AT LBL 17.46 P/N:CC670-34151-5 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA202105040128](https://openairdocs.org/sdr/REXA202105040128.md): Plate · corroded · Mar 13, 2021 · N367CA · Cndair CL6002C10 · Emergency Exits
  > R/H WING EMERGENCY EXIT STEP PLATE CORRODED. - REMOVED & REPLACED RH OVERWING STEP PLATE IAW CRJ 700 SRM 51-42-02-001-001-A01.
- [SDR REXA2021050500194](https://openairdocs.org/sdr/REXA2021050500194.md): Floorbeam · cracked · Mar 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > DURING REPAIR OF R/H FLIGHT DECK DOOR POST, FOUND R/H FLIGHT DECK FLOOR BEAM ANGLE CRACKED. - REMOVED, LOCATED,DRILLED,AND INSTALLED RH FLOOR BEAM (FLIGHT DECK) ANGLE AND GUSSET P/N:CC670-33199-3,CC670-33467-2 IAW CRJ 700 SRM 57-42-06-001-001-A01,51-40-11-001-
- [SDR REXA2021050400140](https://openairdocs.org/sdr/REXA2021050400140.md): Seat Track · corroded · Mar 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 BEGINNING AT APPROX FS 830.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED/INSTALLED SEAT TRACK AT LBL 9 FS 830+8 TO 985+3 IAW CRJ 700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP #712 MTC
- [SDR REXA202105040130](https://openairdocs.org/sdr/REXA202105040130.md): Intercostal · damaged · Mar 11, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 2 INTERCOSTALS BETWEEN FS 265-FS 280 BETWEEN LBL 18 TO LBL 27 UNDER FLIGHT COMPARTMENT FLOOR AFT HOLES ARE DAMAGED. - REPAIRED LBL 38.50 INTERCOSTAL IAW ENDEAVOR AIR ENDEAVOR AIR EA CRJ 753-11254. INSTALLED NEW SERVICEABLE FASTENER ON AFT HOLE OF LBL 27 IAW CR
- [SDR REXA2021050500144](https://openairdocs.org/sdr/REXA2021050500144.md): Seat Track · corroded · Mar 10, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17, SEAT TRACK P/N: SH670-32234-3. WVAC EMP STAMP #738 MTC
- [SDR REXA2021050400137](https://openairdocs.org/sdr/REXA2021050400137.md): Seat Track · corroded · Mar 10, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 27 BEGINNING AT APPROX FS 349.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17. FABBED PER REO 670-53-00-343 REV N DATED 2019-07-16. WVAC EMP STAMP #711 MTC
- [SDR REXA2021031000127](https://openairdocs.org/sdr/REXA2021031000127.md): Seat Track · corroded · Mar 10, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BEGINNING AT APPROX AT RBL 9 BEGINNING AT APPROX AT RBL 9 BEGINNING AT APPROX FS 677.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17.
- [SDR REXA2021050500193](https://openairdocs.org/sdr/REXA2021050500193.md): Floorbeam · cracked · Mar 6, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > DURING REPAIR OF L/H FLIGHT DECK DOOR POST, FOUND L/H FLIGHT DECK FLOOR BEAM ANGLE CRACKED. - REMOVED LH FLIGHT DECK FLOORBEAM ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE ANGLE PN CC670-33199-48 IAW CRJ 700 SRM 51-40-11-001-
- [SDR REXA2021050700309](https://openairdocs.org/sdr/REXA2021050700309.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING @ APPROX FS708 CORRODED IN SEVERAL AREAS - REMOVED AND REPLACED SEAT TRACK IAW CRJ 700 AMM 53-00-49-000/400-801-A03.
- [SDR REXA2021050700308](https://openairdocs.org/sdr/REXA2021050700308.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK BEGINNING AT APPROX FS 969.00 CORRODED. - INSTALLED RH SEAT TRACK BEGINING APPROX FS 969.00 IAW CRJ 700 AMM 53-00-49-400-801(A17.) WVAC EMP STAMP #712 MTC
- [SDR REXA2021050700304](https://openairdocs.org/sdr/REXA2021050700304.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING AT F.S. 579.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK FROM FS 379 TO FS 485 IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP# 780 MTC
- [SDR REXA2021050700301](https://openairdocs.org/sdr/REXA2021050700301.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK BEGINNING AT APPROX FS 485.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED NEW SEAT RH RAIL @ FS 483-573 R/H IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89523
- [SDR REXA202100304](https://openairdocs.org/sdr/REXA202100304.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING AT F.S. 579.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED L/H SIDE SEAT TRACK FROM FS 379 TO FS 485 IAW CRJ 700 AMM 53-00-49-400-801-A03.
- [SDR REXA2021050500302](https://openairdocs.org/sdr/REXA2021050500302.md): Seat Track · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK BEGINNING AT APPROX FS 581.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED R/H SIDE SEAT TRACK BEGINNING AT APPROX. FS 581.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801(A17). WVAC EMP #460661
- [SDR REXA2021030500125](https://openairdocs.org/sdr/REXA2021030500125.md): Angle · corroded · Mar 5, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SILL CLIP AT RBL 42 FS 319.70 IS CORRODED. - REMOVED AND REPLACED CORRODED FLOOR SILL ANGLE AT RBL 42 FS 319.70 WITH NEW SERVICEABLE ANGLE PN SH670-32177-1 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP #835
- [SDR REXA2021031800122](https://openairdocs.org/sdr/REXA2021031800122.md): Nut Plate · corroded · Mar 3, 2021 · N367CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > NUTPLATE ASSY FORWARD SIDE OF FS 364 STR 27 CORRODED. - REPLACED CORRODED NUTPLATE ASSY IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DRAWING #SH670-32456, 2024 T3 0.032". WVAC EMP #460661
- [SDR REXA2021050500196](https://openairdocs.org/sdr/REXA2021050500196.md): Bracket · dented · Mar 2, 2021 · N367CA · Cndair CL6002C10 · Ailerons
  > R/H AILERON CENTER SUPPORT FAIRING BRACKET DENTED/BENT. - INSTALLED NEW RIB P/N: CC620-13022-2 ON R/H AILERON IAW CRJ 700 SRM 51-42-001-001-A01 REV.38 DATED JUL 25/2020. WVAC EMP #460661
- [SDR REXA2021050500146](https://openairdocs.org/sdr/REXA2021050500146.md): Seat Track · corroded · Mar 2, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK BEGINNING AT APPROX. FS 708.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED SIDEWALL SEAT RAIL @ FS 708.0-763.0 RH STR 15 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89351
- [SDR REXA2021030200126](https://openairdocs.org/sdr/REXA2021030200126.md): Floor Support · corroded · Mar 2, 2021 · N367CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SILL PLATE AT RBL 42 IS CORRODED BETWEEN FS 310.00 AND FS 319.70 - REMOVED, LOCATED, DRILLED AND INSTALLED FLOOR SILL AT RBL 42 FS 280 - FS 319.70 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01,51-42-21-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR REXA2021050500145](https://openairdocs.org/sdr/REXA2021050500145.md): Seat Track · corroded · Mar 1, 2021 · N367CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BEGINNING AT APPROX FS 677.00 CORRODED IN SEVERAL LOCATIONS. - INSTALLED SIDE WALL SEAT RAIL AT STR 15L FS 677 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP #89351

Next page: https://openairdocs.org/aircraft/N367CA/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 = 'N367CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N367CA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
