# Service difficulty reports: N368CA

A list on [N368CA](https://openairdocs.org/aircraft/N368CA.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 · 227 reports

- [SDR REXA2026081701541](https://openairdocs.org/sdr/REXA2026081701541.md): Charger · inoperative · Aug 10, 2026 · N368CA · Cndair CL6002C10 · Emergency Lighting
  > INTERIOR EMERGENCY FLOODLIGHT IN CEILING PANEL #3 INOP.ROW 7 PUTTING EMERGENCY FLOOD LIGHT #3 ON MEL IAW MEL 33-51-1B REPAIR CATEGORY C MX PROCEDURES COMPIED WITH,MM02 UPDATED.PLACARD INSTALLED MOC# 103307. RELAMPED EMERGENCY FLOOD LIGHT #3 IAW ESPM 20-34-00
- [SDR REXA2025040700397](https://openairdocs.org/sdr/REXA2025040700397.md): Lamp · inoperative · Mar 31, 2025 · N368CA · Cndair CL6002C10 · Emergency Lighting
  > RH OVERWING EMER LT OUT RELAMPED RH OVERWING EMER LT IAW CRJ 700 AMM 33-51-15, OPS TEST GOOD, P/N OFF/ON: 8GH002473-88
- [SDR REXA2024112101505](https://openairdocs.org/sdr/REXA2024112101505.md): Floor Support · corroded · Oct 31, 2024 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON FLOOR SILL BTW FS280.00 AND 319.70 AT CABIN FLOOR STRUCTURE. FLOOR SILL BTW FS280.00 AND 319.70 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-45-201-001-A01 AND WAS REPLACED PER EA CRJ753-17650 REV A AND CRJ700S SRM 51-42-06
- [SDR REXA2024112001504](https://openairdocs.org/sdr/REXA2024112001504.md): Skin · chafed · Oct 31, 2024 · N368CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > IN REF TO: DURING INSPECTION OF THE TASK CARD 700-53-900-303 IT WAS DETECTED WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R. WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R WAS REPAIRED PER EA CRJ75
- [SDR REXA2024111401478](https://openairdocs.org/sdr/REXA2024111401478.md): Stringer · corroded · Oct 31, 2024 · N368CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AFTER FRAME REMOVAL: CORROSION ON STGR23R AT FS379.00 WAS FOUND. DUE TO EXCESSIVE DAMAGE ON STGR 23RH AT FS379 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01
- [SDR REXA2024111201468](https://openairdocs.org/sdr/REXA2024111201468.md): Web · corroded · Oct 31, 2024 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON LH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON LH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WAS
- [SDR REXA2024111101444](https://openairdocs.org/sdr/REXA2024111101444.md): Web · corroded · Oct 31, 2024 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON RH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-11-10-201-003-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WAS
- [SDR REXA2024111301474](https://openairdocs.org/sdr/REXA2024111301474.md): Floorbeam · corroded · Oct 26, 2024 · N368CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON CROSSBEAM AT FS280.00 BTW LBL45.00/RBL45.00 AT CABIN FLOOR STRUCTURE. CORROSION ON CROSSBEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01; SRM 51-42-21-001-001-A01
- [SDR REXA2021051900362](https://openairdocs.org/sdr/REXA2021051900362.md): Bracket · cracked · May 7, 2021 · N368CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 443BT SECOND MOUNTING TAB FROM AFT IS BROKEN NEEDS REPAIR. - REMOVED & REPLACED SECOND MOUNTING TAB ON PANEL 443BT IAW CRJ 700 SRM 51-42-06-001-001(A01) WVAC EMP #56399
- [SDR REXA2021050700326](https://openairdocs.org/sdr/REXA2021050700326.md): Skin · chafed · May 7, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER SKIN AND RIVETS CHAFFED AT APPROXIMATELY FS985.00 STGR 27. - REPAIRED DAMAGE IAW ENDEAVOR EA CRJ753-11451 REV IR, DATED 4/21/2021
- [SDR REXA2021051900338](https://openairdocs.org/sdr/REXA2021051900338.md): Angle · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE AND LOWER DOUBLER ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-4
- [SDR REXA2021051900337](https://openairdocs.org/sdr/REXA2021051900337.md): Crossbeam · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01. WVAC EMP #6027
- [SDR REXA2021051900336](https://openairdocs.org/sdr/REXA2021051900336.md): Crossbeam · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01.
- [SDR REXA2021051800344](https://openairdocs.org/sdr/REXA2021051800344.md): Angle · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5
- [SDR REXA2021051800343](https://openairdocs.org/sdr/REXA2021051800343.md): Angle · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5
- [SDR REXA2021050600342](https://openairdocs.org/sdr/REXA2021050600342.md): Tee Fitting · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5
- [SDR REXA2021050600341](https://openairdocs.org/sdr/REXA2021050600341.md): Crossbeam · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 5
- [SDR REXA2021051800340](https://openairdocs.org/sdr/REXA2021051800340.md): Crossbeam · corroded · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - LOCATED,DRILLED AND INSTALLED NEW SERVICEABLE FS 280 CROSSBEAM P/N CC670-34175-7 PER CRJ 700 SRM 53-11-41-201-003-A01. WVAC EMP #7322
- [SDR REXA2021051800325](https://openairdocs.org/sdr/REXA2021051800325.md): Frame · gouged · May 6, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT EQUIPMENT BAY RH SIDE FRAME AT FS 1144.00 GOUGED BELOW STGR 10R. - REPAIRED FRAME IAW ENDEAVOR EA CRJ753-11441 REV IR, DATED 5/6/2021.
- [SDR REXA2021052000358](https://openairdocs.org/sdr/REXA2021052000358.md): Angle · corroded · May 5, 2021 · N368CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID CAP ANGLE CORRODED AT STGR 17L BETWEEN FS310.00 & FS 349.00. - REMOVED & REPLACED MID CAP ANGLE, I.A.W. CRJ 700 SRM 51-41-02-001-001-A01, 51-42-06-001-001-A01.
- [SDR REXA2021051900360](https://openairdocs.org/sdr/REXA2021051900360.md): Seat Track · corroded · May 3, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT TRACK AT STR L15 AT FS 752.00 IS CORRODED AROUND FASTENER HOLES - RECEIVED, LOCATED AND INSTALLED REPLACEMENT SEAT TRACK PN SH670-37509-1 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP STAMP #789 MTC
- [SDR REXA2021051900354](https://openairdocs.org/sdr/REXA2021051900354.md): Seat Track · corroded · May 3, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT TRACK AT STR L15 AT FS 752.00 SEAT TRACK U CHANNEL IS CORRODED. - REMOVED AND REPLACED U CHANNEL IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP STAMP #711 MTC
- [SDR REXA2021050300329](https://openairdocs.org/sdr/REXA2021050300329.md): Bracket · corroded · May 3, 2021 · N368CA · Cndair CL6002C10 · Hydraulic System, Main
  > R/H MLG WHEEL WELL FWD BULKHEAD HYDRAULIC BRACKET CORRODED. - REPLACED BRACKET IAW CRJ 700 SRM 51-40-11-001-001-A01. WVAC EMP STAMP #711 MTC
- [SDR REXA2021052000353](https://openairdocs.org/sdr/REXA2021052000353.md): Seat Track · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H CABIN SIDE SEAT TRACK STR R15 AT FS 693.00 TO FS 761.55 U CHANNEL IS CORRODED LOWER EDGE. - FABRICATED R/H U CHANNEL IAW ENDEAVOR EA CRJ 753-11486 REV IR DATED 04/18/21 AND INSTALLED FABRICATED CHANNEL IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP #
- [SDR REXA2021051900361](https://openairdocs.org/sdr/REXA2021051900361.md): Attach Angle · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > RH ELECTRICAL CONNECTOR PLATE ATTACHMENT ANGLE HAS NUMEROUS OVERSIZED HOLES & CORROSION AND REQUIRES REPLACEMENT. P/N: CC670-51876-3. LOCATED @ FS 280 CROSSBEAM - LOCATED, DRILLED, INSTALLED AND TOPCOATED SERVICEABLE RH ATTACH ANGLE IAW CRJ 700 SRM 51-40-11-00
- [SDR REXA2021051900357](https://openairdocs.org/sdr/REXA2021051900357.md): Angle · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR KICKPLATE ANGLE CORRODED AT STRGR 17L BETWEEN FS310.00 AND FS 349.00 - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR KICKPLATE ANGLE P/N SH670-31875-7S IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC
- [SDR REXA2021051900356](https://openairdocs.org/sdr/REXA2021051900356.md): Seat Track · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH CABIN SIDE SEAT TRACK AT STR R15 FS 785.00 TO FS 847.00 IS CORRODED - REMOVED & REPLACED SEAT TRACK AT STR R15 FS713.00 TO FS763.00 IAW CRJ 700 AMM 53-00-49-000/400-801-A03. WVAC EMP STAMP #774 MTC
- [SDR REXA2021051900355](https://openairdocs.org/sdr/REXA2021051900355.md): Seat Track · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT TRACK AT FS 797.00 TO FS 813.00 STR L15 IS CORRODED. - SEAT TRACK WAS REMOVED AND REPLACED AS REQ IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP #161529
- [SDR REXA2021051900352](https://openairdocs.org/sdr/REXA2021051900352.md): Seat Track · corroded · Apr 23, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH CABIN SIDE SEAT RAIL AT STR R15 FS 785.00 TO FS 847.0 SEAT TRACK U CHANNEL CORRODED. - REMOVED & REPLACED U-CHANNEL IAW CRJ 700 SRM 51-41-02-001-001-A01.
- [SDR REXA2021051900359](https://openairdocs.org/sdr/REXA2021051900359.md): Stiffener · cracked · Apr 9, 2021 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FS260 WEBS (R/H & L/H) FOUND 5 VERTICAL STIFFENER ANGLES TO BE CRACKED OR HAVE DAMAGED HOLES (4 ON L/H AND 1 ON R/H SIDE.) - REMOVED,LOCATED AND DRILLED ALSO INSTALLED 5EA NEW SERVICEABLE STIFFENERS AT L/H 280 WEB 4EA AND 1EA AT RH 280 WEB, P/N
- [SDR REXA2021052000351](https://openairdocs.org/sdr/REXA2021052000351.md): Bracket · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD CARGO TIE DOWN RING SUPPORT BRACKET CORRODED AT FS533.00, STRGR 22L TO 23L - REMOVED AND REPLACED CARGO NET TIE DOWN SUPPORT BRACKET IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01
- [SDR REXA2021052000332](https://openairdocs.org/sdr/REXA2021052000332.md): Seat Track · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT LBL 9 BEGINNING AT APPROXIMATELY FS 581.00 CORRODED IN SEVERAL LOCATIONS. - RECEIVED, FABRICATED, LOCATED AND DRILLED REPLACEMENT SEAT TRACK BEGINNING AT LBL 9 FS 581 IAW CRJ 700 SRM 53-00-49-201-002-A01. THEN INSTALLED IAW CRJ 700 AM 53-00
- [SDR REXA2021052000330](https://openairdocs.org/sdr/REXA2021052000330.md): Escape Hatch · no test · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Emergency Exits
  > CREW ESCAPE HATCH FAILED FUNCTIONAL TEST OUTER HANDLE DOES NOT EJECT FROM HANDLE RECESS EVEN AFTER SOAKING IN KROIL FOR HOURS. - REMOVED & REPLACED HANDLE ASSY IAW CRJ 700 SRM 51-42-06-001-001-A01. OP CK'S GOOD. WVAC EMP STAMP #774 MTC
- [SDR REXA2021051800346](https://openairdocs.org/sdr/REXA2021051800346.md): Seat Track · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT IS CORRODED BETWEEN FS 847 TO FS 977 AT RBL 9. - REMOVED AND REPLACED DISCREPANT SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC
- [SDR REXA2021051800345](https://openairdocs.org/sdr/REXA2021051800345.md): Seat Track · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT AT LBL 9 IS CORRODED B/W FS 847 TO FS 977. - REMOVED AND REPLACED DISCREPANT SEAT TRACK B/W FS 847-TO FS 977 @ LBL9 IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC
- [SDR REXA2021040800334](https://openairdocs.org/sdr/REXA2021040800334.md): Seat Track · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT RBL 9 BEGINNING AT APPROXIMATELY FS 485.00 CORRODED IN SEVERAL LOCATIONS. - RECEIVED, FABRICATED, LOCATED AND DRILLED REPLACEMENT MATL FOR SEAT TRACK BEGINNING RBL 9 FS 485 IAW CRJ 700 SRM 53-00-49-201-002-A01. INSTALLED IAW CRJ 700 AM 53-0
- [SDR REXA2021040800331](https://openairdocs.org/sdr/REXA2021040800331.md): Seat Track · corroded · Apr 8, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT LBL27 BEGINNING AT APPROX. FS 354.00 CORRODED IN SEVERAL LOCATIONS. - FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-40-11-001-001-A01 AND AMM 53-00-49-400-801-A17. WVAC EMP #6027
- [SDR REXA2021051900349](https://openairdocs.org/sdr/REXA2021051900349.md): Intercostal · corroded · Mar 29, 2021 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 394.00 - 409.00 AND STR 27-26R HAS CORROSION. - INTERCOSTAL @ FS 394.00-409.00 & STGR 27-26R WERE REPAIRED IAW ENDEAVOR AIR EA CRJ753-11514 REV IR DATED 4-28-2021 & CRJ 753-11513 REV IR DATED 4/16/21. WVAC EMP #161529
- [SDR REXA2021051800333](https://openairdocs.org/sdr/REXA2021051800333.md): Seat Track · corroded · Mar 26, 2021 · N368CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK AT RBL9 BEGINNING AT APPROX. FS 349.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED DISCREPANT SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC
- [SDR REXA2021051900350](https://openairdocs.org/sdr/REXA2021051900350.md): Intercostal · corroded · Mar 17, 2021 · N368CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRG 21L HAS MULITPLE SPOTS OF CORROSION FROM FS 310.0 TO FS 349.00. - UPON FURTHER INVESTIGATION FOUND NO CORROSION ON INTERCOSTAL BETWEEN 310+333 REMOVED & REPLACED INTERCOSTAL BETWEEN FS 349+333 WITH SERVICEABLE IAW CRJ 700 SRM 51-42-11-001-0
- [SDR REXA2021051900348](https://openairdocs.org/sdr/REXA2021051900348.md): Stringer · corroded · Mar 16, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 19R HAS AREAS OF CORROSION FROM F.S. 280.00 TO F.S. 310.00. - REPLACED STRINGER IAW CRJ 700 SRM.
- [SDR REXA2021051900347](https://openairdocs.org/sdr/REXA2021051900347.md): Frame · corroded · Mar 16, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SECTOR AT FS 863 IS CORRODED ON FWD AND AFT SIDE BETWEEN STRG 26R - 26L. - REPAIRED FRAME SECTOR IAW ENDEAVOR AIR EA CRJ753-11438 IR DATED 4/29/2021.
- [SDR REXA2021051800339](https://openairdocs.org/sdr/REXA2021051800339.md): Bulkhead Web · corroded · Mar 16, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > L/H FS 280 BULKHEAD WEB IS CORRODED. - L/H FS 280 BULKHEAD WEB WAS REPAIRED IAW CRJ 700 SRM 53-11-10-201-004-A01. WVAC EMP #161529
- [SDR REXA2021051800335](https://openairdocs.org/sdr/REXA2021051800335.md): Filler · corroded · Mar 16, 2021 · N368CA · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 295 CROSSBEAM FILLER AT LBL 9 IS CORRODED. - REMOVED & REPLACED FILLER FOR CROSSBEAM AT FS295 LBL9 IAW SRM 51-42-06-001-001-A01. WVAC EMP #6027
- [SDR REXA2021051900327](https://openairdocs.org/sdr/REXA2021051900327.md): Bracket · corroded · Mar 8, 2021 · N368CA · Cndair CL6002C10 · Wing Main, Frame Structure
  > L/H WHEEL WELL AT FWD BULKHEAD HYDRAULIC CONNECTION BRACKET IS CORRODED. - REMOVED L/H FWD BULKHEAD HYD CONNECTION BRACKET REMOVED CORROSION FOUND IN ALLOWABLE LIMITS TREATED AND INSTALL SAME SERVICEABLE BRACKET IAW CRJ 700 SRM 51-40-11-001-001-A01. LEAK CK GO
- [SDR REXA2021030800328](https://openairdocs.org/sdr/REXA2021030800328.md): Bracket · corroded · Mar 8, 2021 · N368CA · Cndair CL6002C10 · Wing System Wiring
  > L/H WHEEL WELL AT FWD BULKHEAD ELECTRICAL CONNECTION BRACKET IS CORRODED. - REMOVED AND REPLACED BRACKET IAW CRJ 700 SRM 51-41-02-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND AMM 20-22-00-910-801-A01. WVAC EMP STAMP #711 MT
- [SDR N6WA20191016001](https://openairdocs.org/sdr/N6WA20191016001.md): Light · out of position · Oct 10, 2019 · N368CA · Cndair CL6002C10 · Emergency Lighting
  > EME. EXIT LIGHT NEAR L/H EME. EXIT DOOR IS OUT OF PLACE. RESECURED EXIT LIGHT IAW CRJ 700 AMM 35-51-05 PERFORM OPS CHECK IAW CRJ 700 AMM 33-50-00
- [SDR V0XD20181127010](https://openairdocs.org/sdr/V0XD20181127010.md): Bracket · corroded · Nov 26, 2018 · N368CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR BRACKET HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET (P/N:601R38921-9) IAW CRJ700 SRM 51-42-06.
- [SDR V0XD20181127009](https://openairdocs.org/sdr/V0XD20181127009.md): Bracket · corroded · Nov 26, 2018 · N368CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR BRACKET HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET (P/N:601R318084-1) IAW CRJ700 SRM 51-42-06.
- [SDR V0XD20181127008](https://openairdocs.org/sdr/V0XD20181127008.md): Angle · corroded · Nov 26, 2018 · N368CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N:601R317726-3) IAW CRJ700 SRM 51-42-06.

Next page: https://openairdocs.org/aircraft/N368CA/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 = 'N368CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N368CA/reports

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