# Service difficulty reports: N668CA A list on [N668CA](https://openairdocs.org/aircraft/N668CA.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 · 239 reports - [SDR REXA2026082101545](https://openairdocs.org/sdr/REXA2026082101545.md): Lamp · inoperative · Aug 20, 2026 · N668CA · Cndair CL6002C10 · Emergency Lighting > ONE LAMP IN ENTRANCE EMERGENCY EXIT SIGN AND 1 LAMP IN LEFT OVERWING EMERGENCY EXIT FLOOD LAMP INOP. R & R TWO EMERGENCY EXIT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD. - [SDR REXA2025072900763](https://openairdocs.org/sdr/REXA2025072900763.md): Lamp · inoperative · Jul 26, 2025 · N668CA · Cndair CL6002C10 · Emergency Lighting > CEILING EMERGENCY FLOOD LIGHT FOUND INOP REMOVED AND REPLACED CEILING EMERGENCY FLOOD LIGHT BULB IAW CRJ 700 AMM 33-51-09. OPS CHECK GOOD. - [SDR REXA2024123001616](https://openairdocs.org/sdr/REXA2024123001616.md): Frame · corroded · Dec 28, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > FRAME FS863 BETWEEN STRINGER 27 AND 26R IS CORRODED. REPAIRED FRAME F.S.863 IAW ENDEAVOR AIR EA CRJ753-17338 REV IR DATED 10/9/2024 - [SDR REXA2024111901502](https://openairdocs.org/sdr/REXA2024111901502.md): Angle · corroded · Nov 12, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FOUND JOINT ANGLE AT FS333.00 & STR 21L TO BE CORRODED. REMOVED CORROSION FOR FS 333.00 JOINT ANGLE @ STR 21L IAW CRJ 700 SRM 51-21-06-001-001-A01. UPON FURTHER INVESTIGATION FOUND NO ALLOWED DAMAGE IN THIS AREA & 20% MATERIAL LOST ON JOINT ANGLE, REQUIRE RE - [SDR REXA2024102901090](https://openairdocs.org/sdr/REXA2024102901090.md): Repair · none · Oct 28, 2024 · N668CA · Cndair CL6002C10 · Standard Practices/Structures > PER ENDEAVOR, REMOVE FS 409-426, S14R-17R, EXISTING REPAIR DOUBLER & SHIMS, NDT SKIN FASTENER HOLES AND CUT-OUTS TO ENSURE THERE ARE NO CRACKS. FABRICATE NEW SHIMS & DOUBLER AND INSTALL IAW SRM OR SUBMIT TO ENGINEERING IF REQUIRED. REMOVED PREVIOUS REPAIR DOU - [SDR REXA2024102100898](https://openairdocs.org/sdr/REXA2024102100898.md): Stringer Splice · corroded · Oct 15, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > "SPLICE AT FS333 & STR24R IS CORRODED REMOVED CORROSION ON FS 333.00 SPLICE P/N SH670-32429-4 AT STR 24R IAW CRJ 700 SRM 51-21-06-001-001-A01. MATERIAL REMOVED 0.035"", NOMINAL THICKNESS OF 0.063"". BLENDS ARE BEYOND THE ALLOWABLE DAMAGE LIMITS AS PER CRJ700 S - [SDR REXA2024101400869](https://openairdocs.org/sdr/REXA2024101400869.md): Angle · cracked · Oct 10, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > UPON REMOVAL FOUND FS 364 FACTORY SPLICE (P/N: SH670-32460-1) TO BE CRACKED AND REQUIRES REPLACEMENT. LOCATED AND DRILLED SERVICEABLE FS 364.00 @ STGR 20L IB FACTORY SPLICE (P/N: SH670-32460-1) IAW CRJ 700 SRM 51-40-11-001-001-A01.REF. BARCODE IDENTIFIER HN001 - [SDR REXA2024102200868](https://openairdocs.org/sdr/REXA2024102200868.md): Splice · corroded · Oct 5, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > "CORROSION ON JOINT SPLICE (PN SH670-32429-3) FROM STR 26L AND FS 333. REMOVED CORROSION ON FS 333.00 JOINT PIECE P/N SH670-32429-3 AT STR 26L PER CRJ 700 SRM 51-21-06-001-001-A01. REMOVED.029"" MATERIAL FROM A NOMINAL THICKNESS OF.063"". BLENDS ARE BEYOND T - [SDR REXA2024100300767](https://openairdocs.org/sdr/REXA2024100300767.md): Stringer Splice · corroded · Oct 2, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 26R SPLICE IS CORRODED AT F.S. 333 ON THE FWD SIDE. REMOVED STGR 26R JOINT SPLICE AT FS 333 IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED STGR 26R JOINT SPLICE AT FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 - [SDR REXA2024100300766](https://openairdocs.org/sdr/REXA2024100300766.md): Stringer · corroded · Oct 2, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 19R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. REMOVED STGR 19R (P\N SH670-31632-1) BETWEEN F.S. 280 TO F.S. 319 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 19R P/N SH670-31632-1 IAW CRJ-700 SRM 51-42-06-0 - [SDR REXA2024100100749](https://openairdocs.org/sdr/REXA2024100100749.md): Stringer · corroded · Sep 30, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STRINGER 25R AT FS280 IS CORRODED. REMOVED STR 25R P/N SH670-31212-2 FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 25R, P/N SH670-31212-2, FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-06-0 - [SDR REXA2024100100748](https://openairdocs.org/sdr/REXA2024100100748.md): Stringer · corroded · Sep 29, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER 21R AT FS280 IS CORRODED. REMOVED STR 21R FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. INSTALLED NEW STR 21R (PN SH670-31636-1) FROM FS 280 TO FS 333 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-00 - [SDR REXA2024093000732](https://openairdocs.org/sdr/REXA2024093000732.md): Intercostal · corroded · Sep 28, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26R. REMOVED CORROSION ON INTERCOSTAL BETWEEN STGR 27 AND STGR 26R AND BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO BEING IN A NO DAMAGE - [SDR REXA2024093000731](https://openairdocs.org/sdr/REXA2024093000731.md): Door Sill · corroded · Sep 28, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > "AFT CARGO DOOR SILL PLATE F.S. 1000-1051 LBL 34 CORRODED INCLUDING NUT PLATES AND HOLES BLENDED CORROSION ON AFT CARGO LOWER DOOR SILL PLATE PN MM670-35655-001 IAW CRJ 700 SRM 53-61-23-201-001-A01, AND 51-12-00-001-001-A01. MEASURED BLEND AREA MATERIAL REMOV - [SDR REXA2024110801442](https://openairdocs.org/sdr/REXA2024110801442.md): Intercostal · corroded · Sep 20, 2024 · N668CA · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR MID DD3 FOUND TO BE CORRODED REMOVED PAX DOOR MID INTERCOSTAL DD3 IAW CRJ700 SRM 51-42-006-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR MID DD3 INTERCOSTAL P/N:601R318056-1 IAW CRJ700 SRM 51-40-11-001-001-A01INSTA - [SDR REXA2024110801441](https://openairdocs.org/sdr/REXA2024110801441.md): Intercostal · corroded · Sep 20, 2024 · N668CA · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL MID DD2 FOUND CORRODED REMOVED PAX DOOR INTERCOSTAL MID DD2 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR INTERCOSTAL MID DD2 P/N:601R318053-3 IAW CRJ700 SRM 51-40-11-001-001-A01 - [SDR REXA2024093000740](https://openairdocs.org/sdr/REXA2024093000740.md): Stringer Splice · corroded · Sep 20, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > UPON EVAL DETERMINED THAT CIRCUMFERENTIAL JOINT AT FS333, STR 21R REQUIRES REPLACEMENT DUE TO CORROSION. PON FURTHER INVESTIGATION, IT WAS FOUND THAT THE STRINGER JOINT SPLICE AT STR 21R AT FS 333 IS WHAT REQUIRES REPLACEMENT DUE TO CORROSION IAW CRJ700 SRM 5 - [SDR REXA2024110701438](https://openairdocs.org/sdr/REXA2024110701438.md): Former · damaged · Sep 17, 2024 · N668CA · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR AFT FORMER REQUIRES REPLACEMENT DUE TO PREVIOUS REPAIR REMOVED PAX DOOR AFT FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND THEN INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 - [SDR REXA2024100100751](https://openairdocs.org/sdr/REXA2024100100751.md): Intercostal · corroded · Sep 17, 2024 · N668CA · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR AFT INTERCOSTAL DD5 FOUND CORRODED REQUIRES REPLACEMENT REMOVED PAX DOOR AFT INTERCOSTAL DD5 IAW CRJ700 SRM 51-42-06-001-001-A01. THEN LOCATED DRILLED AND INSTALLED NEW SERVICEABLE AFT INTERCOSTAL DD5 P/N: 601R31902-317A IAW CRJ700 SRM 51-40-11-001-0 - [SDR REXA2025011000034](https://openairdocs.org/sdr/REXA2025011000034.md): Support · corroded · Sep 10, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR HAS 4EA FLOOR PROTECTOR SUPPORTS AND 4EA ANGLES WITH CORROSION. REMOVED AND REPLACED FWD WEB FLOOR PROTECTOR AND 2 EA AFT WEB FLOOR PROTECTOR IAW CRJ700 SRM 51-41-02-001-001-A01. - [SDR REXA2024123101625](https://openairdocs.org/sdr/REXA2024123101625.md): Striker · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Service Doors > AFT SIDE OF THE SERVICE DOOR SEAL STRIKER IS CORRODED AT THE BOTTOM OF THE DOOR ENTRY WAY. REMOVED CORRODED SEAL STRIKER AND INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER SEAL STRIKE P/N:SH670-31412-7. IAW CRJ700 SRM 51-42-06-001-001-A01. - [SDR REXA2024121101574](https://openairdocs.org/sdr/REXA2024121101574.md): Frame Splice · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > STR 25R CIRCUMFERENTIAL JOINT AT FS333 REQUIRES REPLACEMENT DUE TO CORROSION LOCATED AND DRILLED STR 25R CIRCUMFERENTIAL JOINT AT FS333 IAW CRJ 700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE PART, P/N SH670-32429-4S. REFERENCE HN00184967, TASK 6A, FOR THE INS - [SDR REXA2024121101573](https://openairdocs.org/sdr/REXA2024121101573.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 19L IS CORRODED BETWEEN F.S. 349 TO F.S. 394. REPAIRED IAW CRJ700 SRM 53-00-03-201-201-001-A01. - [SDR REXA2024112601514](https://openairdocs.org/sdr/REXA2024112601514.md): Frame · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > F.S. 295 FRAME IS CORRODED BETWEEN STGR 19L TO STGR 20L LOCATED AND DRILLED NEW SERVICEABLE SUB FRAME P/N SH670-31941-3 AT FS295 BETWEEN STR18L AND 20L IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE SUB FRAME P/N SH670-31941-3 AT FS 295 BETW - [SDR REXA2024111901501](https://openairdocs.org/sdr/REXA2024111901501.md): Cup · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FWD AND AFT HANDRAIL CUPS ARE CORRODED. UPON FURTHER INVESTIGATION PAX DOOR FWD HANDRAIL CUPS P/N SH670-31840-3 HAS SEVERE CORROSION BEYOND OUT OF LIMITS IAW CRJ 700 SRM 53-00-00-101-001-A01. REMOVED PAX DOOR FWD HANDRAIL CUPS P/N SH670-31840-3 IAW C - [SDR REXA2024111101458](https://openairdocs.org/sdr/REXA2024111101458.md): Frame · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > F.S. 295 FRAME IS CORRODED BETWEEN STGR 19L TO STGR 20L. REPLACED FRAME PER SRM. - [SDR REXA2024103001191](https://openairdocs.org/sdr/REXA2024103001191.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 19L IS CORRODED BETWEEN F.S. 280 TO F.S. 295. INSTALLED NEW SERVICEABLE STGR 19L (PN: SH670-31207-1) - [SDR REXA2024102200913](https://openairdocs.org/sdr/REXA2024102200913.md): Skin · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin > FUSELAGE SKIN IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND BETWEEN STGR 26R TO STGR 25R. REPAIRED IAW ENDEAVOR AIR EA CRJ753-17310, DATE: 9/16/2024, REV IR. - [SDR REXA2024102200912](https://openairdocs.org/sdr/REXA2024102200912.md): Frame · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > F.S. 364 FRAME IS CORRODED ON THE FWD AND AFT SIDE BETWEEN STGR 19L TO STGR 20L. NEW SEGMENT OF FRAME P/N:SH670-31158-3 WAS INSTALLED IAW CRJ700 SRM TASK 51-42-06-001-001-A01. - [SDR REXA2024102100897](https://openairdocs.org/sdr/REXA2024102100897.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 24R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. EVALUATE CORROSION ON STR 24R FROM FS 280 TO FS 310 UPON FURTHER INVESTIGATION STR 24R FROM FS 280 TO FS 333 HAS DEEP CORROSION ON ATTACHED FLANGE STR 24R THERE IS NO DAMAGE ALLOWED IAW CRJ700 SRM 53-21-03-101 - [SDR REXA2024102100896](https://openairdocs.org/sdr/REXA2024102100896.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 22R IS CORRODED BETWEEN F.S. 333 TO F.S. 349. INSTALLED NEW SERVICEABLE P/N: SH670-31379-1 AT STR22R BETWEEN FS333 AND FS349 IAW CRJ700 SRM 51-42-06-001-001-A01. - [SDR REXA2024102100895](https://openairdocs.org/sdr/REXA2024102100895.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 21R IS CORRODED BETWEEN F.S. 319 TO F.S. 364. UPON INVESTIGATION FOUND STR 21R FROM FS 333 TO FS 379 (P/N SH 670-31383-1) FREE AND ATTACHED FLANGE TO BE HEAVILY CORRODED BETWEEN FS364.00 TO FS379.00 AND BEYOND THE ALLOWABLE DAMAGE LIMITS OF CRJ700 SRM 53- - [SDR REXA2024102100893](https://openairdocs.org/sdr/REXA2024102100893.md): Splice · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STR 25R CIRCUMFERENTIAL JOINT AT FS333 REQUIRES REPLACEMENT DUE TO CORROSION LOCATED AND DRILLED STR 25R CIRCUMFERENTIAL JOINT AT FS333 IAW CRJ 700 SRM 51-40-11-001-001-A01. NEW SERVICEABLE PART, P/N SH670-32429-4S. REFERENCE HN00184967, TASK 6A, FOR THE INS - [SDR REXA2024102100891](https://openairdocs.org/sdr/REXA2024102100891.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 20L IS CORRODED BETWEEN F.S. 379 TO F.S. 394. EVALUATED S20L FOUND 50% MATERIAL LOSS AND NO DAMAGE ALLOWED IN AREA FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01. REMOVED AND REPLACE STGR 20L SH670-31405-1 AT F.S. 349 - F.S. 477 BY FABRICA - [SDR REXA2024101600880](https://openairdocs.org/sdr/REXA2024101600880.md): Intercostal · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AVI DOOR FWD INTERCOSTAL IS CORRODED AT STGR 26R. INSTALLED NEW SERVICEABLE INTERCOSTAL(DIAPHRAGM) IAW CRJ-700 SRM 51-42-06-001-001-A01. - [SDR REXA2024101500876](https://openairdocs.org/sdr/REXA2024101500876.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER 26L CORRODED ON UPPER SURFACE OF ATTACHED FLANGE BETWEEN FS333.00 AND FS349.00. REPAIRED IAW ENDEAVOR AIR EA NO. CRJ753-17445 ISSUE DATE: 10/2/2024 REV. IR. - [SDR REXA2024101000867](https://openairdocs.org/sdr/REXA2024101000867.md): Frame · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > "F.S. 333 IS CORRODED BETWEEN STGR 25L TO STGR 27. REMOVED CORROSION ON FS 333 BETWEEN STGR 25L-27 IAW CRJ 700 SRM 51-21-06-001-001-A01. MINIMUM REMAINING THICKNESS AT ALL BLEND LOCATIONS TO FS333.00 FRAME SEGMENT FROM STR 25L TO STR 26L AND STR 27 TO STR 26R - [SDR REXA2024101000866](https://openairdocs.org/sdr/REXA2024101000866.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 26L IS CORRODED BETWEEN F.S. 295 TO F.S. 310. REMOVED STRINGER 26L (PN: SH670-31634-1) FROM FS 280 TO FS 333 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 26L (PN: SH670-31634-1) FROM FS 280 TO FS 333 IAW - [SDR REXA2024100900862](https://openairdocs.org/sdr/REXA2024100900862.md): Floor Support · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FLOOR BEAM LBL9 FROM FS 549 TO FS 570 AREAS OF CORROSION REPAIRED IAW CRJ-700 SRM 53-00-41-201-001-A01 AND REO 670-53-31-943 REV -- DATED 09-20-2024. - [SDR REXA2024100900861](https://openairdocs.org/sdr/REXA2024100900861.md): Intercostal · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 319 TO F.S. 333 STGR 20R. LOCATED AND DRILLED NEW INTERCOSTAL P/N: SH670-32004-1 BETWEEN FS 319.70 - FS 349 AT STGR 20 RH IAW CRJ 700 SRM 51-40-11-001-001-A01 - [SDR REXA2024100700849](https://openairdocs.org/sdr/REXA2024100700849.md): Intercostal · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED INTERCOSTAL FROM FS 349 TO FS 364 (P/N: SH670-31749-3) FOR ACCESS IAW CRJ700 SRM 51-42-21-001-001-A01. REMOVED UNSERVICEABLE INTERCOSTAL FROM FS 349 TO FS 364 P/N: SH670-31994-1 IAW CRJ - [SDR REXA2024100700848](https://openairdocs.org/sdr/REXA2024100700848.md): Frame · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Frame > F.S. 310 IS CORRODED BETWEEN STGR 26R TO STGR 26L. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01. - [SDR REXA2024100700847](https://openairdocs.org/sdr/REXA2024100700847.md): Intercostal · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 310 TO F.S. 319 STGR 20R. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-21-23-101-002-A01, NOTE 2, THE CORROSION EXCEEDS 30% THE LENGTH OF A MEMBER. REMOVED INTERCOSTAL (PN# SH670-32047-1) FROM FS - [SDR REXA2024100700846](https://openairdocs.org/sdr/REXA2024100700846.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STGR 19L IS CORRODED BETWEEN F.S. 349 TO F.S. 394. REPAIRED IAW CRJ700 SRM 53-00-03-201-201-001-A01. - [SDR REXA2024100400845](https://openairdocs.org/sdr/REXA2024100400845.md): Stringer · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > "STRINGER 26R IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED REMAINING FASTENERS THROUGH SKIN ON STGR 26R BETWEEN FS 333 TO FS 364 IAW CRJ-700 SRM 51-42-06-001-001-A01. REMOVED CORROSION ON STGR 26R BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. - [SDR REXA2024093000730](https://openairdocs.org/sdr/REXA2024093000730.md): Intercostal · corroded · Sep 6, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26L. REMOVED CORROSION ON INTERCOSTAL BETWEEN STGR 27 AND STGR 26L AND BETWEEN FS 349-364 IAW CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO BEING IN A NO DAMAGE - [SDR REXA2025011000032](https://openairdocs.org/sdr/REXA2025011000032.md): Stringer · corroded · Sep 4, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER 19L IS CORRODED BETWEEN FS485 AND FS501 LOCATED AND DRILLED NEW STRINGER 19L FOR FS469-FS501 PN SH670-33143-1A IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STR 19L, PN SH670-33143-1A, FROM FS 469 TO FS 501 IAW CRJ 700 SRM 51-42-06-0 - [SDR REXA2024111101457](https://openairdocs.org/sdr/REXA2024111101457.md): Angle · cracked · Sep 4, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FRAME F.S. 295 REINFORCEMENT ANGLE STR18L IS CRACKED. REPLACED REINFORCEMENT ANGLE PER SRM - [SDR REXA2024111101456](https://openairdocs.org/sdr/REXA2024111101456.md): Floorbeam · corroded · Sep 4, 2024 · N668CA · Cndair CL6002C10 · Fuselage Main, Floor Beam > FLOOR BEAM LBL9 IS CORRODED. REPAIRED PER MHIRJ REO 670-53-31-945/947. - [SDR REXA2024110101358](https://openairdocs.org/sdr/REXA2024110101358.md): Floor Support · corroded · Sep 4, 2024 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FLOOR BEAM CORRODED AT LBL 27 F.S. 985-1031 REPAIRED IAW CRJ700 SRM 53-00-41-201-001-A01 AND MHIRJ REO 670-53-61-2382 REV -- DATED 2024-10-03. Next page: https://openairdocs.org/aircraft/N668CA/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 = 'N668CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N668CA/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.