# Service difficulty reports: N676CA

A list on [N676CA](https://openairdocs.org/aircraft/N676CA.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 6 · 269 reports

- [SDR REXA2026050400422](https://openairdocs.org/sdr/REXA2026050400422.md): Buttstrap · corroded · Apr 11, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN. CORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN WAS REPAIRED PER REO 690-53-21-2118 REV. - -
- [SDR REXA2026080501493](https://openairdocs.org/sdr/REXA2026080501493.md): Fitting · corroded · Mar 13, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FITTING PN: CDSP2019-7C-760 IN FRONT ACCESS 107 (1EA) AND FITTING PN: CDSP2019-7C-620 AFT IN ACCESS 108 (1EA) ON GALLEY SUMMARY OF NRC 290:FITTING (1 EA) AND DOUBLER (1 EA) IN FRONT ACCESS 107 AND FITTING (1 EA) AFT IN ACCESS 108 (1 EA) ON GALLEY
- [SDR REXA2026080501492](https://openairdocs.org/sdr/REXA2026080501492.md): Fitting · corroded · Mar 13, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FITTING IN FRONT ACCESS 107 (1EA) AND FITTING PN: CDSP2019-7C-620 AFT IN ACCESS 108 (1EA) ON GALLEY FITTING (1 EA) AND DOUBLER (1 EA) IN FRONT ACCESS 107 AND FITTING (1 EA) AFT IN ACCESS 108 (1 EA) ON GALLEY WERE REPLACED IAW CMM 25-33-67.
- [SDR REXA2026080501496](https://openairdocs.org/sdr/REXA2026080501496.md): Hinge Fitting · corroded · Mar 12, 2026 · N676CA · Cndair CL6002D24 · Ailerons
  > AFTER BUSHING AND BEARINGS REMOVAL FOUND CORROSION IN LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON WERE REPAIRED PER REO 670-57-61-107 REV. -B.
- [SDR REXA2026080501491](https://openairdocs.org/sdr/REXA2026080501491.md): Hinge Fitting · corroded · Mar 12, 2026 · N676CA · Cndair CL6002D24 · Ailerons
  > CORROSION IN LUG R2 & R5 AT CENTER HINGE FITTING OF FRONT SPAR IN RH AILERON CORROSION AT CENTER FITTING IN LUGS R2 & R5 WERE REMOVED PER REO 670-57-61-107 REV.-B, REO 690-57-61-504 REV-- AND CRJ 900 SRM 51-26-00-001-001-A01 CLEANING, DEFERRAL NUMBERS WO W907
- [SDR REXA2026080501499](https://openairdocs.org/sdr/REXA2026080501499.md): Transcowl · cracked · Mar 11, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust Reverser
  > AFTER REMOVAL OF Z STIFFENER ON LH ENGINE UPPER / LOWER TRANSCOWL, CRACKS WERE FOUND ON ACCOUSTIC PANEL PERFORATED SKIN ACUSTIC PANEL OF TRANSCOWL UPPER LH WAS REPAIRED PER EA CRJ954-21830 REV.IR ACUSTIC PANEL OF TRANSCOWL LOWER LH WAS REPAIRED PER EA CRJ954-2
- [SDR REXA2026080501498](https://openairdocs.org/sdr/REXA2026080501498.md): Transcowl · cracked · Mar 11, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust Reverser
  > AFTER REMOVAL OF Z STIFFENER ON LT ENGINE UPPER / LOWER TRANSCOWL, CRACKS WERE FOUND ON ACCOUSTIC PANEL PERFORATED SKIN ACUSTIC PANEL OF TRANSCOWL UPPER LT WAS REPAIRED PER EA CRJ954-21830 REV.IR ACUSTIC PANEL OF TRANSCOWL LOWER LT WAS REPAIRED PER EA CRJ954-2
- [SDR REXA2026050400421](https://openairdocs.org/sdr/REXA2026050400421.md): Stringer · corroded · Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 18R AND STRINGER 19R BTW STA=453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW STA= 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPH
- [SDR REXA2026050400419](https://openairdocs.org/sdr/REXA2026050400419.md): Stringer · corroded · Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRINGER 19R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.
- [SDR REXA2026050400418](https://openairdocs.org/sdr/REXA2026050400418.md): Stringer · corroded · Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 18R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.
- [SDR REXA2026050400443](https://openairdocs.org/sdr/REXA2026050400443.md): Fitting · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > WEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL
- [SDR REXA2026050400442](https://openairdocs.org/sdr/REXA2026050400442.md): Doubler · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL
- [SDR REXA2026050400441](https://openairdocs.org/sdr/REXA2026050400441.md): Fitting · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > WEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL
- [SDR REXA2026050400440](https://openairdocs.org/sdr/REXA2026050400440.md): Bracket · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSSION AND WEAR ON SENTLEMENT AREA OF WHEEL BIN LH (3 LOCATIONS) AND RH (5 LOCATIONS). NEW WHEEL BEAM STABILIZER P/N: CC670-39221-4 WAS FABRICATED PER DWG CC670-39221 REV NC & EA CRJ953-21866 REV IR
- [SDR REXA2026050400439](https://openairdocs.org/sdr/REXA2026050400439.md): Bracket · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LH/RH) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-
- [SDR REXA2026050400438](https://openairdocs.org/sdr/REXA2026050400438.md): Bracket · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LT/RT) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-8
- [SDR REXA2026050400424](https://openairdocs.org/sdr/REXA2026050400424.md): Hinge · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITS
- [SDR REXA2026050400423](https://openairdocs.org/sdr/REXA2026050400423.md): Hinge · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITS
- [SDR REXA2026050400417](https://openairdocs.org/sdr/REXA2026050400417.md): Latch · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Accessory Compartment Doors
  > CORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITS
- [SDR REXA2026050400416](https://openairdocs.org/sdr/REXA2026050400416.md): Hinge · corroded · Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITS
- [SDR REXA2026080501497](https://openairdocs.org/sdr/REXA2026080501497.md): Door Frame · worn · Mar 7, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Structure
  > WEAR ON LOWER FRAME COVET AT FWD LAVATORY DOOR. NEW TRIM LOWER. (1EA) AT FWD LAVATORY DOOR WAS REPLACED IAW CMM 25-40-76.
- [SDR REXA2026050400437](https://openairdocs.org/sdr/REXA2026050400437.md): Landing · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT LT DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 211AL)(2 LOCATIONS) AFT LT DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 211AL) WAS FABRICATED PER EA. CRJ953-21839 REV. IR AND REPLACED PER SRM 51-42-10-001-001-A01
- [SDR REXA2026050400434](https://openairdocs.org/sdr/REXA2026050400434.md): Drag Angle · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-A01
- [SDR REXA2026050400433](https://openairdocs.org/sdr/REXA2026050400433.md): Drag Angle · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-00
- [SDR REXA2026050400430](https://openairdocs.org/sdr/REXA2026050400430.md): Doubler · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00 WAS REPAIRED PER SRM 53-11-43-201-001-A01 AND PER SRM 53-11-43-201-001-A01
- [SDR REXA2026050400429](https://openairdocs.org/sdr/REXA2026050400429.md): Bracket · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BROKEN WATER SPRAYER BRACKET BTW FS1144.00 TO FS1162.00 AND STGR 9 LH AT AFT EQUIPMENT COMPARTMENT REPLACED PER SRM 51-42-06-001-001-A01.
- [SDR REXA2026050400428](https://openairdocs.org/sdr/REXA2026050400428.md): Drag Angle · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-A
- [SDR REXA2026050400427](https://openairdocs.org/sdr/REXA2026050400427.md): Drag Angle · cracked · Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LT FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED IAW SRM 55-31-00-201-001-
- [SDR REXA2026050400425](https://openairdocs.org/sdr/REXA2026050400425.md): Doubler · worn · Mar 5, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV F
- [SDR REXA2026080501495](https://openairdocs.org/sdr/REXA2026080501495.md): Access Panel · corroded · Mar 4, 2026 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON ACCESS PANEL 832AT, 832CT, 832FT CORROSION ON ACCESS PANEL 832CT WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER SRM 52-11-04-101-001-A01, ACCESS PANEL 832AT WAS REPLACED IAW SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-
- [SDR REXA2026050400415](https://openairdocs.org/sdr/REXA2026050400415.md): Fairing · cracked · Mar 4, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust Reverser
  > CRACKED FAIRING BTW RH ENG. AND PYLON FS 1086 APROX. FAIRING BTW RT ENG. AND PYLON FS 1086 APROX WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
- [SDR REXA2025121801047](https://openairdocs.org/sdr/REXA2025121801047.md): Rod · inoperative · Dec 16, 2025 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > UNABLE TO OPEN PAX DOOR REPLACED PAX DOOR VENT FLAP ROD ASSY
- [SDR REXA2025071100718](https://openairdocs.org/sdr/REXA2025071100718.md): Lamp · inoperative · Jul 9, 2025 · N676CA · Cndair CL6002D24 · Emergency Lighting
  > CEILING EMERGENCY LIGHT AT ROW 10 INOP RELAMPED CEILING EMER LIGHT IAW CRJ 900 AMM 33-51-09 OPS CHECK GOOD
- [SDR REXA2022110200946](https://openairdocs.org/sdr/REXA2022110200946.md): Lamp · inoperative · Oct 30, 2023 · N676CA · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY EXIT SIGN LIGHT INOP, CABIN CEILING. R & R LAMP BULB IAW AMM 33-51-07, PN ON/OFF: 6100945
- [SDR REXA2022060600973](https://openairdocs.org/sdr/REXA2022060600973.md): Splice · corroded · Apr 22, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL 191AB SPLICE JOINT PLATE CORRODED IN MULTIPLE AREAS WITH A DEPTH OF.016". REMOVE AND REPLACE SPLICE JOINT.
- [SDR REXA2022060600972](https://openairdocs.org/sdr/REXA2022060600972.md): Plate · cracked · Apr 18, 2022 · N676CA · Cndair CL6002D24 · Engine Thrust Reverser
  > LH ENGINE LOWER TRANSCOWL BIFURCATION PANEL NYLON PLATE BROKEN MANUFACTURED NEW PLATE PER EA# CRJ954-13327.
- [SDR REXA2022060600971](https://openairdocs.org/sdr/REXA2022060600971.md): Stringer · corroded · Apr 15, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 26L HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS280-333 WITH UP TO 100% MATERIAL LOSS. REMOVE AND REPLACE STR 26L.
- [SDR REXA2022060600970](https://openairdocs.org/sdr/REXA2022060600970.md): Stringer · corroded · Apr 13, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 24L CORRODED BETWEEN FS333-364. CORROSION MEASURES 7.0"X1.0"X.040" DEEP. REMOVE AND REPLACE STRINGER.
- [SDR REXA2022060600969](https://openairdocs.org/sdr/REXA2022060600969.md): Intercostal · corroded · Apr 10, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN FS349-364 JUST RIGHT OF STR27 LOWER FLANGE HAS EXFOLIATED CORROSION. REMOVE AND REPLACE INTERCOSTAL.
- [SDR REXA2022060600968](https://openairdocs.org/sdr/REXA2022060600968.md): Cover · corroded · Apr 8, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR UPPER, FWD AND AFT CORNER COVERS HAVE EXFOLIATED CORROSION. REPLACE CORNER COVERS. AFT P/N 600-31902-287 AND FWD P/N 600-31902-288
- [SDR REXA2022060600967](https://openairdocs.org/sdr/REXA2022060600967.md): Skin · corroded · Apr 8, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FEED BAGGAGE DOOR SURROUND STRUCTURE BACKING SKIN CORRODED BETWEEN STR 24L-25L AND FS 517-565. MULTIPLE SPOTS OF CORROSION WITH A MAX DEPTH OF.007". REPAIRED CORROSION PER EA CRJ953-13302.
- [SDR REXA2022060600966](https://openairdocs.org/sdr/REXA2022060600966.md): Angle · corroded · Apr 6, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE AT STR 22R BETWEEN FS280-295 HAS MULTIPLE SPOTS OF EXFOLIATED CORROSION. REPLACE SUPPORT ANGLE
- [SDR REXA2022060600965](https://openairdocs.org/sdr/REXA2022060600965.md): None · corroded · Apr 4, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS280.00 BUTT STRAP HAS AREAS OF CORROSION FROM STR 26R-26L. DIMENSIONS AFTER BLEND AS FOLLOWS. STR26R-27 10.0"X6.0"X.005" MAX DEPTH, STR26L-27 10.0"X6.0"X.005" MAX DEPTH REPAIRED CORROSION PER EA CRJ953-13363
- [SDR REXA2022060600964](https://openairdocs.org/sdr/REXA2022060600964.md): Stringer · corroded · Apr 1, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 23L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS319-333 WITH UP TO 100% MATERIAL LOSS. REPLACED STR 23L IAW EA CRJ953-13351
- [SDR REXA2022060601022](https://openairdocs.org/sdr/REXA2022060601022.md): None · corroded · Apr 1, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SEAL RETAINER CORRODED. CORROSION MEASURES 10.0"X.200"X100% MATERIAL LOSS. REMOVE AND REPLACE SEAL RETAINER.
- [SDR REXA2022060600963](https://openairdocs.org/sdr/REXA2022060600963.md): Former · corroded · Mar 29, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER HAS EXFOLIATED CORROSION ON THE INNER SIDE. REPLACE AFT FORMER.
- [SDR REXA2022060600962](https://openairdocs.org/sdr/REXA2022060600962.md): Intercostal · corroded · Mar 29, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE WEB. 6TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.
- [SDR REXA2022060600961](https://openairdocs.org/sdr/REXA2022060600961.md): Intercostal · corroded · Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE LOWER FLANGE. 4TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.
- [SDR REXA2022060600960](https://openairdocs.org/sdr/REXA2022060600960.md): Intercostal · corroded · Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SEVENTH INTERCOSTAL DOWN MIDDLE OF PAX DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.
- [SDR REXA2022060600959](https://openairdocs.org/sdr/REXA2022060600959.md): Intercostal · corroded · Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR THIRD INTERCOSTAL DOWN IN MIDDLE OF DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.

Next page: https://openairdocs.org/aircraft/N676CA/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 = 'N676CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N676CA/reports

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