# Service difficulty reports: N245LR A list on [N245LR](https://openairdocs.org/aircraft/N245LR.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 2 · 98 reports - [SDR SWIA2026030975438](https://openairdocs.org/sdr/SWIA2026030975438.md): Window Post · cracked · Sep 25, 2025 · N245LR · Cndair CL6002D24 · Fuselage Main, Structure > DURING AUDIT OF 9 YEAR TASK CARD 53-220-504 - GENERAL VISUAL INSPECTION OF THE INTERNAL FRAME STRUCTURE OF THE WINDSHIELD AND SIDE WINDOWS FOUND THE RH WINDSHIELD SIDE SUPPORT POST CRACKED ON UPPER SIDE. (C-CHECK RO 03/07/2026)R/H WINDSHIELD SIDE SUPPORT POST - [SDR SWIA2026030975437](https://openairdocs.org/sdr/SWIA2026030975437.md): Floor Support · corroded · Sep 19, 2025 · N245LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION AT LONGITUDINAL FLOOR SUPPORT LBL9.00 BTW FS1015.00 TO FS1051.31 UPPER SURFACE. REMOVED DAMAGED SECTION AND REPAIRED FLOOR BEAM AT STA 1031 LBL 9 IN REF TO CRJ900 SRM 51-25-16-001-001-A01, 53-00-41-201-001-A03 FIG. 53-00-41-995-829, AND REO 690- - [SDR SWIA2026030975435](https://openairdocs.org/sdr/SWIA2026030975435.md): Floor Support · corroded · Sep 19, 2025 · N245LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION AT LONGITUDINAL FLOOR SUPPORT LBL 27.00 BTW FS1000.00 TO FS 1051.30. REMOVED DAMAGED LONGITUDINAL FLOOR SUPPORT BS 1025-1037 AND REPAIRED IAW REO 690-53-61-1706 AND SRM 53-00-41-201-001-A01 FIG. 53-00-41-995-829. REMOVED AND REPLACED DAMAGED COMP - [SDR SWIA2026030975434](https://openairdocs.org/sdr/SWIA2026030975434.md): Web · cracked · Sep 18, 2025 · N245LR · Cndair CL6002D24 · Passenger/Crew Doors > CRACKED WEB ON PAX DOOR (MID STEP) FWD SIDE. PERFORMED PERMANENT REPAIR TO PAX DOOR. REF. SRM 52-11-04-201-004-A01. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFOMED. COMPLIED WITH STRUCTRAL REPAIR TASK CARD 52-900-1002-SKY. - [SDR SWIA2026030975482](https://openairdocs.org/sdr/SWIA2026030975482.md): Roller · worn · Sep 9, 2025 · N245LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 2-2 FWD OB AND AFT IB ROLLERS WORN OUT OF LIMITS (C-CHECK RO 03/07/2026)REMOVED AND REPLACED RH SLAT TRACK 2-2 FWD OB AFT IB ROLLERS PER CRJ900 AMM 27-81-44-400-802-A01. FLAPS / SLATS OPS. CHECKED GOOD - [SDR SWIA2026030975481](https://openairdocs.org/sdr/SWIA2026030975481.md): Roller · worn · Sep 9, 2025 · N245LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 1-2 FWD OB AND AFT OB ROLLERS WORN OUT OF LIMITS (C-CHECK RO 03/07/2026)REMOVED & REPLACED RH SLAT TRACK 1-2 FWD OB & AFT OB ROLLERS IAW CRJ900 AMM 27-81-44-000-801-A01 PROCEDURE 4 A 1-7 TOURQE WRENCH: 1113046432 CAL: 5-31-26 - [SDR SWIA2025090875436](https://openairdocs.org/sdr/SWIA2025090875436.md): Landing · cracked · Sep 8, 2025 · N245LR · Cndair CL6002D24 · Fuselage Main, Structure > RIGHT SIDE TRU DOOR LOWER LANDING IS CRACKED AT AFT LATCH. REMOVED AND REPLACED CRACKED R/H SIDE TRU DOOR LANDING WITH A NEW LANDING AS REQ'D REF. SRM 51-42-06-001-001-A01, SEE ATTACHED CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. RVSM REQUIRES DOWNGRADIN - [SDR SWIA2025030975480](https://openairdocs.org/sdr/SWIA2025030975480.md): Roller · worn · Sep 7, 2025 · N245LR · Cndair CL6002D24 · Leading Edge Devices > LH SLAT TRACK 3-2 AFT IB ROLLER WORN OUT OF LIMITS (C-CHECK RO 03/07/2026)REMOVED AND REPLACED LH SLAT TRACK 3-2 AFT I/B ROLLER IAW MHI CRJ 900 AMM TASK 27-81-44-400-803 (A01) STEP 1 TO PAGE 2 STEP 4 A (7). TOURQE WRENCH: 1113046432 CAL: 5-31-26 - [SDR SWIA2025030975479](https://openairdocs.org/sdr/SWIA2025030975479.md): Roller · worn · Sep 7, 2025 · N245LR · Cndair CL6002D24 · Leading Edge Devices > LH SLAT TRACK 2-2 FWD IB ROLLER WORN OUT OF LIMITS (C-CHECK RO 03/07/2026)REMOVED AND REPLACED LH SLAT TRACK 2-2 FWD I/B ROLLER IAW MHI CRJ 900 AMM TASK 27-81-44-400-802 (A01) STEP 1 TO PG 2 STEP4 A (7). - [SDR SWIA2025030975478](https://openairdocs.org/sdr/SWIA2025030975478.md): Roller · worn · Sep 7, 2025 · N245LR · Cndair CL6002D24 · Leading Edge Devices > LH SLAT TRACK 1-2 AFT OB AND FWD OB ROLLERS WORN OUT OF LIMITS (C-CHECK RO 03/07/2026)REMOVED AND REPLACED 1-2 FWD O/B ROLLER BEARING AND INSPECTED AFT O/B ROLLER BEARING PER CRJ900 AMM 27-81-44-400-801-A01/27-81-43-220-801-A01 SEE ATTACHED CONTINUATION CA - [SDR MASA2023122200145](https://openairdocs.org/sdr/MASA2023122200145.md): Bulb · burned out · Dec 22, 2023 · N245LR · Cndair CL6002D24 · Emergency Lighting > L1 DOOR LOWER EXIT SIGN SEVERAL LED OUT. CURRENTLY OUT OF SERVICE. REPLACED 2 BULBS IN SIGN. - [SDR MASA202310010025](https://openairdocs.org/sdr/MASA202310010025.md): Unknown · unknown · Oct 1, 2023 · N245LR · Cndair CL6002D24 · Emergency Lighting > INTERIOR EME LIGHTS EVEY OTHR LIGHT INOP- OP CHECK FOUND TO BE NORMAL CONFIGURATION - [SDR MASA2023062200082](https://openairdocs.org/sdr/MASA2023062200082.md): Smoke Detector · failed · Jun 22, 2023 · N245LR · Cndair CL6002D24 · Smoke Detection > SMOKE FWD LAV WARN (NOT ACTUAL SMOKE) PLACED ON MEL - [SDR MASA2022121000270](https://openairdocs.org/sdr/MASA2022121000270.md): Battery Pack · depleted · Dec 10, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > EMERGENCY LIGHTS INOP - CHARGED EMER BATT PACKS - [SDR MASA2022100100238](https://openairdocs.org/sdr/MASA2022100100238.md): None · none · Oct 1, 2022 · N245LR · Bombdr BD1001A10 · Emergency Lighting > EMER LITES ROW 4 BACK INOP. MX CHARGED EMER BATTERY PACKS. - [SDR MASA2022092500234](https://openairdocs.org/sdr/MASA2022092500234.md): Battery Pack · discharged · Sep 25, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > EMER LT ROW 12 & 13 WN ILLUM. CHARGED EMER LT OPS CK NO DEFECT NOTED. - [SDR MASA2022090900227](https://openairdocs.org/sdr/MASA2022090900227.md): None · unknown · Sep 9, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > EMERGENCY LIGHTS INOP RH/LH ROWS 3 AND 13. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS, OPS CHECK NORMAL, NO DEFECTS NOTED. - [SDR MASA2022081400211](https://openairdocs.org/sdr/MASA2022081400211.md): Light · inoperative · Aug 13, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > CEILING ORDINANCE EMER SIGNS INOP. CURRENTLY OUT OF SERVICE TROUBLE SHOOTING. - [SDR MASA2022072100190](https://openairdocs.org/sdr/MASA2022072100190.md): None · none · Jul 22, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > ALL OVR WING EMER EXIT LIGHS INOP. AIRCRAFT IS STILL CURRENTLY OOS. - [SDR MASA2022071300188](https://openairdocs.org/sdr/MASA2022071300188.md): None · none · Jul 13, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > ALL OVR WING EXIT ROW EMER LIGHTS INOP. CURRENTLY OOS. - [SDR MASA2022070900184](https://openairdocs.org/sdr/MASA2022070900184.md): Light · inoperative · Jul 9, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > MID CABIN - ROW 13 LH/RH EMER LTS INOP - [SDR MASA2022062500171](https://openairdocs.org/sdr/MASA2022062500171.md): None · none · Jun 25, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > CABIN EMER LIGHTS COME ON INTERMITTENTLY. CURRENTLY OOS TROUBLE SHOOTING. - [SDR MASA2022062200168](https://openairdocs.org/sdr/MASA2022062200168.md): None · none · Jun 22, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > CABIN EMER LIGHT AFT 1ST CLASS INOP. CURRENTLY OOS. - [SDR MASA2022040400094](https://openairdocs.org/sdr/MASA2022040400094.md): Bulb · inoperative · Apr 4, 2022 · N245LR · Cndair CL6002D24 · Emergency Lighting > OW LH-RH OUTSIDE EMER LIGHTS INOP - [SDR MASA20220307117](https://openairdocs.org/sdr/MASA20220307117.md): None · none · Mar 7, 2022 · N245LR · Cndair CL600* · Nacelle/Pylon Miscellaneous Structure > THE LH THRUST REVERSER HINGE LINE FAIRING SKIN WAS FOUND TO HAVE WEAR DAMAGE NEAR AN EXISTING SPLICE REPAIR. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) 54-12-01, FIGURE 54-12-01-991-808, ITEM 8 (REV. 38 DATED JUL. 25 2020) B) ILLUSTR - [SDR MASA20220228116](https://openairdocs.org/sdr/MASA20220228116.md): None · none · Feb 28, 2022 · N245LR · Cndair CL6002D24 · Fuselage Structure (General) > THE BULKHEAD FLOOR POST (P/N: CC670-34180-6) AT FS280.00 AND RBL 11.16 WAS FOUND TO HAVE A CORROSION DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-11-10-001-003-A01, FIGURE 53-11-10-991-803 (SHEET 4 OF 7), ITEM 57_8 (REV.33 DATE - [SDR MASA20220224113](https://openairdocs.org/sdr/MASA20220224113.md): None · corroded · Feb 24, 2022 · N245LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN (P/N: SH670-33003-11) BETWEEN FS629.00 - FS645.00 AT STGR0 WAS FOUND TO HAVE CORROSION, SCRATCH AND NICK DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-31-01-001-001-A02, FIGURE 53-31-01-991-802, ITEM 1A, B (REV - [SDR MASA20220223112](https://openairdocs.org/sdr/MASA20220223112.md): None · none · Feb 23, 2022 · N245LR · Cndair CL600* · Nacelle/Pylon, Plate/Skin > THE RH INLET COWL LIPSKIN WAS FOUND TO HAVE CORROSION DAMAGE. THE MINIMUM REMAINING THICKNESSES IN THE BLENDED AREA ES 0.059. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 54-11-05-001-001-A01, FIGURE 54-11-05-991-801, ITEM 1, (REV. 37 DAT - [SDR MASA20220218111](https://openairdocs.org/sdr/MASA20220218111.md): None · none · Feb 18, 2022 · N245LR · Cndair CL600* · Nacelle/Pylon Structure > THE L/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WEDGE WAS FOUND WITH WEAR DAMAGE AT SS407.75. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-13-02 TABLE 1 - [SDR MASA2021121500339](https://openairdocs.org/sdr/MASA2021121500339.md): Flashlight · inoperative · Dec 16, 2021 · N245LR · Cndair CL6002D24 · Life Jacket > FO'S FLASHLIGHT INOP PLACED ON MEL - [SDR V0XD20210126001](https://openairdocs.org/sdr/V0XD20210126001.md): Support Bracket · cracked · Jan 26, 2021 · N245LR · Cndair CL6002D24 · Wing Miscellaneous Structure > LT WING SLAT TRACK BOX 1-3 SUPPORT BRACKET CRACKED. REPAIRED LT WING SLAT BOX 1-3, CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS, IAW BOMBARDIER REO 670-57-42-577 DATED: 2016-12-02. - [SDR MASA2021011200010](https://openairdocs.org/sdr/MASA2021011200010.md): Bulb · inoperative · Jan 12, 2021 · N245LR · Cndair CL6002D24 · Emergency Lighting > GALLEY FLOOR LEVEL EXIT SIGN 2 BULBS INOPERABLE, PLACED ON MEL. - [SDR MASA2021010200002](https://openairdocs.org/sdr/MASA2021010200002.md): Battery · inoperative · Jan 2, 2021 · N245LR · Cndair CL6002D24 · Emergency Lighting > CA FLASHLIGHT IND NOT BLINKING. REPLACED FLASHLIGHT BATTERY. - [SDR V0XD20201222022](https://openairdocs.org/sdr/V0XD20201222022.md): Stringer · corroded · Dec 22, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 24R CORRODED BETWEEN FRAMES 333.00 AND 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1046. - [SDR V0XD20202212016](https://openairdocs.org/sdr/V0XD20202212016.md): Cascade · cracked · Dec 22, 2020 · N245LR · Cndair CL6002D24 · Engine Thrust Reverser > LT THRUST REVERSER IN BOARD LOWER CASCADE CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 4019. - [SDR V0XD20201222021](https://openairdocs.org/sdr/V0XD20201222021.md): Stringer · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 26L CORRODED BETWEEN FRAMES 333.00 AND 364.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1041. - [SDR V0XD20201222020](https://openairdocs.org/sdr/V0XD20201222020.md): Stringer Splice · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 25R SPLICE AT FRAME 333.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1047. - [SDR V0XD20201222019](https://openairdocs.org/sdr/V0XD20201222019.md): Stringer · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 27 CORRODED BETWEEN FRAME 310.00 AND 333.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1070. - [SDR V0XD20202212018](https://openairdocs.org/sdr/V0XD20202212018.md): Stringer · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 26R CORRODED BETWEEN FRAMES 319.00 AND 349.00. CORECCTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1036. - [SDR V0XD20202212015](https://openairdocs.org/sdr/V0XD20202212015.md): Tail Cone · dented · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Aerodynamic Fairings > APU TAILCONE DENTED ON RT SIDE. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 3009. - [SDR V0XD20202212014](https://openairdocs.org/sdr/V0XD20202212014.md): Stringer Splice · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 26R SPLICE AT FRAME 333.00 CORRODED. COERRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1044. - [SDR V0XD20202212013](https://openairdocs.org/sdr/V0XD20202212013.md): Stringer · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 27 CORRODED BETWEEN FRAMES 333.00 AND 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1048. - [SDR V0XD20202212012](https://openairdocs.org/sdr/V0XD20202212012.md): Stringer · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STRINGER 25R CORRODED BETWEEN FRAMES 280.00 TO 310.00 AND 319.00 TO 349.00. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1035. - [SDR V0XD20202212011](https://openairdocs.org/sdr/V0XD20202212011.md): Frame · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Frame > FRAME 310.00 CORRODED BEWTEEN STRINGERS 25L TO 25R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1037. - [SDR V0XD20202212009](https://openairdocs.org/sdr/V0XD20202212009.md): Mount · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Attach Fittings > TCAS ANTENNA MOUNT CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1043. - [SDR V0XD20202212008](https://openairdocs.org/sdr/V0XD20202212008.md): Frame · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Frame > FRAME 333.00 CORRODED BETWEEN STRINGERS 25L TO 24R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1040. - [SDR V0XD20202212007](https://openairdocs.org/sdr/V0XD20202212007.md): Frame · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage Main, Frame > FRAME 319.00 CORRODED BETWEEN STRINGERS 25L AND 26R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1039. - [SDR V0XD20202212002](https://openairdocs.org/sdr/V0XD20202212002.md): Seat Track · corroded · Dec 21, 2020 · N245LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > LT SIDE SEAT RAILS FROM FRAME STATIONS 693.00-813.00 AND 847.00-865.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 2119. CORRODED SEAT TRACKS PART NUMBERS SH970-37543-3, SH690-36284-1, SH690-36285-2, AND SH670-36260-5. - [SDR V0XD20202212006](https://openairdocs.org/sdr/V0XD20202212006.md): Strap · cracked · Dec 19, 2020 · N245LR · Cndair CL6002D24 · Aerodynamic Fairings > AFT WING TO BODY FAIRING STRAP CARCKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX WORK ORDER 80892 WORK CARD 1051. - [SDR V0XD20202212005](https://openairdocs.org/sdr/V0XD20202212005.md): Support Bracket · cracked · Dec 19, 2020 · N245LR · Cndair CL6002D24 · Wing, Attach Fittings > LT SLAT BOX 1-3 SUPPORT BRACKET CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX WORK ORDER 80892 WORK CARD 5041. Next page: https://openairdocs.org/aircraft/N245LR/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 = 'N245LR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N245LR/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.