# Service difficulty reports: N249LR A list on [N249LR](https://openairdocs.org/aircraft/N249LR.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 · 91 reports - [SDR SWIA2026090677100](https://openairdocs.org/sdr/SWIA2026090677100.md): Windshield · cracked · Sep 6, 2026 · N249LR · Cndair CL6002D24 · Flight Compartment Windows > FO WINDSHIELD LOOKS CRACKED ON THE MIDDLE LEFT SIDE VIEWING FROM THE COCKPIT (FLIGHT 6269) REMOVED AND REPLACED RT FO WINDSHIELD IAW TASK CARD 56-220-1000-SKY. OPS CHECK GOOD. LEAK CHECK GOOD. OK FOR RETURN TO SERVICE. - [SDR SWI2025F01525](https://openairdocs.org/sdr/SWI2025F01525.md): Track · out of limits · Aug 27, 2025 · N249LR · Cndair CL6002D24 · Engine Thrust Reverser > L/H UPPER THRUST REVERSER INBD TRACK NYLON INSERT HARDWARE REQUIRES REMOVAL (1EA) (C-CHECK RO 11/07/2025)REMOVED (01EA) SCREW AND REPAIRED 02 HOLES ON L/H UPPER TR INBD TRACK NYLON. IAW CRJ900 SRM 51-41-02, 51-12-00, 51-21-11 AND REO 670-78-30-921 REV B, DAT - [SDR SWIA20251110815](https://openairdocs.org/sdr/SWIA20251110815.md): Drain Mast · scratched · Aug 15, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Structure > AFT DRAIN MAST MATING SURFACE FOUND TO BE SCRATCHED AND SIGNS OF CORROSION (C-CHECK RO 11/07/2025)BLENDED CORROSION DAMAGE TO FUSELAGE SKIN BTW FS1031.00 -FS 1051.30 AND STR27-STR26R, FOUND TO BE WITHIN LIMITS IAW CRJ900 SRM 53-61-01, 51-12-00, MHIRJ REO - [SDR SWIA20251110810](https://openairdocs.org/sdr/SWIA20251110810.md): Rib · cracked · Aug 10, 2025 · N249LR · Cndair CL6002D24 · Wing, Rib/Bulkhead > RH WING LEADING EDGE RIB AT SS58.41 IS CRACKED ON TOP SIDE OF RIB (C-CHECK RO 11/07/2025)PERFORMED REPAIR DAMAGE ON RH WING LEADING EDGE RIB AT SS58.41 IAW CRJ900 AMM 57-41-32, MHI RJ REO 690-57-41-538 REV--(P1) DATE: 2025-08-12, MHI RJ REO 690-57-41-538 REV- - [SDR SWI2025F01531](https://openairdocs.org/sdr/SWI2025F01531.md): Frame · corroded · Aug 6, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > SIGNS OF CORROSION FS985.00 STGR 26R-24L TO INCLUDE 3EA ANGLE BRACKETS (C-CHECK RO 11/07/2025)PERFORMED REPAIR ON FRAME AT FS 985, STGR 26R TO STGR 24L AND REMOVED AND REPLACED 8 EA ANGLE BRACKET PER MHIRJ REO 690-53-61-1672, REV --, DATE 2025-09-15, MHIRJ RE - [SDR SWI2025F01530](https://openairdocs.org/sdr/SWI2025F01530.md): Stringer · corroded · Aug 6, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > SIGNS OF CORROSION ON STGR 27 APPROXIMATELY 3" FWD OF FS985.00 (C-CHECK RO 11/07/2025)PERFORMED REPAIR ON STGR27 AT FWD OF FS985.00 IAW CRJ900 SRM 53-00-03, 51-21-06, 53-61-03, 53-00-00, AMM 21-31-00, 20-70-00 AND MHIRJ REO 690-53-00-635, REV - -, DATE: 2025- - [SDR SWIA20251110806](https://openairdocs.org/sdr/SWIA20251110806.md): Frame · corroded · Aug 6, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > SIGNS OF CORROSION FS1015.00 STGR 27-24L (C-CHECK RO 11/07/2025)PERFORMED REPAIR AT FS 1015.00 STR 27-23L IAW CRJ900 SRM 51-42-06, SRM 53-61-06 AND REO 690-53-61-1664 REV --(P1) DATED 2025-08-27, REO 690-53-61-1664 REV --, 2025-09-10, NDT PERFORMED - [SDR SWIA20251110725](https://openairdocs.org/sdr/SWIA20251110725.md): Frame · corroded · Jul 25, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > SIGNS OF CORROSION AT FS333.0 STR25L TO 23R (C-CHECK RO 11/07/2025)REMOVED AND REPLACED SECTION FRAME AT F.S. 333.00 BTW STGR. 25LH TO STGR. 20RH IAW MHI RJ REO 690-53-21-2007 REV. - -, DATE 2025-08-18, BOMBARDIER REO 670-53-21-799 REV.-A, DATE 2016-11-27, BO - [SDR SWIA20251110724](https://openairdocs.org/sdr/SWIA20251110724.md): Door Frame · corroded · Jul 24, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Structure > RIGHT DOOR POST AT FS280 HAS SIGNS OF CORROSION AT FLOOR LEVEL (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH DOOR POST AT FS280 FLOOR LEVEL IAW CRJ900 SRM 53-11-10, 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-13. NDT PERFORMED - [SDR SWI2025F01532](https://openairdocs.org/sdr/SWI2025F01532.md): Bulkhead Web · corroded · Jul 24, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Bulkhead > LEFT BS280 BULKHEAD WEB AT LBL9 HAS SIGNS OF CORROSION AT FLOOR LEVEL (C-CHECK RO 11/07/2025)PERFORMED REPAIR AT L/H 280 BULK HAED WEB AT LBL9 FLOOR LEVEL IAW CRJ 900 AMM 20-70-00 SRM 51-42-06, 51-42-13, 51-42-20, BOMBARDIER REO 670-53-11-594 REV -A DATE 2015 - [SDR SWIA20251110718](https://openairdocs.org/sdr/SWIA20251110718.md): Hinge · gouged · Jul 18, 2025 · N249LR · Cndair CL6002D24 · Fuselage, Door Hinge > MAIN ENTRY DOOR HINGE GOUGED AT FWD AND AFT ENDS (C-CHECK RO 11/07/2025)PERFORMED REPAIR ON PASSENGER DOOR HINGE REPAIR (DOOR SIDE) IAW REO #670-52-11-511, REV -E, DATE 2017-08-02, NDT PERFORMED - [SDR SWIA2025111000717](https://openairdocs.org/sdr/SWIA2025111000717.md): Skin · corroded · Jul 17, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CENTRAL FUSELAGE HAS AREAS OF POSSIBLE CORROSION EXTERNAL, AT STGR 27 F.S.942.00 TO F.S.954. EVALUATED AND BLEND OUT AREAS ON CENTRAL FUSELAGE AT STGR 27 BS 942 TO 954, FOUND TO BE WITHIN LIMITS IAW REO 690-53-51-491, SRM 53-51-01, SRM 51-12-00. PERFORMED ND - [SDR SWI2025F01523](https://openairdocs.org/sdr/SWI2025F01523.md): Slat Track · damaged · Jul 16, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 3-1 HAS AREAS WITH SIGNS OF PITTING ON THE UPPER SURFACE (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH SLAT TRACK 3-1 UPPER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1279 REV-- DATE 2025-08-15. NDT PERFORMED. - [SDR SWIA20251110716](https://openairdocs.org/sdr/SWIA20251110716.md): Slat Track · damaged · Jul 16, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > RIGHT SLAT TRACK 2-3 HAS AREAS WITH SIGNS OF PITTING ON UPPER SURFACE (C-CHECK RO 11/07/2025)REPAIRED DAMAGED RH SLAT TRACK 2-3 UPPER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1274 REV-- DATE 2025-08-11. - [SDR SWI2025F01522](https://openairdocs.org/sdr/SWI2025F01522.md): Slat Track · damaged · Jul 16, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 2-1 HAS AREAS WITH SIGNS OF PITTING ON UPPER SURFACE (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH SLAT TRACK 2-1 UPPER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1281 REV-- DATE 2025-08-19. NDT PERFORMED. - [SDR SWI2025F01521](https://openairdocs.org/sdr/SWI2025F01521.md): Slat Track · damaged · Jul 16, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 1-1 HAS AREAS WITH SIGNS OF PITTING ON UPPER SURFACE (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH SLAT TRACK 1-1 UPPER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1277 REV-- DATE 2025-08-15. NDT PERFORMED. - [SDR SWI2025F01520](https://openairdocs.org/sdr/SWI2025F01520.md): Slat Track · damaged · Jul 16, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > RH SLAT TRACK 2-2 HAS AREAS WITH SIGNS OF PITTING ON UPPER AND LOWER SURFACES (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO RH SLAT TRACK 2-2 UPPER AND LOWER SURFACE IAW CRJ900 SRM 51-12-00, MHIRJ REO 690-57-42-1280 REV-P1 DATE 2025-08-22, REV-- DATE 2025-10-03. N - [SDR SWI2025F01534](https://openairdocs.org/sdr/SWI2025F01534.md): Slat Track · damaged · Jul 15, 2025 · N249LR · Cndair CL6002D24 · Leading Edge Devices > LH SLAT TRACK 1-2 HAS AREAS WITH SIGNS OF PITTING ON UPPER AND LOWER SURFACES (C-CHECK RO 11/07/2025)REPAIRED DAMAGE TO LH SLAT TRACK 1-2 UPPER AND LOWER SURFACE IAW CRJ900 SRM 51-12-00, MHIRJ REO 690-57-42-1270, REV-P1, DATE 2025-07-29, REV-- DATE 2025-10-0 - [SDR SWI2025F01533](https://openairdocs.org/sdr/SWI2025F01533.md): Slat Track · damaged · Jul 15, 2025 · N249LR · Cndair CL6002D24 · Wing, Fuselage Attach Fittings > RH SLAT TRACK 1-2 HAS AREAS WITH SIGNS OF PITTING ON UPPER AND LOWER SURFACES (C-CHECK RO 11/07/2025)REPAIRED DAMAGED RH SLAT TRACK 1-2 UPPER AND LOWER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1269 REV-- DATE 2025-07-28. NDT PERFORMED. - [SDR SWIA20251110715](https://openairdocs.org/sdr/SWIA20251110715.md): Slat Track · damaged · Jul 15, 2025 · N249LR · Cndair CL6002D24 · Wing, Fuselage Attach Fittings > LH SLAT TRACK 2-2 HAS SIGNS OF PITTING ON LOWER SURFACE (C-CHECK RO 11/07/2025)PERFORMED REPAIR LWR SURFACE AT L:H SLAT TRACK 2-2, MATERIAL LOSS.004", FOUND WITHIN LIMITS IAW REO 690-57-42-1276 REV-- DATE: 2025-08-11, CRJ900 SRM 51-12-00, AMM 57-42-26, NDT - [SDR SWIA20251110708](https://openairdocs.org/sdr/SWIA20251110708.md): Skin · corroded · Jul 8, 2025 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SIGNS OF CORROSION AT LOWER EXTERIOR RH FWD FUSELAGE BETWEEN STGR23RH AND STGR25RH AT FS285.00 (C-CHECK RO 11/07/2025)PERFORMED REPAIR TO LOWER FUSELAGE SKIN BTW FS280.00, FS295.00 STR22R- STR25R IAW CRJ900 SRM 53-21-01, 51-26-01, 51-42-06, 51-42-21, 51-25-1 - [SDR MASA2024120800004](https://openairdocs.org/sdr/MASA2024120800004.md): Target · out of range · Dec 8, 2024 · N249LR · Cndair CL6002D24 · Landing Gear Position and Warning > LANDING GEAR DISAGREE, RETURN TO FIELD, EMERGENCY DECLARED. FOUND PX11 AND PX03 NLG TARGETS OUT OF RANGE. ADJUSTED TARGETS AND PERFORMED GEAR SWINGS. ALL FAULTS CLEARED. - [SDR MASA20240423009](https://openairdocs.org/sdr/MASA20240423009.md): Frame · cracked · Apr 14, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > NOSE RING SEGMENT/STRINGER 193 CRACKED. DAMAGE SURR.STRUCTURE AT FS193 STRG.2LH-3LH, ADG RESTOW PUMP ASSY DAMAGED FROM BIRDSTRIKE, RH TRU DENTED FROM BIRDS STRIKE - [SDR MASA20240705018](https://openairdocs.org/sdr/MASA20240705018.md): Door Frame · damaged · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Structure > BIRDSTRIKE STRIKE: MAJOR REPAIR: FS193.00 FRAME REPAIR / R&R FS 193.00/REPAIRED PER: C/W ALL STEPS CRJ9-51-4380. - [SDR MASA20240705017](https://openairdocs.org/sdr/MASA20240705017.md): Skin · gouged · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > BIRD STRIKE: MAJOR REPAIR: GOUGE TO ELECTRICAL BAY FLOOR WEB BETWEEN FS177.00-FS185.00 & OUTBOARD OF RBL22.00 BLENDED GOUGE TO ELECTRICAL BAY FLOOR WEB.BETWEEN FS177.00-FS185.00 & OUTBOARD OF RBL22-.00 PER RO# CRJ9-53-5310 - [SDR MASA20240705016](https://openairdocs.org/sdr/MASA20240705016.md): Skin · damaged · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > BIRD STRIKE: MAJOR REPAIR: LH FWD LOWER SKIN DAMAGED AT FS193-202. LH FWD LOWER SKIN REPLACED AT FS193-202 PER: RO# CRJS-53-5311 - [SDR MASA20240705015](https://openairdocs.org/sdr/MASA20240705015.md): Skin · dented · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > DENT ABOVE RH PILOT PROBE IN RVSM AREA AFTER BIRDSTRIKE. REMOVED AND REPLACED RH UPPER SKIN FS202-280 (DENT ABOVE RH PILOT PROBE IN RVSM AREA) PER RO# CRJ9-53-5313 - [SDR MASA20240705014](https://openairdocs.org/sdr/MASA20240705014.md): Skin · dented · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > DENT IN SKIN PANEL AFTER BIRDSTRIKE BETWEEN FS177.00- FS185.00 BELOW ADG BAY. C/W DRESS-BACK OF DENT IN SKIN PANEL BETWEEN FS177.00 - FS185.00 BELOW ADG BAY PER RO# CRJ9-51-4379 - [SDR MASA20240705013](https://openairdocs.org/sdr/MASA20240705013.md): Skin · damaged · Apr 1, 2024 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > RH FWD SKIN DAMAGED AFTER BIRDSTRIKE AT FS 193-202/REPLACED LH FWD LOWER SKIN PER RO# CRJS-53-5312 - [SDR MASA2022122600278](https://openairdocs.org/sdr/MASA2022122600278.md): Bulb · inoperative · Dec 26, 2022 · N249LR · Cndair CL6002D24 · Emergency Lighting > PAX DR FLR LVL EXIT SIGN (2) BULBS INOPERATIVE. REPLACED BULBS - [SDR MASA2022021200045](https://openairdocs.org/sdr/MASA2022021200045.md): None · none · Feb 12, 2022 · N249LR · Cndair CL6002D24 · Emergency Lighting > PAX DOOR FLOOR LEVEL EXIT SIGN-2 BULBS INOP. PLACED ON MEL. - [SDR MASA2021111300297](https://openairdocs.org/sdr/MASA2021111300297.md): None · none · Nov 13, 2021 · N249LR · Cndair CL6002D24 · Emergency Lighting > AFT EMER FLOOD LIGHT INOP. PLACED ON MEL. - [SDR V0XD2021819001](https://openairdocs.org/sdr/V0XD2021819001.md): Drag Angle · cracked · Aug 19, 2021 · N249LR · Cndair CL6002D24 · Vertical Stabilizer > VERTICAL STABILIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10, AND REO 53-31-063 REV. -- DATED 2021-08-18. - [SDR V0XD20210816006](https://openairdocs.org/sdr/V0XD20210816006.md): Frame · corroded · Aug 14, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > AVIONICS COMPARTMENT FRAME 349 IS CORRODED FROM THE INBOARD INTERCOSTAL TO STGR 26R. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME 349 IAW CRJ 900 SRM 51-42-06 - [SDR V0XD20210816005](https://openairdocs.org/sdr/V0XD20210816005.md): Stringer · corroded · Aug 14, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AVIONICS COMPARTMENT STRINGER 27 IS CORRODED AT FRAME 295 TO THE TCAS ANTENNA BRACKET. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 27 IAW CRJ 900 SRM 51-42-06 - [SDR V0XD20210816004](https://openairdocs.org/sdr/V0XD20210816004.md): Stringer · corroded · Aug 14, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AVIONICS COMPARTMENT STRINGER 26R IS CORRODED FROM FRAME 295 TO FRAME 310. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R IAW CRJ 900 SRM 51-42-06 - [SDR V0XD20210811001](https://openairdocs.org/sdr/V0XD20210811001.md): Hinge Fitting · gouged · Aug 11, 2021 · N249LR · Cndair CL6002D24 · Ailerons > L/H AILERON CENTER HINGE FITTING LUG IS GOUGED. CORRECTIVE ACTION: REPAIRED THE LUG BY BLENDING DAMAGE IAW STS ENGINEERING SOLUTIONS EA 69-2021-125 P1 DATED 8/4/2021, P2 DATED 8/6/2021 AND IR DATED 8/10/2021. REQUIRES A DTA WITHIN 12 MONTHS OF RTS. - [SDR V0XD20210810008](https://openairdocs.org/sdr/V0XD20210810008.md): Skin · dented · Aug 10, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin > THERE IS A DENT ON THE FWD R/H FUSELAGE BETWEEN FS 177.00 AND F.S. 185 AT STGR 23R. CORRECTIVE ACTION: BLENDED DISCREPANT AREA IAW STS ENGINEERING SOLUTIONS ENGINEERING AUTHORIZATION 69-2021-124 IR DATED 8/6/2021. ***DTE REQUIRED WITHIN 12 MONTHS OF RTS. - [SDR V0XD20210810007](https://openairdocs.org/sdr/V0XD20210810007.md): Frame · corroded · Aug 10, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > AVIONICS BAY, FRAME 295 FROM STGR 26R TO 26L IS CORRODED. CORRECTIVE ACTION: PERFORMED A REPAIR TO FRAME 295 BY CUTTING OUT DAMAGED FRAME(PN: SH670-31353-1) AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-21-1308 REV. - DATED 2016-09-06 AND 670-53-21-799 - [SDR V0XD20210810006](https://openairdocs.org/sdr/V0XD20210810006.md): Frame · corroded · Aug 10, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > AVIONICS BAY, FRAME 310 FROM STGR 25R TO 26L IS CORRODED. CORRECTIVE ACTION: PERFORMED A REPAIR TO FRAME 310 BY CUTTING OUT DAMAGED FRAME(PN: SH670-31354-3) AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-21-1308 REV. - DATED 2016-09-06 AND 670-53-21-799 - [SDR V0XD20210810005](https://openairdocs.org/sdr/V0XD20210810005.md): Frame · corroded · Aug 10, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Frame > AVIONICS BAY, FRAME 319 FROM STGR 26R TO 26L IS CORRODED. CORRECTIVE ACTION: PERFORMED A REPAIR TO FRAME 319 BY CUTTING OUT DAMAGED FRAME(PN: SH670-31355-1) AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-21-1305 REV. - DATED 2016-09-06 AND 670-53-21-799 - [SDR V0XD20210810004](https://openairdocs.org/sdr/V0XD20210810004.md): Stringer · corroded · Aug 10, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AVIONICS BAY, STRINGER 25R FROM F.S.295 TO F.S. 310 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 25R(PN:SH670-31212-2) IAW CRJ 900 SRM 51-42-06. - [SDR V0XD20210810002](https://openairdocs.org/sdr/V0XD20210810002.md): Channel · corroded · Aug 9, 2021 · N249LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY THE TCAS ANTENNA CHANNEL IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE TCAS CHANEL(PN:SH670-32364-7) IAW CRJ 900 SRM 51-42-06. - [SDR V0XD202108101002](https://openairdocs.org/sdr/V0XD202108101002.md): Stringer · cracked · Aug 9, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > PASSENGER DOOR LINTEL STRINGER AT F.S. 280.00 IS CRACKED. CORRECTIVE ACTION: PERFORMED THE REPAIR TO THE PASSENGER DOOR LINTEL STRINGER AT F.S. 280 BY CUTTING OUT DAMAGE, FABRICCATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-21-493 REV. D DATED 20 - [SDR V0XD20210810001](https://openairdocs.org/sdr/V0XD20210810001.md): Angle · corroded · Aug 9, 2021 · N249LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY AT F.S. 280 THE FLOOR SUPPORT ANGLE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE(PN:CC670-34256-3) AT F.S. 280 IAW CRJ 900 SRM 51-42-00, 51-42-06, AND 51-42-13. - [SDR V0XD20210808003](https://openairdocs.org/sdr/V0XD20210808003.md): Floorbeam · cracked · Aug 8, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Floor Beam > THE L/H SIDE OF THE R.S. 280.00 CROSSBEAM IS CRACKED ON THE BOTTOM SIDE AT LBL12. CORRECTIVE ACTION: REMOVED AND REPLACED TH L/H SIDE OF THE F.S 280.00 CROSSBEAM(PN:CC670-34094-1) IAW CRJ 900 SRM 51-42-21,51-42-13,51-42-21 AND 51-42-06. - [SDR V0XD20210808002](https://openairdocs.org/sdr/V0XD20210808002.md): Floorbeam · cracked · Aug 8, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Floor Beam > AT F.S. 280.00 THE FLOORBEAM ATTACH ANGLE AT LBL12 IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED THEATTACH ANGLE(PN:CC670-34269-35) AT F.S. 280.00 IAW CRJ 900 SRM 51-42-21 - [SDR V0XD20210808001](https://openairdocs.org/sdr/V0XD20210808001.md): Floorbeam · cracked · Aug 8, 2021 · N249LR · Cndair CL6002D24 · Fuselage Main, Floor Beam > AT F.S. 280.00 THE FLOORBEAM ATTACH ANGLE AT RBL12 IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED THEATTACH ANGLE(PN:CC670-34269-40) AT F.S. 280.00 IAW CRJ 900 SRM 51-42-21 - [SDR V0XD20210816001](https://openairdocs.org/sdr/V0XD20210816001.md): Striker · gouged · Aug 3, 2021 · N249LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PASSENGER DOOR SURROUND STRUCTURE FWD SIDE OF THE SEAL STRIKER FLANGE HAS A GOUGE HALF WAY UP THE FLANGE. CORRECTIVE ACTION: REPAIRED THE SEAL STRIKER FLANGE BY CUTTING OUT THE DAMAGE FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-22-001 REV - [SDR V0XD20210804001](https://openairdocs.org/sdr/V0XD20210804001.md): Angle · corroded · Aug 3, 2021 · N249LR · Cndair CL6002D24 · Aerodynamic Fairings > AFT WING TO BODY FAIRING SUPPRT STRUCTURE ANGLE AT FS 881 AND STGR 27 IS CORRODED BEYOND LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE(PN: SH690-3933-7-1) IAW CRJ 900 SRM 51-42-06. Next page: https://openairdocs.org/aircraft/N249LR/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 = 'N249LR' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N249LR/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.