N246LR

Service difficulty reports · 128

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N246LR' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026101877759None · noneSMELL OF SMOKE IN FWD CABIN, SMOKE ALARM WENT OFF IN FWD LAV FOR 60 SECONDS, RECEIVED SMOKE LAV WARNING MESSAGE. FLIGHT 6355. ON ARRIVAL, INSPECTED FWD LAV FOR ANY SIGNS OF BURNED WIRING, LIGHT BULBS OR ELECT ISSUES, NONE FOUND. OPERATED PACKS AND RAN BOTOct 18, 2026 · N246LR · Cndair CL6002D24 · Standard Practices/StructuresSDR SWIA2026012875774Skin · crackedFOUND CRACKED ON SKIN, HYDRAULIC BAY AT 193.00 SKIN. REMOVED AND REPLACED HYD. BAY AT FS193.00 SKIN. REF. REF. REO 690-53-11-2152 REV. -- . C/W SKYWEST TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIRMAJOR REPAIR C/PAINT DEFERRED TO SKYWEST AFTER REPAIRS ANJan 28, 2026 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025101675773Skin · chafedAFT FUSELAGE SKIN CHAFED AT FS920 STR27. REPAIRED AFT FUSELAGE SKIN AT FS920 STR27 IN REF TO REO 670-53-00-290 REV. -F AND REO 690-53-00-649 REV. -. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURIZATION LEAK CHECKED GOOD.Oct 16, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025101575784Roller · wornRH SLAT TRACK 3-2 FWD IB AND FWD OB SIDE ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH SLAT TRACK 3-2 FWD OB ROLLER PER CRJ 900 AMM 27-81-44-400-803 (CONFIG A01) AND REEVALUATED RH SLAT TRACK 3-2 FWD IB ROLLER FOUND TO BE WITHIN LIMITS PER CRJ 900 AMM 2Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101575783Roller · wornRH SLAT TRACK 2-2 AFT IB SIDE ROLLER WORN OUT OF LIMITS. REEVALUEATED RH SLAT TRACK 2-2 AFT SIDE ROLLER FOUND TO BE WITHIN LIMITS PER CRJ 900 AMM 27-81-43-220-801 (CONFIG A01) STEP 4. E. (1) - (7) AND REINSTALLED PER CRJ 900 AMM 27-81-44-400-802 (CONFIG A01)Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101575782Roller · wornRH SLAT TRACK 1-2 FWD AND AFT IB SIDE ROLLERS AND AFT OB SIDE ROLLER WORN OUT OF LIMITS (C-CHECK RO 04/17/2026)REMOVED AND REPLACED RH SLAT TRACK 1-2 FWD IB ROLLER PER CRJ 900 AMM 27-81-44-400-801 (CONFIG A01) AND REEVALUATED RH SLAT TRACK 1-2 AFT OB ROLLER AOct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101575781Roller · wornLH SLAT TRACK 3-2 FWD OB SIDE ROLLER AND AFT IB SIDE ROLLER WORN OT OF LIMITS. REEVALUATED LH SLAT TRACK 3-2 FWD OB SIDE ROLLER AND AFT IB SIDE ROLLER AND FOUND TO BE IN LIMITS PER CRJ 900 AMM 27-81-43-220-801 STEP 4. E. (1) - (7) REINSTALLED PER CRJ 900 AMM Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101575780Roller · wornLH SLAT TRACK 2-2 FWD AND AFT IB SIDE ROLLERS AND FWD OB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACE LH SLAT TRACK 2-2 FWD IB AND OB ROLLERS PER AMM 27-81-44-400-802 (CONFIG A01) AND REEVALUATED AFT IB ROLLER FOUND TO WITHIN LIMMITS PER AMM 27-81-43-2Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101575779Roller · wornLH SLAT TRACK 1-2 FWD AND AFT OB SIDE ROLLERS AND FWD IB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 1-2 IB AND OB FWD ROLLERS PER AMM 27-81-44-400-801 (CONFIG A01) REEVALUATED LH SLAT TRACK 1-2 AFT OB SIDE ROLLER FOUND TO BE WITHIN LIMOct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025101375776Skin · corrodedCORROSION FOUND ON SKIN @ R1 DOOR SKIN CUTOUT 2 INCHES BELOW LWR EDGE (C-CHECK RO 04/17/2026)BLENDED OUT CORROSION IN DICREPANT AREA. AREA WAS BLESSED WITHIN LIMITS AS PER MHIRJ REO 690-53-21-2046 REV. -- DATED: 2025-11-04. COMPLIED WITH ALL STEPS OF REO. SEEOct 13, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025101275777Landing · crackedR/H TRU BAY DOOR LAND HAS POSSIBLE CRACK AT AFT LATCH CUTOUT. REMOVED AND RAPLACED TRU BAY DOOR LANDING R/H P/N CC670-33151-6 P.O. # CPT837 IAW SRM 51-42-06-001-001-A01 PG 7 PARA 6 (A) AND SRM 51-42-13-001-001-A01 PG 8 PARA 6 (A). NO WEIGHT CHANGES NOTED, REOct 12, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025101275775Skin · crackedRIGHT FUSELAGE ADG SKIN HAS POSSIBLE CRACK AT AFT LOWER CORNER OF TRU BAY DOOR OPENING (C-CHECK RO 04/17/2026)REMOVED AND REPLACED ADG SKIN AT RH FUSELAGE IN REF. TO CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6.B, 51-42-13-001-001-A01 PAR. 6.B AND REO #690-53-11-Oct 12, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025082275778Roller · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-2, TOP FORWARD - SLAT 1 ( REMOVED AND REPLACED RH TRACK ROLLER SEALED TRACK 1-2 , TOP FORWARD SLAT 1 IAW AMM CRJ900 27-81-43Aug 22, 2025 · N246LR · Cndair CL6002D24 · Leading Edge DevicesSDR MASA202401050002Window · failedFO WINDSHEILD SHATTERED RTF EMERGENCY DECLARED. CURRENTLY OOS - REPLACE WINDOW IN WORK.Jan 5, 2024 · N246LR · Cndair CL6002D24 · Flight Compartment WindowsSDR MASA2022112000260Lamp · inoperativeROW 18 OVRHD CEILING EMER FLOOD LT INOP. RELAMPED.Nov 20, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022091200229Switch · noneEMR LTS ON W SW IN ARMD POSTN RESET CIRCUIT BREAKER. PERFORMED OPERATION CHECK OF THE EMERGENCY LIGHTS. OPS CHECK GOOD.Sep 12, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022041000102None · noneSVC DOOR EXIT SIGN 1 BULB INOP. REPLACED BULB.Apr 10, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022041000101None · nonePAX DOOR EXIT SIGN 1 BULB INOP. REPLACED BULBApr 10, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022040700096None · noneLH FWD OVERWING EXTERNAL EMERGENCY EXIT WING LT INOPERATIVE.- PLACED ON MELApr 7, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022040700095None · noneLH AFT EXTERNAL OVERWING EXIT LIGHT INOPERATIVE. -PLACED ON MELApr 7, 2022 · N246LR · Cndair CL6002D24 · Emergency LightingSDR MASA2022021200046None · noneAFT LAV SMOKE DETECTOR WENT OFF IN FLIGHT (FALSE INDICATION). CLEANED SMOKE DETECTOR, OPS CHECK GOOD.Feb 12, 2022 · N246LR · Cndair CL6002D24 · Smoke DetectionSDR MASA20211123568None · noneRH LOWER FORWARD CORE COWL Z MEMBER ON THE AFT EDGE WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10, FIGURE 4-23-10-991-801, ITEM 10, EA 69-2021-196.Nov 23, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon StructureSDR MASA20211123569None · noneRH UPPER FAN COWL DOOR HINGE FITTING (PN -CN622-0306-206) AND ITS MATING STRUCTURE, THE PYLON TIE BAR (PN -CN624-4203-207) WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-05-001-001-A01, 54-24-01-001-002-A01, EA12-2021Nov 22, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR MASA20211119565None · noneOUTBOARD LOWER FACING SHEET OF THE RH UPPER CORE COWL BONDMENT ASSEMBLY WAS FOUND TO HAVE 2EA GOUGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-15, 54-23-15-991-801, ITEM 2, EA 72-2021-212. DEFECT LOCATION: RH FWD CORE COWL BONDMENT ASSEMBLNov 17, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon StructureSDR MASA20211119564None · noneLOWER SUPPORT ANGLE OF THE FWD BAGGAGE BAY DOOR SURROUND STRUCTURE WAS FOUND BENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-23, FIGURE 53-31-2-991-802, ITEM 74 EA 72-2021-203.Nov 17, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)SDR MASA20211117561None · noneFUSELAGE SKIN AND JOINT PANEL LOCATED IN THE UPPER CORNER OF THE FORWARD BAGGAGE DOOR SURROUND STRUCTURE AT FS571.300 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-31-01, FIGURE 53-31-01-995-801, ITEM 1A AND 53-31-23, FIGURE 53-3Nov 16, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20211117560None · noneSEVEN DENTS WERE FOUND AFFECTING THE LOWER SKIN OF LEFT INBOARD FLAP LOCATED AT APPROXIMATELY FSL 20. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01, FIGURE 57-52-01-991-801, ITEM 27A.Nov 16, 2021 · N246LR · Cndair CL600* · Aileron TabsSDR MASA20211117559None · noneFUSELAGE SKIN AT FS629.00-FS661.00+16.00 AND STGR21L-STGR25L WAS FOUND TO HAVE NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1B, EA 72-2021-209.Nov 16, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20211115558None · dentedNBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND TO HAVE (2) DENTS AT FLS 24.00. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM57-52-01, ITEM 28A, B, EA 80-2021-153Nov 12, 2021 · N246LR · Cndair CL6002D24 · Aileron TabsSDR MASA20211112557None · noneR/H LOWER FORWARD CORE COWL REINFORCING LATCH WAS FOUND TO HAVE WEAR DAMAGE, WHICH IS LOCATED AT THE FREE EDGE AT THE LATCH, LOCATED ALONG THE EDGE WHERE THE DOOR LATCH ENGAGES AND CAUSES WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-10-001Nov 12, 2021 · N246LR · Cndair CL600* · Nacelle/Pylon StructureSDR MASA20211111556None · noneWEAR DAMAGE WAS FOUND ON THE L/H INBOARD FLAP UPPER ACCESS PANEL 584EB, THE DAMAGE IS LOCATED IN THE FORWARD EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01-001-001-A01, DATED AUG-20-2010, EA 20-2021-199.Nov 11, 2021 · N246LR · Cndair CL6002D24 · Aileron TabsSDR MASA20211109554None · noneLH OUTBOARD FLAP UPPER AND LOWER SKINS FROM LIGTHNING STRIKES ON THE TRAILING EDGE AFTER REMOVING A TEMPORARY REPAIR INSTALLED PER AN OEM REO, THE DAMAGE HAS 8 LOCATIONS, AT WS266, WS256, WS243, WS235, WS227, WS219, WS213 AND WS207. PERFORMED PERMANENT REPAIR Nov 9, 2021 · N246LR · Cndair CL6002D24 · Trailing Edge FlapsSDR MASA20211109553None · noneOUTER SKIN AND DOUBLER OF THE FORWARD BAGGAGE BAY DOOR WERE FOUND TO HAVE GOUGE DAMAGE AT THE FORWARD EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-35-01, FIGURE 52-35-01-991-801, ITEMS 1, 2, EA 72-2021-194. DEFECT LOCATION: FWD BAG BAY DOOR. FWD EDGNov 9, 2021 · N246LR · Cndair CL6002D24 · DoorsSDR MASA20211109552None · damagedAFT LAVATORY SERVICE DOOR.(196ER) INSTALLED ON THE WING-TO-BODY FAIRING PANEL 196DR WAS FOUND TO HAVE DAMAGE ON ONE OF THE TWO HINGES. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 52-45-01, FIGURE 1, ITEM 30, EA 81-2021-084.Nov 9, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)SDR MASA20211109551None · damagedDAMAGE TO THE RH AILERON LOWER LEADING EDGE ACCESS PANEL 699AB AND 699BB WAS FOUND. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-61-02-001-001-A02 ITEMS 16, 34, AND 36, EA 81-2021-087.Nov 9, 2021 · N246LR · Cndair CL6002D24 · Wing StructureSDR MASA20211109550None · dentedFUSELAGE SKIN PANEL BETWEEN FS 169 -FS 173 WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-01, 53-00-01-101-001-A01, EA 20-2021-195.Nov 8, 2021 · N246LR · Cndair CL6002D24 · Wing StructureSDR MASA20211105529None · damagedTHE AFT LAVATORY SERVICE DOOR(196ER) INSTALLED ON THE WING-TO-BODY FAIRING PANEL 196DR WAS FOUND TO HAVE DAMAGE ON ONE OF THE TWO HNGES. PERFORMED PERMANENT REPAIR IAW CRJ700/900 IPC 52-45-01, FIGURE 1, ITEM 30, EA 81-2021-084 | DEFECT LOCATION:AFT LAV SERVICENov 5, 2021 · N246LR · Cndair CL600* · Air Conditioning DoorsSDR MASA20211105528None · noneWEAR DAMAGE WAS ACCIDENTALLY CAUSED TO CROSS BEAMS (P/N MM670-35314-009 AND MM670-35319-001} AT THE JOINT WITH CLIP (P/N MM670-35335- 001} LOCATED AT FS1015.00 DURING MTC ACTIVITIES WHEN FLOOR BEAM WAS REMOVED. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53Nov 5, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)SDR MASA20211105531None · corrodedPASSENGER DOOR INTERCOSTAL DD6 WEB AND AN ATTACH BRACKET AT FS 311.75, BETWEEN INTERCOSTALS DD5 AND DD06, WERE FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-11-06-001-001-A01, " PASSENGER DOOR STRUCTURE".Nov 4, 2021 · N246LR · Cndair CL600* · DoorsSDR MASA20211105530None · corrodedFUSELAGE FRAME AT FS 1000 WAS FOUND WITH CORROSION DAMAGE AT THE THREE LOCATIONS BETWEEN STR 23R AND STR 25L. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-185Nov 4, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20211105537None · corrodedFUSELAGE FRAME AT FS 985 WAS FOUND WITH CORROSION DAMAGE BETWEEN STR 25R AND STR 26R, THE DAMAGE IS ON THE OUTBOARD FLANGE INTERNAL SURFACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-189.Nov 2, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20211105535None · nonePASSENGER DOOR LATCH MECHANISM HOUSING STOP WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 52-11-02-05-PSA REV B, FIGURE 5, ITEM 410, EA 79-2021-245. DEFECT LOCATION: LATCH MECHANISM, PAX DOORNov 2, 2021 · N246LR · Cndair CL600* · DoorsSDR MASA20211102522None · crackedPASSENGER DOOR AFT SIDE PANEL COMMON TO THE AIRSTAIR WAS FOUND TO HAVE A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-11-04, FIGURE 52-11-04-991-801, ITEM 1B, EA 32-2021-021.Nov 2, 2021 · N246LR · Cndair CL600* · DoorsSDR MASA20211105533Doubler · corrodedDOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEECT LNov 1, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20211102523Doubler · corrodedDOUBLER FOR THE POTABLE WATER SERVICING SURROUND STRUCTURE OF THE CENTER FUSELAGE WAS FOUND TO HAVE CORROSION DAMAGE AT 33 LOCATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23-001-002-A01, FIGURE 53-51-23-991-803, ITEM 3A, EA 48-2021-049. DEFECT Nov 1, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)SDR MASA20220329145None · corrodedCORROSION WERE FOUND ON SPLICES FS 333, STRGR.25R AND 26L IN REF SB 53-057C AT MAIN AVIONICS COMP| SPLICE WAS INSTALLED PER. CRJ-900 SRM 51-42-06Oct 28, 2021 · N246LR · Cndair CL6002D24 · Standard Practices/StructuresSDR MASA20220329143Intercostal · corrodedCORROSION ON INTERCOSTAL 20RH BETWEEN FS310 AND FS319 AT MAIN AVIONICS COMPARMENT. NTERCOSTAL 20RH BETWEEN FS310 AND FS319 WAS REMPLACED PER CRJ/900 SRM 51-42-21.Oct 28, 2021 · N246LR · Cndair CL6002D24 · Standard Practices/StructuresSDR MASA20220329141None · corrodedCORROSION ON ANGLE MOUNTING OF LOWER SILL AT GALLEY SERVICE DOOR. ANGLE MOUNTING OF LOWER SILL AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01Oct 28, 2021 · N246LR · Cndair CL6002D24 · Fuselage Main, StructureSDR MASA20211026519Skin · crackedLEADING EDGE SKIN BETWEEN SS144.94 AND SS210.69, WAS FOUND WITH A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-41-01, FIGURE 57-41-01-991-801, ITEM 35D, EA 83-2021-048Oct 26, 2021 · N246LR · Cndair CL6002D24 · Wing, Fuselage Attach FittingsSDR MASA20220329149None · corrodedCORROSION ON LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN LEFT FLOOR SEAT RAIL FS374-FS485 BL 9.0 AT PAX CABIN WAS REPLACED PER AMM 53-00-49Oct 25, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)
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