N244LR

Service difficulty reports · 92

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 = 'N244LR' 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 SWIA20250702Landing · crackedRIGHT HAND TRU BAY, LAND HAS A SUSPECTED CRACK JUST ABOVE THE AFT LATCH RECEPTACLE. PERFORMED PERMANENT REPAIR (PART REPLACEMENT). COMPLIED WITH M-337. SEE CAMP 30869266 FOR RVSM MAPPING REFERRAL. REF. CRJ 900 SRM 51-40-11-001-001-A01.Jul 2, 2025 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWI2025F01507Slat Track · wornRH SLAT TRACK 2-2 AFT IB, AFT OB AND FWD OB ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH SLAT TRACK 2-2 AFT IB, AFT OB, AND FWD OB ROLLERS IAW AMM 27-81-44-000-802/27-81-44-400-802. PERFORMED OPS CHECK OF FLAP AND SLAT SYSTEMS IAW CRJ 900 AMM 27-50-00Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWI2025F01506Slat Track · wornRIGHT SLAT TRACK 1-2 AFT IB, AFT OB, FWD IB, AND FWD OB ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH TRACK 1-2 AFT IB, AFT OB, FWD IB, AND FWD OB ROLLERS IAW AMM 27-81-44-400-801 (CONFIG A01).PERFORMED OPERATIONAL CHECK OF SLAT TRACK IAW AMM 27-50-00-7Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWI2025F01505Slat Track · wornLH SLAT TRACK 3-2 AFT IB ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 3-2 IB SIDE ROLLER PER AMM 27-81-44-000-803/27-81-44-400-803. PERFORMED OPERATIONAL CHECK OFLH SLAT TRACKS IAW AMM 27-50-00-710-801.OPS CHECK GOOD AT THIS TIME.Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025110400624Slat Track · wornLEFT SLAT TRACK 1-2 AFT OB AND FWD IB ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 1-2 AFT OB AND FWD IB ROLLERS PER AMM 27-81-44-400-801OPS CHECK REQUIRED. PERFORMED OPERATIONAL CHECK OF SLAT TRACKS IAW AMM 27-50-00-710-801OPS CHECK GOODJun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR MASA2024061600060Battery Pack · dischargedALL EMER LIGHTS INOP/BATT DRAIN/SW OFF. ALOWED BATTERIES TO CHARGE/FA SW LEFT ONJun 16, 2024 · N244LR · Cndair CL6002D24 · Emergency LightingSDR MASA2023090800113Fire Loop · failedLH BLEED DUCT WARNING/ ANTI-ICE OFF. REPOSITIONED FIRE LOOPS PREFORMED ENG RUNS NO FURTHER DEFECTSep 8, 2023 · N244LR · Cndair CL6002D24 · Fire DetectionSDR MASA2023072300095Unknown · unknownRT BLEED DUCT WARNING MESSAGE- MX SECURED A LOOSE DUCTING CLAMPJul 23, 2023 · N244LR · Cndair CL6002D24 · Engine Bleed Air SystemSDR MASA2023051100073Unknown · unknownLH BLEED DUCT CAUT/DEPRESSURIZATON EMER DECLARED. INSP LOOP MT142 AND ACM PRE COOLER, NO DEFECTS.May 11, 2023 · N244LR · Cndair CL6002D24 · Air Conditioning SystemSDR MASA2022032500086Light · inoperativeCAPT.'S FLASHLIGHT RED LED INOP. PLACED ON MEL.Mar 25, 2022 · N244LR · Cndair CL6002D24 · Emergency LightingSDR MASA20210907397Floor Panel · damagedPASSENGER COMPARTMENT FLOOR PANEL 231BLF WAS FOUND TO HAVE FRAYING DAMAGE ON THE OUTER STYLE 120 FIBERGLASS SCRIM PLY. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 53-00-47, FIGURE 5E, CMM COMCMM-030, EA 72-2021-141. DEFECT LOCATION:FS280.00 - FS349.00 231BLSep 7, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA20210907396Skin · corrodedFUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE BETWEEN FS 927 - FS 942, STR 21R -STR 22R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-101-003-A04, IPC 53-82-83 FIGURE 10, EA 20-2021-161.Sep 6, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR MASA20210831390Skin · damagedLOWER FUSELAGE SKIN PANEL WAS FOUND WITH BURN DAMAGE AT FS565.00 BETWEEN STR 24R & STR 25R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-991-806, ITEM 1B, EA 69-2021-129.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR MASA20210831389Access Panel · damagedRH LOWER ACCESS PANEL 684GB BETWEEN FLS 61 & FLS 69 WAS FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01, FIGURE 57-52-01-991-802, EA 83-2021-036. DEFECT LOCATION: RH LNBOARD FLAP, 684GB, FLS 61 TO FLS 69Aug 30, 2021 · N244LR · Cndair CL6002D24 · Trailing Edge FlapsSDR MASA20210831388Floor Panel · delaminatedFWD BAGGAGE COMPARTMENT FLOOR PANELS (PN - A842101-501, A842106-501 & A842103-501) WERE FOUND TO HAVE (4) DELAMINATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 CMM 25-52-17, EA 12-2021-199.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA20210831387Slat Track · corrodedSLAT TRACK 3-2 OF THE SLAT #3 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 10, ITEM 90, EA 69-2021-131Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20210831386Slat Track · corrodedSLAT TRACK 2-2 OF THE SLAT #2 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 85, EA 69-2021-132.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20210831385Slat Track · corrodedSLAT TRACK 1-2 OF THE SLAT #1 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 85, EA 69-2021-133.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20210831384Fitting · damagedFS343.04 HANDRAIL FITTING (P/N: SH670-31905-6) AND CABLE ANCHOR FITTING (P/N:SH670-31882-19) WERE FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-23, FIGURE 53-21-23-995-818, ITEM 758, EA 72-2021-142. DEFECT LOCATION: HANDRAIL/FAug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR MASA20210831383Floor Support · corrodedUPPER CAP OF THE LBL27.00 FLOOR BEAM BETWEEN FS1015.00 - FS1031.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 3C, EA 79-2021-211.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210831382Floor Support · corrodedUPPER CAP OF THE RBL9.00 FLOOR BEAM BETWEEN FS1000.00 - FS1088.20 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 2C, EA 79-2021-212.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210831381Skin · dentedLH WING INBOARD GROUND SPOILER LOWER SKIN WAS FOUND WITH TWO DENTS AT_SPS 21.80. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 57-71-02-001-001-A01, FIGURE 57-71-02-991-801, ITEM 5A, EA 79-2021-216.Aug 30, 2021 · N244LR · Cndair CL6002D24 · SpoilersSDR MASA20210831380Floor Support · corrodedFLOOR BEAM BETWEEN FS1000.00 AND FS1088.00 AT LBL 9.0 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43, FIGURE 53-31-43-991-801, ITEM 2A, EA 83-2021-034.Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210827377Floor Panel · damagedPASSENGER COMPARTMENT FLOOR PANEL 231BLF WAS FOUND TO HAVE FRAYING DAMAGE ON THE OUTER STYLE 120 FIBERGLASS SCRIM PLY. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 53-00-47, FIGURE 5E, ITEM 25B, CMM COMCMM-030, EA 72-2021-141.Aug 26, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA20210827378Skin · corrodedFUSELAGE SKIN WAS FOUND TO HAVE CORROSION DAMAGE BETWEEN FS927 - FS942, STR. 21R -STR. 22R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-101-003-A04, EA 20-2021-161.Aug 19, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR MASA20210827379Floor Support · corrodedTHE UPPER CAP OF THE LBL27.00 FLOOR SUPPORT BETWEEN FS1015.00 - FS1031.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 3C, EA 79-2021-211.Aug 16, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA2021061100137Bulb · inoperativeTWO EMERGENCY EXIT LIGHTS INOP IN GALLEY. REPLACED BULBSJun 11, 2021 · N244LR · Cndair CL6002D24 · Emergency LightingSDR MASA2019122512205Landing Gear · inoperativeGEAR DISAGREE, NLG WOULD NOT RETRACT. PLACED ON MEL.Dec 25, 2019 · N244LR · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR MASA2019122092189Selector Valve · inoperativeGEAR DISAGREE WARNING REPLACED LAND GEAR SELECTOR VALVEDec 19, 2019 · N244LR · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR WVER2019051119Doubler · corrodedPERFORMED A MAJOR REPAIR BY REMOVING TCAS ANTENNA DOUBLER AND STRINGER 27 FORWARD SECTION AT FS 295 TO FS 310. INSTALLING A NEW SERVICABLE TCAS DOUBLER P/N SH670-32364-7 AND THE SAME SERVICABLE STRINGER 27 FORWARD SECTION IAW SRM 51-40-11-001-001-A01, 51-47-06May 11, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR WVER2019051118Intercostal · chafedPERFORMED A MAJOR REPAIR BY REMOVING, FABRICATING AND INSTALLING CARGO BEAM INTERCOSTAL AT FS 1031 TO FS 1047, P/N MM670-35328, IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND MM670-35328-S01. REF MWC JOB# 41523351 OP# 79.May 11, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WVER2019051017Skin Panel · chafedFUSELAGE LOWER SKIN PANEL BETWEEN 910 TO 927 HAS SEVERAL CHAFES AT STIRINGER 27. REPAIRED FUSELAGE LOWER SKIN PANEL IAW REO 670-53-00-290 REV. E.May 10, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR WVER2019050515Seat Track · corrodedSEAT RAIL AT LBL 9, FS 661-672 IS CORRODED IN SEVERAL LOCATIONS.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050514Seat Track · corrodedRBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 661.00+32 AND 672.00.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050513Seat Track · corrodedLBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 374.00 AND 483.00.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050512Intercostal · corrodedLT AND RT STRINGER 27 INTERCOSTALS ARE CORRODED BETWEEN FS 349.00 AND 364.00.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WVER2019050511Frame · corrodedFS 319.70 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, FrameSDR WVER2019050510Frame · corrodedFS 333.00 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, FrameSDR WVER2019050418Structure · corrodedFS280.0 CIRCUMFRENCIAL JOINT CORRODED BETWEEN STRINGER 25R AND 26L.May 4, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WVER2019050309Stringer · corrodedSTRINGER 26R HAS TWO SMALL AREAS OF CORROSION BETWEEN FS 295.00 AND 310.00.May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR WVER2019050308Longeron · corrodedCORROSION ON STRINGER 25R AFT OF FS 333.00.May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR WVER2019050307Stringer · corrodedCORROSION ON STRINGER 26R AFT OF FS 333.00.May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR WVER2019050306Stringer · corrodedCORROSION ON STRINGER 25R FWD OF F.S. 333.00.May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR WVER2019050205Seat Track · corrodedSEAT RAIL AT LBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.May 2, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050204Seat Track · corrodedSEAT RAIL AT RBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.May 2, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050103Floor Support · corrodedPERFORMED A MAJOR REPAIR BY REMOVING AND INSTALLING THE FS 280.00 FORWARD FLOOR SUPPORT ANGLE P/N: CC670-34094-1S, DUE TO CORROSION. IAW SRM 51-40-11-001-001-A01, 51-40-06-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. REF MWC JOB# 41523351 OP# 1May 1, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WVER2019042500402Seat Track · corrodedSEAT TRACK IS CORRODED IN SEVERAL LOCATIONS AT RBL 9.0 AND F.S. 477.00.Apr 25, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019042501Seat Track · corrodedSEAT RAIL AT RBL 9.0 AT APPROX FS 349.00 IS CORRODED IN SEVERAL LOCATIONS.Apr 25, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WVER2019050516Crossbeam · corrodedFS 280 LT AND RT CROSSBEAMS CORRODED.Apr 19, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WVER2019051421Support Angle · corrodedSERVICE DOOR CUT OUT MOUNTING ANGLE AND THRESHOLD BRACKET SUPPORT ANGLES ARE CORRODED.Apr 16, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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