# Service difficulty reports: N244LR

A list on [N244LR](https://openairdocs.org/aircraft/N244LR.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 · 92 reports

- [SDR SWIA20250702](https://openairdocs.org/sdr/SWIA20250702.md): Landing · cracked · Jul 2, 2025 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > RIGHT 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.
- [SDR SWI2025F01507](https://openairdocs.org/sdr/SWI2025F01507.md): Slat Track · worn · Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > RH 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 27-50-00
- [SDR SWI2025F01506](https://openairdocs.org/sdr/SWI2025F01506.md): Slat Track · worn · Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT 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 27-50-00-7
- [SDR SWI2025F01505](https://openairdocs.org/sdr/SWI2025F01505.md): Slat Track · worn · Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > LH 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.
- [SDR SWIA2025110400624](https://openairdocs.org/sdr/SWIA2025110400624.md): Slat Track · worn · Jun 24, 2025 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > LEFT 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 GOOD
- [SDR MASA2024061600060](https://openairdocs.org/sdr/MASA2024061600060.md): Battery Pack · discharged · Jun 16, 2024 · N244LR · Cndair CL6002D24 · Emergency Lighting
  > ALL EMER LIGHTS INOP/BATT DRAIN/SW OFF. ALOWED BATTERIES TO CHARGE/FA SW LEFT ON
- [SDR MASA2023090800113](https://openairdocs.org/sdr/MASA2023090800113.md): Fire Loop · failed · Sep 8, 2023 · N244LR · Cndair CL6002D24 · Fire Detection
  > LH BLEED DUCT WARNING/ ANTI-ICE OFF. REPOSITIONED FIRE LOOPS PREFORMED ENG RUNS NO FURTHER DEFECT
- [SDR MASA2023072300095](https://openairdocs.org/sdr/MASA2023072300095.md): Unknown · unknown · Jul 23, 2023 · N244LR · Cndair CL6002D24 · Engine Bleed Air System
  > RT BLEED DUCT WARNING MESSAGE- MX SECURED A LOOSE DUCTING CLAMP
- [SDR MASA2023051100073](https://openairdocs.org/sdr/MASA2023051100073.md): Unknown · unknown · May 11, 2023 · N244LR · Cndair CL6002D24 · Air Conditioning System
  > LH BLEED DUCT CAUT/DEPRESSURIZATON EMER DECLARED. INSP LOOP MT142 AND ACM PRE COOLER, NO DEFECTS.
- [SDR MASA2022032500086](https://openairdocs.org/sdr/MASA2022032500086.md): Light · inoperative · Mar 25, 2022 · N244LR · Cndair CL6002D24 · Emergency Lighting
  > CAPT.'S FLASHLIGHT RED LED INOP. PLACED ON MEL.
- [SDR MASA20210907397](https://openairdocs.org/sdr/MASA20210907397.md): Floor Panel · damaged · Sep 7, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor Panel
  > PASSENGER 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 231BL
- [SDR MASA20210907396](https://openairdocs.org/sdr/MASA20210907396.md): Skin · corroded · Sep 6, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR MASA20210831390](https://openairdocs.org/sdr/MASA20210831390.md): Skin · damaged · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LOWER 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.
- [SDR MASA20210831389](https://openairdocs.org/sdr/MASA20210831389.md): Access Panel · damaged · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Trailing Edge Flaps
  > RH 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 69
- [SDR MASA20210831388](https://openairdocs.org/sdr/MASA20210831388.md): Floor Panel · delaminated · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor Panel
  > FWD 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.
- [SDR MASA20210831387](https://openairdocs.org/sdr/MASA20210831387.md): Slat Track · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > SLAT 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 69-2021-131
- [SDR MASA20210831386](https://openairdocs.org/sdr/MASA20210831386.md): Slat Track · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > SLAT 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.
- [SDR MASA20210831385](https://openairdocs.org/sdr/MASA20210831385.md): Slat Track · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Leading Edge Devices
  > SLAT 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.
- [SDR MASA20210831384](https://openairdocs.org/sdr/MASA20210831384.md): Fitting · damaged · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FS343.04 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/F
- [SDR MASA20210831383](https://openairdocs.org/sdr/MASA20210831383.md): Floor Support · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPPER 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.
- [SDR MASA20210831382](https://openairdocs.org/sdr/MASA20210831382.md): Floor Support · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPPER 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.
- [SDR MASA20210831381](https://openairdocs.org/sdr/MASA20210831381.md): Skin · dented · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Spoilers
  > LH 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.
- [SDR MASA20210831380](https://openairdocs.org/sdr/MASA20210831380.md): Floor Support · corroded · Aug 30, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR MASA20210827377](https://openairdocs.org/sdr/MASA20210827377.md): Floor Panel · damaged · Aug 26, 2021 · N244LR · Cndair CL6002D24 · Fuselage Floor Panel
  > PASSENGER 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.
- [SDR MASA20210827378](https://openairdocs.org/sdr/MASA20210827378.md): Skin · corroded · Aug 19, 2021 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR MASA20210827379](https://openairdocs.org/sdr/MASA20210827379.md): Floor Support · corroded · Aug 16, 2021 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > THE 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.
- [SDR MASA2021061100137](https://openairdocs.org/sdr/MASA2021061100137.md): Bulb · inoperative · Jun 11, 2021 · N244LR · Cndair CL6002D24 · Emergency Lighting
  > TWO EMERGENCY EXIT LIGHTS INOP IN GALLEY. REPLACED BULBS
- [SDR MASA2019122512205](https://openairdocs.org/sdr/MASA2019122512205.md): Landing Gear · inoperative · Dec 25, 2019 · N244LR · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE, NLG WOULD NOT RETRACT. PLACED ON MEL.
- [SDR MASA2019122092189](https://openairdocs.org/sdr/MASA2019122092189.md): Selector Valve · inoperative · Dec 19, 2019 · N244LR · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING REPLACED LAND GEAR SELECTOR VALVE
- [SDR WVER2019051119](https://openairdocs.org/sdr/WVER2019051119.md): Doubler · corroded · May 11, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > PERFORMED 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, 51-47-06
- [SDR WVER2019051118](https://openairdocs.org/sdr/WVER2019051118.md): Intercostal · chafed · May 11, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PERFORMED 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.
- [SDR WVER2019051017](https://openairdocs.org/sdr/WVER2019051017.md): Skin Panel · chafed · May 10, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR WVER2019050515](https://openairdocs.org/sdr/WVER2019050515.md): Seat Track · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL 9, FS 661-672 IS CORRODED IN SEVERAL LOCATIONS.
- [SDR WVER2019050514](https://openairdocs.org/sdr/WVER2019050514.md): Seat Track · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 661.00+32 AND 672.00.
- [SDR WVER2019050513](https://openairdocs.org/sdr/WVER2019050513.md): Seat Track · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 374.00 AND 483.00.
- [SDR WVER2019050512](https://openairdocs.org/sdr/WVER2019050512.md): Intercostal · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LT AND RT STRINGER 27 INTERCOSTALS ARE CORRODED BETWEEN FS 349.00 AND 364.00.
- [SDR WVER2019050511](https://openairdocs.org/sdr/WVER2019050511.md): Frame · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 319.70 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.
- [SDR WVER2019050510](https://openairdocs.org/sdr/WVER2019050510.md): Frame · corroded · May 5, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 333.00 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.
- [SDR WVER2019050418](https://openairdocs.org/sdr/WVER2019050418.md): Structure · corroded · May 4, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS280.0 CIRCUMFRENCIAL JOINT CORRODED BETWEEN STRINGER 25R AND 26L.
- [SDR WVER2019050309](https://openairdocs.org/sdr/WVER2019050309.md): Stringer · corroded · May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R HAS TWO SMALL AREAS OF CORROSION BETWEEN FS 295.00 AND 310.00.
- [SDR WVER2019050308](https://openairdocs.org/sdr/WVER2019050308.md): Longeron · corroded · May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 25R AFT OF FS 333.00.
- [SDR WVER2019050307](https://openairdocs.org/sdr/WVER2019050307.md): Stringer · corroded · May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26R AFT OF FS 333.00.
- [SDR WVER2019050306](https://openairdocs.org/sdr/WVER2019050306.md): Stringer · corroded · May 3, 2019 · N244LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 25R FWD OF F.S. 333.00.
- [SDR WVER2019050205](https://openairdocs.org/sdr/WVER2019050205.md): Seat Track · corroded · May 2, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.
- [SDR WVER2019050204](https://openairdocs.org/sdr/WVER2019050204.md): Seat Track · corroded · May 2, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT RBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.
- [SDR WVER2019050103](https://openairdocs.org/sdr/WVER2019050103.md): Floor Support · corroded · May 1, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PERFORMED 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# 1
- [SDR WVER2019042500402](https://openairdocs.org/sdr/WVER2019042500402.md): Seat Track · corroded · Apr 25, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED IN SEVERAL LOCATIONS AT RBL 9.0 AND F.S. 477.00.
- [SDR WVER2019042501](https://openairdocs.org/sdr/WVER2019042501.md): Seat Track · corroded · Apr 25, 2019 · N244LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT RBL 9.0 AT APPROX FS 349.00 IS CORRODED IN SEVERAL LOCATIONS.
- [SDR WVER2019050516](https://openairdocs.org/sdr/WVER2019050516.md): Crossbeam · corroded · Apr 19, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 LT AND RT CROSSBEAMS CORRODED.
- [SDR WVER2019051421](https://openairdocs.org/sdr/WVER2019051421.md): Support Angle · corroded · Apr 16, 2019 · N244LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR CUT OUT MOUNTING ANGLE AND THRESHOLD BRACKET SUPPORT ANGLES ARE CORRODED.

Next page: https://openairdocs.org/aircraft/N244LR/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 = 'N244LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N244LR/reports

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