# Service difficulty reports: N246LR

A list on [N246LR](https://openairdocs.org/aircraft/N246LR.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 3 · 128 reports

- [SDR SWIA2026101877759](https://openairdocs.org/sdr/SWIA2026101877759.md): None · none · Oct 18, 2026 · N246LR · Cndair CL6002D24 · Standard Practices/Structures
  > SMELL 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 BOT
- [SDR SWIA2026012875774](https://openairdocs.org/sdr/SWIA2026012875774.md): Skin · cracked · Jan 28, 2026 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FOUND 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 AN
- [SDR SWIA2025101675773](https://openairdocs.org/sdr/SWIA2025101675773.md): Skin · chafed · Oct 16, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT 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.
- [SDR SWIA2025101575784](https://openairdocs.org/sdr/SWIA2025101575784.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > RH 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 2
- [SDR SWIA2025101575783](https://openairdocs.org/sdr/SWIA2025101575783.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > RH 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)
- [SDR SWIA2025101575782](https://openairdocs.org/sdr/SWIA2025101575782.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > RH 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 A
- [SDR SWIA2025101575781](https://openairdocs.org/sdr/SWIA2025101575781.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > LH 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
- [SDR SWIA2025101575780](https://openairdocs.org/sdr/SWIA2025101575780.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > LH 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 27-81-43-2
- [SDR SWIA2025101575779](https://openairdocs.org/sdr/SWIA2025101575779.md): Roller · worn · Oct 15, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > LH 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 LIM
- [SDR SWIA2025101375776](https://openairdocs.org/sdr/SWIA2025101375776.md): Skin · corroded · Oct 13, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION 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. SEE
- [SDR SWIA2025101275777](https://openairdocs.org/sdr/SWIA2025101275777.md): Landing · cracked · Oct 12, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Structure
  > R/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, RE
- [SDR SWIA2025101275775](https://openairdocs.org/sdr/SWIA2025101275775.md): Skin · cracked · Oct 12, 2025 · N246LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > RIGHT 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-
- [SDR SWIA2025082275778](https://openairdocs.org/sdr/SWIA2025082275778.md): Roller · out of limits · Aug 22, 2025 · N246LR · Cndair CL6002D24 · Leading Edge Devices
  > COMPLY 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 27-81-43
- [SDR MASA202401050002](https://openairdocs.org/sdr/MASA202401050002.md): Window · failed · Jan 5, 2024 · N246LR · Cndair CL6002D24 · Flight Compartment Windows
  > FO WINDSHEILD SHATTERED RTF EMERGENCY DECLARED. CURRENTLY OOS - REPLACE WINDOW IN WORK.
- [SDR MASA2022112000260](https://openairdocs.org/sdr/MASA2022112000260.md): Lamp · inoperative · Nov 20, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > ROW 18 OVRHD CEILING EMER FLOOD LT INOP. RELAMPED.
- [SDR MASA2022091200229](https://openairdocs.org/sdr/MASA2022091200229.md): Switch · none · Sep 12, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > EMR LTS ON W SW IN ARMD POSTN RESET CIRCUIT BREAKER. PERFORMED OPERATION CHECK OF THE EMERGENCY LIGHTS. OPS CHECK GOOD.
- [SDR MASA2022041000102](https://openairdocs.org/sdr/MASA2022041000102.md): None · none · Apr 10, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > SVC DOOR EXIT SIGN 1 BULB INOP. REPLACED BULB.
- [SDR MASA2022041000101](https://openairdocs.org/sdr/MASA2022041000101.md): None · none · Apr 10, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > PAX DOOR EXIT SIGN 1 BULB INOP. REPLACED BULB
- [SDR MASA2022040700096](https://openairdocs.org/sdr/MASA2022040700096.md): None · none · Apr 7, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > LH FWD OVERWING EXTERNAL EMERGENCY EXIT WING LT INOPERATIVE.- PLACED ON MEL
- [SDR MASA2022040700095](https://openairdocs.org/sdr/MASA2022040700095.md): None · none · Apr 7, 2022 · N246LR · Cndair CL6002D24 · Emergency Lighting
  > LH AFT EXTERNAL OVERWING EXIT LIGHT INOPERATIVE. -PLACED ON MEL
- [SDR MASA2022021200046](https://openairdocs.org/sdr/MASA2022021200046.md): None · none · Feb 12, 2022 · N246LR · Cndair CL6002D24 · Smoke Detection
  > AFT LAV SMOKE DETECTOR WENT OFF IN FLIGHT (FALSE INDICATION). CLEANED SMOKE DETECTOR, OPS CHECK GOOD.
- [SDR MASA20211123568](https://openairdocs.org/sdr/MASA20211123568.md): None · none · Nov 23, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon Structure
  > RH 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.
- [SDR MASA20211123569](https://openairdocs.org/sdr/MASA20211123569.md): None · none · Nov 22, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin
  > RH 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, EA12-2021
- [SDR MASA20211119565](https://openairdocs.org/sdr/MASA20211119565.md): None · none · Nov 17, 2021 · N246LR · Cndair CL6002D24 · Nacelle/Pylon Structure
  > OUTBOARD 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 ASSEMBL
- [SDR MASA20211119564](https://openairdocs.org/sdr/MASA20211119564.md): None · none · Nov 17, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)
  > LOWER 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.
- [SDR MASA20211117561](https://openairdocs.org/sdr/MASA20211117561.md): None · none · Nov 16, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE 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 53-3
- [SDR MASA20211117560](https://openairdocs.org/sdr/MASA20211117560.md): None · none · Nov 16, 2021 · N246LR · Cndair CL600* · Aileron Tabs
  > SEVEN 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.
- [SDR MASA20211117559](https://openairdocs.org/sdr/MASA20211117559.md): None · none · Nov 16, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE 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.
- [SDR MASA20211115558](https://openairdocs.org/sdr/MASA20211115558.md): None · dented · Nov 12, 2021 · N246LR · Cndair CL6002D24 · Aileron Tabs
  > NBOARD 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 80-2021-153
- [SDR MASA20211112557](https://openairdocs.org/sdr/MASA20211112557.md): None · none · Nov 12, 2021 · N246LR · Cndair CL600* · Nacelle/Pylon Structure
  > R/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 54-23-10-001
- [SDR MASA20211111556](https://openairdocs.org/sdr/MASA20211111556.md): None · none · Nov 11, 2021 · N246LR · Cndair CL6002D24 · Aileron Tabs
  > WEAR 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.
- [SDR MASA20211109554](https://openairdocs.org/sdr/MASA20211109554.md): None · none · Nov 9, 2021 · N246LR · Cndair CL6002D24 · Trailing Edge Flaps
  > LH 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
- [SDR MASA20211109553](https://openairdocs.org/sdr/MASA20211109553.md): None · none · Nov 9, 2021 · N246LR · Cndair CL6002D24 · Doors
  > OUTER 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 EDG
- [SDR MASA20211109552](https://openairdocs.org/sdr/MASA20211109552.md): None · damaged · Nov 9, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)
  > AFT 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.
- [SDR MASA20211109551](https://openairdocs.org/sdr/MASA20211109551.md): None · damaged · Nov 9, 2021 · N246LR · Cndair CL6002D24 · Wing Structure
  > DAMAGE 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.
- [SDR MASA20211109550](https://openairdocs.org/sdr/MASA20211109550.md): None · dented · Nov 8, 2021 · N246LR · Cndair CL6002D24 · Wing Structure
  > FUSELAGE 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.
- [SDR MASA20211105529](https://openairdocs.org/sdr/MASA20211105529.md): None · damaged · Nov 5, 2021 · N246LR · Cndair CL600* · Air Conditioning Doors
  > THE 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 SERVICE
- [SDR MASA20211105528](https://openairdocs.org/sdr/MASA20211105528.md): None · none · Nov 5, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)
  > WEAR 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 53
- [SDR MASA20211105531](https://openairdocs.org/sdr/MASA20211105531.md): None · corroded · Nov 4, 2021 · N246LR · Cndair CL600* · Doors
  > PASSENGER 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".
- [SDR MASA20211105530](https://openairdocs.org/sdr/MASA20211105530.md): None · corroded · Nov 4, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE 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 69-2021-185
- [SDR MASA20211105537](https://openairdocs.org/sdr/MASA20211105537.md): None · corroded · Nov 2, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > FUSELAGE 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.
- [SDR MASA20211105535](https://openairdocs.org/sdr/MASA20211105535.md): None · none · Nov 2, 2021 · N246LR · Cndair CL600* · Doors
  > PASSENGER 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 DOOR
- [SDR MASA20211102522](https://openairdocs.org/sdr/MASA20211102522.md): None · cracked · Nov 2, 2021 · N246LR · Cndair CL600* · Doors
  > PASSENGER 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.
- [SDR MASA20211105533](https://openairdocs.org/sdr/MASA20211105533.md): Doubler · corroded · Nov 1, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > DOUBLER 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 L
- [SDR MASA20211102523](https://openairdocs.org/sdr/MASA20211102523.md): Doubler · corroded · Nov 1, 2021 · N246LR · Cndair CL600* · Fuselage Structure (General)
  > DOUBLER 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
- [SDR MASA20220329145](https://openairdocs.org/sdr/MASA20220329145.md): None · corroded · Oct 28, 2021 · N246LR · Cndair CL6002D24 · Standard Practices/Structures
  > CORROSION 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 51-42-06
- [SDR MASA20220329143](https://openairdocs.org/sdr/MASA20220329143.md): Intercostal · corroded · Oct 28, 2021 · N246LR · Cndair CL6002D24 · Standard Practices/Structures
  > CORROSION 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.
- [SDR MASA20220329141](https://openairdocs.org/sdr/MASA20220329141.md): None · corroded · Oct 28, 2021 · N246LR · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION 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-A01
- [SDR MASA20211026519](https://openairdocs.org/sdr/MASA20211026519.md): Skin · cracked · Oct 26, 2021 · N246LR · Cndair CL6002D24 · Wing, Fuselage Attach Fittings
  > LEADING 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 83-2021-048
- [SDR MASA20220329149](https://openairdocs.org/sdr/MASA20220329149.md): None · corroded · Oct 25, 2021 · N246LR · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION 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 53-00-49

Next page: https://openairdocs.org/aircraft/N246LR/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 = 'N246LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N246LR/reports

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