N709BR

Service difficulty reports · 206

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 = 'N709BR' 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 SWIA2026052576032Controller · faultedWING OVHT WARNING MESSAGE. RAN THE QRH PROCEDURE AND STAYED OUT OF ICING CONDITIONS. (FLIGHT 6076)TROUBLESHOT THE WING OVHT MESSAGE IN REFERENCE TO FIM 30-10-00 FIG.103. NO FAULTS FOUND, SYSTEM NORMAL. REMOVED AND REPLACED THE ANTI-ICE CONTROLLER FOR RELIABILMay 25, 2026 · N709BR · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA2026022375305Floor Support · corrodedRIGHT UPPER SURFACE PRESSURE FLOOR SILL STRUCTURE SHOWING SIGN OF CORROSION AT BS 424 - 449. REMOVED, & TREATED CORROSION ON RT FLOOR SILL IAW REO 601R-53-41-666, REV C, SRM-51-21-11, SRM-51-25-06, & SRM-51-25-16. ORIGINAL THICKNESS MEASURED 0.080", REMAININNov 13, 2025 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022375304Frame · crackedBS 280 FRAME CRACKED AT STRINGER 3L REPAIRED THE FRAME IAW REO 601R-53-11-4041 REV --. ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS OF THE ISSUE DATE OF THIS REPAIR. THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROMOct 25, 2025 · N709BR · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022375303Stringer · crackedSTRINGER 3L CRACKED AT FS379 (C-CHECK RO 02/20/2026)REPAIRED STGR 3L AT FS 379.00 IAW CRJ200 SRM 53-00-03Oct 25, 2025 · N709BR · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2026022375306Seat Track · corrodedLBL 9 SEAT TRACK HAS CORROSION FROM BS409 - 409+128. ACCOMPLISHED A REPAIR ON THE SEAT TRACK BEAM IAW SRM 53-00-43, REPAIR 2, SRM 51-42-06, SRM 51-42-11, SRM 51-42-21, SRM 51-25-16, SRM 51-25-06, SRM 51-40-11, SRM 51-45-00, AMM 53-04-11-400-802, AND REO 601R-Oct 24, 2025 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20250702001Skin · damagedDURING LIGHTING STRIKE INSPECTION FOUND DAMAGE TO RH ELEVATOR TRAILING EDGE LOWER SKIN COMPLIED WITH REO 601R-55-21-609 REV"A" DATED: 2025-07-01 TEMPORARY DISPOSITION FOR BLENDED/TRIMMED LIGHTNING STRIKE DAMAGE TO RHS ELEVATOR TRAILING EDGE LOWER SKIN AT RIBJul 1, 2025 · N709BR · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202411151010Floor Support · corrodedR/H PRESSURE FLOOR SILL AT FS449.85 BLENDED CORROSION DAMAGE IS BEYOND ACCEPTABLE LIMITS OF REO 601R-53-41-666 REV "-C" DATED 2012-11-06. (FILED CLOSED)COMPLIED WITH REO 601R-53-41-3268 REV "--" DATED: 2024-10-13 REPAIR TO PRESSURE FLOOR SILL BETWEEN FS439.0-FOct 10, 2024 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024102310Pressure Deck · corrodedR/H PRESSURE FLOOR SILL AT FS449.85 BLENDED CORROSION DAMAGE IS BEYOND ACCEPTABLE LIMITS OF REO 601R-53-41-666 REV "-C" DATED 2012-11-06. (FILED OPEN)COMPLIED WITH REO 601R-53-41-3268 REV "--" DATED: 2024-10-13 REPAIR TO PRESSURE FLOOR SILL BETWEEN FS439.0-FS4Oct 10, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20241009Pressure Deck · corrodedCORROSION FOUND ON THE R/H PRESSURE FLOOR JUST FWD OF FS559.0 (FILED CLOSED)BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL BETWEEN JUST FWD FS559.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51Oct 9, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024101000009Pressure Deck · corrodedCORROSION FOUND ON THE R/H PRESSURE FLOOR JUST FWD OF FS559.0 (FILED OPEN)Oct 9, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20241008Vane · damagedRH FLAP VANE HAS DAMAGE ON THE LEADING EDGE APPROXIMATELY WS135.00 (JUST OUTBOARD OF THE RIGHT #2 FLAP ACTUATOR) (FILED CLOSED)DETERMINED LOCATION OF DAMAGE ON RH INBOARD FLAP VANE LEADING EDGE TO BE OUTBOARD OF FLAP STATION 137.012. PERFORMED TEMPORARY REPAOct 8, 2024 · N709BR · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20241008001Vane · damagedRH FLAP VANE HAS DAMAGE ON THE LEADING EDGE APPROXIMATELY WS135.00 (JUST OUTBOARD OF THE RIGHT #2 FLAP ACTUATOR) (FILED OPEN)Oct 8, 2024 · N709BR · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2024110802Pressure Deck · corrodedCORROSION FOUND ON L/H PRESSURE FLOOR AFT OF FS424.00 (MARKED WITH TAPE) (FILED CLOSED)BLENDED 2 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL AFT OF FS424.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01105Pressure Deck · corroded5 SPOTS OF CORROSION FOUND ON THE R/H PRESSURE FLOOR BETWEEN FS449.85 AND FS484.00. (MARKED WITH TAPE) (FILED CLOSED)BLENDED 5 SPOTS CORROSION ON THE RH PRESSURE FLOOR SILL BETWEEN FS449.85 AND FS484.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING TOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01104Pressure Deck · corroded2 SPOTS OF CORROSION FOUND ON THE R/H PRESSURE FLOOR JUST AFT OF FS484.00 (MARKED WITH TAPE) (FILED CLOSED)BLENDED 2 SPOTS CORROSION ON THE RH PRESSURE FLOOR SILL AFT OF FS484.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WIOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01103Pressure Deck · corroded2 SPOTS OF CORROSION FOUND ON THE L/H PRESSURE FLOOR AFT OF FS473.15 (MARKED WITH TAPE) (FILED CLOSED)BLENDED 2 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL AFT OF FS473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01102Floor Support · corrodedCORROSION ON THE L/H PRESSURE FLOOR BETWEEN FS529.0 TO FS559.0, 3 SPOTS. (MARKED WITH TAPE) (FILED CLOSED)BLENDED 3 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL FS 529.0 TO FS 559.0 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENTOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024F01032Pressure Deck · corroded2 SPOTS OF CORROSION FOUND ON THE R/H PRESSURE FLOOR JUST AFT OF FS484.00 (MARKED WITH TAPE) (FILED OPEN)BLENDED 2 SPOTS CORROSION ON THE RH PRESSURE FLOOR SILL AFT OF FS484.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITHOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024F01031Pressure Deck · corrodedCORROSION FOUND ON L/H PRESSURE FLOOR AFT OF FS424.00 (MARKED WITH TAPE) (FILED OPEN)BLENDED 2 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL AFT OF FS424.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PAOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024F01030Pressure Deck · corroded2 SPOTS OF CORROSION FOUND ON THE L/H PRESSURE FLOOR AFT OF FS473.15 (MARKED WITH TAPE) (FILED OPEN)BLENDED 2 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL AFT OF FS473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFEROct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024F01029Pressure Deck · corrodedCORROSION ON THE L/H PRESSURE FLOOR BETWEEN FS529.0 TO FS559.0, 3 SPOTS. (MARKED WITH TAPE) (FILED OPEN)BLENDED 3 SPOTS CORROSION ON THE LH PRESSURE FLOOR SILL FS 529.0 TO FS 559.0 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WOct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20241001Mount · crackedCARGO DOOR FWD TRACK, LOWER MOUNT CHANNEL NEAR LIGHT SWITCH CRACKED. (FILED CLOSED)REMOVED AND REPLACED CARGO DOOR FWD TRACK LOWER MOUNT CHANNEL NEAR LIGHT SWITCH WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.Oct 1, 2024 · N709BR · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA20241001001Track · crackedCARGO DOOR FWD TRACK, LOWER MOUNT CHANNEL NEAR LIGHT SWITCH CRACKED. (FILED OPEN)Oct 1, 2024 · N709BR · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202411040930Pressure Blkhd · gougedREAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS 5 GOUGES ON THE BULKHEAD FACE AND 6 GOUGED RIVET HEADS. (FILED CLOSED)REPAIRED REAR PRESSURE BULKHEAD FS621.00 FWD FACE 5 GOUGES AND 6 GOUGED FASTENER HEADS WITH REFERENCE TO REO 601R-53-61-8238 REV "--" DATED 2024-Sep 30, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA20241023930Pressure Blkhd · gougedREAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS 5 GOUGES ON THE BULKHEAD FACE AND 6 GOUGED RIVET HEADS. (FILED OPEN)REPAIRED REAR PRESSURE BULKHEAD FS621.00 FWD FACE 5 GOUGES AND 6 GOUGED FASTENER HEADS WITH REFERENCE TO REO 601R-53-61-8238 REV "--" DATED 2024-10Sep 30, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202411040929Access Panel · corrodedCORROSION FOUND ON FUEL ACCESS PANEL OPENING 610BB. FWD JUST OUTBOARD OF CENTER. (MARKED) (FILED CLOSED)REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 610BB, FWD JUST OUTBOARD OF CENTER WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DATED 2014-02-05. PSep 29, 2024 · N709BR · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20241023929Access Panel · corrodedCORROSION FOUND ON FUEL ACCESS PANEL OPENING 610BB. FWD JUST OUTBOARD OF CENTER. (MARKED) (FILED OPEN)REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 610BB, FWD JUST OUTBOARD OF CENTER WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DATED 2014-02-05. PERSep 29, 2024 · N709BR · Cndair CL6002B19 · Fuel StorageSDR SWIA202053020Windshield · failedCLIMBING THRU 12,000 I NOTICED ARCING ON THE LOWER PORTION OF THE CAPTAINS WINDSHIELD AND SHORTLY AFTER THAT THE WINDSHIELD SHATTERED. WE COMPLIED WITH THE QRH 11-19 PROCEDURE AND THEN RETURNED TO KMLU AND LANDED WITHOUT INCIDENT. FILED CLOSED RO 10/5/2020. Oct 3, 2020 · N709BR · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2020032649398Stiffener · crackedREPLACE CRACKED STIFFENER AT FS621 AFT BULKHEAD AT LBL 36 PART # 601R36008-51 (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW STIFFENER AT LBL 36 REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILSMar 4, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649396Skin · corrodedRT O/B FLAP UPPER SKIN SEVERAL RIVETS WITH FRETTING CORROSION UNDER RIVET HEAD ON THE FOLLOWING RIBS; W/STA 226.15, W/STA 235.96, W/STA 254.96. ALSO ON REAR SPAR FROM W/STA 226.15 TO W/STA 278.00 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED FASTENER ON RFeb 26, 2020 · N709BR · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020032649395Skin · corrodedLT O/B FLAP UPPER SKIN SEVERAL RIVETS WITH FRETTING CORROSION UNDER RIVET HEADS ON AFT SPAR BETWEEN W/STA 226.15 TO W/STA 234.25 & W/STA 245.84 TO W/STA 254.96. (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED FASTENER ON LH OTBD FLAP UPPER SKIN REF REO. SEEFeb 26, 2020 · N709BR · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020032649394Fitting · crackedL/H WING AUX SPAR END ASSY AT WS.58.88 HAS CRACKED VERTICAL JOINT FITTING P/N 601R10205-29 . (C-CHECK) RO 3/25/2020 REMOVED LH WING AUX SPAR END DICREAPANT VERTICLE JOINT FITTING AT WS 58.88 AND INSTALLED REPLACEMENT FITTING REF CRJ 200 SRM AND BOMBARDIERFeb 23, 2020 · N709BR · Cndair CL6002B19 · Wing SparSDR SWIA2020032649393Rib · crackedL/H WING REAR SPAR BATT RIB AT WS.53.60 HAS CRAK IN UPPER AFT CORNER . (C-CHECK) RO 3/25/2020 REPAIRED THE BATT RIB ASSY AT WS 53.60 LHS PER REO.Feb 23, 2020 · N709BR · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020032649392Skin · chafedL/H APRON SKIN PANEL HAS DEEP CHAFE DAMAGE ALONG CONTACT LINE WITH WING INBD UPPER PANELS SEALS . (C-CHECK) RO 3/25/2020 BLENDED OUT DAMAGED AREA OF L/H APRON SKIN REF REO. BLENDED AREA FOUND TO BE OUT OF LIMITS REF R.E.O. REPAIRED L/H APRON SKIN PANEL, CFeb 23, 2020 · N709BR · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020032649407Seat Track · corroded* FLOOR SEAT RAIL FROM FS409+128 TO FS559, LBL9, IS CORRODED IN MULTIPLE SPOTS. (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR SEAT RAIL FROM FS409+128 TO FS559, LBL9. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK. REF CRJ 200 AMM TUC1234 Feb 19, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032649391Hinge · wornREMOVE/REPLACE/INSTALL PASSENGER DOOR HINGE HALF (FUSELAGE SIDE) LUG BORES ARE EXCESSIVELY WORN. (C-CHECK) RO 3/25/2020 INSTALLED NEW PAX DOOR PIANO HINGE ON FUSELAGE SIDE REF CRJ200 SRM AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILSFeb 19, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2020032649410Anchor Fitting · corroded* FORWARD PAX DOOR ANCHOR FITTING IS CORRODED, MARKED. (C-CHECK) RO 3/25/2020 NO ALLOWABLE LIMITS FOR FITTING, REPLACED FWD PAX DOOR ANCHOR FITTING, SERRATED PLATE, SWIVLE LEVER AND HARDWARE REF CRJ 200 AMM, SEE CONTINUE CARD FOR WORK PERFORMED.Feb 13, 2020 · N709BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020032649390Trunnion · crackedWHILE COMPLYING WITH SB 601R-57-046 ON R/H MLG TRUNNION, FOUND 1EA OVERSIZE HOLE ( HOLE #14 ) AND 1EA HOLE WITH CRACK INDICATION ( HOLE #22 ) (C-CHECK) RO 3/25/2020 REPAIRED R/H MLG TRUNNION 2 FASTENER HOLES REF BOMBARDIER REO. SEE CONTINUATION CARD FOR Feb 13, 2020 · N709BR · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA2020032649389Trunnion · crackedWHILE COMPLYING SB 601R-57-046 ON L/H MLG TRUNNION FOUND 6EA HOLES WITH CRACK INDICATIONS. (HOLES #16-21) (C-CHECK) RO 3/25/2020 REPAIRED L/H MLG TRUNNION 6EA HOLES WITH CRACK INDICATIONS. (HOLES #16-21) REF. REO.Feb 13, 2020 · N709BR · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA2020032649388Skin · damaged* LH WING €“ RADIUS OF LANDING FOR PANEL 550HB HAS SIGNS OF PITTING IN MULTIPLE LOCATIONS AROUND PERIPHERY. (C-CHECK) RO 3/25/2020 REPAIRED L/H WING LANDING FOR ACCESS PANEL 550HB REF REO SEE. CONTINUATION CARD FOR DETAILSFeb 13, 2020 · N709BR · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020032649387Skin · damaged* LH WING €“ LANDING FOR ACCESS PANEL 540BB HAS PITTING (AREA MARKED). (C-CHECK) RO 3/25/2020 REPAIRED L/H WING ACCESS PANEL CUTOUT AT 540BB REF REO. SEE CONTINUATION CARD FOR DETAILSFeb 13, 2020 · N709BR · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020032649385Anchor Fitting · corroded* INTERCOSTAL FORWARD OF THE PAX DOOR FORWARD ANCHOR FITTING IS CORRODED, MARKED. (C-CHECK) RO 3/25/2020 COMPLIED WITH ALL STEPS LISTED IN BOMBARDIER REO. DISPOSITION 1: ENSURED BLEND OUTS OF CORROSION DAMAGE WERE PERFORMED IN ACCORDANCE WITH CRJ200 SRM UFeb 13, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649384Fitting · crackedL/H FS 625.0 CLIP IS CRACKED AT STR 15 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED THE L/H 625.0 CLIP AT STR 15. REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILSFeb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649383Fitting · crackedR/H FS 625.0 CLIP IS CRACKED AT STR 14 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED THE RH 625.0 CLIP AT STR 14. REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILSFeb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649382Fitting · crackedL/H FS 625.0 CLIP IS CRACKED AT STR 14 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED THE L/H 625.0 CLIP AT STR 14. REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILSFeb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649381Intercostal · cracked* INTERCOSTAL COMMON TO THE SKIN, BETWEEN FS621 AND FS625, STR14L, IS CRACKED. (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW INTERCOSTAL COMMON TO THE SKIN, BETWEEN FS621 AND FS625, STR14L REF CRJ 200 SRM, AND BOMBARDIER DRAWING. SEE CONTINUATION CARFeb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649380Intercostal · cracked* INTERCOSTAL COMMON TO THE SKIN, BETWEEN FS621 AND FS625, STR13L, IS CRACKED. (C-CHECK) RO 3/25/2020 REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW P/N: 601R350121-9 BETWEEN FS 621.00 AND FS 625.00 STGR 13L REF DWG, REF CRJ200 SRM. AND SEE CONTINUATION CFeb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020032649409Retainer · corroded* CORROSION ON LH SIDE SEAT RAIL TRIM RETAINER LOWER FLANGE BETWEEN FS409+18 AND FS409+70 (MARKED). (C-CHECK) RO 3/25/2020 REMOVED THE CORROSION FROM THE LH SIDE SEAT RAIL TRIM RETAINER FROM FS409.00+18 TO FS409.00+112 REFERENCE CRJ200 SRM. EVALUATED AND FFeb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032649408Retainer · corroded* CORROSION ON LH SIDE SEAT RAIL TRIM RETAINER LOWER FLANGE BETWEEN FS364 AND FS409+16 (MARKED). (C-CHECK) RO 3/25/2020 REMOVED THE CORROSION FROM THE LH SIDE SEAT RAIL TRIM RETAINER FROM FS364 TO FS409+16 REFERENCE CRJ200 SRM. EVALUATED AND FOUND TO BE OUFeb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032649406Seat Track · corroded* CORROSION ON RH SIDE SEAT TRACK BETWEEN FS548 AND FS559+23 (MARKED). (C-CHECK) RO 3/25/2020 REMOVED THE CORROSION FROM THE RH SIDE SEAT TRACK, FOUND TO BE OUT OF LIMITS REFERENCE CRJ200 SRM. REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS548 AND FS55Feb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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