# Service difficulty reports: N709BR

A list on [N709BR](https://openairdocs.org/aircraft/N709BR.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 5 · 206 reports

- [SDR SWIA2026052576032](https://openairdocs.org/sdr/SWIA2026052576032.md): Controller · faulted · May 25, 2026 · N709BR · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING 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 RELIABIL
- [SDR SWIA2026022375305](https://openairdocs.org/sdr/SWIA2026022375305.md): Floor Support · corroded · Nov 13, 2025 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT 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", REMAININ
- [SDR SWIA2026022375304](https://openairdocs.org/sdr/SWIA2026022375304.md): Frame · cracked · Oct 25, 2025 · N709BR · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 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 FROM
- [SDR SWIA2026022375303](https://openairdocs.org/sdr/SWIA2026022375303.md): Stringer · cracked · Oct 25, 2025 · N709BR · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L CRACKED AT FS379 (C-CHECK RO 02/20/2026)REPAIRED STGR 3L AT FS 379.00 IAW CRJ200 SRM 53-00-03
- [SDR SWIA2026022375306](https://openairdocs.org/sdr/SWIA2026022375306.md): Seat Track · corroded · Oct 24, 2025 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 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-
- [SDR SWIA20250702001](https://openairdocs.org/sdr/SWIA20250702001.md): Skin · damaged · Jul 1, 2025 · N709BR · Cndair CL6002B19 · Elevator, Plate/Skin
  > DURING 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 RIB
- [SDR SWIA202411151010](https://openairdocs.org/sdr/SWIA202411151010.md): Floor Support · corroded · Oct 10, 2024 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/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-F
- [SDR SWIA2024102310](https://openairdocs.org/sdr/SWIA2024102310.md): Pressure Deck · corroded · Oct 10, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > R/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-FS4
- [SDR SWIA20241009](https://openairdocs.org/sdr/SWIA20241009.md): Pressure Deck · corroded · Oct 9, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION 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 51
- [SDR SWIA2024101000009](https://openairdocs.org/sdr/SWIA2024101000009.md): Pressure Deck · corroded · Oct 9, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ON THE R/H PRESSURE FLOOR JUST FWD OF FS559.0 (FILED OPEN)
- [SDR SWIA20241008](https://openairdocs.org/sdr/SWIA20241008.md): Vane · damaged · Oct 8, 2024 · N709BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RH 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 REPA
- [SDR SWIA20241008001](https://openairdocs.org/sdr/SWIA20241008001.md): Vane · damaged · Oct 8, 2024 · N709BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP VANE HAS DAMAGE ON THE LEADING EDGE APPROXIMATELY WS135.00 (JUST OUTBOARD OF THE RIGHT #2 FLAP ACTUATOR) (FILED OPEN)
- [SDR SWIA2024110802](https://openairdocs.org/sdr/SWIA2024110802.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION 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
- [SDR SWI2024F01105](https://openairdocs.org/sdr/SWI2024F01105.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > 5 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 T
- [SDR SWI2024F01104](https://openairdocs.org/sdr/SWI2024F01104.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > 2 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 WI
- [SDR SWI2024F01103](https://openairdocs.org/sdr/SWI2024F01103.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > 2 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 REF
- [SDR SWI2024F01102](https://openairdocs.org/sdr/SWI2024F01102.md): Floor Support · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 MEASUREMENT
- [SDR SWIA2024F01032](https://openairdocs.org/sdr/SWIA2024F01032.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > 2 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 WITH
- [SDR SWIA2024F01031](https://openairdocs.org/sdr/SWIA2024F01031.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION 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 PA
- [SDR SWIA2024F01030](https://openairdocs.org/sdr/SWIA2024F01030.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > 2 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 REFER
- [SDR SWIA2024F01029](https://openairdocs.org/sdr/SWIA2024F01029.md): Pressure Deck · corroded · Oct 2, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION 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 W
- [SDR SWIA20241001](https://openairdocs.org/sdr/SWIA20241001.md): Mount · cracked · Oct 1, 2024 · N709BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO 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.
- [SDR SWIA20241001001](https://openairdocs.org/sdr/SWIA20241001001.md): Track · cracked · Oct 1, 2024 · N709BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK, LOWER MOUNT CHANNEL NEAR LIGHT SWITCH CRACKED. (FILED OPEN)
- [SDR SWIA202411040930](https://openairdocs.org/sdr/SWIA202411040930.md): Pressure Blkhd · gouged · Sep 30, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR 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-
- [SDR SWIA20241023930](https://openairdocs.org/sdr/SWIA20241023930.md): Pressure Blkhd · gouged · Sep 30, 2024 · N709BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR 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 2024-10
- [SDR SWIA202411040929](https://openairdocs.org/sdr/SWIA202411040929.md): Access Panel · corroded · Sep 29, 2024 · N709BR · Cndair CL6002B19 · Wing, Plate/Skin
  > CORROSION 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. P
- [SDR SWIA20241023929](https://openairdocs.org/sdr/SWIA20241023929.md): Access Panel · corroded · Sep 29, 2024 · N709BR · Cndair CL6002B19 · Fuel Storage
  > CORROSION 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. PER
- [SDR SWIA202053020](https://openairdocs.org/sdr/SWIA202053020.md): Windshield · failed · Oct 3, 2020 · N709BR · Cndair CL6002B19 · Flight Compartment Windows
  > CLIMBING 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.
- [SDR SWIA2020032649398](https://openairdocs.org/sdr/SWIA2020032649398.md): Stiffener · cracked · Mar 4, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPLACE 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 DETAILS
- [SDR SWIA2020032649396](https://openairdocs.org/sdr/SWIA2020032649396.md): Skin · corroded · Feb 26, 2020 · N709BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT 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 R
- [SDR SWIA2020032649395](https://openairdocs.org/sdr/SWIA2020032649395.md): Skin · corroded · Feb 26, 2020 · N709BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT 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. SEE
- [SDR SWIA2020032649394](https://openairdocs.org/sdr/SWIA2020032649394.md): Fitting · cracked · Feb 23, 2020 · N709BR · Cndair CL6002B19 · Wing Spar
  > L/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 BOMBARDIER
- [SDR SWIA2020032649393](https://openairdocs.org/sdr/SWIA2020032649393.md): Rib · cracked · Feb 23, 2020 · N709BR · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > L/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.
- [SDR SWIA2020032649392](https://openairdocs.org/sdr/SWIA2020032649392.md): Skin · chafed · Feb 23, 2020 · N709BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > L/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, C
- [SDR SWIA2020032649407](https://openairdocs.org/sdr/SWIA2020032649407.md): Seat Track · corroded · Feb 19, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * 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
- [SDR SWIA2020032649391](https://openairdocs.org/sdr/SWIA2020032649391.md): Hinge · worn · Feb 19, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Door Hinge
  > REMOVE/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 DETAILS
- [SDR SWIA2020032649410](https://openairdocs.org/sdr/SWIA2020032649410.md): Anchor Fitting · corroded · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Passenger/Crew Doors
  > * 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.
- [SDR SWIA2020032649390](https://openairdocs.org/sdr/SWIA2020032649390.md): Trunnion · cracked · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Main Landing Gear Attach Section
  > WHILE 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
- [SDR SWIA2020032649389](https://openairdocs.org/sdr/SWIA2020032649389.md): Trunnion · cracked · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Main Landing Gear Attach Section
  > WHILE 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.
- [SDR SWIA2020032649388](https://openairdocs.org/sdr/SWIA2020032649388.md): Skin · damaged · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Wing, Plate/Skin
  > * 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 DETAILS
- [SDR SWIA2020032649387](https://openairdocs.org/sdr/SWIA2020032649387.md): Skin · damaged · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Wing, Plate/Skin
  > * 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 DETAILS
- [SDR SWIA2020032649385](https://openairdocs.org/sdr/SWIA2020032649385.md): Anchor Fitting · corroded · Feb 13, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * 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 U
- [SDR SWIA2020032649384](https://openairdocs.org/sdr/SWIA2020032649384.md): Fitting · cracked · Feb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/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 DETAILS
- [SDR SWIA2020032649383](https://openairdocs.org/sdr/SWIA2020032649383.md): Fitting · cracked · Feb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/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 DETAILS
- [SDR SWIA2020032649382](https://openairdocs.org/sdr/SWIA2020032649382.md): Fitting · cracked · Feb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/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 DETAILS
- [SDR SWIA2020032649381](https://openairdocs.org/sdr/SWIA2020032649381.md): Intercostal · cracked · Feb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * 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 CAR
- [SDR SWIA2020032649380](https://openairdocs.org/sdr/SWIA2020032649380.md): Intercostal · cracked · Feb 12, 2020 · N709BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * 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 C
- [SDR SWIA2020032649409](https://openairdocs.org/sdr/SWIA2020032649409.md): Retainer · corroded · Feb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * 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 F
- [SDR SWIA2020032649408](https://openairdocs.org/sdr/SWIA2020032649408.md): Retainer · corroded · Feb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * 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 OU
- [SDR SWIA2020032649406](https://openairdocs.org/sdr/SWIA2020032649406.md): Seat Track · corroded · Feb 11, 2020 · N709BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * 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 FS55

Next page: https://openairdocs.org/aircraft/N709BR/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 = 'N709BR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N709BR/reports

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