# Service difficulty reports: N699BR

A list on [N699BR](https://openairdocs.org/aircraft/N699BR.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 · 148 reports

- [SDR SWIA2026082177613](https://openairdocs.org/sdr/SWIA2026082177613.md): Seat Track · corroded · Aug 21, 2026 · N699BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON RT SEAT TRACK BTWN BS 529 - 559.16. REMOVED AND INSTALLED A NEW SEAT TRACK IAW SRM 51-41-02.
- [SDR SWIA2026082177612](https://openairdocs.org/sdr/SWIA2026082177612.md): Seat Track · chafed · Aug 21, 2026 · N699BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT UPPER SEAT TRACK FOUND CHAFED BETWEEN BS 544 - 559. REMOVED & REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, REO 601R-53-00-764, & SRM 51-41-02.
- [SDR SWIA2026082077611](https://openairdocs.org/sdr/SWIA2026082077611.md): Pressure Deck · cracked · Aug 20, 2026 · N699BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK IN THE PRESSURE FLOOR AT BS 525, JUST BELOW THE LEFT SILL NEAR LBL 36. THE PRESSURE FLOOR WAS REPAIRED IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-15, & SRM 51-23-00.
- [SDR SWIA2026082077610](https://openairdocs.org/sdr/SWIA2026082077610.md): Frame · corroded · Aug 20, 2026 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME, BS 379, S19L POSSIBLE CORROSION. THE FRAME WAS REWORKED & REPAIRED IAW SRM 53-00-15, PAGE 204, FIGURE 202.
- [SDR SWIA2026081977609](https://openairdocs.org/sdr/SWIA2026081977609.md): Frame · corroded · Aug 19, 2026 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > EVALUATION OF POSSIBLE CORROSION ON FRAME, BS 589, STRINGERS 21L - 21R. REMOVED AND REPLACED THE FRAME SECTOR, BS 589 BWTN S21L - 21R IAW SRM 51-42-06.
- [SDR SWIA2026012775099](https://openairdocs.org/sdr/SWIA2026012775099.md): Actuator · failed · Jan 27, 2026 · N699BR · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL CAUTION AT FLAPS 20 COMING INTO ORD (FLIGHT 5402) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31611749. SEE CP 31611779 FOR FLAP FAIL AD SEE CP 31612902 FOR LT FLAP DRIVE LINE TORQUE CHECKED. SEE CP 31612918 FOR REPLACEMENT OF LT FLAP ACTUATOR N
- [SDR SWI2025F01321](https://openairdocs.org/sdr/SWI2025F01321.md): Bushing · damaged · Sep 10, 2025 · N699BR · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > WHILE REMOVING LH MLG ASSY DAMAGED OCCURRED ON THE LH AFT MLG PIVOT BUSHING. (FILED CLOSED)COMPLIED WITH REO 601R-57-21-3972 DATED: 2025-09-11 TEMPORARY DISPOSITION FOR BLENDING GOUGE DAMAGE ON FACE OF FWD AND AFT MLG TRUNNION BUSHINGS, LHS. ALL NDT'S COMPLIE
- [SDR SWIA2025091900001](https://openairdocs.org/sdr/SWIA2025091900001.md): Trunnion · damaged · Sep 10, 2025 · N699BR · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > WHILE REMOVING LH MLG ASSY DAMAGED OCCURRED ON THE LH MLG MOUNTING TRUNNION. (FILED CLOSED)COMPLIED WITH REO 601R-57-21-3971 DATED: 2025-09-11 PERMANENT DISPOSITION FOR BLENDED GOUGE DAMAGE TO MLG TRUNNION FITTING FWD AND AFT LUG FACES, LHS ALL NDT'S COMPLIED
- [SDR SWIA2025091901320](https://openairdocs.org/sdr/SWIA2025091901320.md): Skin · dented · Sep 7, 2025 · N699BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND DENT LOCATED AT APROXIMATELY FS181 AND JUST BELOW PANEL 122AR. (FILED CLOSED) COMPLIED WITH REO 601R-53-11-4017 DATED: 2025-09-08 REV: -- TEMPORARY DISPOSITION FOR DENTS ON FUSELAGE SKINS BTW FS185.00 - FS193.00 AND STR 23L - STR24L & FS177.00 - FS185.
- [SDR SWIA2025091900007](https://openairdocs.org/sdr/SWIA2025091900007.md): Skin · dented · Sep 7, 2025 · N699BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND DENT LOCATED AT APROXIMATELY FS187.5 AND BELOW PANEL 121AL (FILED CLOSED) COMPLIED WITH REO 601R-53-11-4017 DATED: 2025-09-08 REV: -- TEMPORARY DISPOSITION FOR DENTS ON FUSELAGE SKINS BTW FS185.00 - FS193.00 AND STR 23L - STR24L & FS177.00 - FS185.00
- [SDR SWI2024F00495](https://openairdocs.org/sdr/SWI2024F00495.md): Actuator · failed · Jun 17, 2024 · N699BR · Cndair CL6002B19 · Landing Gear Actuator
  > GEAR DISAGREE WARNING MESSAGE ON APPROACH QUICK CYCLE TO UP POSITION THEN DOWN RESOLVED IT NEXT STEP QRH (FLIGHT 5434 - FILED CLOSED) ON TASK CARD 32-730-764, THE FOLLOWING TOOL WAS ENTERED: TORQUE WRENCH SN- 0606507170 EXPIRATION- 10/12/24.REMOVED AND RE
- [SDR SWIA202404290026](https://openairdocs.org/sdr/SWIA202404290026.md): Landing Gear · warning message · Apr 26, 2024 · N699BR · Cndair CL6002B19 · Landing Gear Position and Warning
  > *CAT II DOWNGRADED*D:LEFT MAIN GEAR DISAGREE ON FINAL AFTER SELECTING GEAR DOWN.C:MEL 32-30-1CAT "A" DUE 1 FLT DAY 04/27/2024MX ACTION COMPLIED WITH. GEAR PINS INSTALLED.LEFT MAIN GEAR DISAGREE ON FINAL AFTER SELECTING GEAR DOWN. (FLIGHT 5535 FILED CLOSED)APR
- [SDR SWIA2024021200002](https://openairdocs.org/sdr/SWIA2024021200002.md): Wire Harness · faulted · Feb 10, 2024 · N699BR · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DESCENT RECEIVED STEERING INOP CAUTION MESSAGE. AFTER APPROXIMATELY 1 MINUTE RECEIVED WOW INPUT CAUTION FOLLOWED BY WOW OUTPUT FAIL STATUS MESSAGE. PERFORMED QRH AND MESSAGES REMAINED. ON GEAR EXTENSION MESSAGES EXTINGUISHED. NORMAL STEERING RESTORED AFTER
- [SDR SWIA20230628524](https://openairdocs.org/sdr/SWIA20230628524.md): Unknown · chafed · May 24, 2023 · N699BR · Cndair CL6002B19 · Wing Structure
  > R/WING AILERON UPPER FIXED LEADING EDGE NEEDS TO REPLACE DURING CHAFFED DAMAGE OUT OF LIMIT. (C-CHECK RO 6/25/2023) REPLACED R/WING AILERON UPPER FIXED LEADING EDGE SKIN WITH NEW PN PN CC670-13052-4 PO# T- 7801-00009 REF CRJ 200 SRM 51-42-21 AND BOMB
- [SDR SWIA20230519](https://openairdocs.org/sdr/SWIA20230519.md): Unknown · corroded · May 19, 2023 · N699BR · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > UPON REMOVAL ON JOB 2780195 OP 89 CAMP# 26584720, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY. P/N 600-24043-1 @ ES16.52 TO BE CORRODED IN BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK RO 6/25/2023) REMOVED AND REPLACED L/H ELEVATOR HINGE FITTING AS
- [SDR SWI2023F00102](https://openairdocs.org/sdr/SWI2023F00102.md): Unknown · corroded · May 17, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RIGHT HAND FLOOR SEAT RAIL BETWEEN FS399.0 TO FS409.00+4 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW RH CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 399.0 TO FS 409.00+4 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CON
- [SDR SWI2023F00101](https://openairdocs.org/sdr/SWI2023F00101.md): Unknown · corroded · May 17, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LEFT HAND FLOOR SEAT RAIL BETWEEN FS399.0 TO FS409.00+4 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW L/H CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 399 TO FS 409.00+4 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTI
- [SDR SWI2023F00100](https://openairdocs.org/sdr/SWI2023F00100.md): Unknown · corroded · May 17, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LEFT HAND FLOOR SEAT RAIL BETWEEN FS364 TO FS399.0 CORRODED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW L/H CABIN FLOOR SEAT TRACK RAIL BETWEEN FS 364 TO FS 399.0 REF CRJ-200-AMM 53-01-11-000-802 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION C
- [SDR SWIA202306280517](https://openairdocs.org/sdr/SWIA202306280517.md): Unknown · corroded · May 17, 2023 · N699BR · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR LOWER SILL. TOP SIDE OF THE LOWER SILL, UNDER THE FORWARD LOCK FITTING CORRODED. (C-CHECK RO 6/25/2023) REPLACED SERVICE DOOR LOWER SILL ANGLE PN 601R38303-253 PO# T000068450 REF. CRJ200 SRM 51-42-36 REV 39, DATED MARCH 10, 2021, CRJ200 SR
- [SDR SWIA202306280515](https://openairdocs.org/sdr/SWIA202306280515.md): Unknown · corroded · May 15, 2023 · N699BR · Cndair CL6002B19 · Aerodynamic Fairings
  > RH WING TO FUSE/MLG SIDE BRACKET FWD, SEALANT COVERING NUT WAS NOT COMPLETLY SEALED AND APPEARS TO HAVE RUST BLEEDING FROM IT. SEALANT NEEDS TO BE REMOVED FOR INSPECTION. FLAGGED (C-CHECK RO 6/25/2023) REMOVED RH MLG SIDE-BRACE SHAFT FITTING CAP SEAL AN
- [SDR SWIA20230628513](https://openairdocs.org/sdr/SWIA20230628513.md): Unknown · corroded · May 13, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK IS CORRODED FS559+112 - 574.00 LBL9 (C-CHECK RO 6/25/2023) REMOVED SEAT TRACK AT FS559+112 - 574.00 LBL9 REF CRJ 200 AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK.. REF CRJ 200 AMM 53-00-49-400-801. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWI2023F00099](https://openairdocs.org/sdr/SWI2023F00099.md): Unknown · chafed · May 12, 2023 · N699BR · Cndair CL6002B19 · Wing Miscellaneous Structure
  > CHAFFING IN SEVERAL AREAS ON LH LOWER WING PLANK AT APPROX WS45 FS513.0 (MARKED) (C-CHECK RO 6/25/2023) REPAIRED LH LOWER WING PLANK AT APPROX WS45 FS513.0 REF REO 601R-57-21-3758 REV -- DATED 2023-05-31 AND REO 601R-57-21-880 REV D DATED 2017-03-06
- [SDR SWI2023F00098](https://openairdocs.org/sdr/SWI2023F00098.md): Unknown · chafed · May 12, 2023 · N699BR · Cndair CL6002B19 · Wing Miscellaneous Structure
  > CHAFFING IN SEVERAL AREAS ON RH LOWER WING PLANK AT APPROX WS45 FS513.0 (MARKED) (C-CHECK RO 6/25/2023) REPAIRED RH LOWER WING PLANK AT APPROX WS45 FS513.0 REF REO 601R-57-21-3758 REV -- DATED 2023-05-31 AND REO 601R-57-21-880 REV D DATED 2017-03-06.
- [SDR SWI2023F00097](https://openairdocs.org/sdr/SWI2023F00097.md): Unknown · cracked · May 12, 2023 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > CLIP ATTACHED TO FS202 BULKHEAD IN HYD COMPARTMENT AREA IS APPEARS CRACKED (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW REPLACEMENT BRACKET ATTACHED TO FS202 BULKHEAD IN HYD COMPARTMENT.REF CRJ200 SRM 51-42-21,DWG NO:600-33042 REV AB. COMP
- [SDR SWIA202306280512](https://openairdocs.org/sdr/SWIA202306280512.md): Unknown · dented · May 12, 2023 · N699BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR LOWER AFT DR SEAL SUPPORT IS DENTED (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW CARGO DOOR LOWER AFT SEAL DOOR SUPPORT REF CRJ-200 SRM 51-42-06 AND DWG CC670-38702 REV C. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTI
- [SDR SWIA2023062800511](https://openairdocs.org/sdr/SWIA2023062800511.md): Unknown · cracked · May 11, 2023 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACKED CLEAT AT FS193 STRG16L (C-CHECK RO 6/25/2023) FABRICATED REPAIR CLEAT AT FS 193.00 STR 16 LH 2024 T3.032 PO#T66202 REF CRJ 200 SRM 51-24-21 AND DRAWING GC215-0094 REV NCREMOVED AND REPLACED CLEAT WITH NEW PART AT FS 193.00 STRG 16 LH REF CRJ 20
- [SDR SWI2023F00096](https://openairdocs.org/sdr/SWI2023F00096.md): Unknown · cracked · May 11, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RIGHT WHEEL WELL WS48.30 - BATT RIB IS CRACKED AT THE FORWARD AND AFT END. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND REPLACED RIGHT WHEEL WELL WS48.30 - BATT RIB. REF DRAWING NUMBER 600-10389 REV NC AND CRJ200 SRM 51-42-21 RRESTORED FINISH. REF: CRJ-2
- [SDR SWI2023F00095](https://openairdocs.org/sdr/SWI2023F00095.md): Unknown · corroded · May 11, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LEFT WHEEL WELL WS53.60 - FORWARD END OF THE BATT RIB DOUBLER IS CORRODED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW DOUBLER PN 601R13203-33 PER CRJ 200 SRM 51-42-06 AND DWG # 601R10203 REV -G. COMPLIED WITH 51-900-1003-SKY AND M-337. SE
- [SDR SWI2023F00094](https://openairdocs.org/sdr/SWI2023F00094.md): Unknown · corroded · May 11, 2023 · N699BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LEFT WHEEL WELL WS53.60 - FORWARD END OF THE BATT RIB CHANNEL IS CORRODED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW CHANNEL P/N 601R10203-27 ON LH WHEEL WELL WS53.60 PER CRJ 200 SRM 51-42-21 AND DWG # 601R10203 REV -G. COMPLIED WITH 51-
- [SDR SWI2023F00093](https://openairdocs.org/sdr/SWI2023F00093.md): Unknown · cracked · May 11, 2023 · N699BR · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING WS48.30 - BATT RIB ANGLE IS CRACKED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW LH WING AT WS48.30 - BATT RIB ANGLE PER CRJ 200 SRM 51-42-21 AND DWG # 600-10204 REV-K COMPLIED WITH 51-900-1003-SKY AND M-337. SEE CONTINUE CARD F
- [SDR SWIA202306280511](https://openairdocs.org/sdr/SWIA202306280511.md): Unknown · cracked · May 11, 2023 · N699BR · Cndair CL6002B19 · Wing Structure
  > LEFT WING WS48.30 - BATT RIB IS CRACKED. (MARKED) (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW BATT RIB AT WS 48.30 PER CRJ 200 SRM 51-42-21 AND DWG # 601R10203 REV -GCOMPLIED WITH TASK CARD 51-900-1003-SKY
- [SDR SWIA202306280509](https://openairdocs.org/sdr/SWIA202306280509.md): Unknown · corroded · May 9, 2023 · N699BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED MULTIPLE SURFACES (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW PAX DOOR AFT DD4 INTERCOSTAL REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV N. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATI
- [SDR SWI2023F00092](https://openairdocs.org/sdr/SWI2023F00092.md): Unknown · elongated · May 8, 2023 · N699BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HINGE (ACFT. SIDE) HAS MULTIPLE LUG HOLES ELONGATED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW HINGE (FUSELAGE SIDE) PN 601R31671-15 REF CRJ 200 SRM 53-21-23 STEP 4.R-U, BOMBARDIER DWG 601R31527 REV AM AND REO 601R-53-21-656 REV A DATED
- [SDR SWIA20230628508](https://openairdocs.org/sdr/SWIA20230628508.md): Unknown · bent · May 8, 2023 · N699BR · Cndair CL6002B19 · Air Conditioning Doors
  > GROUND AIR CONDITIONING DOOR SILL LANDING FWD AND AFT ARE BENT INWARD (MARKED) (C-CHECK RO 6/25/2023) INSTALLED NEW REPLACEMENT 601R35226-31 FWD LANDING ANGLE FS576.83 STRINGER 22R TO STRINGER 24R REF CRJ200 SRM 51-42-06. DWG 601R35226 REV-N SEE CONTIN
- [SDR SWIA20230628505](https://openairdocs.org/sdr/SWIA20230628505.md): Unknown · dented · May 5, 2023 · N699BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L (C-CHECK RO 6/25/2023) REPAIRED EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L REF REO 601R-53-11-3867 REV -- DATED 2023-06-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUA
- [SDR SWIA2023062800503](https://openairdocs.org/sdr/SWIA2023062800503.md): Unknown · corroded · May 3, 2023 · N699BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 (MID) CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW DD6 MID INTERCOSTAL REF CRJ200 SRM 51-42-06, SRM 51-42-21 AND DWG 601R31702 REV -N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD
- [SDR SWIA20230628503](https://openairdocs.org/sdr/SWIA20230628503.md): Unknown · corroded · May 3, 2023 · N699BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER SECTION @ FS 313.56 CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW FORMER P/N 601R318086-1 AT FS313.56 REF CRJ200 SRM 51-42-06, SRM 51-42-13 AND DWG # 601R31702 REV -N.. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD
- [SDR SWIA202306280503](https://openairdocs.org/sdr/SWIA202306280503.md): Unknown · corroded · May 3, 2023 · N699BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD. FORMER @ FS 311.75 CORRODED. (C-CHECK RO 6/25/2023) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER ASSEMBLY FS311.75 REF CRJ200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-13 AND DWG 601R31702 REV -N. COMPLIED WITH 51-900-1003-SKY AND PRESSURE
- [SDR SWIA202265970](https://openairdocs.org/sdr/SWIA202265970.md): None · failed · Jun 27, 2022 · N699BR · Cndair CL6002B19 · Landing Gear Door Actuator
  > AFTER TAKEOFF WE GOT A GEAR DISAGREE AND NOSE DOOR OPEN MASTER WARNING. RAN QRC FOR NOSE DOOR OPEN FIRST AND THAT FIXED BOTH MESSAGES. (FLIGHT 3570 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25062266 WITH THE FOLLOWING CORRECTIVE ACTIO
- [SDR SWIA2019091846327](https://openairdocs.org/sdr/SWIA2019091846327.md): Strap · corroded · Sep 17, 2019 · N699BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND FLOOR SUPPORT STRAP CORRODDED AT FS 559.0 FROM LBL 43 TO LBL 27 MARKED. (C-CHECK) 09/14/19 BLENDED OUT CORROSION ON LEFT HAND FLOOR SUPPORT STRAP. REMOVED AND INSTALLED NEW STRAP IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019091846326](https://openairdocs.org/sdr/SWIA2019091846326.md): Frame · corroded · Sep 17, 2019 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 605.0 CORRODDED ON FORWARD SIDE FROM APROX LEFT STR 18 TO RIGHT STR 25 MARKED. (C-CHECK) RO: 09/14/19 REMOVED AND INSTALLED NEW FRAME SECTOR IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019091846331](https://openairdocs.org/sdr/SWIA2019091846331.md): Strap · corroded · Aug 28, 2019 · N699BR · Cndair CL6002B19 · Aerodynamic Fairings
  > EXTERNAL FUSELAGE FS559 ATTACHMENT FLANGE FOR FAIRING 163AB FUSELAGE SIDE HAS DETERIORATED SEALANT PAD AND CORROSION ALL THE WAY ACROSS. (C-CHECK) RO: 09/14/19 REMOVED CORROSION ON EXTERNAL FUSELAGE ATTACHMENT FLANGE FOR FAIRING. REMOVED AND REPLACED 2 EA STR
- [SDR SWIA2019091846330](https://openairdocs.org/sdr/SWIA2019091846330.md): Floor Support · corroded · Aug 2, 2019 · N699BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM LIP CORRODDED FROM FS621 TO 574 LBL 9 MARKED. (C-CHECK) RO: 09/14/19 BLENDED OUT CORROSION ON FLOORBEAM LIP IAW SRM.
- [SDR SWIA2019091846324](https://openairdocs.org/sdr/SWIA2019091846324.md): Support Angle · cracked · Aug 1, 2019 · N699BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AT LBL 32 FS 484.0 MARKED. (C-CHECK) RO: 09/14/19 REMOVED AND REPLACED CRACKED ANGLE WITH FABRICATED NEW ONE IAW REO. LEAK CHECK GOOD.
- [SDR SWIA2019091846329](https://openairdocs.org/sdr/SWIA2019091846329.md): Intercostal · corroded · Jul 31, 2019 · N699BR · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR INTERCOSTAL AT HINGE ARM MECHANISM HAS CORROSION. (C-CHECK) RO: 09/14/19 BLENDED OUT CORRISION ON THE SERVICE DOOR INTERCOSTAL IAW SRM. ALL CHECKS GOOD AND THE CORROSION DAMAGE FOUND IS ACCEPTABLE IAW REO.
- [SDR SWIA2019091846328](https://openairdocs.org/sdr/SWIA2019091846328.md): Hinge Arm · chafed · Jul 31, 2019 · N699BR · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR HINGE ARM CHAFED. (C-CHECK) RO: 09/14/19 REMOVED CHAFE ON SERVICE DOOOR HINGE ARM IAW REO. ALL CHECKS GOOD.
- [SDR SWIA2019091846323](https://openairdocs.org/sdr/SWIA2019091846323.md): Frame · corroded · Jul 31, 2019 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON LOWER FRAME SECTOR FS409.0 AFT LOWER ANGLE BETWEEN STR 26L- STR 26R. (C-CHECK) RO: 09/14/19 FOUND LOWER FRAME SECTOR FS409.0 AFT LOWER ANGLE BETWEEN STR 26L- STR 26R. TO BE OUT OF LIMITS, REPLACED WITH NEW LOWER ANGLE IAW SRM. LEAK CHECK GOO
- [SDR SWIA2019091846320](https://openairdocs.org/sdr/SWIA2019091846320.md): Frame · corroded · Jul 31, 2019 · N699BR · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON LOWER FRAME SECTOR AT FS349.00 BETWEEN STR 26L- STR 26R. (C-CHECK) RO: 09/14/19 FOUND LOWER FRAME SECTOR AT FS349.00 BETWEEN STGR 26L- STGR 26R TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW FRAME SECTOR IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2019091846319](https://openairdocs.org/sdr/SWIA2019091846319.md): Strap · corroded · Jul 31, 2019 · N699BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HAND FLOOR SUPPORT STRAP CORRODDED AT FS 559.0 FROM RBL 43 TO RBL 27 MARKED. (C-CHECK) RO: 09/14/19 BLENDED OUT CORROSION ON RIGHT HAND FLOOR SUPPORT STRAP AT FS 559.0 FROM LBL 43 TO LBL 27, FOUND STRAP TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW STR
- [SDR SWIA2019091846318](https://openairdocs.org/sdr/SWIA2019091846318.md): Stringer · cracked · Jul 30, 2019 · N699BR · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PASSENGER CABIN STR 3L AFT OF FS379.0 IS CRACKED. (C-CHECK) RO: 09/14/19 COMPLETED STRINGER REPAIR IAW SRM. INSTALLED NEW STRINGER SECTION WITH 2 EA SPLICES. LEAK CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N699BR/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 = 'N699BR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N699BR/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.