# Service difficulty reports: N685BR

A list on [N685BR](https://openairdocs.org/aircraft/N685BR.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 REXA2022061701296](https://openairdocs.org/sdr/REXA2022061701296.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, "DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT"; A CRACK WAS FOUND AT THE BOTTOM OF THE RBL 27 VERTICAL POST ON THE OB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF
- [SDR REXA2022061701295](https://openairdocs.org/sdr/REXA2022061701295.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, "DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT"; A CRACK WAS FOUND AT THE BOTTOM OF THE LBL 27 VERTICAL POST ON THE OB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF
- [SDR REXA2022061701237](https://openairdocs.org/sdr/REXA2022061701237.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > "DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, ""DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT""; A CRACK WAS FOUND AT THE BOTTOM OF THE LBL 18 VERTICAL POST ON THE OB SIDE. THE CRACK ORIGINATES FROM THE BOT
- [SDR REXA2022061701236](https://openairdocs.org/sdr/REXA2022061701236.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, "DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT"; A CRACK WAS FOUND AT THE BOTTOM OF THE LBL 27 VERTICAL POST ON THE IB SIDE. THE CRACK ORIGINATE FROM THE BOTTOM OF
- [SDR REXA2022061701235](https://openairdocs.org/sdr/REXA2022061701235.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, "DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT"; A CRACK WAS FOUND AT THE BOTTOM OF THE RBL 18 VERTICAL POST ON THE OB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF
- [SDR REXA2022061701234](https://openairdocs.org/sdr/REXA2022061701234.md): Post · cracked · Jun 10, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING COMPLIANCE OF CRJ200 JOB CARD 53-160-604, "DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR 21 LEFT AND RIGHT"; A CRACK WAS FOUND AT THE BOTTOM OF THE RBL 27 VERTICAL POST ON THE IB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF
- [SDR REXA2022061001170](https://openairdocs.org/sdr/REXA2022061001170.md): Beam · cracked · Jun 8, 2022 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT ENGINE SUPPORT BEAM LOWER WEB REPAIR - SDI, FOUND A 2" CRACK ON THE PREVIOUSLY INSTALLED DOUBLER. "REPAIR HAS BEEN COMPLETED USING REO 601R-53-61-0358. "
- [SDR REXA2021031900158](https://openairdocs.org/sdr/REXA2021031900158.md): Rib · cracked · Mar 10, 2021 · N685BR · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > BATT RIB IS CRACKED ABOVE THE UPPER RIVET AT L/H WS 53.60. REPAIRED BATT RIB IAW BOMBA REO 601R-57-51-046 REV B REPAIR TYPE 2
- [SDR REXA2021031900156](https://openairdocs.org/sdr/REXA2021031900156.md): Floorbeam · corroded · Mar 10, 2021 · N685BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 HAS CORROSION AT AFT ANGLE. REMOVED CORRODED AFT ANGLE AND REPLACED WITH NEW ANGLE. IAW CRJ 200 SRM 51-42-21 AND 51-42-06 AND RESTORES TO ORIG FINISH IAW CRJ 200 SRM 53-00-00
- [SDR REXA2021031900155](https://openairdocs.org/sdr/REXA2021031900155.md): Floorbeam · cracked · Mar 10, 2021 · N685BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 LBL9, I/B CLIP IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE(FABRICATED) IAW CRJ200 SRM 51-24-16 AND RESTORED TO ORIG FINISH IAW CRJ 200 SRM 51-21-11, 51-25-16, 51-25-06
- [SDR REXA2021031900154](https://openairdocs.org/sdr/REXA2021031900154.md): Floorbeam · cracked · Mar 10, 2021 · N685BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 RBL9, I/B, O/B CLIPS CRACKED AT FWD AND AFT FLOOR. REMOVED CRACKED CLIPS AND REPLACED WITH NEW FABRICATED CLIPS. IAW 53-21-43 AND 51-24-16
- [SDR REXA2021031900153](https://openairdocs.org/sdr/REXA2021031900153.md): Rib · cracked · Mar 10, 2021 · N685BR · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > BATT RIB IS CRACKED ABOVE THE UPPER RIVET AT R/H WS 53.60. REPAIRED BATT RIB IAW BOMBA REO 601R-57-51-046 REV B REPAIR TYPE 2
- [SDR REXA2021031900157](https://openairdocs.org/sdr/REXA2021031900157.md): Frame · corroded · Mar 6, 2021 · N685BR · Cndair CL6002B19 · Fuselage Main, Frame
  > FS605 FRAME CORRODED UNDER CARGO FLOOR PANEL 281 DLF. REMOVED CORROSION ON FRAME 605 AND FOUNT TO BE OUT OF LIMITS IAW CRJ200 SRM53-00-00 REPAIRED FS605 FRAME UNDER CARGO FLOOR PANEL 281 DLF IAW EA#CRJ253-11320
- [SDR SWIA2019022145536](https://openairdocs.org/sdr/SWIA2019022145536.md): Handle · failed · Feb 21, 2019 · N685BR · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF THE LANDING GEAR WON`T RETRACT WITH THE LANDING GEAR LEVER IN THE UP POSITION. SHORTLY AFTER PARK BRAKE SOV? AND A/SKID INBD? CAUTION MESSAGES. RETURNED TO FIELD. (FLT#3500) REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY IAW AMM. PERFO
- [SDR SWIA2019021945529](https://openairdocs.org/sdr/SWIA2019021945529.md): Control Handle · failed · Feb 18, 2019 · N685BR · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF. ANTI SKI INBOARD CAUTION; PARKING BRAKE SOV CAUTION, AND A GEAR DISAGREE WARNING MESSAGE. AFTER RUNNING THE QRH, THE GEAR RETRACTED. (FLT#3951) REMOVED AND REPLACED LANDING GEAR HANDLE ASSY IAW AMM. OPS CHECK GOOD NO FURTHER FAULTS FOUND A/C OK
- [SDR SWIA2019021245513](https://openairdocs.org/sdr/SWIA2019021245513.md): Accumulator · failed · Feb 12, 2019 · N685BR · Cndair CL6002B19 · Hydraulic System, Main
  > AFTER TAKEOFF GEAR DISAGREE MESSAGE. BEFORE WE COULD RUN THE QRH, THE CHECKLIST MESSAGE WENT AWAY AND GEAR CAME UP AND LOCKED. (FLT#3997) REMOVED AND REPLACED HYDRAULIC 3 ACCUMULATOR IAW AMM. EXTENSION/RETRACTION TESTS GOOD IAW AMM.
- [SDR SWIA2019012945475](https://openairdocs.org/sdr/SWIA2019012945475.md): Hydraulic System · contaminated · Jan 29, 2019 · N685BR · Cndair CL6002B19 · Hydraulic System, Main
  > UPON TAKEOFF RECEIVED A HYD 3 LO PRESS CAUTION MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE WITH THE LANDING GEAR HANDLE SELECTED IN THE €ŒUP€? POSITION. COMPLIED WITH QRH AND RETURNED TO FIELD FOR A NORMAL LANDING. (FLT 4981) CLOSED INSPECTED AND FOU
- [SDR SWIA2018092745095](https://openairdocs.org/sdr/SWIA2018092745095.md): Landing Gear · warning light · Sep 26, 2018 · N685BR · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE DURING GO AROUND ON APPROACH, INITIATED AFTER MICROBURSTS ON THE FIELD. GEAR WAS NEVER SELECTED UP AND NOTICED THIS AT 230KTS, AFTER WHICH GEAR HANDLE WAS SELECTED UP, CAUSING THE MESSAGE. GEAR RETRACTED AS AIRPLANE SLOWED THROUGH
- [SDR SWIA2018080244956](https://openairdocs.org/sdr/SWIA2018080244956.md): Not Reported · dented · Jun 28, 2018 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DENT AT FS559.00+16 BETWEEN STRINGERS 15R AND 16R. (C-CHECK) RO: 08/01/2018 DRESSED DENT DAMAGE BACK TO ORIGINAL CONTOUR IAW REO.
- [SDR SWIA2018080244946](https://openairdocs.org/sdr/SWIA2018080244946.md): Skin · dented · Jun 27, 2018 · N685BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AT FS409.00+18.5 STR24L ON EXTERIOR SKIN. (C-CHECK) RO: 08/01/2018 REPAIRED DENT AT FS409.00+18.5 STR 24L IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2018080244955](https://openairdocs.org/sdr/SWIA2018080244955.md): Intercostal · corroded · Jun 26, 2018 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD6 HAS CORROSION BETWEEN FS338 AND FS347. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 IAW SRM. PRESSURE LEAK CHK GOOD.
- [SDR SWIA2018080244954](https://openairdocs.org/sdr/SWIA2018080244954.md): Intercostal · corroded · Jun 26, 2018 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD4 HAS CORROSION BETWEEN FS320 AND FS338. (C-CHECK) RO: 08/01/2018 REMOVED & REPLACED PAX DOOR INTERCOSTAL DD4 IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2018080244953](https://openairdocs.org/sdr/SWIA2018080244953.md): Intercostal · corroded · Jun 26, 2018 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD7 HAS CORROSION BETWEEN FS338 AND FS347. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD7 BETWEEN FS338 AND FS347 IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2018080244952](https://openairdocs.org/sdr/SWIA2018080244952.md): Intercostal · corroded · Jun 26, 2018 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD7 HAS CORROSION BETWEEN FS311 AND FS320. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2018080244950](https://openairdocs.org/sdr/SWIA2018080244950.md): Vane · chafed · Jun 25, 2018 · N685BR · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE THE RT INBD FLAP CENTER VANE CAP. (C-CHECK) RO: 08/01/2018 REPLACED RT INBD FLAP CENTER VANE CAP WITH NEW PART IAW SRM.
- [SDR SWIA2018080244947](https://openairdocs.org/sdr/SWIA2018080244947.md): Skin · dented · Jun 24, 2018 · N685BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP, DENT ON LOWER SKIN NEAR TRAILING EDGE APPROXIMATE WS72.00. (C-CHECK) RO: 08/01/2018 REPAIRED THE RIGHT HAND INBOARD FLAP LOWER SKIN AT WS 72.00 IAW SRM.
- [SDR SWIA2018080244951](https://openairdocs.org/sdr/SWIA2018080244951.md): Skin · chafed · Jun 23, 2018 · N685BR · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON, BOTH LOWER SKIN SHROUDS ARE CHAFED. AILERON STATIONS 323.843, 329.875 & 370.031, 375.857. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED RT AILERON LOWER SHROUDS (INB AND OUTB) IAW SRM.
- [SDR SWIA2018080244949](https://openairdocs.org/sdr/SWIA2018080244949.md): Vane · chafed · Jun 23, 2018 · N685BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT SIDE INBOARD FLAP( VANE) HAS CHAFING WEAR AT INBOARD, CENTER, AND OUTBOARD LEADING EDGE SECTION OF FLAP VANE. (C-CHECK) RO: 08/01/2018 REMOVED DAMAGE FROM INBD FLAP VANE CAPS IAW REO.
- [SDR SWIA2018080244948](https://openairdocs.org/sdr/SWIA2018080244948.md): Intercostal · corroded · Jun 23, 2018 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CORROSION ON THE DD6 INTERCOSTAL. (C-CHECK) RO: 08/01/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD6 IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2017120543887](https://openairdocs.org/sdr/SWIA2017120543887.md): Downlock Sensor · failed · Oct 19, 2017 · N685BR · Cndair CL6002B19 · Landing Gear Position and Warning
  > RECEIVED NOSE DOOR WARNING ALONG WITH GEAR DISAGREE. COMPLIED WITH QRH ALL THREE GEAR DOWN AND GREEN. RETURNED TO FIELD. DID NOT DECLARE EMERGENCY. (FLT 4584) REMOVED AND REPLACED THE NLG DOWNLOCK NR 2 SENSOR AND HARNESS ASSY IAW AMM. REMOVED AND REPLACED THE
- [SDR SWIA201642361](https://openairdocs.org/sdr/SWIA201642361.md): Skin · dented · Jul 7, 2016 · N685BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT AFT OF 10TH STAGE GROUND BLEED AIR SUPPLY DOOR AT BS 672 AND STRINGER 20L. COLD WORKED AND HAND DRESSED OUT DENT BACK TO ORIGINAL CONTOUR IAW EA.
- [SDR SWIA201642360](https://openairdocs.org/sdr/SWIA201642360.md): Floor Support · corroded · Jul 6, 2016 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT AFT OF BS 349 HAS EVIDENCE OF CORROSION BS 349 TO 356. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA201642359](https://openairdocs.org/sdr/SWIA201642359.md): Floor Support · corroded · Jul 2, 2016 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CARGO FLOOR EDGE MEMBER HAS CORROSION AT THE NUT-PLATE LOCATIONS FROM BS 621 TO 559+80. REPLACED IAW REO.
- [SDR SWIA201642358](https://openairdocs.org/sdr/SWIA201642358.md): Angle · corroded · Jul 1, 2016 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL LONGERON VERTICAL LEG HAS EVIDENCE OF CORROSION AROUND SEVERAL NUT PLATE AND GROUND STUD LOCATIONS. REPLACED PAX DOOR SILL FLOOR SUPPORT ANGLE IAW SRM. ALL OP CHECKED GOOD.
- [SDR SWIA201642357](https://openairdocs.org/sdr/SWIA201642357.md): Web · corroded · Jun 30, 2016 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR, THE AFT FIXED STAIR WEB/PANEL HAS SEVERAL SPOTS OF CORROSION. REPAIRED THE STAIR WEB IAW EA.
- [SDR SWIA201642356](https://openairdocs.org/sdr/SWIA201642356.md): Web · corroded · Jun 30, 2016 · N685BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR, THE FWD FIXED STAIR WEB PANEL HAS SEVERAL SPOTS OF CORROSION. REPAIRED THE PAX DOOR WEB IAW STS EA.
- [SDR SWIA201439212](https://openairdocs.org/sdr/SWIA201439212.md): Fcu · unknown · Aug 24, 2014 · N685BR · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > LEFT ENGINE SHUTDOWN ON DESCENT. COMPLIED WITH QRH AND LANDED NORMALLY. R & R LEFT ENGINE FUEL PUMP AND FUEL CONTROL. LEAK AND OPS CHECKED GOOD.
- [SDR SWIA201438590](https://openairdocs.org/sdr/SWIA201438590.md): Light · inoperative · Jul 5, 2014 · N685BR · Cndair CL6002B19 · Emergency Lighting
  > LEFT LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R LT LOWER EMERGENCY EXIT LIGHT AND INVERTER IAW AMM.
- [SDR SWIA201438467](https://openairdocs.org/sdr/SWIA201438467.md): Web · cracked · Jun 25, 2014 · N685BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VISUAL INSPECTION OF THE ESB, LOWER WEB, CRACK FOUND AT LBL 11.0 AFT EDGE CRACK IS GOING THROUGH RIVET. C-CHECK, COMPLIED WITH PERMANENT REPAIR FOR CRACK ON ESB LOWER WEB AT LBL 11.0, AFT EDGE, IAW REO.
- [SDR SWIA201438473](https://openairdocs.org/sdr/SWIA201438473.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK AT RBL 9, BS 559 +3 TO 559 +85 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438472](https://openairdocs.org/sdr/SWIA201438472.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK AT RBL 9 BS 559 + 85 - 559 + 96 HAS CORROSION. C-CHECK R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438471](https://openairdocs.org/sdr/SWIA201438471.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK AT RBL 27 BS 559 + 78 - 559 + 96 CORRODED. C-CHECK R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438470](https://openairdocs.org/sdr/SWIA201438470.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK AT RBL 9 BS 559 + 109 -- 570 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438469](https://openairdocs.org/sdr/SWIA201438469.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT LBL 9, BS 559 + 85 - 559 + 96 CORRODED. R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438468](https://openairdocs.org/sdr/SWIA201438468.md): Seat Track · corroded · Jun 13, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT LBL 9 BS 559 + 109 - 570 CORRODED. R & R SEAT TRACK IAW AMM.
- [SDR SWIA201438475](https://openairdocs.org/sdr/SWIA201438475.md): Skin · corroded · Jun 12, 2014 · N685BR · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK THRU FUEL ACCESS PANEL 540BB, PITTING CORROSION SOME AREAS. BLENDED DAMAGED AREA AND REMOVED CORROSION IAW REO.
- [SDR SWIA201438474](https://openairdocs.org/sdr/SWIA201438474.md): Hinge · gouged · Jun 12, 2014 · N685BR · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE, FUSELAGE SIDE, HAS GOUGE ON HINGE LUG, 7TH BACK FROM FRONT. C-CHECK, REPAIRED PAX DOOR HINGE, FUSELAGE SIDE HINGE LUG, 7TH BACK FROM FRONT IAW REO.
- [SDR SWIA201438476](https://openairdocs.org/sdr/SWIA201438476.md): Connecting Rod · gouged · Jun 11, 2014 · N685BR · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR CONNECTING ROD, THE INBD END AT THE HEIM BALL, THE FWD SIDE IS GOUGED. C-CHECK, REPAIRED GOUGING DAMAGE ON LT MLG DOOR CONNECTING ROD IAW REO.
- [SDR SWIA201438479](https://openairdocs.org/sdr/SWIA201438479.md): Skin · chafed · Jun 10, 2014 · N685BR · Cndair CL6002B19 · Trailing Edge Flaps
  > FLAP VANE SKIN, RT SIDE HAS CHAFING MARK AT L/E INBD SIDE. C-CHECK, REPAIRED FLAP VANE SKIN, RT SIDE, IAW SRM AND REO.
- [SDR SWIA201438478](https://openairdocs.org/sdr/SWIA201438478.md): Skin · chafed · Jun 10, 2014 · N685BR · Cndair CL6002B19 · Trailing Edge Flaps
  > FLAP VANE SKIN, RT SIDE HAS CHAFING MARK AT L/E CENTER SIDE. C-CHECK, REPAIRED FLAP VANE SKIN, RT SIDE, IAW SRM AND REO.

Next page: https://openairdocs.org/aircraft/N685BR/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 = 'N685BR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N685BR/reports

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