# Service difficulty reports: N8698A A list on [N8698A](https://openairdocs.org/aircraft/N8698A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR REXA2014030400254](https://openairdocs.org/sdr/REXA2014030400254.md): Battery Pack · discharged · Mar 4, 2014 · N8698A · Cndair CL6002B19 · Emergency Lighting > ON ARRIVAL TO ACFT, FOUND EMERGENCY LIGHT WITH A DEAD BATTERIES. APPLIED ACFT POWER & CHARGED EMERGENCY BATTERIES FOR 6 HOURS IAW CMM 25-60-03. PERFORMED OPS TEST OF EMERGENCY LIGHT SYS IAW AMM 33-51-00. CHECKED GOOD, ACFT OK FOR SERVICE. - [SDR REXA2013112102270](https://openairdocs.org/sdr/REXA2013112102270.md): Seal · broken · Nov 21, 2013 · N8698A · Cndair CL6002B19 · Emergency Equipment > FIRST AID KIT SEAL BROKEN. RESEALED FIRST AID KIT IAW AMM 25-60-00. - [SDR REXA2013061701194](https://openairdocs.org/sdr/REXA2013061701194.md): Stowage Box · broken · Jun 17, 2013 · N8698A · Cndair CL6002B19 · Fuselage Main, Structure > FIRST OFFICER OXYGEN STOWAGE BOX BROKEN. R & R STOWAGE BOX IAW AMM 35-11-04. CHECKED GOOD. - [SDR REXA2013041000629](https://openairdocs.org/sdr/REXA2013041000629.md): Vane · chafed · Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge Flaps > FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004. - [SDR REXA2013041000628](https://openairdocs.org/sdr/REXA2013041000628.md): Vane · chafed · Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge Flaps > FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004. - [SDR REXA2013041000627](https://openairdocs.org/sdr/REXA2013041000627.md): Vane · chafed · Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge Flaps > INBOARD FLAP VANE LEADING EDGE IS CHAFED INBOARD OF THE INBOARD ACTUATOR. REPAIRED IAW SRM 51-24-28. - [SDR REXA2013041000626](https://openairdocs.org/sdr/REXA2013041000626.md): Skin · chafed · Apr 9, 2013 · N8698A · Cndair CL6002B19 · Ailerons > LEFT AILERON UPPER LEADING EDGE SKIN CHAFED OUT OF LIMITS. REPLACED IAW SRM 51-42-21. - [SDR REXA2013041000625](https://openairdocs.org/sdr/REXA2013041000625.md): Structure · damaged · Apr 9, 2013 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FORWARD RIGHT ACCESS PANEL DOOR SURROUND DOUBLER AT FS 235 HAS DAMAGED HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-11-162. - [SDR REXA2013020200215](https://openairdocs.org/sdr/REXA2013020200215.md): Life Vest · unserviceable · Feb 2, 2013 · N8698A · Cndair CL6002B19 · Life Jacket > 1 INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A. - [SDR REXA2013012100174](https://openairdocs.org/sdr/REXA2013012100174.md): Flex Drive · faulty · Jan 21, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge Flap Actuator > ON FLIGHT 4099 (BTV TO DTW) CREW RECEIVED FLAP FAIL AT 0 DEGREE. AIRCRAFT LANDED IN DTW SAFELY. REMOVED AND REPLACED NR 1, 2 & 3 FLEX SHAFT IAW AMM 27-53-10. REMOVED AND REPLACED NR 3 LEFT ACT IAW CRJ 200 AMM 27-53-05. PERFORMED TORQUE CHECK OF LEFT AND RI - [SDR REXA2012121201765](https://openairdocs.org/sdr/REXA2012121201765.md): Stowage Box · damaged · Dec 12, 2012 · N8698A · Cndair CL6002B19 · Crew Oxygen System > O2 BOX DOOR BROKE. REMOVED AND REPLACED O2 STORAGE BOX IAW AMM 35-11-15. LEAK AND OPS CHECK GOOD. OK FOR SERVICE. - [SDR REXA2012110101445](https://openairdocs.org/sdr/REXA2012110101445.md): Warning System · false activation · Nov 1, 2012 · N8698A · Cndair CL6002B19 · Smoke Detection > SMOKE TOILET MASTER CAUTION AFTER TAKEOFF. A/C WAS DEICED BEFORE FLIGHT WITH ALL TIMES ADHERED TO, APU OFF, BLEEDS ON THE ENGINES, AND OAT 1C ORH COMPLETE. COMPLIED WITH SMOKE/FUMES IN CABIN/FLIGHT DECK/SMOKE TOILET MSG WORKS COPE, NO DISCREPANCY NOTED. COU - [SDR REXA2012102601430](https://openairdocs.org/sdr/REXA2012102601430.md): Life Vest · unserviceable · Oct 26, 2012 · N8698A · Cndair CL6002B19 · Life Jacket > PILOT LIFE VEST BAG TORN. REMOVED AND REPLACED PILOTS LIFE VEST IAW AMM 25-61-03. - [SDR REXA2012071701166](https://openairdocs.org/sdr/REXA2012071701166.md): Shutoff Valve · failed · Jul 17, 2012 · N8698A · Cndair CL6002B19 · Cabin Pressure Control System > FLIGHT 4285, RIGHT PACK DROPPED OFF LINE ON CLIMB THRU 15000. RESET PACK, PACK CLOSED WITH TEMP THRU 20000. RESET PACK, PACK CLOSED HIGH TEMP CAUTION SECOND TIME WITHIN 90 SECONDS OF PREVIOUS RESET AT 23000. EXECUTED EMERGENCY DESCENT TO 10000. FLIGHT COMP - [SDR REXA2012020600187](https://openairdocs.org/sdr/REXA2012020600187.md): Isis · activated · Feb 6, 2012 · N8698A · Cndair CL6002B19 · Integrated Flight System > AIR RETURN FOR ISIS UNRELIABLE- SHOWING AS MUCH AS 30 DEGREE NOSE DOWN WHILE STRAIGHT AND LEVEL AND UP TO 90 DEGREE BANKS L/R WHEN STRAIGHT. ATTITUDE INDICATION AFFECTED ONLY. SPEED AND ALTITUDE OK. REMOVED AND REPLACED ISIS IAW AMM 34-14-01. A/C OK FOR SE - [SDR REXA201100895](https://openairdocs.org/sdr/REXA201100895.md): Battery · discharged · Dec 1, 2011 · N8698A · Cndair CL6002B19 · Emergency Equipment > FIRST OFFICER FLASHLIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY IN F/O'S FLASHLIGHT IAW CRJ AMM 25-61-01. OPS CHECKS GOOD. PART EFFECTIVITY VERIFIED. - [SDR REXA201100770](https://openairdocs.org/sdr/REXA201100770.md): Valve · malfunctioned · Oct 22, 2011 · N8698A · Cndair CL6002B19 · Fuel Transfer Valve > FUEL GRAVITY X-FLOW VALVE WILL NOT OPEN INOP. PERFORMED OPERATIONAL TEST OF GRAVITY X FLOW VALVE IAW AMM 28-13-16. OP CHECK GOOD. OK FOR SERVICE. - [SDR REXA201100628](https://openairdocs.org/sdr/REXA201100628.md): Autopilot Sys · malfunctioned · Sep 28, 2011 · N8698A · Cndair CL6002B19 · Autopilot System > AUTOPILOT PITCH TRIM CAUTION IN FLIGHT QRH COMPLETE. OPS CHECK AFTER RESET OPS CHECKED GOOD IAW AMM 27-41-15, OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR REXA201100493](https://openairdocs.org/sdr/REXA201100493.md): Web · damaged · Jul 16, 2011 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 559.0 RT WEB HAS INDICATION NOTED I/B OF RBL 18.0 WL 59.10 APPROX.2" IN LENGTH 50 PERCENT FSH AND O/B OF RBL 9.0 WL 58.7 APPROX.3" IN LENGTH 80 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-41-609 REV - [SDR REXA201100451](https://openairdocs.org/sdr/REXA201100451.md): Web · damaged · Jul 13, 2011 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FOUND FS 559.00 RT SIDE WEB HAS INDICATIONS NOTED I/B OF RBL 18.0 WL 59.10 APPROX.2 INCH IN LENGTH 50 PERCENT FSH AND O/B OF RBL 9.0 WL 58.70 APPROX.3 INCH IN LENGTH 80 PERCENT FSH. FAILED NDT. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E; REO 601R-53- - [SDR REXA201100230](https://openairdocs.org/sdr/REXA201100230.md): Warning System · activated · Apr 11, 2011 · N8698A · Cndair CL6002B19 · Landing Gear Steering System > NWS INOP CAUTION MSG AFTER GEAR RETRACTION IN WORK JFK, REPEAT ISSUE FROM 4-11-11. - [SDR REXA201100084](https://openairdocs.org/sdr/REXA201100084.md): Hinge Fitting · damaged · Feb 4, 2011 · N8698A · Cndair CL6002B19 · Trailing Edge Flaps > LIGHTENING STRIKE DAMAGE WAS FOUND ON THE LEFT OUTBOARD FLAP CENTER HINGE BOX FITTING (P/N 601R10119-95). ONE OF THE DAMAGE LOCATIONS SHOWED SIGNS OF MELTING AND IT MEASURED 0.311 X 0.144 X 0.045. REPAIRED IAW STS ENGINEERING EA 09-2011-031. - [SDR REXA201000238](https://openairdocs.org/sdr/REXA201000238.md): Doubler · leaking · Nov 2, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/Skin > PREVIOUS FUSELAGE SKIN REPAIR PATCH PERFORMED AT WVAV IAW REO 601R-53-19698 AT FS 409+64 - FS 409+96 AND STR 1L - 1R WAS FOUND LEAKING UNDER PRESSURE CAUSING A HIGH PITCHED NOISE UNDER PRESSURE IN RDU. FERRY FLY FROM RDU TO CKB (WVAC) IAW BOMBARDIER REO 601R- - [SDR REXA201000214](https://openairdocs.org/sdr/REXA201000214.md): Frame · worn · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Frame > THE FUSELAGE FRAME AT FS 718.00 HAS WEAR DAMAGE AND A HOLE BETWEEN STRINGER 16L AND 17L. REPAIRED THE FRAME AT FS 718.00 BETWEEN STRINGER 16L AND 17L IAW BOMBARDIER SERVICES CORPORATION EO 601R-53-19680. - [SDR REXA201000213](https://openairdocs.org/sdr/REXA201000213.md): Sill · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT CABIN FLOOR SIDE SILL HAS AREAS OF MINOR CORROSION AT FS 506.00 AND FS 559.00. REPAIRED RT CABIN FLOOR SIDE SILL AT FS 506.00 AND FS 559.00 IAW BOMBARDIER REO 601R-53-41-666. - [SDR REXA201000207](https://openairdocs.org/sdr/REXA201000207.md): Bulkhead · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 280.00 BULKHEAD WEB CORRODED AND FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9, ALSO CRACKED O/B OF LBL 9 AND RBL 9, ALONG WITH FLOOR SUPPORT CLIPS LBL 9 I/B AND O/B. REPAIRED FS 280.00 BULKHEAD WEB, ANGLES AND CLIPS IAW BOMBARDIER REO 601R-53-11-926 REV B. - [SDR REXA201000206](https://openairdocs.org/sdr/REXA201000206.md): Floor Support · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 280.00 FWD FLOOR SUPPORT J-ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED FS 280.00 FWD FLOOR SUPPORT J-ANGLE BETWEEN LBL 9 AND RBL 9 IAW CRJ 200 SRM 51-40-11 AND 51-42-06. - [SDR REXA201000205](https://openairdocs.org/sdr/REXA201000205.md): Skin · gouged · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/Skin > DURING REMOVAL OF ADF ANTENNA FOUND BAD NUT PLATES AND FUSELAGE SKIN GOUGED. PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT FS 409.00+64 TO FS 409.00+96 BETWEEN STRINGERS 1R TO 1L AFT OF ADF ANTENNA BY CUTTING AWAY THE DAMAGE, FABRICATING REPAIR PAR - [SDR REXA201000204](https://openairdocs.org/sdr/REXA201000204.md): Seat Track · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LT CABIN SIDE SEAT TRACK CORRODED FROM FS 484 TO 559+80. REMOVED AND REPLACED SEAT TRACK IAW CRJ AMM 53-01-11-400-802. - [SDR REXA201000203](https://openairdocs.org/sdr/REXA201000203.md): Seat Track · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RT CABIN SIDE SEAT TRACKS CORRODED FROM FS 409+18.02 TO 559+80. REMOVED AND REPLACED RT CABIN SIDE SEAT TRACKS FROM FS 409+18.02 TO FS 559+80 IAW CRJ 200 SRM 51-40-11, CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802. - [SDR REXA201000202](https://openairdocs.org/sdr/REXA201000202.md): Bracket · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CONNECTORS BRACKETS (2) ATTACHED TO PAX DOOR SILL ANGLE CORRODED AT PAX DOOR ENTRANCE. REMOVED AND REPLACED CONNECTORS BRACKETS IAW CRJ 200 SRM 51-40-06 AND 51-42-06. - [SDR REXA201000201](https://openairdocs.org/sdr/REXA201000201.md): Sill · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO SILL PLATE FS 574 TO FS 621 IS CORRODED. REPLACED AS PER REO 601R-53-61-1574. - [SDR REXA201000200](https://openairdocs.org/sdr/REXA201000200.md): Skin · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS MINOR CORROSION AROUND DRAIN HOLE AT FS 559+64 BETWEEN STR 26L AND 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A. - [SDR REXA201000199](https://openairdocs.org/sdr/REXA201000199.md): Skin · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS MINOR CORROSION AT FS 559+64 BETWEEN STR 23R AND 24R. REPAIRED IAW BOMBARDIER REO 601R-53-19685A. - [SDR REXA201000198](https://openairdocs.org/sdr/REXA201000198.md): Skin · corroded · Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN HAS MINOR CORROSION AT FS 559+80 AT STR 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A. - [SDR REXA201000176](https://openairdocs.org/sdr/REXA201000176.md): Pressure Panel · damaged · Oct 3, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Bulkhead > OUTBOARD FLANGE AT FS 529.00 RBL 27.00 HAS MISS-DRILLED/ DOUBLE DRILLED HOLES THROUGH THE PRESSURE FLOOR AND FLOORBEAM FLANGE INBOARD FLANGE. THE HOLE IS 0.35" (EDGE TO EDGE) X 0.2. COMPLIED WITH BSC EO 601R-53-19683. - [SDR REXA201000174](https://openairdocs.org/sdr/REXA201000174.md): Bulkhead · cracked · Oct 2, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Bulkhead > S 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. C/W REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A. - [SDR REXA201000166](https://openairdocs.org/sdr/REXA201000166.md): Bracket · corroded · Sep 30, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CONNECTOR BRACKETS P/N 601R31771-1 (2 EACH) ATTACHED TO PASSENGER DOOR SILL BETWEEN FS 319 AND FS 349 ARE CORRODED. REMOVED AND REPLACED CONNECTOR BRACKETS IAW CRJ 200 SRM 51-40-06 AND 51-42-06. - [SDR REXA201000150](https://openairdocs.org/sdr/REXA201000150.md): Fairing · chafed · Sep 17, 2010 · N8698A · Cndair CL6002B19 · Trailing Edge Flaps > RT WING FLAP STUB FAIRING ASSEMBLY (P/N 601R31199) WAS FOUND WITH CHAFE DAMAGE. THE DAMAGE IS THE RESULT OF A FASTENER / PACKER THAT SECURES THE P/N 601R14016 SEAL TO THE INBOARD FLAP PROTRUDING AND CONTACTING THE STUB FAIRING DURING NORMAL FLAP MOVEMENT. CH - [SDR REXA200900050](https://openairdocs.org/sdr/REXA200900050.md): Fcu · failed · May 14, 2009 · N8698A · Cndair CL6002B19 · Trailing Edge Flap Control System > FLIGHT 2453 ICT/MSP CREW RECEIVED FLAP FAIL CAUTION MESSAGE WHILE BOARDING PASSENGERS. MAINTENANCE PERFORMED FIM TROUBLES SHOOTING PER AD 2009-06-12 FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) SHOWING CODE FOR INTERNAL FAILURE. FECU REMOVED AND REPLACED PER AM - [SDR REX2009F00025](https://openairdocs.org/sdr/REX2009F00025.md): Scavenge Pump · defective · Jan 30, 2009 · N8698A · Cndair CL6002B19 · Turbine Engine Oil System > IN CRUISE FLIGHT, THE FLIGHT CREW NOTICED A LOSS OF RT ENGINE OIL PRESSURE AND THE ASSOCIATED WARNINGS. THE FLIGHT CREW EXECUTED THE QRH, SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MX INSPECTED THE ENGI - [SDR REXA200800019](https://openairdocs.org/sdr/REXA200800019.md): Tire · failed · May 31, 2008 · N8698A · Cndair CL6002B19 · Tire > UPON ROTATION DEPARTING KJAN CREW NOTICED SUDDEN AND SHARP ROLLING MOTION AND TUG TO THE LEFT. SUSPECTED TO BE BLOWN TIRE. NO OTHER INDICATIONS NOTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO DAMAGE OR DEFECTS NOTED AND A/C HANDLED NORMALLY. MAI - [SDR REXA200700029](https://openairdocs.org/sdr/REXA200700029.md): Flap System · unknown · Feb 3, 2007 · N8698A · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAP FAIL, SECOND OCCURNACE WITHIN 72 HOURS. - [SDR REX2005F00002](https://openairdocs.org/sdr/REX2005F00002.md): Acm · inoperative · Aug 2, 2005 · N8698A · Cndair CL6002B19 · Cabin Cooling System > (REF NR: 05-094) IN FLIGHT CABIN HAD FUMES AND POSSIBLE SMOKE. QRH FOLLOWED DIVERTED WITH UNEVENTFUL LANDING. TROUBLESHOT AIRCRAFT AND ENGINES DOWN TO THE RT AIR CYCLE MACHINE (ACM). REMOVED AND REPLACED RT ACM IAW AMM. OPS CHECKED GOOD. (K) - [SDR REXA2005056](https://openairdocs.org/sdr/REXA2005056.md): Proximity Sensor · out of adjust · Apr 28, 2005 · N8698A · Cndair CL6002B19 · Landing Gear Position and Warning > GEAR DISAGREE LIGHT ON SHORT FINAL. UNEVENTFUL LANDING. ADJUSTED NLG OLEO PROX SENSOR IAW AMM. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. (K) - [SDR REXA2005055](https://openairdocs.org/sdr/REXA2005055.md): Indication Sys · malfunctioned · Apr 26, 2005 · N8698A · Cndair CL6002B19 · Landing Gear Position and Warning > UPON GEAR EXTENSION FOR LANDING, NOSE LANDING GEAR WOULD NOT SHOW DOWN. DECLARED EMERGENCY, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED GEAR SWING IAW AMM. NO DEFECTS NOTED, OK FOR SERVICE. (K) ## 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 = 'N8698A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8698A/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.