N8698A

Service difficulty reports · 46

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 = 'N8698A' 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 REXA2014030400254Battery Pack · dischargedON 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.Mar 4, 2014 · N8698A · Cndair CL6002B19 · Emergency LightingSDR REXA2013112102270Seal · brokenFIRST AID KIT SEAL BROKEN. RESEALED FIRST AID KIT IAW AMM 25-60-00.Nov 21, 2013 · N8698A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2013061701194Stowage Box · brokenFIRST OFFICER OXYGEN STOWAGE BOX BROKEN. R & R STOWAGE BOX IAW AMM 35-11-04. CHECKED GOOD.Jun 17, 2013 · N8698A · Cndair CL6002B19 · Fuselage Main, StructureSDR REXA2013041000629Vane · chafedFLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013041000628Vane · chafedFLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE ACTUATOR. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013041000627Vane · chafedINBOARD FLAP VANE LEADING EDGE IS CHAFED INBOARD OF THE INBOARD ACTUATOR. REPAIRED IAW SRM 51-24-28.Apr 9, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA2013041000626Skin · chafedLEFT AILERON UPPER LEADING EDGE SKIN CHAFED OUT OF LIMITS. REPLACED IAW SRM 51-42-21.Apr 9, 2013 · N8698A · Cndair CL6002B19 · AileronsSDR REXA2013041000625Structure · damagedFORWARD RIGHT ACCESS PANEL DOOR SURROUND DOUBLER AT FS 235 HAS DAMAGED HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-11-162.Apr 9, 2013 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2013020200215Life Vest · unserviceable1 INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.Feb 2, 2013 · N8698A · Cndair CL6002B19 · Life JacketSDR REXA2013012100174Flex Drive · faultyON 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 RIJan 21, 2013 · N8698A · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR REXA2012121201765Stowage Box · damagedO2 BOX DOOR BROKE. REMOVED AND REPLACED O2 STORAGE BOX IAW AMM 35-11-15. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.Dec 12, 2012 · N8698A · Cndair CL6002B19 · Crew Oxygen SystemSDR REXA2012110101445Warning System · false activationSMOKE 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. COUNov 1, 2012 · N8698A · Cndair CL6002B19 · Smoke DetectionSDR REXA2012102601430Life Vest · unserviceablePILOT LIFE VEST BAG TORN. REMOVED AND REPLACED PILOTS LIFE VEST IAW AMM 25-61-03.Oct 26, 2012 · N8698A · Cndair CL6002B19 · Life JacketSDR REXA2012071701166Shutoff Valve · failedFLIGHT 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 COMPJul 17, 2012 · N8698A · Cndair CL6002B19 · Cabin Pressure Control SystemSDR REXA2012020600187Isis · activatedAIR 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 SEFeb 6, 2012 · N8698A · Cndair CL6002B19 · Integrated Flight SystemSDR REXA201100895Battery · dischargedFIRST 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.Dec 1, 2011 · N8698A · Cndair CL6002B19 · Emergency EquipmentSDR REXA201100770Valve · malfunctionedFUEL 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.Oct 22, 2011 · N8698A · Cndair CL6002B19 · Fuel Transfer ValveSDR REXA201100628Autopilot Sys · malfunctionedAUTOPILOT 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.Sep 28, 2011 · N8698A · Cndair CL6002B19 · Autopilot SystemSDR REXA201100493Web · damagedFS 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 REVJul 16, 2011 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100451Web · damagedFOUND 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-Jul 13, 2011 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201100230Warning System · activatedNWS INOP CAUTION MSG AFTER GEAR RETRACTION IN WORK JFK, REPEAT ISSUE FROM 4-11-11.Apr 11, 2011 · N8698A · Cndair CL6002B19 · Landing Gear Steering SystemSDR REXA201100084Hinge Fitting · damagedLIGHTENING 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.Feb 4, 2011 · N8698A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA201000238Doubler · leakingPREVIOUS 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-Nov 2, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000214Frame · wornTHE 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.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, FrameSDR REXA201000213Sill · corrodedRT 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.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000207Bulkhead · corrodedFS 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. Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000206Floor Support · corrodedFS 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.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000205Skin · gougedDURING 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 PAROct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000204Seat Track · corrodedLT CABIN SIDE SEAT TRACK CORRODED FROM FS 484 TO 559+80. REMOVED AND REPLACED SEAT TRACK IAW CRJ AMM 53-01-11-400-802.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA201000203Seat Track · corrodedRT 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.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR REXA201000202Bracket · corrodedCONNECTORS 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.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000201Sill · corrodedCARGO SILL PLATE FS 574 TO FS 621 IS CORRODED. REPLACED AS PER REO 601R-53-61-1574.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000200Skin · corrodedFUSELAGE SKIN HAS MINOR CORROSION AROUND DRAIN HOLE AT FS 559+64 BETWEEN STR 26L AND 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000199Skin · corrodedFUSELAGE SKIN HAS MINOR CORROSION AT FS 559+64 BETWEEN STR 23R AND 24R. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000198Skin · corrodedFUSELAGE SKIN HAS MINOR CORROSION AT FS 559+80 AT STR 27. REPAIRED IAW BOMBARDIER REO 601R-53-19685A.Oct 15, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000176Pressure Panel · damagedOUTBOARD 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.Oct 3, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000174Bulkhead · crackedS 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.Oct 2, 2010 · N8698A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201000166Bracket · corrodedCONNECTOR 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.Sep 30, 2010 · N8698A · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA201000150Fairing · chafedRT 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. CHSep 17, 2010 · N8698A · Cndair CL6002B19 · Trailing Edge FlapsSDR REXA200900050Fcu · failedFLIGHT 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 AMMay 14, 2009 · N8698A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2009F00025Scavenge Pump · defectiveIN 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 ENGIJan 30, 2009 · N8698A · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA200800019Tire · failedUPON 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. MAIMay 31, 2008 · N8698A · Cndair CL6002B19 · TireSDR REXA200700029Flap System · unknownFLAP FAIL, SECOND OCCURNACE WITHIN 72 HOURS.Feb 3, 2007 · N8698A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00002Acm · inoperative(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)Aug 2, 2005 · N8698A · Cndair CL6002B19 · Cabin Cooling SystemSDR REXA2005056Proximity Sensor · out of adjustGEAR 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)Apr 28, 2005 · N8698A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2005055Indication Sys · malfunctionedUPON 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)Apr 26, 2005 · N8698A · Cndair CL6002B19 · Landing Gear Position and Warning
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