N8646A

Service difficulty reports · 23

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 = 'N8646A' 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 REXA2013071401358Autopilot Sys · malfunctionedAUTOPILOT LEFT AND RIGHT ROLL CONTROL WEAK. AUTOPILOT TRIM ROLL CAUTION.Jul 14, 2013 · N8646A · Cndair CL6002B19 · Autopilot SystemSDR REXA2013051300659Skin · damagedDURING ROUTINE LINE MAINTENANCE AT MSP MAINTENANCE FOUND LIGHTNING DAMAGE TO THE FUSELAGE SKIN IN TWO PLACES BETWEEN FS 275 AND FS 280 ALONG THE DOUBLE RIVET LINES COMMON TO S-24R. REPAIRED IAW EA CRJ253-01581 AND ASSOCIATED 8110-3.May 12, 2013 · N8646A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2013040200714Apu · shutdownAFTER TAKEOFF THE APU SHUTDOWN ON IT'S OWN. NO INDICATIONS WITH IT, JUST TURNED OFF. WE HAD THE AIRCRAFT DE-ICED AT THE OUTSTATION AND SMELLED DE-ICE FLUID AFTER TAKEOFF BEFORE THE APU SHUT DOWN NEARING DTW. WE RESTARTED THE APU. (CONTINUED ON REMARKS CAT)Apr 2, 2013 · N8646A · Cndair CL6002B19 · APU Core EngineSDR REXA2013021900355Life Vest · unserviceableFIRST OFFICER'S LIFE VEST BAG TORN. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.Feb 19, 2013 · N8646A · Cndair CL6002B19 · Life JacketSDR REXA2013021900354Life Vest · unserviceable1 INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST PA 25-096A.Feb 19, 2013 · N8646A · Cndair CL6002B19 · Life JacketSDR REXA2013020900285Battery Pack · dischargedCREW REPORT EMERGENCY LIGHT SYSTEM INOPERABLE UPON ARRIVAL IN DTW. REPLACED ALL FOUR EMERGENCY BATTERY PACKS IAW CRJ 200 AMM 33-51-04. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Feb 9, 2013 · N8646A · Cndair CL6002B19 · Emergency LightingSDR REXA2012122701825Bracket · bentON FLIGHT 4056 (DTW TO CAK) CREW RECEIVED A GEAR DISAGREE ON CLIMBOUT AFTER THE GEAR HANDLE WAS SELECTED UP. NOSE GEAR REMAINED DOWN. ON ORIGINAL PUSHBACK STRAP GOT STUCK IN NOSE GEAR. FOUND NLG CENTERING BRACKET BENT FOR NLG CENTERED/EXTENDED PROX SWITCH BRDec 27, 2012 · N8646A · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REXA2012100601383Life Vest · tornCAPTAIN'S LIFE VEST BACK TORN. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03.Oct 7, 2012 · N8646A · Cndair CL6002B19 · Life JacketSDR REXA2012082101281Battery · inoperativeFIRST OFFICERS FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD, OK FOR SERVICE.Aug 21, 2012 · N8646A · Cndair CL6002B19 · Emergency EquipmentSDR REXA2012070101039Unknown · unknownAT SPEEDS ABOVE 250 KTS OR SLOW SPEEDS WITH FLAPS OUT AILERON CONTROL IS SLOPPY. IT THEN OPTS HARD THEN CATCHES IN THE BANK CAUSING OVER CONTROLLING. PERFORMED PA 27-0660 FOR AILERON BINDING. LUBRICATED REAR QUADRANT PULLEYS HEARINGS IAW AMM 12-20-07-640-80Jul 1, 2012 · N8646A · Cndair CL6002B19 · Flight Control SystemSDR REXA2012062000860Skin · dentedMAINTENANCE FOUND THE SKIN TO BE DENTED AT APPROXIMATELY FS 374 JUST BELOW S16R. THE DENT MEASURES 1 15/32 X 15/16 X 0.094 DEEP. REPAIRED IAW EA CRJ253-00649 AND ASSOCIATED 8110-3.Jun 19, 2012 · N8646A · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA2012062100861Bulkhead · gougedAFT PRESSURE BULKHEAD FORWARD FACE HAS GOUGES ON WEB AT LBL 9 ABOVE THE FLOOR MEASURING 0.004 INCH DEEP. REPAIRED IAW SRM 51-12-00.May 23, 2012 · N8646A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2012040700476Cable · brokenPAX DOOR ICE BREAK CABLE BROKEN. REMOVED AND REPLACED PAX DOOR ICE BREAK CABLE IAW AMM 52-11-15.Apr 7, 2012 · N8646A · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA2012030900350Warning System · false activationSMOKE TOILET CAUTION ON FINAL APPROACH MESSAGE CAME ON AFTER STARTING APU. F/A CONFIRMED NO FIRE AND HALON BOTTLE DID NOT DISCHARGE. MESSAGE LASTED FOR APPROX A MINUTE AND THEN WENT OUT, IT DID NOT COME BACK ON. PERFORMED OP CHECK OF LAV SMOKE DET AND INSPEMar 9, 2012 · N8646A · Cndair CL6002B19 · Smoke DetectionSDR REXA2012030400338Warning System · activatedFLT 3759 FSD-DTW ABORTED TAKEOFF AT LESS THAN 50 KTS DUE TO HIGH LT ENGINE OIL PRESSURE CAUTION. THE CREW ONLY HAD THE ENGINE RUNNING FOR FOUR MINUTES BEFORE ATTEMPTING THE TAKEOFF. THE CREW IS GOING TO LET THE ENGINE RUN FOR LONGER TO WARM UP AND THE ATTEMPMar 4, 2012 · N8646A · Cndair CL6002B19 · Engine Oil PressureSDR REXA201101014Seat Belt · unsecureSEAT 9B SEAT BELT CAME OFF. RESECURED SEAT 9B SEAT BELT IAW CRJ 200 AMM 25-24-01, OPS CHECK GOOD. OK FOR SVC.Dec 24, 2011 · N8646A · Cndair CL6002B19 · Passenger Compartment EquipmentSDR REXA201100717Floorbeam · corrodedLBL 27 FLOORBEAM CAP HAS CORROSION AROUND NUT PLATES FROM FS 574-FS 621. REPAIRED IAW SRM 53-61-43.Nov 20, 2011 · N8646A · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR REXA201100501ALanding Gear · malfunctionedCREW DECLARED AN EMERGENCY REPORTED GEAR DISAGREE ON APPROACH, NOSE GEAR WOULDN'T RELEASE FOLLOWED QRH CYCLED GEAR GOT 3 GREENS FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDENT DEFERRED & PINNED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-01DM-48162.Jul 29, 2011 · N8646A · Cndair CL6002B19 · Nose/Tail Landing GearSDR REXA201100228Flap · failedFLAPS FAILED AT 20 DEGREES ON APPROACH "NO" EMERGENCY DECLARED. PERFORMED T/S PER BOMBARDIER FIM REV 34 IAW AD 2009-06-12 PARAGRAPH (N) (B) (I) AMOC DATED DEC 18 2009 AND PA AD27-052G. FOUND FAULT FOR FLAP CONT LEVER. RESET & OP CHECKED SYSTEM IAW AMM 27-51Apr 10, 2011 · N8646A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA201100190Flap · failedFLAPS FAIL DEFERRED PER MEL 27-50-00 AUTH 40782.Mar 22, 2011 · N8646A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200900124ABulkhead · crackedFOUND CRACKS AT FS 559 BULKHEAD WEB HAS 2 INDICATIONS OF CRACKS NOTED ON RT SIDE WL 59.10 I/B OF RBL 18 APPROX .3 INCH IN LENGTH AND WL 58.70 O/B OF RBL 9, APPROX .2 INCH IN LENGTH AND RT FS 559 CAP ANGLE HAS INDICATION NOTE AT RBL 18 APPROX .2 INCH IN LENGTH Nov 19, 2009 · N8646A · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REX2008F00000Warning System · malfunctionedRECEIVED STAB/MACH TRIM CAUTION MESSAGE IN FLIGHT QRH FOLLOWED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MESSAGE CLEARED AFTER LANDING WITH NO REPEAT. ACFT WAS POWERED DOWN AND BACK ON. NO FURTHER MESSAGES RECEIVED. (S)Jul 2, 2008 · N8646A · Cndair CL6002B19 · Central WarningSDR REXA200600108Fcu · failedFLAPS FAILED ON TAXI OUT. RETURNED TO GATE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM.Nov 29, 2006 · N8646A · Cndair CL6002B19 · Trailing Edge Flap Control System
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