N587CA, cancelled Aug 28, 2017

Service difficulty reports · 22

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 = 'N587CA' AND deregistration_id = 'N587CA-2017-08-28'
  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 RDS121112SDRPitot Tube · failedNR 2 PITOT SWITCH TRIPPED IN-FLIGHT, PULLED CIRCUIT BREAKER AS PRECAUTION, SMELLED "ELECTRICAL" ODOR PRIOR TO PITOT TRIPPING. NR 2 PITOT SYS CHECK. ALL ELECTRICAL CONNECTIONS AND BREAKER, NO "ELECTRICAL" ODOR. ALL IAW MM 34-11-1, PAGE 200-(3).Feb 23, 2011 · N587CA · Cvac 440 · Pitot/Static SystemSDR RDS121108Processor · failedTCAS INOP. FLAGGED ON ALL INDICATORS. SMELLED SMOKE. TCAS C/B PULLED. R & R TCAS PROCESSOR, PN 066-500002120, SN OFF 1547, SN ON 1687. TEST IAW CV640, MM CH 34-45-1, PG 400-1A.Aug 5, 2010 · N587CA · Cvac STC440T · Air Collision Avoidance SystemSDR RDS121107Relay · failedNR1 ENGINE FIRE LIGHT CAME ON INTERMITTENTLY DURING TURBULENCE AND ROUGH PAVEMENT. R & R FIRE DETECTOR BOX PN 33958-3, SN OFF 3654, ON 829 TEST OK. TEST IAW CH 20-1-PAGE 1-20.1-2-3 CV 440 MM. "NOTE" TAPPING ON FIRE DETECTOR PANEL COVER SIMULATED THE LIGHT CAug 3, 2010 · N587CA · Cvac 440 · Fire DetectionSDR RDS121092Pcu · failedON 6/18/09, WHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, THE ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT. THE CAUSE OF PROPELLER MOVEMENT WAS THE INTERNAL FAILURE OFJan 27, 2010 · N587CA · Cvac 440 · Propeller Controlling SystemSDR JRA2009F00001Engine · overtempWHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT, CAUSE OF PROPELLER MOVEMENT AT THIS TIME UNKNOWN. THE ENGINE NEEDS TO BE REJun 18, 2009 · N587CA · Cvac 440 · Engine (Turbine/Turboprop)SDR JRA2009F00000Filter · dirtyRT FUEL FILTER BLOCKED LIGHT CAME ON DURING TAKEOFF. TAKEOFF WAS WITH WATER METH (ON) AND WAS ABORTED, THE WARNING LIGHT WENT OUT ON POWER REDUCTION. MX PERFORMED AN INSP OF THE NR 2 FUEL FILTER, REMOVED AND REPLACED FUEL FILTER ENGINE NR 2, RUN UP CHECKED SMar 7, 2009 · N587CA · Cvac 440 · Engine Fuel DistributionSDR JRA2008F00000Spring Assy · stretchedAILERON CONTROL CABLES BINDING TO THE RIGHT FROM FULL LEFT POSITION. INSPECTION OF AILERON CONTROL CABLES REVEALED STRETCHED SPRING AT RUDDER INTERCONNECT. REMOVED AND REPLACED SPRING IAW 440 MM, SEC 8-2, PAGE 26. OPS CHECK OK. (K)Nov 14, 2008 · N587CA · Cvac STC440 · Aileron Control SystemSDR RDS12120061Axle · crackedWHEN REMOVING NOSE AXLE TO C/W AD83-01-02 FOR THE 12,000 HOUR MAGNETIC PARTICLE TESTING. A CRACK AROUND THE AXLE FLANGE THAT THE BEARING SPACER RIDES AGAINST WAS NOTICED. REMOVED AND REPLACED WITH NEW AXLE, RETURNED AIRCRAFT TO SERVICE.Oct 18, 2006 · N587CA · Cvac 440 · Nose/Tail Landing Gear Strut/AxleSDR JRAA587062305Skin Panel · corrodedSURFACE CORROSION WAS FOUND ON THE RT IB SKIN PANEL AT APPROX STA 96.91. THIS CORRODION WAS NOTED UNDER THE INSULATION PANEL LOWER SIDE. REPLACEMENT OF SKIN PANEL IN PROGRESS. (K)Jun 23, 2005 · N587CA · Cvac 640340D · Nacelle/Pylon, Plate/SkinSDR JRAA587060705Longeron · corrodedINTERGRANULAR CORROSION WAS FOUND ON THE LONGERON CHANNEL AT FUSELAGE BUTTOCK LINE 0, WING STATION 403.0. THIS CORROSION NOTED ON THE LT SIDE, 10 INCHES FORWARD OF THE REAR LOWER WING SPAR. ACCESS THROUGH THE LT WING IB DRY BAY PANEL. (K)Jun 7, 2005 · N587CA · Cvac 440 · Wing, Longeron/StringerSDR 2004F00349Check Valve · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00347Tube · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAAAug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00346Transmitter · corrodedDUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00344Door · corrodedBAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00343Bellmouth · corrodedDURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR JRAA0520042Floorbeam · corrodedDURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROGRESSED THROUGH 50 PEMay 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor BeamSDR JRAA0520041Floorbeam · corrodedDURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTACH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACEMENT IN PROGRESS AT May 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor BeamSDR JRAA0520043Beltframe · corrodedDURING A SCID INSPECTION, CORROSION WAS FOUND ON RT BELTFRAME STATION 665.0 AT FLOOR LINE. APPROX. 8.5 INCHES OF THE BELTFRAME IS CORRODED AT THE FLOORBEAM ATTACH POINT. SOME OF THE CORROSION EXTENDS BELOW THE FLOOR LINE. REPAIR IN PROGRESS AT THIS TIME.May 20, 2004 · N587CA · Cvac STC440 · Fuselage Main, FrameSDR JRA2003F00000Line · leakingAFTER MOVING THE LANDING GEAR HANDLE (DOWN) AND SELECTING FLAPS (DOWN); THE HYDRAULIC PRESSURE GAUGE READ ZERO PSI. NO FLUID WAS VISIBLE IN THE HYDRAULIC RESERVOIR SIGHT TUBE. WITH BYPASS VALVE SELECTOR (UP) BRAKES OPERATED. HYDRAULIC LINE WAS REPAIRED.Feb 27, 2003 · N587CA · Cvac 640340D · Hydraulic System, MainSDR JRA2002F00003Battery · overheatedAFTER ARRIVAL, AIRCRAFT POWERED BY BATTERY FOR 30 MIN. - FANS, LIGHTS, CARGO DOOR, ECT. WHEN POWERED UP, NOTED 18 V, TURNED ON BATT INTERLOCK OVERRIDE FOR A FEW MINUTES WITH GPU ON- BATTERY TEMP 120 DEGREES, FOLLOWED COM PROCEDURE AND LOWERED BATTERIES. BATApr 24, 2002 · N587CA · Cvac 640340D · Battery/Charger SystemSDR GAIA9644Frame · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE INBOARD LEFT NACELLE FRAME AT STATION 150. THE ABOVE DAMAGE WAS REPAIRED IAW KHA. EA NR CV-54-31. BY SPLICING IN A NEW SECTION OF NACELLE FRAME. THE ABOVE EA NR CV-54-31 WAS (DER) APPROVED ON FAA FORM 8110-3Dec 10, 1996 · N587CA · Cvac 440 · Nacelle/Pylon, Frame/Spar/RibSDR GAIA9623AInverter · failedYIP/OKC - FLT 587 - TWENTY NM FROM COLUMBIA, MISSOURI, THE ACFT FDR AND GPWS WARNING LIGHTS ILLUMINATED. ABOUT TEN SECONDS LATER, THE FLIGHT CREW NOTED SMOKE IN THE COCKPIT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES, NOTIFIED ATC, DECLARED AN EMERGENCY Jul 12, 1996 · N587CA · Cvac 440 · AC Inverter
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