N214AM, cancelled Aug 12, 2010

Service difficulty reports · 28

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 = 'N214AM' AND deregistration_id = 'N214AM-2010-08-12'
  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 ASMF200709004Switch · out of positionAIRCRAFT PERFORMED AN EMERGENCY DESCENT 20 MINUTES PRIOR TO LANDING, DUE TO UNCONTROLLABLE DEPRESSURATION. MAINTENANCE PERSONNEL VERIFIED THE PNEUMATIC SYSTEM FOR LEAKS AS WELL AS THE AIR CONDITIONED SYSTEM AND THE DUCTS OF ANTI-ICE SYSTEM IAW MPCM 36-10-00, Sep 12, 2007 · N214AM · Doug DC987 · Cabin Pressure Control SystemSDR ASMF200708003Shutoff Valve · leakingAIRCRAFT RETURN TO PLATFORM DURING TAXI, CREW SELECTED SLATS EXTEND AND THE HYDRAULIC QUANTITY LIGHT TURNED ON. MAINTENANCE DETECTED HYDRAULIC LEAK IN RT SYSTEM AND QUANTITY ZERO, SO THE SYSTEM WAS SERVICED AND HYDRAULIC PRESSURE WAS APPLIED AND THE LEAK WAS Aug 12, 2007 · N214AM · Doug DC987 · Hydraulic System, MainSDR ASMF200707005Switch · failedAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT THE LT INLET FUEL LOW PRESSURE AND MASTER CAUTION LIGHTS TURNED ON. REPORT WAS DEFERRED IAW MEL 73-3. DURING OVERNIGHT CHECK AT MEX, MAINTENANCE PERSONNEL REPLACED THE LOW FUEL PRESSURE CAUTION SWITCH Jul 5, 2007 · N214AM · Doug DC987 · Fuel Controlling SystemSDR ASMF200707002A/C Pack · leakingAIR TURNED BACK DUE TO HIGH TEMPERATURE IN TAIL CONE, LIGHT TURNED ON AND RT ENGINE WITH LOW ACCELERATION. MAINTENANCE CORRECTED PNEUMATIC LEAKS IN THE LT AND RT AIR-CONDITIONED SYSTEMS IAW MM 36-20-02 AND MPCM 21-10-00; ADDITIONALLY, THE ACCELERATION CAMS ANJul 1, 2007 · N214AM · Doug DC987 · Air Distribution SystemSDR ASMF200610014Strake · damagedDURING TRANSIT CHECK, THE RIGHT FUSELAGE NOSE STRAKE WAS DETECTED DAMAGED WITH 1 INCH LENGTH X .7500 INCH WIDTH AND .1875 INCH OF DEPTH. RT FUSELAGE NOSE STRAKE WAS REPLACED IAW MM 53-30-01, TESTED CORRECT.Oct 31, 2006 · N214AM · Doug DC987 · Fuselage Main, Plate/SkinSDR ASMF200605012Door · ground damageDURING TRANSIT CHECK, AIRCRAFT WAS STRUCK ON THE MAIN PASSENGERS DOOR BY MOBIL STAIRS. AIRCRAFT WAS INSPECTED IAW SRM 51-02 AND DAMAGE WAS WITHIN LIMITS. DURING OVERNIGHT CHECK AT MEX, FINAL REPAIR WAS PERFORMED IAW SRM 51-02, FIG 1, ALL CORRECT.May 20, 2006 · N214AM · Doug DC987 · Passenger/Crew DoorsSDR ASMF200604011Gcu · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AC CROSS TIE LIGHT TURNED ON. AT PLATFORM, THE RIGHT GCU WAS REPLACED IAW MM 24-20-04, TESTED CORRECT IAW MM 24-20-00.Apr 22, 2006 · N214AM · Doug DC987 · AC Generation SystemSDR ASMF200603015Hydraulic Line · leakingAIRCRAFT RETURNED FLIGHT, AFTER TAKEOFF AND LANDING GEARS UP, THE RIGHT HYDRAULIC FLUID QUANTITY WENT DOWN TO 2 QUARTS. AFTER LANDING, THE BRAKES TEMPERATURE REACHED 350 °C AND GOT STUCK. DURING MAINTENANCE REVISION A RIGHT HYDRAULIC SYSTEM LEAK WAS DETECTEDMar 28, 2006 · N214AM · Doug DC987 · Hydraulic System, MainSDR ASMF200505005Computer · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR INDICATOR WAS OUT OF SERVICE. EPR TRANSMMITER WAS REPLACED IAW MM 77-11-02, ENGINE WAS TESTED, ALL CORRECT.May 3, 2005 · N214AM · Doug DC987 · Engine Pressure Ratio (EPR)SDR ASMF200504018Fcu · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING, THE LEFT ENGINE GENERATOR WENT OUT OF ITS BAR TURNING ON THE MASTER CAUTION LIGHT AND THE LEFT OIL PRESSURE WAS LOW (30 PSI). DURING ENGINE CHECK THE FCU DID NOT MAINTAIN THE RPMS IN IDLE AND DEApr 22, 2005 · N214AM · Doug DC987 · Fuel Control/Turbine EnginesSDR ASMF200504016Transmitter · dirtyAIRCRAFT RETURNED TO PLATFORM. DURING PUSH BACK, LT ENGINE STARTED NORMALLY AND AFTER RT ENGINE STARTED, THE LT ENGINE PRESSURE DECREASE TO 35 PSI’S. DURING REVISION WAS DETECTED OVERFILL OIL. THE EXCESS OIL WAS DRAINED AND PRESS OIL TRANSMITTER CONNECTOR WAS Apr 19, 2005 · N214AM · Doug DC987 · Engine Oil PressureSDR ASMF200504009Starter · failedDURING ENGINES STARTING, CAPTAIN REPORTED THAT THERE WAS NOT LEFT ENGINE PARAMETERS INDICATION. THE PNEUMATIC PRESSURE AND STARTER VALVE OPENING WERE VERIFIED IAW MM 80-00-00, BEING CORRECT, SO IT WAS DETERMINED THE STARTER REPLACEMENT. THE LEFT ENGINE WAS STAApr 10, 2005 · N214AM · Doug DC987 · Engine StarterSDR ASMF200502013Fuel Control · failedCAPTAIN REPORTED LEFT ENGINE WITH OSCILLATIONS IN ALL ITS PARAMETERS. THE COMBUSTION CHAMBER WAS SERVICED AND WATER TRAMP WAS DRAINED IAW 72-40-01, ALL CORRECT. DURING OVERNIGHT SERVICE LEFT FCU WAS REPLACED IAW MM 73-12-01 AND THE LEFT ENGINE WAS TESTED IAWFeb 24, 2005 · N214AM · Doug DC987 · Fuel Control/Turbine EnginesSDR ASMF200412006Ignition Unit · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES STARTING, IGNITION SYSTEM FAILED IN BOTH ENGINES. DURING MAINTENANCE REVISION WAS DETECTED THAT 115VAC WAS NOT AVAILABLE AND SWITCH FASTENERS LOOSEN IN TWO LINES. FASTENERS WERE TIGHTENED AND EDec 17, 2004 · N214AM · Doug DC987 · Ignition Power SupplySDR ASMF200411005Ignition Unit · failedDURING ENGINES STARTING, LT ENGINE DID NOT START. CIRCUIT BREAKER WAS CHECKED AND EDP TEST WAS PERFORMED IAW MM 72-21-01, ALL CORRECT. LT ENGINE START WAS PERFORMED AND FAIL CONTINUE, EGT AND RPM INDICATIONS WERE NOT SHOWN. IGNITION BOX AND EXCITER PLUG CABLENov 9, 2004 · N214AM · Doug DC987 · Ignition Power SupplySDR ASMF200406023Tab · damagedDURING OVERNIGHT SERVICE LIGHTING STRIKE DAMAGE WAS DETECTED IN LT ELEVATOR TAB, WITH 1 INCH OF DIAMETER. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00 AND ELEVATOR TAB WAS REPLACED IAW MM 27-30-03, TEST CORRECT.Jun 21, 2004 · N214AM · Doug DC987 · Elevator, Tab StructureSDR ASMF200404001Computer · failedAIRCRAFT SUSPENDED TAKE OF AT 100 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE RIGHT ENGINE DID NOT REACH THE TAKE OF THRUST, IT ONLY REACHED 1.6 OF EPR. AT MEX PLATFORM, TECHNICAL PERSONNEL PERFORMED AN ACCELERATION TEST REACHING ONLY 1.7 OF EPR'S. Apr 1, 2004 · N214AM · Doug DC987 · Engine Emergency Shutdown SystemSDR ASMF200403008Controller · malfunctionedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 33,000 FEET, AFT CARGO DOOR AND AFT STAIRWAY DOOR LIGHTS TURNED ON AND CABIN STARTED TO DEPRESSURIZE. CARGO COMPARTMENT DOORS WERE CHECKED, ALL CORRECT. AIRCRAFT WAS PRESSURIZED WITH A GROUND PNMar 15, 2004 · N214AM · Doug DC987 · Cabin Pressure ControllerSDR MEX2004041Bungee Cylinder · damagedCAPTAIN REPORTED THAT THE NLG RED LIGHT TURNE ON AND OFF SEVERAL TIMES DURING CLIMB, CRUISE AND DESCENT. AT PLATFORM IT AWS PERFORMED A BITE TO THE PROXIMITY SWITCH UNIT IAW MM. TEST, OK, AFTER CAPTAIN REPORTED THAT DURING CLIMB, A LOUD NOISE WAS HEARD IN THFeb 1, 2004 · N214AM · Doug DC987 · Main Landing Gear Strut/Axle/TruckSDR MEX2004020Duct · brokenAIRCRAFT RETURNED DUE TO LIGHT OF TAIL CONE HIGH TEMPERATURE CAME ON, AFTER 3 MINUTES THAT THE ANTI-ICE PROTECTION WAS USED. AIRCRAFT WAS CARRIED TO THE HANGAR TO ATTEND REPORT. AT OVERNIGHT SERVICE, THE ANTI-ICE DUCT ASSY WAS REPLACED AND SYSTEM WAS TESTED Jan 16, 2004 · N214AM · Doug DC987 · Ice/Rain Protection SystemSDR MEX2003558Blade · damagedAIRCRAFT AIR TURN BACK, DURING CLIMB THE RIGHT ENGINE STALLED. AT PLATFORM, IT WAS DETECTED DAMAGES IN FOUR C1 BLADES AND IN 2 C2 BLADES. INSPECTOR AND TECHNICAL PERSONNEL WERE SENT TO EVALUATE THE DAMAGES AND START THE CORRECTIVE ACTIONS. ENGINE WAS REPLACDec 21, 2003 · N214AM · Doug DC987 · Turbine Engine Compressor SectionSDR MEX2003433Control Valve · malfunctionedAIRCRAFT RETURN TO PLATFORM DUE TO DURING TAXI THE FOURTH ANTI-SKID LIGHT TURNED ON. CIRCUIT BREAKERS WERE RESET AND ANTI-SKID BOX CONNECTORS WERE CLEANED NON REPRODUCING THE FAIL. AFTER WORKS, CAPTAIN REPORTED THE ANTISIDE LIGHTS TURNED ON AGAIN. DURING CHSep 17, 2003 · N214AM · Doug DC987 · Brake Anti-Skid SectionSDR MEX2003379Battery · overheatedFLT 519 - MEX-VSA - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF HOT BATTERIES AND SMOKE UNDER THE FUSELAGE. DURING REVISION DETECTED BATTERIES AND BATTERIES CHARGER WITH OVERHEAT. THE BATTERIES AND BATTERY CHARGER WAS REPLACED IAW MM 24-30-01/02, ALL CORRECT. (Aug 21, 2003 · N214AM · Doug DC987 · Battery/Charger SystemSDR MEX2002306Exciter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AN IGNITION FAILURE IN RT ENGINE. AT PLATFORM THE TECH TRIED TO START THE ENGINE BUT THERE WAS TROUBLE WITH THE EXCITER IGNITION BOX. UNIT WAS REPLACED IAW MM.Sep 20, 2002 · N214AM · Doug DC987 · ExciterSDR MEX2002238Engine · failedCREW REPORTED THE PRESENCE OF SMOKE IN CABIN DUE TO AN OIL LEAK IN THE LT A/C PACK. THE MAGNETIC CAP OF THE COOLING TURBINE HAD METAL CHIPS, A/C PACK WAS INOPERATIVE PER MEL. APU WAS REPLACED IAW MM, FOR LACK OF OIL AND LEAKAGE THROUG THE LOAD CONTROL VALVEJul 24, 2002 · N214AM · Doug DC987 · APU Core EngineSDR MEX2002060Fuel Control · failedFLT 419 - MEX-VSA - PILOT REPORTED A MISALIGNMENT OF MORE THAN .5 INCH BETWEEN THROTTLE LEVERS. ROD END OF FCU WAS REPLACED AND RIGGING AND OPERATIONAL TEST TRIM, WERE PERFORMED IAW MM 71-00-01. (M)Mar 8, 2002 · N214AM · Doug DC987 · Fuel Control/Turbine EnginesSDR MEX2002136Computer · failedFLT 478 - MZT-HMO - THE CAPTAIN REPORT THAT DURING CLIMB MZT-HMO, THE AIRCRAFT HAD HEADING PROBLEMS. THE FO'S WAS OUT OF SERVICE AND THE FLIGHT DIRECTOR BARS WERE LOST WHEN EFIS BOTH WAS SELECTED ON 1, THE PROBLEM WAS INTERMITTENT DURING ALL THE FLIGHT. AT HMar 5, 2002 · N214AM · Doug DC987 · Integrated Flight SystemSDR MEX2002046Control Valve · failedHMO-LAS - WHEN LANDING GEAR GOT DOWN, ANTI-SKID IGHTS TURNED ON. AS CONSEQUENCE OF SPARE PARTS MISSING, AN AIRCRAFT CHANGE TOOK PLACE. LEFT ANTI-SKID DUAL CONTROL VALVE WAS REPLACED IAW MM 32-43-02, TESTS WERE PERFORMED OK.Feb 21, 2002 · N214AM · Doug DC987 · Brake Anti-Skid Section
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