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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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, SDR 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 SDR 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 SDR 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 ANSDR 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.SDR 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.SDR 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.SDR 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 DETECTEDSDR 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.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 DESDR 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 SDR 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 STASDR 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 IAWSDR 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 ESDR 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 CABLESDR 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.SDR 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. SDR 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 PNSDR 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 THSDR 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 SDR 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 REPLACSDR 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 CHSDR 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. (SDR 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.SDR 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 VALVESDR 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)SDR 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 HSDR 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.
Back to N214AM, cancelled Aug 12, 2010