N805AM, cancelled Jul 31, 2012
Service difficulty reports · 21
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 = 'N805AM' AND deregistration_id = 'N805AM-2012-07-31' 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 = 'N805AM' AND deregistration_id = 'N805AM-2012-07-31' 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 ASMF200707009Landing Gear · inoperativeAIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, TECH DETECTED THE LOCK PIN OF THE NOSE LANDING GEAR INSTALLED, SO IT WAS REMOVED AND AIRCRAFT WAS DISPATCHED. OVERWEIGHT LANDING INSPECTION WAS NOT NECESSARY, AIRCRAFT LANDED WITH 73900 POUNDSSDR ASMF200703004Idg · leakingAIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO (L GEN) LIGHT TURNED ON IN EICAS. DURING MAINTENANCE CHECK, THE LT IDG WAS DETECTED WITH LOW OIL LEVEL. FAILURE WAS DEFERRED BY MEL 24-00-1, THE LANDING GEAR AND BRAKES WERE CHECKED BY CONDITION, BEING ALL CORRECT. SDR ASM200608020Actuator · leakingDURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT RUDDER ACTUATOR. RUDDER ACTUATOR WAS REPLACED IAW MM 27-21-20, TESTED CORRECT.SDR ASMF200607017Pdu · malfunctionedCAPTAIN REPORTED THAT DURING APPROACH THE LT FLAP/SLAT SYSTEM DID NOT OPERATE HYDRAULICALLY IN NORMAL MODE PROCEEDING TO THE ALTERNATE MODE AND FLAPS DISAGREE MESSAGE APPEARED IN EICAS. FIM 27-51-00 PROCEDURE AND BITE 27-7 WERE PERFORMED TO FSEU SHOWING PDU/TSDR ASMF200512015Iru · failedDURING TRANSIT CHECK, THE LT RDMI SHOWED HDG AND VOR FLAGS. THE SENSORS WERE CHECKED IN FMC SHOWING THAT THE THREE INERTIAL UNITS WERE CORRECT; THE LT AND CENTRAL IRS ALIGN PROCEDURE WAS PERFORMED AND THE RMIS WERE INTERCHANGED, BUT FAILURE CONTINUED. THE RT ASDR ASMF200511009Starter · damagedDURING LT ENGINE STARTING, THE PNEUMATIC STARTER FAILED. DURING MAINTENANCE REVISION WAS DETECTED THE PNEUMATIC STARTER WITH DAMAGE, SO IT WAS REPLACED IAW MM 80-11-01 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT.SDR ASMF200506013Idg · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING THE LEFT ENGINE STARTED, THE N2 REACHED 30 PERCENT AND IT DID NOT INCREASE. THE LEFT ENGINE WAS STARTED AGAIN OPENING THE STARTER VALVE MANUALLY AND IT STARTED TO SLOW, APPEARING THE L DRIVE AND L GEN OSDR ASMF200506003Idg · failedAIRCRAFT RETURNED, LT GENERATOR FAILURE, APU DID NOT START AT 35 000 FT, 24 22 25 EICAS MESSAGES, 01 GEN OFF DISPLAYED AND 01 AS BUSS OFF REMAINED ILLUMINATED. QRH ABNORMAL PROCEDURE WAS PERFORMED, PAGE 09-03, RETURNING. DURING TEST WAS DETECTED LOW QUANTITY OSDR ASMF200505027Engine · failedCAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITCH WAS SHUT OFF AND THE ACCELERATOR WAS HELD BUT LIGHT CONTINUED. ENGINE WAS SHUT DOWN. AT PLATFORSDR ASMF200409004Heat Exchanger · leakingDURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AND LEAK INCREASED. FUEL/OIL HEAT EXCHANGER WAS REPLACED IAW MM 79-21-00, TEST CORRECT. DURING OVERNIGHT SERVICE, ENGINE RUNNING WAS PERFORMESDR ASMF200405027Valve · failedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL STATUS WERE CHECKED, ALL CORRECT. LT SPAR FUEL SHUTOFF VALVE WAS OPERATED MANUALLY AND IT WAS WITH FASDR MEX2004019Thrust Reverser · failedDURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN COVERS. THE CABLE BESDR MEX2003560Indicator · leakingFLT 494 - MEX-LAX - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING IN GDL AS CONSEQUENCE OF THE RIGHT QUANTITY INDICATION DECREASE TO .08 QUARTS. AT PLATFORM, THE HYDRAULIC SYSTEM WAS REPLENISHED TO DETECT THE LEAKAGE, THE DIFFERENTIAL PRESSURE INDICATOR WAS REPLASDR MEX2003534Pitot Tube · damagedAIRCRAFT RETURNED TO GATE DUE TO (R AUX PITOT) LIGHT WAS TURNED ON AND THE CABIN TEMPERATURE CONTROL HAD A FAILURE, TEMP REACHED 37 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RELATED PITOT WIRES/CONNECTORS AND THE CABIN SDR MEX2003273Antenna · failedAIRCRAFT ARRIVED WITH CAPTAIN REPORT RADAR OUT OF SERVICE. DURING REVISION WAS DETECTED WAVE GUIDE WITH DAMAGE. AIRCRAFT WAS SENT TO THE HANGAR, AND THE WAVE GUIDE WAS REPLACED IAW 34-40-01. ADDITIONALLY AS A PREVENTIVE ACTION ANTENNA RADAR WAS REPLACED, ALSDR MEX2003150Control Unit · failedDURING TRANSIT CHECK CAPTAIN REPORTED NORM ANTI-SKID AND ALTN ANTI-SKID MESSAGES IN EICAS. MESSAGE APPEARED EVERY TIME THAT THE PARKING BRAKES WERE USED. FIM PROCEDURE WAS ACCOMPLISHED BUT NO FAILURE CODE APPEARS. AIRCRAFT WAS SENT TO THE HANGAR. ANIT-SKIDSDR MEX2003016Warning System · malfunctionedFLT 600 - MEX-ALT - AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, MESSAGE EICAS STATUS MAIN BATTERY CHARGE. RESET PROCEDURE WAS PERFORMED AND MESSAGES WAS ERASED, BUT WHEN BATTERY AND BARS WERE DISCONNECTED MESSAGES EICAS STATUS LEFT AND RIGHT CONTRSDR MEX2002346Indicator · malfunctionedFLT 171 - JIJ- DURING TAKEOFF EPR INDICATIONS WAS BLANK RIGHT ENGINE AND N1 WITH FLUCTUATIONS AT REDUCE POWER ON RIGHT ENGINE AFTER 5 MINUTES INDICATIONS WAS NORMAL. AFTER 35 MINUTES IN FLIGHT RETURNED TO AIRPORT. AT PLATFORM, TECHNICAL PERSONNEL CHECKED CHPSDR MEX2002297Hydraulic Line · leakingFLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN REVIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A PIPELINE FROM THE FILTERS TO THE WHEELS. PIPELINE WAS REPLACED IAW MM 29-11-17, TESTS OK. (M)SDR MEX2002145Warning System · activatedFLT 902 - MEX-MTY - AIRCRAFT RETURN TO GATE DUE TO CENTRAL AND LEFT HYDRAULIC SYSTEM RSVR LIGHT CAME ON. SUPPLY LINES AND DEPRESSURIZATION VALVES WERE CHECKED NO DAMAGE WAS FOUND. NITROGEN SYSTEM WAS SERVICED AND WAS TESTED IAW MM 29-11-00. DURING OVERNIGHTSDR MEX2002187Slide · out of adjustFLT 170 - MEX-TIJ - CAPTAIN REPORTED THAT THE DOOR NR 1 SLIDE WAS NOT ARMED. DURING CHECK WAS DETECTED THAT THE ARMED LIGHT WAS INOPERATIVE AND THE ACTIVATION MECHANISM WAS IN AN ABNORMAL POSITION. TECHNICAL PERSONNEL TRIED TO REMOVED THE DOOR COVER AND THE
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