N359AM
Service difficulty reports not matched to an aircraft · 16
They name N359AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N359AM' AND registry_match IS NULL 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 = 'N359AM' AND registry_match IS NULL 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 ASMF201503005Flap · crackedDURING TRANSIT CHECK, THE LT OTBD AFTER FLAP WAS DETECTED CRACKED. PERFORMED REVISION IN THE LT FLAP DETECTING A CRACK OF 8.0” LENGTH & A PUNCTURE OF 1.0” DIAMETER, A DENT OF 4.0” LENGTH, 0.090” DEPTH, 2.375” WIDE AT STATION OTEF 96.65, A DENT OF 2.125” LENGTSDR ASMF201501020Light · inoperativeDURING FUELING, THE LT AFT EMER EXIT LIGHT WAS DETECTED INOPERATIVE. THE FUELING WAS STOPPED & THE EMER EXIT LIGHT WAS REPLACED IAW AMM 33-50-00, TESTED CORRECT.SDR ASMF2014061706005Fuel Heater · leakingDURING RT ENG TEST RUNNING, DETECTED A FUEL LEAK AT RT ENG FUEL SERVO HEATER. THE SERVO HEATER WAS REPLACED IAW AMM 73-11-07, TESTED CORRECT.SDR ASMF201403016Warning Light · false indicationAIRCRAFT REJECTED TAKEOFF AT 50 KNOTS, DUE TO AFT CARGO DOOR LIGHT TURNED ON. PERFORMED REVISION TO THE AFT CARGO DOOR, NO FAILURE WAS DETECTED.SDR ASMF201403001Adiru · inoperativeAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO DURING CRUISE THE RT ADIRU WAS INOPERATIVE. AT HMO, MX PERFORMED THE LT ADIRU OPERATIONAL TEST IAW AMM 34-21-01, TESTED CORRECT. THE RT ADIRU REPORT WAS DEFERRED IAW MEL 34-35 CAT B. AT GDL, MX REPLACSDR ASMF201402002Regulator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG. MX PERSONNEL DETECTED THE RT ENG BLEED AIR REGULATOR DRAIN WITH FUEL LEAK WITHIN OPERATIONAL IAW MM 71-00-00, DISPATCHING THE AIRCRAFT IN SUCH CONDITION. AT GDL, MX PERSONNEL REPLACED RT ENG BLSDR ASMF201312009Engine · dirtyCAPTAIN REPORTED THAT DURING TAKEOFF, THE LT ENG REACHED 977 CELSIUS DEGREES OF EGT FOR AROUND 1 SECOND. PERFORMED FIM 71-06 TASK 805 PROCEDURE, LT ENG GAS PATH CLEANING IAW AMM 72-00-00 TASK 803 & IDLE LEAK CHECK IAW AMM 71-00-00, TESTED CORRECT.SDR ASMF2013110800008Receiver · failedACFT RETURNED OF FLIGHT DUE TO EICAS MESSAGE FRM’S 342 - 440-00, 345 - 030-02, 345 - 050-02 AND 345 - 060-02. MAINTENANCE PERFORMED THE FIM 34-51 TASK’S 801, 802, 805 AND 806 PROCEDURE. VOR/MARKER AND FMC WERE REPLACED IAW AMM 34-51-01 AND AMM 34-61-02, TESTSDR ASMF201303007Snubber · crackedDURING TRANSIT CHECK, IT WAS DETECTED A CRACK AT THE EXTERNAL SKIN LOWER HINGE. MX PERSONNEL PERFORMED REVISION DETECTING THE EXTERNAL SKIN LOWER HINGE OUT OF LIMITS IAW SRM 52-10-01 PARA B (1)(A). THE ACFT WAS INSPECTED AND FOUND SAFE FOR THE INTENDED SPECISDR ASMF201204008Blade · damagedDURING A BORESCOPE INSPECTION OF THE HPT 1ST STAGE BLADES OF THE LT ENGINE WAS DETECTED 1 BLADE OF THE HPT 1ST STAGE WITH A CRACK OUT OF LIMITS IAW MM 72-00-00 PARAGRAPH G 1(A), WITH DIMENSIONS OF 0.125" LONG IN THE T/E AREA. MX PERSONNEL REPLACED AND TESTED SDR ASMF20120420007Probe · damagedCAPTAIN REPORTED THAT DURING TAKEOFF, THE LT ENGINE WAS REACHED 969 C FOR AROUND 12 SECONDS; SO FLIGHT CREW IMMEDIATELY REDUCING THRUST AND AFTER THE REDUCTION, THE LT ENGINE INDICATION WAS SHOWED NORMAL AND IT WAS ACCOMPLISHED THE QRH 8.5 PROCEDURE AND CONTINSDR ASMF201111008Regulator · failedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CLIMB THE LT ENGINE PURGE INDICATED 5 PSI, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE. MX PERFORMED THE FIM 36-10, TASK 804 DETECTING VALUES WITHIN LIMITS, NO FAILURE WAS FOUND; REFUEL WAS PERFORMED. ASDR ASMF201111007Circuit Breaker · failedACFT REJECTED TAKEOFF AT 60 KNOTS AND A GROSS WEIGHT OF 57,800 KG DUE TO LT FWD AND AFT EMERGENCY EXIT OVERWING LIGHTS TURNED ON. MX RESEATED THE PRIMARY PSEU IAW FIM 52-20 TASK 806 AND MM 52-22-00, NO FAILURES FOUND; AS PRECAUTION MX DEFERRED THE REPORT IAW SDR ASMF201109008Valve · damagedCAPTAIN REPORTED MAIN TANKS FUEL IMBALANCE FROM 300 KGS TO 400 KGS. MX PERFORMED CROSS FEED VALVE OPS TEST IAW MM 28-22-00, DETECTING THE RESULTS WERE OPS OUT OF LIMITS, BEING THE FUEL TRANSFERENCE OF 500 KGS IN TWO MINUTES. THE FUEL CROSSFEED VALVE WAS REPLASDR ASMF201108009Valve · leakingDURING TRANSIT CHECK IT WAS DETECTED A FUEL LEAK IN THE RT ENGINE WITH MORE THAN 180 DROPS PER MINUTE. MX PERFORMED REVISION DETECTING THE HPTACC VALVE WITH LEAK OUT OF OPERATION LIMIT, SO THE HPTACC VALVE WAS REPLACED IAW MM 75-21-01, TESTED CORRECT.SDR ASMF201006003Pseu · malfunctionedACFT REJECTED TAKEOFF AT 60 KNOTS DUE TO RT FWD AND AFT OVERWING LIGHTS TURNED ON. MX PERSONNEL RESEATED THE PRIMARY PSEU IAW FIM 52-20 TASK 806 AND ALL LIGHTS EXTINGUISHED, DELIVERING ACFT TO SERVICE, ALL CORRECT. THE HIGH ENERGY STOP INSP WAS NOT NECESSARY D
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