N957AM
Service difficulty reports · 24
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 = 'N957AM' AND registry_match = 'registration' 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 = 'N957AM' AND registry_match = 'registration' 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 ASMF2025070400449Anti-Skid Sys · inoperativeANTI SKID INOP, AND WAS CARRY OUT BITE AND XDCR WAS CONNECTEDSDR 2024FA0000625Tire · deflatedAC ARRIVES WITH TIRE #3 DEFLATEDSDR 2022FA0000064None · noneCAPTAIN REPORTED THAT WITH 0 UNITS OF RUDDER TRIM CONTROL WHEEL WAS LOCATED 1 UNIT TO THE LEFT. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-21 TASK 806 PROCEDURE, DETECTING THE RUDDER TRIM CONTROL WHEEL WAS NOT MOVED FREELY; SO RUDDER TRIM CONTROL WHEEL ADJUSTMSDR 2021F00354None · noneRUDDER TRIM CONTROL WHEEL WAS NOT MOVED FREELY, CAPTAIN REPORTED THAT WITH 0 UNITS OF RUDDER TRIM CONTROL WHEEL WAS LOCATED 1 UNIT TO THE LEFT. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-21 TASK 806 PROCEDURE, DETECTING THE RUDDER TRIM CONTROL WHEEL WAS NOT MOSDR 2022FA0000062Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN BRAKE ACCUMULATOR. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT BRAKE ACCUMULATOR LINE P/N AS154A04EN0294K, S/S WITH TSN 24941, CSN 9340, MANUFACTURER BOEING COMPANY; SO THE LINE WASDR 2021F00339Line · crackedHYDRAULIC LEAK IN BRAKE ACCUMULATOR. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN BRAKE ACCUMULATOR. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT BRAKE ACCUMULATOR LINE P/N AS154A04EN0294K, S/S WITH TSN 24941, CSN 9340, MANUFASDR ASMF202110010None · noneDURING TRANSIT CHECK, THE HYDRAULIC SYSTEM B WAS SHOWED WITH QUANTITY OF CERO. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING LINE TUBE HYDRAULIC SYSTEM B MAIN BAY MLG RIGHT SIDE REAR LEAKAGE; SO THE REFILL HYDRAULIC RESERVOIR A AND B STANDBY SYSTEM WAS ADSDR ASMF202110003None · noneDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE MAIN LANDING GEAR PIT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT BRAKE ACCUMULATOR LINE AT HYDRAULIC SYSTEM B IAW FIM 29-30 TASK 815 PROCEDURE; SO THE HYDRAULIC BRAKE ACCUMULSDR 2021F00237Accumulator · leaking12.07.2021 14:26 HYDRAULIC LEAK IN THE MAIN LANDING GEAR PIT. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE MAIN LANDING GEAR PIT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT BRAKE ACCUMULATOR LINE AT HYDRAULIC SYSTEM B ISDR ASMF20210621001Acoustic Panel · dentedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A DENT ON RIGHT ENGINE INLET COWL INNER BARREL ACOUSTIC PANEL LOWER QUADRANT. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.156" DIAMETER, 0.011" DEPTH AT 06:00 HOURS POSITION OF RIGHT SDR ASMF2020090707Engine · failedIAW CNR 20200615014 OF REMOTE DIAGNOSTIC GE/CFM SYSTEM, THE RIGHT ENGINE INCREASE OF VIBRATION IN CRUISE. IF NECESSARY PERFORM THE RE-LOCATION OF THE FAN BLADES ACCORDING TO THE PROCEDURE WITH THE COMPUTED METHOD MAPPING PROCEDURE, IAW AMM TASK 72-21-02-900-8SDR ASMF20200602012Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE MESSAGE IN EICAS AND STATUS OF SPOILER APPEARS AND FLAPS/SLATS INDICATOR STAYS IN POSITION 1 AND FLAP/SLAT LEVER IN POSITION 5. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING MESSAGE OF FAILURSDR ASMF202006009Computer · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXIING. MAINTENANCE PERSONNEL PERFORMED THE FIM 27-31 TASK 812/813 PROCEDURE CONTINUING FAILURE. ELEVATOR FEEL COMPUTER WAS REPLACED IAW MM 27-31-37-000/400-801, TEST CORRECT.SDR ASMF20200602008Pump · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE EDP LEAKING. THE RIGHT ENGINE EDP WAS REPLACED IAW AMM 29-11-11 AND FLUSHING TO BOTH HYDRAULIC AND STAND BY SYSTEMS WERE PERFORMSDR ASMF2019042315Antenna · failedDURING TRANSIT CHECK, MAINTENANCE PERSONNEL DETECTED FAILED OF TCAS TEST; SO MAINTENANCE PERSONNEL PERFORMED FIM 34-45 TASK 801 PROCEDURE SHOWING FAILED ON TCAS ANTENNA BOTTOM; IT WAS PERFORMED REPLACEMENT OF TCAS ANTENNA I.A.W. AMM 34-45-02,OPERATIONAL TESTSDR ASMF2019042312Trim System · malfunctionedCAPTAIN REPORTED THAT DURING TAXING TO PLATFORM, MAIN ELECTRICAL TRIM NOT WORKING; SO MAINTENANCE PERSONNEL PERFORMED OPERATIONAL TEST I.A.W.AMM 27-41-00-700-803, ALL CORRECT.SDR ASMF20180918002Actuator · failedCAPTAIN REPORTED FAILURE WITH AILERON TRIM FRM 27105042. MAINTENANCE PERSONNEL PERFORMED INSPECTION CONFIRMING FAILURE. THEREFORE ACTUATOR ELECTRONIC TRIM WAS REPLACED IAW AMM 27-11-54 AND AILERON ADJUST WAS PERFORMED IAW AMM 27-11-00, ALL TESTED CORRECT.SDR ASMF201708007Deu · malfunctionedAIRCRAFT REJECTED TAKEOFF AT 80 KNOTS DUE TO BOTH DISPLAY SOURCE OFF LIGHTS TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO CDS DEU IAW AMM 31-62-00 TASK 801 AND THE RIGHT DEU SOFTWARE WAS RESEATED IAW AMM 31-62-00 TASK 810, TESTED CORRECT.SDR ASMF201704011Warning Light · illuminatedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE ELECTRICAL HYDRAULIC PUMP SYSTEM B LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORM RESET TO CIRCUIT BREAKER OF THE ELECTRICAL HYDRAULIC PUMP IAW AMM 29-11-21 AND THE CONNECTORS WERE CHECKED IAW WDM 29-11-12, ASDR ASMF201700301004Brake · damagedDURING TRANSIT CHECK, IT WAS DETECTED THE BRAKE ASSEMBLY NUMBER 2 WITH DAMAGE. MAINTENANCE PERSONNEL PERFORMED AN INSPECTION, DETECTING CARBON FRAGMENTS AND DISC LOCK LOOSE; SO THE MAIN LANDING GEAR BRAKE AND WHEEL NUMBER 2 WERE REPLACED IAW AMM 32-41-41 AND ASDR ASMF201612012Skin · dentedDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED THE INBOARD TRAILING EDGE FLAP AND INBOARD AFT FLAP WITH DAMAGES BY FOD. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING A DENT OF 25.0” LENGTH, 55.0” WIDTH, 0.625” DEPTH BETWEEN ITEF 112.55 AND ITEF 138.05SDR ASMF20161216009Contactor · failedDURING TRANSIT CHECK, THE TRANSFER BUSS OFF LIGHT TURNED ON WITH APU AND EXTERNAL POWER. MAINTENANCE PERSONNEL PERFORMED BITE TO GCU AND BPCU IAW FIM 24-41 TASK 801 PROCEDURE, DETECTING THAT TRANSFER BAR DID NOT FEED ELECTRIC CURRENT DUE TO THE LEFT GENERATOR SDR ASMF20161216001Hmu · failedAIRCRAFT REJECTED TAKEOFF AT 70 KNOTS DUE TO RIGHT EICAS MESSAGE MASTER CAUTION AND ENGINE CONTROL LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 7.14 PROCEDURE, CONFIRMING THE FAILURE. MAINTENANCE PERSONNEL PERFORM THE FIM 73-06 TASK 801 PROCEDURE, DETECTSDR ASMF201510200001Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER START ENGINES THE ILS & GLS LIGHTS TURNED ON IN THE IRS DISPLAY PANEL WHEN MASTER CAUTION PUSHED. PERFORMED THE FIM 34-31 TASK 801 PROCEDURE, NO CONFIRMING FAILURE, TESTED CORRECT.
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