N906AM
Service difficulty reports not matched to an aircraft · 33
They name N906AM, 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 = 'N906AM' 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 = 'N906AM' 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 ASMF20180821005Actuator · leakingDURING A PERIODIC CHECK, DETECTED A HYDRAULIC LEAK THROUGH THE BODY OF LEFT MAIN LANDING GEAR RETRACT ACTUATOR. MAINTENANCE REPLACED THE LEFT MLG RETRACT ACTUATOR IAW MM 32-32-11, TESTED CORRECT.SDR ASMF201801006Window · crackedDURING A TRANSIT CHECK, FOUND THE RIGHT SIDE WINDOW CRACKED. MAINTENANCE PERFORMED AMM 56-12-11, CONFIRMING THE RIGHT SIDE WINDOW CRACKED AND OPERATIONAL OUT OF LIMITS. THE RIGHT SIDE WINDOW WAS REPLACED IAW AMM 56-12-11.SDR ASMF201710090001Static Inverter · failedCAPTAIN REPORTED THAT DURING TAXING TO PLATFORM, THE ELEC LIGHT TURNED ON. MAINTENANCE PERFORMED ELECTRICAL SYSTEM AUTO TEST IAW FIM 24-31, TASK 801 PROCEDURE, SHOWING FAILURE CODE IN P5-13 AND DETECTING THE STATIC INVERTER FAILED. THE STATIC INVERTER WAS SDR ASMF201611022Bleed Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RIGHT ENGINE. THE PLATFORM WAS CLEANED AND MAINTENANCE PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE WITH 4 DROPS PER MINUTE WITHIN OPERATION LIMITS IAW AMM 71-71-00 PAGE 6, DISPASDR ASMF201606002Unknown · malfunctionedCAPTAIN REPORTED THAT DURING CLIMB, THE MAIN AND NOSE LANDING GEARS WERE NOT RETRACTED WHEN LANDING GEAR LEVER MOVED TO UP POSITION AFTER TAKEOFF. THE FLIGHT CREW ACCOMPLISHED THE QRH 14.8 PROCEDURE AND MANUAL GEAR EXTENSION ACCESS DOOR CYCLED OPEN, CLOSE GEASDR ASMF201510020Sensor · failedDURING START ENGINES, THE LE FLAPS TRANSIT LIGHT TURNED ON. PERFORMED BITE TO FSEU IAW FIM 27-88 TASK 810 PROCEDURE, SHOWING FAILURE CODE 27-81215 SL8 PROX INBD, SO SLAT NR 8 WAS DEFERRED IAW MEL 27-4-6 CAT C. DURING OVERNIGHT CHECK, THE FIM 27-88 TASK 804 PRSDR ASMF201507015Window · crackedCAPTAIN REPORTED THAT AT 39,000 FEET, THE LT WINDOW NR 1 CRACKED. ACCOMPLISHED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE & CONTINUING TO DESTINATION. REPLACED THE LT WINDOW NR 1 & WINDOW HEAT CONTROLLER MODULE IAW AMM 56-12-11 & AMM 30-41-11, TESTED CORSDR ASMF201503019Actuator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. PERFORMED BITE TO FSEU IAW FIM 31-51 TASK 801, NO CONFIRMING FAILURE, TESTED CORRECT. THE ACFT WAS SENT TO THE HANGAR & AS PRECAUTIONARY ACTIONS, THE AUTO SPEED BRAKE ACTUATOR WAS RSDR ASMF201503016Pump · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL LEAK WAS DETECTED. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERFORMED REVISION, DETECTING FUEL LEAK IN THE MAIN FUEL PUMP DRAIN PORT. THE RT ENG WAS MOTORING, AFTER IT WAS STARTED & ENG OPERATISDR ASMF201503015Static Inverter · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ELEC LIGHT TURNED ON. PERFORMED ELEC SYS AUTO TEST IAW FIM 34-31 TASK 801, DETECTING THE STATIC INVERTER WITH FAILURE. THE STATIC INVERTER WAS REPLACED IAW AMM 24-34-21, TESTED CORRECT.SDR ASMF201501025O-Ring · damagedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL & HYD LEAKS WERE DETECTED. THE PLATFORM WAS CLEANED. PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VLV DRAIN PORT. THE RT ENG WAS MOTORING AFTER IT WAS STARTED & ENG OPERATIONSDR ASMF201409004Transceiver · failedCAPTAIN REPORTED THAT DURING CRUISE, THE WXR FAIL ON BOTH SIDES LIGHT TURNED ON WITH INTERMITTENT FAULT. PERFORMED REVISION DETECTING THE RADAR FAILED, SO THE WEATHER RADAR & WEATHER RADAR SINGLE MOUNT WERE REPLACED IAW AMM 34-43-41 & AMM 34-43-31, TESTED CORRSDR ASMF201409003Transceiver · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MSGS. PWS FAIL & WXR FAIL. PERFORMED REVISION DETECTING THE TRANSCEIVER FAILED, SO THE WEATHER RADAR TRANSCEIVER & WEATHER RADAR SINGLE MOUNT WERE REPLACED IAW AMM 34-43-41 & AMM 34-43-31, TESTED CORRECTSDR ASMF2014061706009Windshield · abnormalDURING TRANSIT CHECK, IT WAS DETECTED SCRATCHES IN BOTH COCKPIT WINDSHIELD. PERFORMED REVISION DETECTING SCRATCHES OUT OF LIMITS SO BOTH COCKPIT WINDSHIELDS WERE REPLACED IAW AMM 56-11-21, TESTED CORRECT.SDR ASMF201403004Blade · lack of lubeAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG VIBRATION REACHED 0.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE RT ENG FAN ROTOR BLADES & FAN DISK IAW AMM 72-21-02 & VIBRATION TEST NR 7 WAS PERFORMED IAW MM 72-00-00, SDR ASMF201403003Winglet · damagedDURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED IN RT WINGLET TE. MXL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES OUT OF LIMITS IN THE RT WINGLET. ACFT WAS SENT TO THE HANGAR & THE NRC A0214857 & A0214858 WERE ISSUED TO RESDR ASMF201402006Nose Cowl · scratchedDURING TRANSIT CHECK, DETECTED A SCRATCH IN THE LT NOSE COWLING AT 05:30 HRS POSITION. MX PERSONNEL PERFORMED REVISION DETECTING A SCRATCH OF 2” LENGTH IN THE LT NOSE COWLING OUT OF LIMITS IAW SRM 54-10-01 ALLOWABLE DAMAGE 1, FIGURE 103 DETAIL C. THE NRC A02SDR ASMF201301004Seal · leakingAIRCRAFT RETURNED TO PLATFORM, NLG SHOCK STRUT HYD LEAK. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE ACTIVE SEALS IAW MM 32-21-11, TESTED CORRECT.SDR ASMF201211001Regulator · damagedREJECTED TAKEOFF AT 60 KNOTS DUE TO LT ENGINE PRESSURE DROP OF 15 PSI IN PNEUMATIC DUCT AND LT OVER WING LIGHT TURNED ON. MX PERSONNEL REPLACED THE BLEED AIR REGULATOR, 450 DEGREE THERMOSTAT, PRSOV AND PRECOOLER CONTROL VALVE WERE REPLACED IAW MM 36-11-03, MMSDR ASMF201112003Skin · dentedDURING OVERNIGHT CHECK, MX DETECTED A DENT IN THE RT HORIZONTAL STAB L/E AT STA 181.23 OF 4.150" LONG AND 0.270" DEPTH, IT WAS CONFIRMED THAT DENT WAS OUT OF LIMIT IAW SRM 55-10-01. THE HORIZONTAL STAB L/E WAS REWORKED IAW SRM 55-10-01 PARAGRAPH 4 (D) (3) FIGUSDR ASMF201108010Door · out of adjustACFT RETURNED TO DEPARTURE DURING CLIMB, THE ACFT DID NOT PRESSURIZE WITH DOOR TOTALLY CLOSED AND PRESSURE LIGHT REMAINING OFF. DURING MX REVISION, THE FORWARD ENTRY DOOR WAS DETECTED .5" MISADJUSTED, BEING NECESSARY TO PERFORM SEVERAL CYCLES UNTIL CLOSE, AS SDR ASMF20110712Manifold · leakingDURING FUELING SERVICE, DETECTED A FUEL LEAK THROUGH THE ACFT FUEL MANIFOLD, MX TIGHTEN THE SCREWS IAW AMM 28-21-11 CORRECTING THE LEAK.SDR ASMF201010003Carbon Seal · damagedDURING TRANSIT CHECK, TECH DETECTED AN OIL LACK IN THE IDG GEARBOX CARBON SEAL IN THE LT ENGINE. ACFT WAS SENT; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 72-60-00 AND MM 24-11-11, ALL CORRECT.SDR ASMF201009008Seal · out of positionACFT RETURNED, DURING TAKEOFF AND INITIAL CLIMB, A FUEL LEAK WAS FOUND ON RT WING. MX PERFORMED FUSELAGE AND WING INSP DETECTING FUEL LEAK ON RT LOWER WING DUE TO THE SEAL OF THE FUEL TANK ACCESS DOOR PANEL, NR 533BB, WAS FOUND OUT OF POSITION, SO IT WAS REPLASDR ASMF201009005Skin · dentedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT OF 12.00 X 3.50 INCHES, WITH 0.400 INCH DEPTH LOCATED IN STA 78.5. THE RT SIDE HORIZONTAL STABILIZER L/E WAS SDR ASMF200904004Engine · failedCAPTAIN REPORTED THAT DURING CRUISE THE RT ENGINE LOW OIL PRESS ALERT CAME ON, SO THEY PERFORMED THE SPECIAL ENGINE OIL PRESS PROCEDURE AND SHUTDOWN THE ENGINE. MX PERSONNEL SENT THE ACFT TO THE HANGAR AND REPLACED THE RT ENGINE IAW AMM 72-00-02, TESTED CORRECSDR ASMF20090404Engine · failedCAPTAIN REPORTED THAT DURING CRUISE, IN THE ENG, NR 2 THE LOW OIL PRESS ALERT CAME ON, THE QRH PROCEDURE WAS FOLLOWED BY AN ENGINE FAILURE OR SHUTDOWN PROCEDURE. MX PERSONNEL SENT THE ACFT TO THE HANGAR AND WAS REPLACED AND TESTED THE ENGINE NR 2 IAW AMM 72-00SDR ASMF200710007Engine · low pressureCAPTAIN REPORTED LT ENGINE WITH LOW PNEUMATIC PRESSURE INDICATION, RT ENGINE 40 PSI AND LT 20 PSI. MAINTENANCE PERSONNEL PERFORMED THE FIM PROCEDURE 36-10, TESTED CORRECT.SDR ASMF200708004Eec · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXI, LT ENGINE CONTROL LIGHT TURNED ON AND STAY ILLUMINATED. MAINTENANCE CLEANED PS3 AIR TUBE WITH HIGH PRESSURE NITROGEN, PERFORMED THE FIM PROCEDURE 73-26 TASK 803 AND VERIFIED AND TEST THE ELECTRICAL CONNECTOR PLUGS ON SDR ASMF200606014Engine · fodAIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE INGESTED A PLASTIC BAG DURING TAXING. RT ENGINE WAS INSPECTED IAW MM 71-00-00, SECONDARY FLOW AREA WAS CLEANED AND ENGINE WAS STARTED, ALL CORRECT. AIRCRAFT WAS DISPATCHED BUT RETURNED TO PLATFORM AGAIN, SMOKE IN TSDR ASMF200602005Unknown · unknownAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF THE 3 LAVATORIES WERE INOPERATIVE WITH NO FAILURE INDICATIONS. DURING CHECK WAS DETECTED THE BLOWER VACUUM INOPERATIVE. THE BLOWER VACUUM WAS REPLACED BUT FAILURE CONTINUED. CIRCUIT BREAKER AT E/E COMPARTMENSDR ASMF200503015Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, N1 WAS INCREASED SLOWLY AFTER EGT INDICATION. THE FAULT ISOLATION PROCEDURE 80-07, TASK 802 WAS PERFORMED AND THE RIGHT ENGINE WAS STARTED IAW MM 71-00-00, TESTED CORRECT.SDR ASMF200503007Module · failedCAPTAIN REPORTED THAT MESSAGE (SPD LIM FLAG IN PFD) WAS SHOWN. REPORT WAS DEFERRED IAW MEL 34-2-1. AIRCRAFT RETURNED TO PLATFORM BECAUSE OF MACH TRIM, AUTO SLAT, LIGHT SPEED TRIM AND YAW DAMPER FAILED. FIM 22-11 TASK 810-811 WAS PERFORMED AND THE SMYD WAS REPL
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