N859AM
Service difficulty reports · 31
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 = 'N859AM' 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 = 'N859AM' 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 ASMF20190109011Sensor · defectiveCAPTAIN REPORTED THAT BEFORE TAXYING, THE LE FLAPS TRANSIT LIGHT TURNED ON; MAINTENANCE PERSONNEL PERFORMED CHECK AND LIGHT LE FLAP TRANSIT WAS DEFERRED IAW MEL 27-04-02B; AIRCRAFT REJECTED TAKEOFF AT 20 KNOTS, DUE TO LE FLAPS EXT LIGHT TURN ON; MAINTENANCE PESDR ASMF20180918015Fuse · brokenDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING THAT THE HYDRAULIC LEAK WAS OUT OF LIMIT AND HYDRAULIC PRESSURE FUSE WITH THEIR LEVER BROKEN. THE HYDSDR ASMF20180918003Pin · damagedDURING TRANSIT CHECK, THE CREW OXYGEN FIRST OFFICER TEST WAS NOT SATISFACTORY WITH YELLOW LIGHT TURNED OFF. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE FIRST OFFICER OXYGEN MASK PANEL DOOR PIN DAMAGED; THEREFORE THE OXYGEN MASK PANEL DOOR PIN WAS RESDR ASMF201706001Adc · damagedAIRCRAFT REJECTED TAKE OFF AT 82 KNOTS DUE TO SPEED AND ALT FLAGS ON LEFT PDF, MAINTENANCE REPLACED THE LEFT ADM PITOT IAW AMM 34-21-04, TESTED CORRECT.SDR ASMF201704009Slide · low pressureDURING THE TRANSIT CHECK, THE ESCAPE SLIDES OF THE FORWARD AND REAR LEFT DOORS WERE FOUND OUT OF RANGE OF PRESSURE. THEREFORE MAINTENANCE PERSONNEL REPLACED THE ESCAPE SLIDE PACKS IAW AMM 25-66-01, TESTED CORRECT.SDR ASMF201702002Actuator · failedAIRCRAFT RETURNED TO GATE DUE TO THE LEFT ENGINE AT START AN CONTROL LIGHT TURNED ILLUMINATED. PERFORMED A BITE TO THE LEFT EEC IAW AMM 73-21-00, SHOWING FAILURE CODE 73-31481. THE LEFT REVERSER SLEEVE POSITION SIGNAL OUT OF RANGE. THE LEFT REVERSER ACTUATOSDR ASMF201611023Hydraulic Line · looseDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR PIT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK IN THE MODULAR PACKAGE FLIGHT CONTROL PRESSURE LINE IAW AMM 29-11-00. THE LINE WAS TIGHTENED IAW AMM SDR ASMF201611019Shutoff Valve · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESSURE LOW INDICATION IN THE RIGHT ENGINE, SHOWING 5 PSI. MAINTENANCE PERSONNEL PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE RIGHT ENGINE PRSOV. THE RIGHT ENGINE PRSOV AND THE RIGHT PRECOOLER SDR ASMF201611004Fastener · damagedDURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED ON LEFT WINGLET TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES IN THREE FASTENERS AND IN THE LEFT WINGLET TRAILING EDGE SKIN OF 2.2 INCHES LENSDR ASMF201610013Skin · damagedDURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED ON LEFT WINGLET TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES IN THREE FASTENERS AND IN THE LEFT WINGLET TRAILING EDGE SKIN OF 2.2” LENGTH, 0SDR ASMF201610005Static Inverter · failedCAPTAIN REPORTED THAT DURING TAXING TO PLATFORM, THE ELEC LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED ELECTRIC SYSTEM AUTO TEST IAW FIM 24-31 TASK 801 PROCEDURE, DETECTING THE STATIC INVERTER WITH FAILURE; SO THE STATIC INVERTER WAS REPLACED IAW AMM 24-34SDR ASMF20160620006Gasket · damagedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CRUISE AT 370 FL, THE
EICAS MESSAGE OF ENGINE FLAMEOUT AND LT ENGINE SHUTDOWN. THE FLIGHT CREW PERFORMED THE QRH 7.18 PROCEDURE WITH 2 INTENTS OF LT ENGINE START AND NOT INCREASE OF EGT, CONFIRMING THE SDR ASMF201602003Coupling · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE MAIN BRAKE NR 4. PERFORMED REVISION DETECTING HYD LINE COUPLE LEAKING OF THE MAIN BRAKE NR 4, THE HYD LINE COUPLE & PACKING SEAL WERE REPLACED IAW AMM 32-41-11, TESTED CORRECT.SDR ASMF201511006Unknown · smokeDURING TRANSIT CHECK, BURNING ODOR WITH NO EVIDENCE OF SMOKE WAS DETECTED IN AFTER GALLEY. PERFORMED SMOKE OR FUMES CONDITIONAL INSPECTION IN CABIN IAW MM 05-51-56 & FIM 21-00 TASK 806 PROCEDURE, NO ODOR OR SMOKE EVIDENCES WERE FOUND. THE AIR CONDITIONING SYSDR ASMF201511004Sealant · deterioratedDURING OVERNIGHT CHECK, TECHNICAL PERSONNEL DETECTED A FUEL LEAK BY SEALANT DETERIORATED ON LT WING LOWER SKIN AT STRINGER L9 & WS 523 - 292. REPLACED THE SEALANT DETERIORATED IAW AMM 28-11-00, ALL CORRECT.SDR ASMF201510031Blade · faultyDURING CLIMB, THE RT ENG VIBRATION REACHED 4.6 UNITS. ACCOMPLISHED THE QRH 7.24 PROCEDURE & THE VIBRATION WAS STABILIZED IN 4.0 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED A BORESCOPE INSPECTION TO BOOSTER BLADES STAGES 2 - 4 & LPT STAGES 1 - 3 IAW AMMSDR ASMF201510026Fan · lack of lubeDURING CLIMB, THE RT ENG VIBRATION REACHED 2.0 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. A BORESCOPE INSPECTION TO LPT STAGES 1 - 3 IAW AMM 72-00-00, NO DAMAGES WERE FOUND. LSDR ASMF201501021Pump · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE RT ENG. PERFORMED REVISION DETECTING HYD LEAK AT THE ENG DRIVEN PUMP DRAIN PORT. THE ENG DRIVEN PUMP WAS REPLACED IAW MM 29-11-11, TESTED CORRECT.SDR ASMF201501019Blade · damagedDURING TRANSIT CHECK, IT WAS DETECTED NICKS IN TWO INLET CASE FAN BLADES OF THE RT ENG. PERFORMED REVISION DETECTING TWO NICKS OUT OF LIMIT IAW AMM 72-24-02. INSPECTION PERSONNEL EVALUATED THE DAMAGE, CONFIRMING THE NICKS OUT OF LIMITS IAW AMM 72-24-02. THESDR ASMF201409010Warning System · false activationAIRCRAFT REJECTED TAKE OFF AT 60 KNOTS DUE TO THE ENTRY DOOR LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, NO CONFIRMING THE FAILURE & INITIATING AGAIN SEQUENCE OF TAKEOFF. AS PRECAUTIONARY ACTION, PERFORMED BITE TO ENTRY DOOR FLIGHT LOOKSDR ASMF201408003Connector · looseDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED OF 2 DROPS PER MINUTE IN THE NOSE WHEEL STEERING. DURING MX REVISION, THE RT NOSE WHEEL STEERING CYLINDER CONNECTOR WAS DETECTED LEAKING WITHIN LIMITS, SO THE STEERING CYLINDER CONNECTOR WAS TIGHTENED & CLEANED IASDR ASMF201311223001Bleed Valve · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG WITH 50 DROPS PER MINUTE. MX PERSONNEL DETECTED TRANSIENT BLEED VLV WITH LEAK WITHIN OPERATION LIMITS IAW MM 71-71-00 PAGE 6, DISPATCHING THE ACFT IN SUCH CONDITION. AT GDL, MX PERSONNEL REPLACSDR ASMF201311080001Door · out of adjustDURING CLIMB ACFT DID NOT PRESURIZE. AIRCRAFT RETURNED TO DEPARTURE. MAINTENANCE PERFORMED ADJUSTMENT OF THE PASSENGERS DOOR IAW AMM 52-11-00-820-801 AND TESTED IAW AMM 52-11-00-700-804, ALL CORRECT.SDR ASMF201304001Rib · brokenDURING TRANSIT CHECK, THE LOWER CAP RIB IN LT MAIN OTBD FLAP T/E WAS DETECTED BROKEN. MX PERSONNEL REPLACED THE LT WING OTBD AFTER FLAP IAW AMM 27-51-22, ALL CORRECT.SDR ASMF201211003Pressure Switch · failedACFT RETURNED TO DEPARTURE, DURING CRUISE BOTH AUTOPILOTS WERE OUT OF SERVICE. MX PERSONNEL DEFERRED THE REPORT IAW MEL 22-1, CAT B. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE ACFT LANDED WITH 62,900 KILOGRAMS AND THE MAXIMUM ALLOWABLE LANDING WEISDR ASMF201204005Skin · damagedDURING OVERNIGHT CHECK, MX PERSONNEL DETECTED A SCRATCH IN THE SKIN FUSELAGE OF THE 1.5" LONG, 0.084" WIDE BETWEEN LONGERONS 22 AND 23, AT STATION 848. FOUND WITHIN LIMITS IAW SRM 51-00-01 ALLOWABLE DAMAGE 1, PARAGRAPH 4B (2) (A) FIGURE 103 DETAILS P AND Q. SDR ASMF201204004Bypass Valve · stuckACFT RETURNED TO PLATFORM DUE TO DURING TAXING THE NOSE WHEEL STEERING WAS STUCK. MX PERSONNEL PERFORMED THE FIM32-51 TASK 808, DETECTING THE BYPASS VALVE STUCK; SO THE VALVE ASSY WAS LUBRICATED IAW FIM TASK 32-51-00-200-801, TESTED CORRECT.SDR ASMF20120216007Skin · dentedDURING TRANSIT CHECK, MX PERSONNEL DETECTED A DENT OF 1.750" LONG, 1.5" WIDE AND 0.061" DEPTH ON FUSELAGE SKIN AT STA 384, BETWEEN STRINGERS 21 AND 22 RT SIDE. MX PERSONNEL CONFIRMED THAT THE DENT WAS OUT OF LIMITS IAW SRM 53-00-01. MX PERSONNEL ISSUED THE NONSDR ASMF201108002Brake Assy · cloggedCAPTAIN REPORTED UNUSUAL RT LANDING GEAR VIBRATION DURING PUSH BACK; MX INSPECTED THE RT LANDING GEAR, DETECTING THE MLG BRAKE NR 3 WITH 3 PISTONS CLOGGED, BRAKE WAS REPLACED IAW AMM 32-41-41, TESTED CORRECT.SDR ASMF201107001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL, NR 532QB; SO IT WAS TIGHTEN AND THE FUEL LEAK WAS EVALUATED IAW MM 28-11-00 FOUND IT WITHIN LIMITS, DISPATCHING THE ACFT IN THIS CONDITION. SDR ASMF201105006Fuel Control · leakingDURING ENGINES START, A FUEL LEAK WAS DETECTED IN THE LT ENGINE. MX PERFORMED GENERAL VISUAL INSP IAW MM 73-21-00 AND LT ENGINE WAS STARTED IAW MM 80-00-00, NO LEAKS WERE DETECTED.
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