N484HA
Service difficulty reports · 72
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 = 'N484HA' 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 = 'N484HA' 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 HALA2010042900199Wire · disconnectedSEAT MOUNTED EXIT LIGHT INOP ROW 13. RECONNECTED WIRE, OPS CK GOOD.SDR HALA2010040400151Reservoir · leakingAFTER LANDING, LINE SERVICE REPORT SLATS HOT. R & R WING PRESSURE RESERVOIR & SLAT VALVE IAW AMM 30-11-01. OPS & LEAK CHECK OK.SDR HALA2009093000444Skin · damagedUPON LANDING IN HILO INFORMED THAT AFT CARGO OPENING (ON FUSELAGE) WAS DAMAGED. LWR RT PORTION HAD A .5" BY 1.5" PIECE OF METAL SEPARATED FROM FUSELAGE. FOUND SCUFF PLATE DAMAGED ONLY. REPOSITIONED SCUFF PLATE SURROUNDING AREA CHECK OK EDDY CURRENT CHECK OK.SDR HALA2009081100363Unknown · odorON LANDING, SMELLED BURNING ELECTICAL ODOR AFTER LANDING, GOT RT PACK OVERHEAT ON DISPLAY. IAW QRH TURNED RT PACK OFF. OK TO CONTINUE IAW MEL 21-51-01 VERFIED RT FLOW CONTROL VALVE IN CLOSED POSITION AND SECURED. OPENSDR HALA2008121100881Unknown · odorELECTRICAL SMOKE DETECTED LIGHTLY ON FLT 120, BUT ON FLT 119 THE CABIN AND PAX INQUIRED. ALSO, ICE. RAN LT AND RT PACKS GASPER FANS ENG TURNED GALLEY PWR ON. NO DEFECTS, ALL INT LTS TURNED ON, NO DEFECTS. ALSO, COCKPIT INTERIOR LIGHTS CHECK OK.SDR HALA0800574Warning Light · illuminatedAFTER ENG START RT AND LT ENG FAILURE ALERTS CAME ON. ACCOMP FIM 73-22-806 AND 807 RTS CK GOOD. OK FOR SERVICE.SDR HALA0800444Windshield · crackedATB - F/O WINDSHIELD HAS A ONE INCH CRACK LOCATED UPPER RIGHT CORNER. REMOVED F/O'S WINDSHIELD PER AMM56-11-02. INSTALLED F/O WINDSHIELD PER AMM56-11-02 FINISHED STEP 4 E(17), FINISHED M/M56-11-02 COND AND OPS CK GOOD.SDR HALA0800432Cartridge · malfunctioned"AGENT NR 1 LOW" ON. REMOVED AND REPLACED NR 1 FIRE BOTTLE PER AMM 26-21-01, OPS CHK GOOD OK TO CONTINUE. REMOVED AND REPLACED FIRE CONTAINER DISCHARGE CARTRIDGE PER AMM 26-21-02.SDR HALA0700236Skin · corrodedMODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432, JUST FWD OF STRINGER NR 2 13/8" BY 2" BY .030"DEEP. CLEANED, TREATED CORROSION PER SRM 51-10-9. REPAIRED PER M105 FILE NR 484084. PRIMED AND PAINTED.SDR HALA0700239Door Frame · crackedFOUND 3/16" CRACK ON FWD DOOR JAMB FRAME, TOP EDGE, RT WHEELWELL. BLENDED OUT CRACK PER HAL M105 FILE NR 484083. PRIMED AND PAINTED.SDR HALA0700238Fairing · crackedCRACK ON LT WING FLAP INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL M 105, FILE B10195. FABRICATED AND INSTALLED DOUBLER. INSTALLED WITH PR1440. PRIMED AND PAINTED.SDR HALA0700237Fairing · crackedCRACK ON RT WING INBOARD TRACK FAIRING (ELEPHANT EAR). REPAIRED PER HAL 105, FILE NR B10195. FABRICATED AND INSTALLED DOUBLER WITH PR1440, CORROSION PROTECT. PRIMED AND PAINTED.SDR HALA0700235Skin · corrodedMODERATE CORROSION ON SURFACE SKIN AROUND FUELING CAP AT APPROX STATION 432 BETWEEN STRINGERS NR 2 AND NR 3, 1 3/4" BY 3/4" BY .029" DEEP. CLEANED AND TREATED CORROSION PER SRM 51-10-9. PRIMED AND PAINTED.SDR HALA0700024Cable · damagedON APPROACH WHEN FLAPS WERE SEL TO 13 GOT A SLIGHT ROLL TO LEFT. AFTER LDG WHEN FLAPS WERE SEL TO 18 GOT FLAP DISAG ALEART AND CONFIG PG SHOWED L FLAP AT 13 AND R FLAP AT 19. FOUND FLAP BUS CABLE 3XA BROKEN AND BUSS 33B CRUSHED. REMOVED AND REPLACED FLAP BUSDR HALA0600877Pump · failedBTB - AFTER START NR 2 ENG RT HYD PUMP FAIL.. REPLACED NR 2 ENG DRIVEN HYD PUMP PER AMM 29-11-01. LEAK/OPS CHKS OK.SDR HALA0600842Cylinder · leakingON PUSHBACK LINE SVC OBSERVED OIL LEAK FROM NOSE WHEEL AREA. REMOVED AND REPLACED NOSE LANDING GEAR RETRACT CYLINDER IAW AMM 32-35-01 SECURITY AND LEAK CHECK OK.SDR HALA0600807Engine · faultedDURING TAXI LT ENGINE SYSTEM FAULT. INTERROGATED EEC1 NO FAULTS NOTED. ACCOMPLISHED SYS RETURN TO SERVICE TEST IAW FIM 73-21 TEST PASSED.SDR HALA0600445A/C Pack · malfunctionedBTB - RT AIR PACK SHUTDOWN (AUTO) DURING TAXI OUT. THIS FOLLOWED A OVERHEAT WARNING THAT WENT OUT BY ITSELF. PERFORMED FIM 21-22-00-810-802, NO DEFECTS NOTED, OPS CHECK USING APU AND ENG BLEED AIR.SDR HALA0600441Blade · damagedNR 1 ENGINE 1ST STAGE FOUND FOD ON 2 BLADES. ONE DAMAGED 2 INCHES FROM THE TOP, DAMAGE DEPTH - .1875 INCH, LENGTH - .5 INCH. SECOND BLADE L/E 4 INCHES FROM THE ROOT, LENGTH/DEPTH - .125 INCH. REMOVED LPC STAGE 1 BLADES PER AMM 72-38-15 INSP, ROTOR DISK PER SDR HALA0500873Eec · failedENGINE RT SYSTEM FAIL MESSAGE ILLUMINATED. REMOVED AND REPLACED EEC, OPS CHECK OK. AIRCRAFT RELEASED FOR SERVICE. (K)SDR HALA0400278Bulkhead · crackedDURING 2A CHECK, TWO CRACKS MEASURING 2.0 INCHES AND 1.5 INCHES WERE FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD AT STA 1178.225 AT LONGERON 17L, IN THE CAPS FORWARD FLANGE. REPAIR IN WORK.SDR HALA0100296Computer · malfunctionedHNL - FLT 191 - FLT CONTROL COLUMN DISCONNECT LIGHT ON IN FLIGHT. AIRCRAFT RETURNED TO HNL WHERE A UNEVENTFUL LANDING WAS MADE. REPLACED AND DATA CONCENTRATOR UNIT PER 2730 TASK 807. (M)
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