N30UA, cancelled Oct 28, 2004
Service difficulty reports · 20
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 = 'N30UA' AND deregistration_id = 'N30UA-2004-10-28' 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 = 'N30UA' AND deregistration_id = 'N30UA-2004-10-28' 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 ARWA20021101Angle · corrodedDURING "B" CHECK THE FOLLOWING WAS FOUND; CORROSION IN ANGLE IN RT WHEEL WELL UPPER FORWARD AREA AT STA 857 AND CW STA. 46. CUT OUT CORRODED AREA, TREATED AND PRIMED AREA. FABRICATED ANGLE AND INSTALLED FASTENERS AND FABRICATED SPLICE ANGLE AND INSTALLED ASDR ARWA20021002Engine · failedDURING CRUISE AT 280, NR 1 ENGINE ANTI-ICE LIGHT ON. NR 2 ERATIC FOLLOWED BY COMPRESSOR STALL. COULD NOT GET POWER OUT OF ENGINE. AT FL 280 UNABLE TO CLOSE 2N ANTI-ICE VALVE NO NR 1 ENGINE STARTED BACKFIRING AND REDUCED POWER TO PREVENT IT UNTIL POWER COMPLESDR ARWA20020807Connector · damagedNR 1 ENGINE FIRE WARNING IN-FLIGHT. PERFORMED EMERGENCY CHECK LIST AND DIVERTED TO SAN JUAN (TJST). CHECK NR 1 ENGINE FOR EVIDENCE OF FIRE OR PNEUMATIC LEAK, NONE FOUND. FOUND BOTTOM LOOP SENSOR CANNON PLUG DAMAGED; REMOVED AND REPLACED CANNON PLUG. REMOVESDR ARWA20020602Feel Unit · malfunctionedRUDDER OPERATION ERRATIC FOLLOWED ABNORMAL PROCEDURES BUT DID NOT HELP. LANDED AT MIA WITHOUT ANY FURTHER INCIDENTS. REMOVED AND REPLACED RUDDER LOAD FEEL AND TRIM MECHANISM ADJUSTMENT AND TESTED ON GROUND FOUND NORMAL IAW MM 27-23-1 AND 27-20-0. PRECAUTIONSDR ARWA20011217Oil Cap · looseDURING PUSHBACK MECHANIC REPORTED OIL LEAK ON NR 3 ENGINE, SHUTDOWN NR 3 ENGINE AND RETURNED TO RAMP UNDER TOW. FOUND NR 3 STARTER OIL CAP LOOSE, SERVICED AND SECURED OIL CAP IAW MM 80-10-0. LEAK CK ON RUN UP, NO LEAKS NOTED DURING RUN UP IAW MM 71-00. AIRCSDR ARWA0011013Thermocouple · faultyIN CRUISE AT FL 29.0 NR 1 ENGINE EGT FLUCTUATED FROM 210 C TO 380 C, ALL OTHER PARAMETERS AS FOLLOWS: EPR 1.74, N2 97.5 PERCENT, FF 4900 LBS, N1 102.5 PERCENT, OIL TEMP 76 C, OIL PRESS 52 PSI, OAT -19 C. PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLISTSDR ARWA0010717Filter · cloggedDURING FLIGHT AT LEVEL 31.0 NR 3 ENGINE FLAMED OUT, RESTARTED ENGINE FOLLOWING ABNORMAL CHECK LIST PROCEDURES. REMOVED AND REPLACED FUEL FILTERS OF NR 3 FUEL TEMPERATURE REGULATOR IAW MM 73-11-1, NO LEAKS NOTED. OPERATIONAL CHECK ON RUN UP IAW MM 71-00, FOUNSDR ARWA0010502Actuator · failedAFTER TAKEOFF RIGHT GEAR UNSAFE LIGHT ILLUMINATED AND DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR, NO HELP. RETURNED TO SAL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATING CYLINDER PER J/C 6209 SYSTEM OPERATISDR 2000ZZZX469Skin · corrodedDURING B-CHECK INSPECTION, FOUND THE FOLLLOWING: CORROSION DAMAGE LEFT FUSELAGE ABOVE NLG DOOR AT STA 52.00. REPAIRED CORROSION DAMAGE IAW SRM 53-2-1. (X)SDR 2000ZZZX468Line · failedDURING LANDING ROLL-OUT AT SDQ, BELOW 100 KNOTS, CREW OBSERVED AN ELECTRICAL SPARK AND SMALL FIRE AND A HIGH AIR PRESSURE 'HISSING' SOUND COMING FROM THE FORWARD OBSERVER OXYGEN PANEL. INSPECTION FOUND THE MAIN OXYGEN LINE BLOWN OFF AT THE CONNECTOR AND FOUNDSDR 99ZZZM636Line · chafedAFTER TAKEOFF MIA, EXPERIENCED HYDRAULIC QTY LOSS AND PRESSURE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE CHAFED AT NR 3 ENGIEN HYDRAULIC PUMP. REPLACED LINE, CHECKED FILTERS, SERVICED SYSTEM AND RETURNED AIRCRSDR 2000ZZZX471Line · chafedAFTER TAKEOFF FROM MIA, EXPERIENCED HYDRAULIC QUANTITY LOSS AND PRESSURE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE CHAFED AT NR 3 ENGINE HYDRAULIC PUMP. REPLACED LINE AND CHECKED FILTERS. SERVICED SYSTEM AND RSDR 98ZZZM441Duct · looseDURING CRUISE MASTER FIRE WARNING LIGHT CAME ON. VERIFIED NR 2 ENGINE AT FAULT. REDUCED POWER AND LIGHT WENT OUT. TESTED FIRE WARNING SYSTEM WHICH WAS SATISFACTORY. RESTORED POWER AND NO FURTHER INDICATION. GROUND INSPECTION REVEALED LOW PRESS PNEUMATIC DSDR 98ZZZM253Fire Loop · defectiveDURING CRUISE NR 4 ENGINE FIRE WARNING CAME ON. SHUT DOWN ENGINE AND FIRE WARNING CONTINUED. DISCHARGED FIRE EXTINGUISHER AND FIRE WARNING CEASED. GROUND INSPECTION REVEALED NO EVIDENCE OF FIRE. FOUND DETECTION ELEMENT DEFECTIVE ON LOWER ELEMENT ASSY. REPSDR 98ZZZM175Ballast · overheatedON LANDING AT MIA EXPERIENCED ELECTRICAL WIRE OVERHEAT ODOR IN COCKPIT. GROUND INSPECTION REVEALED OVERHEATED BALLASTS FOR FLOURESCENT LIGHTS IN COCKPIT. REPLACED BOTH BALLASTS, SYSTEM CHECKED NORMAL. (M)SDR 97ZZZM788Anti-Skid Box · malfunctionedON APPROACH MIA, EXPERIENCED ERRATIC OPERATION OF THE ANTI-SKID/SPOILER CONTROL SYSTEM. INVESTIGATION REVEALED THE ANTI-SKID CONTROL BOX WAS NOT MODIFIED IAW DACO S/B 32-130. REPLACED ANTI-SKID CONTROL BOX WITH MODIFIED BOX AND SYSTEM CHECKED NORMAL. RETURNSDR 97ZZZM243Turbine · failedMIAMI - ON TAKEOFF, NR 1 ENGINE BEGAN TO STALL SEVERELY AT 400 FEET. TOWER REPORTED FLAMES OUT OF NR 1 ENGINE. ENGINE WAS SHUT DOWN. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED NO EVIDENCE OF FIRE, BUT METAL IN TAIL PIPE. REPLACED ESDR 96ZZZX5829Tee Cap · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STA Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5, PAGES 15 ANSDR 96ZZZM1539Bulkhead Tee · crackedDURING INSPECTION OF AFT PRESSURE BULKHEAD AT STATION Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS AT CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RIGHT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5 PAGE SDR 96ZZZM325Skin · crackedDUIRNG C-CHECK INSPECTION, FOUND LEFT WING LOWER SURFACE SKIN CRACK AT STATION XW204. REPAIRED LEFT WING LOWER SURFACE SKIN CRACK BY CUTTING OUT 2 INCH BY 5.4 INCH SKIN AND INSTALLED A 7075-T6 .188 2 INCH BY 5.4 INCH FILLER AND INSTALLED A 15 INCH BY 15 INCH
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