N71314, cancelled Feb 19, 2004
Service difficulty reports · 23
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 = 'N71314' AND deregistration_id = 'N71314-2004-02-19' 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 = 'N71314' AND deregistration_id = 'N71314-2004-02-19' 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 CALA0300047Pressure Panel · crackedINSPECTION FOUND A .75 INCH CRACK IN BOTH THE LEFT HAND AND RIGHT HAND PRESSURE DECK AT STA 663.75. BOTH LOCATIONS WERE REPAIRED IAW SRM 53-60-51.SDR CALA0101018Web · corrodedINSPECTION FOUND AFT CARGO DOOR THRESHOLD SILL WEB CORRODED ON TOP AND UNDER SIDE. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02.SDR CALA0101012Frame · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME CORRODED AT STA 794.3, STRINGER 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1.SDR CALA0101011Angle · corrodedINSPECTION FOUND FORWARD L-ANGLE SUPPORT FOR SILL WEB CORRODED AT THRESHOLD OF AFT PIT, STA 704, STRINGER 25R. A NEW ANGLE WAS INSTALLED IAW BOEING DRAWING 69-43233 AND SRM 51-40-02.SDR CALA0101008Skin · crackedINSPECTION FOUND A 2" CRACK IN L/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01608.SDR CALA011007Angle · corrodedINSPECTION FOUND AFT L-ANGLE SUPPORT FOR SILL WEB CORRODED AT AFT PIT THRESHOLD, STA 870, LONGERON 25L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00.SDR CALA011006Frame · crackedINSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR FORWARD FRAME BETWEEN #3 & #4 STOP FITTINGS. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02.SDR CALA0101002Skin · gougedINSPECTION FOUND THE R/H O/B FOREFLAP L/E O/B EDGE WITH SEVERAL DEEP GOUGES IN SKIN. A REPAIR WAS INSTALLED IAW SRM 57-53-01.SDR CALA0100998Skin · crackedINSPECTION FOUND A 1.3" CRACK IN KEEL BEAM SKIN AT STA 699, RBL 5 AND A 1/2" CRACK WAS FOUND IN KEEL BEAM SKIN AT STA 699, LBL 5. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-60-12.SDR CALA0100997Skin · crackedINSPECTION FOUND A 3.5" CRACK IN KEEL BEAM SKIN AT STA 674, RBL 5. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-12, FIGURE 202.SDR CALA9901131Bulkhead Web · crackedINSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD WEB CRACKED IN FOUR PLACES AT FASTENER HOLES AT STA 1016, STRINGER 6L-7L. ALSO, SEVERAL ELONGATED HOLES WERE FOUND. REPAIRED IAW ECRA 5310-03917.SDR CALA9901097Floorbeam · corrodedINSPECTION FOUND RT AND LT AFT LAV FLOORBEAM CORRODED ON NUT PLATE HOLES AT STA 1016, RBL 0 TO RBL 50 AND LBL 0 TO LBL 40. REPAIRED IAW ECRA 5310-03906.SDR CALA9901096Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 985.5 FROM LBL 18 TO R-2 DOOR JAMB. REPAIRED IAW ECRA 5310-03906.SDR CALA9901077Seat Track · corrodedINSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 328-344. REPAIRED IAW SRM 53-00-52, FIGURE 202, SHEET 1.SDR CALA9901066Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 14 TO RBL 12. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.SDR CALA9901059Floorbeam · corrodedINSPECTION FOUND CORROSION ON FLOORBEAM WITH FASTENERS PULLED THROUGH AT STA 328, LBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51.SDR CALA9901056Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312 BETWEEN LBL 10 AND RBL 32. INSTALLED REPAIR IAW SRM 53-10-51, FIGURE 205.SDR CALA9800728Skin · wrinkledRIGHT WING O/B FOREFLAP HAS WRINKLED SKIN. REPLACED RIGHT WING O/B FOREFLAP PER MM 27-51-37.SDR CALA9800007Sensor · out of adjustTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE GEAR HANDLE WOULD NOT GO PAST OFF POSITION. MAINTENANCE FOUND THE MAIN GEAR AIR SAFETY SENSOR OUT OF ADJUSTMENT. THE AIR SAFETY SENSOR WAS ADJUSTED/TESTED IAW MM 32-09-01 AND GEAR HANDLE OPERATISDR CALA9600905Hyd Line · leakingTHE A-HYDRAULIC SYSTEM FLUID WAS LOST ON FINAL APPROACH TO EWR. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 BRAKE LINE LEAKING. THE BRAKE LINE WAS REMOVED AND REPLACED AND THE BRAKES WERE BLED,SDR CAL960334Uplock Act · inoperativeIAH - FLT 1703 - THE RT MLG GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A TOWER FLYBY VERIFIED THE RT GEAR WAS NOT EXTENDED. A MANUAL GEAR EXTENSION WAS PERFORMED WITH 3 GREEN LIGHTS INDICATED AND A SECOND TOWER FLYBY CONFIRMESDR CAL960111Fan · inoperativeFLT NR 1082 - CLE - A SMOKEY ODOR IN REAR OF CABIN WAS REPORTED TWICE DURING FLIGHT. THE AIR WAS CLEARED BOTH TIMES BY USING HIGH POSITION ON BOTH PACKS. MAINTENANCE RAN BOTH PACKS AND INSPECTED THE WATER SEPARATOR BAGS. MAINTENANCE WAS UNABLE TO REPRODUCE SDR CAL950868Hyd Pump · inoperativeIAH - FLT 1769 - THE B-SYSTEM HYDRAULIC QUANTITY DECREASED TO JUST ABOVE ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE DRIVE
Back to N71314, cancelled Feb 19, 2004