N753NA
Service difficulty reports not matched to an aircraft · 27
They name N753NA, 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 = 'N753NA' 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 = 'N753NA' 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 NOCA00810Sill · corroded4L DOOR SILL CORROSION AT BS 1674 LBL 56. REPLACED GUTTER SUPPORT BRACKET PER SRM 51-10-02.SDR RYNA200700026Skin · damagedLOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 510 AND BETWEEN STR 26R - 27R. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01.SDR RYNA200700022Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 324-377 AND BETWEEN BL 0 AND RBL 3, WATER LINE 208. REPLACED CABIN FLOOR SUPPORT.SDR RYNA200700023Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 1640-1661 AND RBL 13, WATER LINE 208. REPLACED CABIN FLOOR SUPPORT BOTH INTERCOSTALS WHICH ARE FABRICATED FROM BOC1508-240-707ST73511 EXTRUSION PER QQA-200-111.SDR RYNA200700015Skin · dentedFUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 405 AND BETWEEN STG 24R AND 25R. REPAIRED IAW EO C00-5-53-483-07.SDR RYNA200700019Skin · wornUPPER FUSELAGE SKIN TAIL CONE AREA HAS EVIDENCE OF WEAR AT BS 1800 BETWEEN STR 15L AND 16L. REPAIRED IAW EO C00-5-53-499-07.SDR RYNA200700020Floorbeam · corrodedPASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN LBL 48 AND LBL 58. REPAIRED IAW EO C00-5-53-507-07.SDR RYNA200700021Floorbeam · corrodedPASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN RBL 38 AND RBL 60, WATER LINE 208. REPAIRED IAW EO C00-5-53-502-07.SDR RYNA200700018Skin · dentedFUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 431 AND STG 4L. REPAIRED IAW EO C00-5-53-490-07.SDR RYNA200700013Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 1691-1693 & BETWEEN STR 12L - 13L. REPAIRED DENT IAW EO COO-5-53-487-07.SDR RYNA200700009Skin · dentedFUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 596 - 603 & BETWEEN STR 27LT AND 27RT. REPAIRED IAW EO C00-5-53-492-07.SDR RYNA200700006Skin · damagedUPPER FUSELAGE SKIN HAS "BLEND OUT" AT BS 444.5 & STR 4LT. REPAIRED FUSELAGE SKIN AT BS 444.5 & STR 4LT PER SRM 53-00-01 FIGURE 201 SECTION I & II.SDR RYNA200700011Floorbeam · corrodedPASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1661 & BETWEEN LBL 45 - RBL 58 & WL 208. REPAIRED IAW EO C00-5-53-494-07.SDR RYNA200700024Skin · damagedLOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1348 AND BETWEEN STR 25L - 26L. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01, REPAIR 4.SDR RYNA200700016Skin · dentedFUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 1356 AND BETWEEN STG 25R AND 37R. REPAIRED IAW EO C00-5-53-493-07.SDR RYNA200700017Skin · dentedFUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 1420 AND BETWEEN STG 26R AND 27R. REPAIRED IAW EO C00-5-53-495-07.SDR RYNA200700014Skin · dentedFOUND FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 541-543 AND BETWEEN STG 20R AND 23R. REPAIRED IAW EO C00-5-53-486-07.SDR RYNA200700012Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 18L. REPAIRED DENT IAW EO C00-5-53-489-07.SDR RYNA200700010Skin · dentedFUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 16L. REPAIRED IAW EO C00-5-53-489-07.SDR RYNA200700025Skin · damagedLOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1483 AND BETWEEN STR 21R - 22R. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01, REPAIR 6.SDR RYNA200600009Skin · damagedEVIDENCE OF LIGHNTING STRIKE AT FS 224.870 (24.5") LBL 14.5. INSTALLED DOUBLER REPAIR AT FS 224.870 AS PER B757 SRM 53-00-01 FIG 201. IAW AVBORNE RES 26449-2, DATED 09/14/06 AND 8110-3 DATED 9/14/06. MATERIAL USED FOR DOUBLER 2024-T3 .071 SIZE OF REPAIR 4.5 SDR RYNA200600008Skin · damagedEVIDENCE OF LIGHNTING STRIKE AT FS 237.620 (37.25") LBL 17 (37.25"). INSTALLED DOUBLER REPAIR AT FS 237.620 AS PER B757 SRM 53-00-01 FIG 201, IAW AVBORNE RES 26449-2, DATED 09/14/06 AND 8110-3 DATED 9/14/06. MATERIAL USED FOR DOUBLER 2024-T3 071 SIZE OF REPASDR RYNA200600003Circuit Card · faultyDURING CRUISE, RECEIVED A CABIN ALTITUDE WARNING EICAS MESSAGE . CAPTAIN AND FIRST OFFICER WENT ON OXYGEN, ADVISED ATC, AND BEGAN EMERGENCY DESCENT TO 10000 FT. FIRST OFFICER ATTEMPTED TO REGAIN CONTROL OF CABIN PRESSURE. AT OR ABOUT 24000 FT, CABIN PRESSURSDR RYNA200500029Line · leakingEICAS MESSAGE LEFT HYDRAULIC QUANTITY AND PRESSURE LOST. QUANTITY LEVEL 0.10 LT. REMOVED AND REPLACED RIGHT DOWNLOCK ACTUATOR RETURN LINE. LEAK CHECK GOOD, ALSO FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED ENGINE DRIVE PUMP AND PRESDR RYNA200500015Warning Light · illuminatedAFTER TAKEOFF FROM NKW, EXPERIENCED AN APU FIRE WARNING INDICATION WITH ALL FIRE WARNING LIGHTS BUT NO HORN DURING CLIMB. APU WAS SHUTDOWN BEFORE TAXI. CREW FOLLOWED EMERGENCY PROCEDURES, DISCHARGED THE FIRE BOTTLE AND RETURNED TO UKW. AIRCRAFT LANDED WITHOSDR RYNA200500012Transmitter · inoperativeDURING CLIMB-OUT ABOVE 14,000, THE CREW NOTICED AN ABNORMAL SPLIT IN ENGINE PARAMETERS WITH THRUST LEVERS MATCHED UP. WHEN TRYING TO MATCH EPR, THERE WAS A HUGE SPLIT IN THRUST LEVER POSITION AND N1, N2, N3, EGT AND FUEL FLOW. AIRCRAFT RETURNED TO ORD AND LASDR RYNA200500013Tube · crackedDURING CLIMB FROM ORD, THE NR 2 ENGINE N1 WAS INDICATING .16 LOWER THAN THE NR 1 ENGINE. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CRACKED TUBE OFF NR 2 ENGINE P1 PROBE. OPERATIONAL CHECK NORMAL.
Back to N753NA