N989TA, cancelled Mar 25, 2023
Service difficulty reports · 25
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 = 'N989TA' AND deregistration_id = 'N989TA-2023-03-25' 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 = 'N989TA' AND deregistration_id = 'N989TA-2023-03-25' 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 RJEF20190123001Warning System · false activationDURING PUSHBACK OF FLIGHT TAI367 FROM IAH TO SAL, THE AIRCRAFT HAD EICAS FAILURE MESSAGE OF RAM AIR VALVE FAULT, DUE THAT REASON RETURNED TO THE GATE FOR MAINTENANCE. MAINTENANCE PERSONNEL PERFORMED FAULT ANALYSIS AND RESET THE SYSTEM IN ACCORDANCE WITH FIM 21SDR RJEF201812121002Windshield · crackedDURING CRUISE OF FLIGHT TA441 FROM DFW TO SAL THE LH WINDSHIELD PRESENTED CRACKING, DUE THAT SITUATION THE AIRCRAFT DIVERTED TO IAH. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FOLLOWING TWO ITEMS: 1) "LEFT WINDSHIELD CRACKED DURING CRUISE LEVEL FL370";SDR EE4Y2017110205082Clevis · wornTHRUST REVERSER PRESSURE RELIEF DOOR HINGE CLEVIS WORN. REPLACED THE DAMAGED CLEVIS.SDR EE4Y2017110205085Web · crackedPAX CABIN SEAT WEB CRACKED OUT OF LIMITS. THE WEB WAS REPLACED.SDR EE4Y2017110205086Floor Support · corrodedFWD FUSELAGE, PAX CABIN BETWEEN FRAMES 17 AND 20, AT -X49 FLOOR SUPPORT CORRODED. REPLACED.SDR EE4Y2017103105048Skin · corrodedRT WING UPPER SKIN T/E AREA BETWEEN RIB 11 AND RIB 20 SKIN WITH CORROSION AND THERE IS NOT ALLOWABLE DAMAGE TO EVALUATE THE DAMAGED AREA. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD2017-190-091058.SDR EE4Y2017103105047Skin · dentedFWD FUSELAGE SKIN WITH SEVERAL DAMAGED (DENTS, EXISTING REWORK, CREASE, BLIND RIVET INSTALLED) IN THE ADJACENT BAY BETWEEN FR9 AND FR11, BETWEEN STR15L AND STR19L. THE CORRECTIVE ACTION WAS HANDLE UNDER THE OEM DISPOSITION ETD2017-190-089131.SDR RJEF20171005001Actuator · faultyAFTER TAKE OFF, THE SLAT FAILED TO RETRACT, RETURNED TO DEPARTURE. AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE SLAT FAILED DURING RETRACTION AFTER TAKE OFF. MAINTENANCE PERFORMED FAULT ANALYSIS IAW FIM 27-81-00-810-805-A, FOUND ONE ATTACHMENT BOLT OFSDR EE4Y2015112500428Shear Tie · corrodedLOWER FUSELAGE FRAME 86, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-88. SHEAR TIE WAS REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS.SDR EE4Y2015112500427Shear Tie · corrodedLOWER FUSELAGE FRAME 87 SHEAR TIE, BETWEEN STR 27R AND STR 28R CORRODED. SHEAR TIE WAS REPLACED UNDER DWG.SDR EE4Y2015112500426Shear Tie · corrodedLOWER FUSELAGE FRAME 85, BETWEEN STR 27R AND STR 28R WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-89. SHEAR TIE WAS REPLACED UNDER DWG, PN 170-65180-447, INSTRUCTIONS.SDR EE4Y2015112500425Frame · corrodedLOWER FUSELAGE FR 88, BETWEEN STR 27 AND STR 29 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-71. FRAME SECTION WAS REPLACED UNDER DWG INSTRUCTIONS.SDR EE4Y2015112500423Skin · crackedNR 2 ENGINE PYLON FWD PANEL SKIN WITH CRACKS. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON-ROUTINE ITEM A1D208,4-56. THE PART WAS REPLACED.SDR EE4Y2015112400422Stringer · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT,STR 27 RT, BETWEEN FRAME 87 AND FRAME 88 WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-83. REPAIR NAS BEEN ACCOMPLISHED UNDER ETD2015-190-105185 REV A, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400421Beam · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT, LOWER BEAM WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-70. REPAIR NAS BEEN ACCOMPLISHED UNDER ETD2015-190-104303,INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400420Finger Doubler · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT, CARGO DOOR CENTER FUSELAGE III, FINGER PLATE WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-69. REPAIR NAS BEEN ACCOMPLISHED UNDER ETD2015-190-104335, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400419Skin · bulgedTAIL CONE AT X34707 RT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER A NON ROUTINE ITEM A1D208,1-40. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103976, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400418Skin · bulgedTAIL CONE AT X34707 LT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-39. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103976, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400417Housing · corrodedRT WING L/E TIP LENS ASSY WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER A NON ROUTINE ITEM A1D208,6-24. THE REPAIR HAS BEEN ACCOMPLISHED ACCORDING TO CMM 33-42-77, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400416Housing · corrodedLT WING L/E TIP LENS ASSEMBLY WITH CORROSION. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,5-25. THE REPAIR HAS BEEN ACCOMPLISHED ACCORDING CMM 33-42-77, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400415Seal Rest · corrodedLOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT SECTION LOWER SEAL REST CORRODED HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-51. THE PART WAS REPLACED.SDR EE4Y2015111700414Structure · corrodedTAIL CONE STATION X34737, LOWER SECTION CHORD WITH CORROSION. DAMAGE HAS BEEN REPORTED & MANAGED UNDER NON-ROUTINE ITEM A1D208 1-53. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103992, INSTRUCTIONS & APPROVED.SDR RJEF20151028001Sensor · out of adjustDURING TAXIING, AS FLIGHT TAI-311, THE PILOT REPORTED STEERING FAILURE, SO THE ACFT WAS RETURNED TO THE GATE. IAW FIM 32-53-00-810-817-A, THE STEERING FEEDBACK SENSORS WERE ADJUSTED & FUNCTIONAL TEST PERFORMED IAW AMM 32-53-09 500 WITH NO EICAS FAILURE MSGS. SDR RJEF20150728001Warning System · false activationPREVIOUS TO DISPATCH OF FLIGHT TA-367, THE PILOT IN COMMAND REPORTED, EICAS MSG, NAV COM 1 WAS FAILED. IT WAS PERFORMED A FAULT ANALYSIS IAW FIM 34-02-01-810-804-A & REPLACED THE NIM 1 IAW AMM 34-02-000-801-A34-02-400-801-A. PERFORMED OPERATIONAL TEST WITH NSDR RJEF20150411001Circuit Card · unserviceableDURING FLIGHT TAI 425, THE PILOT REPORTED AMS CTRL FAIL MSG ON EICAS AT FL370. THEREFORE, THE FLIGHT WAS DIVERTED TO ITS ALTERNATE AIRPORT. NO OWL WAS REPORTED. REPLACED THE AMS CONTROLLER CHA 1 & CHA 2 IAW FIM 21-00-00-810-805-A & AMM 21-00-01-000 400-801-
Back to N989TA, cancelled Mar 25, 2023