N955AT

Service difficulty reports · 197

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 = 'N955AT' 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.

SDR DALA2018031001590Structure · dentedDENT ON THE AFT CARGO DOOR. REPAIRED IAW SRM 53-02-01-2R-1, FIG 202, SHEET 1, AND SRM 51-41-02.Mar 9, 2018 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030901526Access Panel · corrodedCORROSION ON FUEL ACCESS PLATES #620EB, 620CB, 620DT, AND 620AT. (AD) (PTAS). NRC 00491: DUE TO EXCESSIVE DAMAGE BY CORROSION 2, FUEL ACCESS PLATES #620AT, 620EB, AND 620DT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 AND FUEL ACCESS PLATE #620CB WAS REPLACEDMar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030801487Floor Support · crackedCRACK ON FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX (CPAX). NRC 00260: FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX WERE REPLACED PER B717 SRM 51-41-02-0G , 51-41-05-0G , 51-40-08-0G. (LP #0Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2022030201331None · noneFAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566546-14 AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR ASSOCIATED ER/A 95-566546 ADDED Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030901589Bulkhead · corrodedSEVERAL CORROSION POINTS ON FWD BULKHEAD. THE BULKHEAD WAS REPAIRED IAW ER/A 566355-14, REV ORIGINAL, AND ETI-17-18-027 REV 1.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2018030901528Access Panel · crackedCRACKED FUEL ACCESS PANLE. THE ACCESS PANEL WAS REPLACED.Mar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030901527Access Panel · crackedCRACKED FUEL ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.Mar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030901525Skin · crackedCRACKED SKIN, BS 1076, BETWEEN LONGERONS 13L TO 14L. THE SKIN WAS REPAIRED IAW ER/A 566546-14, REV ORIGINAL, AND ETI-17-18-022, REV 2.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030901518Floor Panel · crackedCRACKED CHANNEL OF FLOOR PANEL: THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50-2R-5, REPAIR 5.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018030901516Web · crackedCRACKED WEB BETWEEN BEAMS 4 & 5, THE WEB WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9955763, REV M.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030801515Former · crackedCRACKED LT AND RT FORMERS AT BS 679. THE FORMERS WERE REPAIRED IAW SRM 53-00-06-2R-2.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018030801483Floor Panel · damagedCRACK IN CHANNEL, ALSO BENT CHANNEL AND SKIN OF FLOOR PANEL 222AQF AND 222XF. FLOOR PANELS WERE REPAIRED (PERMANENT REPAIR) PER SRM 51-20-09-0G, SRM 53-20-50-2R-5, & SRM 51-41-02-0G.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018030801481Lanyard · damagedBROKEN STRANDS ON L1 AND R1 EMERGENCY SLIDE LANYARDS. LANYARDS WERE REPLACED PER AMM 25-61-01 400-801.Mar 7, 2018 · N955AT · Boeing 717200 · Escape SlideSDR DALA2018030801479Support · wornWEAR ON RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER SRM 52-10-02-2R REPAIR 16.Mar 7, 2018 · N955AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018030801478Former · crackedCRACKED LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018030801477Access Panel · crackedCRACK ON FUEL ACCESS PLATES 520CB. FUEL ACCESS PLATE WAS REPLACE PER IPC 57-23-01-01 ITEM 442J.Mar 7, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030801476Former · crackedCRACKED LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018030801475Skin · crackedCRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.Mar 7, 2018 · N955AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018030801474Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1043 TO Y=1053 X=54. LEVEL CORROSION 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030801472Longeron · crackedCRACK ON LONG 8 RT STA Y=1022 AT CPAX. LONGERON 8R WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R, 51-41-02-0G, & 51-41-05-0G.Mar 7, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030701454Longeron · crackedCRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Mar 6, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030701453Longeron · crackedCRACKED LONGERON 8L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Mar 6, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030701451Fitting · crackedCRACKED FITTING BETWEEN BEAMS 4 & 5, AFT EDGE AT AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.Mar 6, 2018 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030601402Pan · crackedCRACK UPPER PAN, MID SECTION ON FWD CARGO COMPARTMENT DOOR. UPPER PAN ON MID SECTION WAS REPAIRED PER SRM 52-30-02-2R.Mar 5, 2018 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030601401Cusp Web · crackedCRACK WAS FOUND ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 DURING CORROSION REMOVAL AT CAB PAX. CRACK WAS BLENDED OUT PER SRM 53-00-00-1A FIG. 101 (ET) HFEC INSPECTION WAS PERFORMED ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 AT CAB PAX ON BLEND OUT. NO CRACKS WEREMar 5, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030601399Fitting · crackedCRACK ON SHEAR CLIP STA Y=1022 BTW LONG 13R TO 14R AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.Mar 5, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030601398Fitting · crackedCRACK SHEAR CLIP STA Y=1022 BTW LONG 13L TO 14L AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.Mar 5, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030601396Angle · wornWEAR ON LT ANGLE ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. ANGLE WAS REPLACE PER SRM 51-41-04-0G, 51-41-05-0G, 51-41-02-0G, AND DWG 9929480 REV BW.Mar 5, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030601395Cusp Web · crackedA CRACK WAS FOUND ON THE CUSP WEB BTW STA Y=370 AND 389 X=-58 DURING CORROSION REMOVAL AT CAB PAX. CUSP WEB BTW STA Y=370 AND 380 X=-58 WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4., 51-41-02-0G.Mar 5, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030501394Plate · corrodedCORROSION ON AFT LT LAVATORY FLOOR AREA STA Y=1073 X=22 Z=-1. CORROSION LEVEL 2, PLATE WAS REPLACED PER SRM 51-41-05-0G.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030501393Longeron · crackedCRACK ON LONG 4 LT STA Y=1022 AT CPAX. LONG 4 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030501392Longeron · crackedCRACK ON LONG 6 LT STA Y=1022 AT CPAX. LONG 6 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030501391Longeron · crackedCRACK ON LONG 13 RT STA Y=1037 AT CPAX. CRACK ON LONG 13 RT STA Y=1037 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R-2 FIG 201.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018030501390Cusp Web · corrodedCORROSION ON LT CUSP WEB IN STA Y=877 TO Y=889, AND X=54 TO X=60. CORROSION LEVEL 2, CUSP WEB WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4 FIG 211 SHEET 1 AND FIG 215 SHEET 1.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030501389Beam · crackedCRACK ON BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR. BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR WAS REPLACED PER SRM 51-41-02 AND 51-41-05.Mar 4, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030501387Beam · crackedCRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 202.Mar 4, 2018 · N955AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018030501386Beam · crackedCRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 201.Mar 4, 2018 · N955AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018030901587Access Panel · damagedCRACK AND DENTS ON AILERON ACCESS PANEL 530HA, LT WING. REPAIRED IAW ER/A 566323-14 REV. ORIGINAL ASSOCIATED ER/A 00-566323.Mar 3, 2018 · N955AT · Boeing 717200 · AileronsSDR DALA2018030501384Beam · crackedCRACK ON BEAM NR 6 MID SECTION AT THE PASSENGER DOOR. REPAIRED IAW ER/A 559578-14MA, REV ORIGINAL.Mar 3, 2018 · N955AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018030301379Floorbeam · corrodedCORROSION ON THE FLOORBEAM AT BS 148, BETWEEN RBL 30 AND 44. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-01-2, FIG 1, AND 51-40-08-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018030301378Cusp Web · corrodedCORROSION ON CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 224.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301376Splice · corrodedCORROSION ON FUSELAGE SPLICE BETWEEN BS 579 TO 598, LONGERON 18R AND 19R. THE SPLICE WAS REPLACED IAW DWG 9910151, REV BL, AND SRM 51-41-05-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030301375Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 579 TO 598, RBL 54 - 60. THE CUSP WEB WAS REPLACED IAW DWG 9910151, REV BL, SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030201316Cusp Web · crackedCRACK ON THE RT CUSP WEB BS 218 TO 237, BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.Mar 1, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030101315Access Panel · corrodedCORROSION ON FUEL ACCESS PANELS 520CT AND 620CT. THE ACCESS PANELS WERE REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.Feb 28, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022801272Pan · crackedCRACKED UPPER AFT CORNER OF THE RT WINDOW RING PAN BS 851. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801271Pan · crackedCRACKED UPPER FWD CORNER OF THE LT WINDOW RING PAN BS 696. THE PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801270Pan · crackedCRACKED LOWER FWD CORNER OF THE RT WINDOW RING PAN BS 889. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801269Pan · crackedCRACKED AFT UPPER CORNER OF THE LT WINDOW RING PAN AT BS 889 AND 870. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801268Pan · crackedCRACKED LOWER FWD CORNER OF THE LEFT WINDOW RING PAN BS 579 AND 908. THE WINDOW RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, Structure
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