N978AT

Service difficulty reports · 226

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 = 'N978AT' 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 DALA2024111510967Seat Track · corrodedCORROSION ON LH SEAT TRACK STA X=56 AND BTW STA Y=545-548 AT PAX CABIN. SUMMARY OF NRC 00686: CORROSION LEVEL 2. SEAT TRACK ON LH STA X=56 AND BTW STA Y=545 TO 548 AT PAX CABIN WAS REPAIR PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #0660518)Nov 14, 2024 · N978AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024111410951Floor Panel · corrodedCORROSION ON FLOOR PANELS 221GF & 222MF. SUMMARY OF NRC 00320: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL 221GF & 222MF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED WITHIN LIMITS FOR FLOOR PANEL 221GF. BUT FLOOR PANEL 222MF WAS REPAIRED PER DRAWING Nov 14, 2024 · N978AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2024111410950Retainer · crackedCRACK WAS FOUND ON LH CLEARVIEW WINDOW REATINER. SUMMARY OF NRC 00667: UPPER AFT LH CORNER ON LH CLEARVIEW WINDOW RETAINER WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0659031)Nov 14, 2024 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024111410949Frame · crackedCRACKS ON UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX. SUMMARY OF NRC 00487: UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX WAS REPAIRED PER ER/A 622035-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 622035-14 REV 1. ASSOCIATED ER/A 14-622035 ADDED FOR Nov 14, 2024 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024111210891Strap · corrodedCORROSION ON FLOOR PANEL STRAP AND WEB (LINES BOTTOM FLOOR PANELS) AT LOWER SILL. SUMMARY OF NRC 00456: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL STRAP AND WEB WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED. PANEL STRAP IS WITHIN OF LIMITS BUT WEB ISNov 12, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024111210890Floor Panel · corrodedCRACK AND CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF. SUMMARY OF NRC 00168: CORROSION LEVEL 2. CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND PANELS EVALUATED. FOUND WITHIN OF LIMITS ON FLOOR PANELS 211PF & 211LNov 12, 2024 · N978AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2024111210888Vane · dentedDENT ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS FOUND OUT OF LIMITS DUE TO DISTANCE. SUMMARY OF NRC 00674: AREA BTW XF 85 TO XF 95 ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL INNov 12, 2024 · N978AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024111410946Door · corrodedCORROSION ON STAIRWELL DOOR. ALSO RUSTED HINGE. SUMMARY OF NRC 00071: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B717 AMM 52-63-01. (LP #0653912)Nov 10, 2024 · N978AT · Boeing 717200 · Entrance StairsSDR DALA2024111110798Frame · crackedCRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00381: CRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R, PROCEDURE 4, REPAIR 4. (LP #0650804)Nov 8, 2024 · N978AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024111110796Longeron · crackedCRACKS ON LONGERONS 17R, 13R, 12L, AND 13L STA Y 1037 AT C. PAX. SUMMARY OF NRC 00485: (ET) HFEC INSPECTION WAS PERFORMED. CRACK WAS FOUND ON LONG 13R, THE REST NO CRACKS WERE FOUND PER B717 DC/MD NDT SPM PART 6, 06-10-01.001. LONGERON 13R STA Y 1037 AT C. PAXNov 8, 2024 · N978AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024080807884Unknown · unknownER/A 610692-14 SECTION II INSPECTIONS. ER/A 610692-14, REV A AT OR PRIOR TO 46,893 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000 FLIGHT CYCLES THEREAFTER ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. AT THE TIME OF THIS LP CREATION, /FOR IAI SHOWS AIRPLANJul 31, 2024 · N978AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2023080706362Unknown · unknownDAMAGE T: DURING JACK REACTION AND CENTER OF GRAVITY FOR NOSE LANDING GEAR STRUT SEAL REPLACEMENT, CRACK WAS FOUND FROM STA Y=371 TO Y=375 BTW LONG 30 TO LONG 29 RH AT EXTERNAL FUSELAGE SKIN IN REF AMDS 3221-4002. SUMMARY OF NRC 00084: EXTERNAL FUSELAGE SKIN FAug 4, 2023 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024080807883Unknown · unknownDTE REQUIRED WITHIN 12 MONTHS OF ER/A 610692-14 ACCOMPLISHMENT ASSOCIATED ER/A 00-610692 ADDED FOR AC 9543. ER/A 610692-14, REV IR. DTE RESTRICTION IS FOR 12 MONTHS OF SERVICE. RTS DATE AT TIME OF REPAIR ACCOMPLISHMENT WAS 10AUG23. THEREFORE, THIS LP IS UPDATEAug 3, 2023 · N978AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2023080306279Unknown · unknownDENT ON INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING. SUMMARY OF NRC 00104: INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING, WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1 REPAIR 1. (LP #2897695)Aug 2, 2023 · N978AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023080206249Unknown · unknownCORROSION ON DOOR JAMB AFT CARGO (C2) STA=954 TO STA=980 APROX. SUMMARY OF NRC 00031: CORROSION LEVEL 2. DOOR JAMB AFT CARGO C2 STA=954 TO STA=980 APROX WAS REPLACED PER B717 SRM 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #2896570)Aug 1, 2023 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023060704646Unknown · unknownSHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIEJun 5, 2023 · N978AT · Boeing 717200 · Airborne Auxiliary Power Unit (APU) SystemSDR DALA2023060604563Unknown · unknownSHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIEJun 5, 2023 · N978AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2023042703287Unknown · unknown12TH HOLE ABOVE ZFS=52.267 HAS CRACK INDICATION ON VERT STAB R /H SIDE REF ERA 560946-14AD REV O AND LOG 0252731. REMOVED VERTICAL STAB L/E PER B717 AMM TASK CARD 55-32-01 00-802. CLEANED AND REINSPECTED 12TH HOLE ABOVE ZFS=52.267 PER ERA 560946-14AD ORIG. NO Apr 19, 2023 · N978AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023031601914None · noneONE CATWALK CEILING EMERGENCY LIGHT IN THE TAIL COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE PSU ASSEMBLY ABOVE THE AFT RIGHT LAVATORY. OPERATIONAL CHECK WAS GOOD. (LP #4026860)Mar 15, 2023 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2022071904969Slide · failed inspTHE SERVICE DOOR SLIDE FAILED THE DEPLOYMENT TEST PER FORECAST #95-0525-8-0121 MAINTENANCE REMOVED AND INSTALLED THE FORWARD SERVICE DOOR SLIDE REF WORK CARD 2561- 9005. (LP #9240753)Jul 17, 2022 · N978AT · Boeing 717200 · Escape SlideSDR DALA2021081804777Skin · corrodedCORROSION ON AFT CARGO SKIN. SUMMARY SEE NRC 105-0008:5331-2001/012 00365: BLENDED AND CHECKED LIMITS IN SKIN PER B717 SRM 53-00-00- 1A. REPLACED SKIN CLIP PER DWG #9912243 AND B717 SRM 51-40-02. (LP #1915089)Aug 17, 2021 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020091403052Battery Pack · inoperativeTHE EXIT SIGN ABOVE THE FORWARD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT B-5-235, PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL.Sep 14, 2020 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2020090802970Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS OUT IN CABIN ON WALK AROUND. MAINTENANCE REPLACED 2 EMERGEGENCY BATTERY PACKS PER B717 AMM 33-53. OPERATIONAL CHECK WAS GOOD.Sep 6, 2020 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2024061106028Skin · crackedCRACKS WERE FOUND AFFECTING SKIN 5936436-101. AND FINGER DOUBLER 5936436-39 (M/F 0.025 7075-T6 CLAD SHEET) AT STA 1037 & L14L. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MOct 6, 2019 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018081600053Tab · delaminatedDURING INSPECTION, FOUND DELAMINATION ON UPPER AND LOWER SKIN SURFACE OF THE LT AILERON TAB.Aug 16, 2018 · N978AT · Boeing 717200 · Aileron TabsSDR DALA2017111408134Lens · detachedEXIT SIGN LENS ABOVE THE L1 DOOR DETACHES. SECURED THE SIGN LENS. ACFT OK FOR SERVICE.Nov 12, 2017 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2017103107855Sign · missingDOOR 1L EXIT SIGN IS MISSING. MAINTENANCE INSTALLED THE EXIT SIGN AS PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.Oct 30, 2017 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2017102907835Sign · unsecureEMERGENCY EXIT SIGN COVER LOOSE AT LOCATION 601. EXIT SIGN FALLS OFF WHILE CLOSING INTERIOR DOOR. RE-SECURED EXIT SIGN AS REQUIRED.Oct 27, 2017 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2017101507570Access Panel · crackedFUEL ACCESS PANEL CRACKED. REPLACED THE ACCESS PANEL.Oct 14, 2017 · N978AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017101507521Clamp · wornWORN RT CABLE CLAMP OF TAIL CONE RELEASE SYSTEM ALSO RUSTED HARDWARE ON PULLEY AT 11 HRS POSITION. THE CABLE CLAMP WAS REPLACED IAW AMM 53-52-01 AND HARDWARE ON PULLEY WAS REPLACED IAW AMM 20-00-02.Oct 14, 2017 · N978AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017101507515Wire · brokenBROKEN WIRES ON THE L1 DOOR SLIDE LANYARD. THE LANYARD WAS REPLACED IAW AMM 25-61-01-400-801.Oct 14, 2017 · N978AT · Boeing 717200 · Escape SlideSDR DALA2017101507510Access Panel · corrodedCORROSION COUNTERSINK ON FUEL ACCESS PANEL 141AL. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2.Oct 14, 2017 · N978AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017101307476Spar Cap · crackedCRACK INDICATION ON OPEN HOLE OF SPAR CAP AFT FLANGE AT ZFS=52.767 ON THE RIGHT SIDE VERTICAL STABILIZER. REPAIRED IAW ER/A 56094-14AD, REV ORG. AND ETI-17-17-175, REV 3. SECTION II.Oct 12, 2017 · N978AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017101307474Beam · corrodedCORROSION ON AFT CARGO BAY LOWER DOOR FRAME BEAM BETWEEN BS 954 TO 994. THE BEAM BTW WAS REPAIRED IAW SRM 53-20-15-2R-7.Oct 12, 2017 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017101307473Frame · corrodedCORROSION OUT OF LIMITS ON FRAME BS 1022, BETWEEN LONGERONS 29 - 30L IN THE AFT CARGO BAY. THE FRAME WAS REPAIRED IAW SRM 53-00-00-2R, PROCEDURE 2.Oct 12, 2017 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017101307471Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL BS 1037 - 1053, LONGERONS 21 - 22L. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 5911423, REV CD.Oct 12, 2017 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017101207448Seal Depressor · crackedCRACK ON THE LOWER CARGO DOOR FRAME SEAL DEPRESSOR BETWEEN BS 980 TO 985. THE LOWER SEAL DEPRESSOR WAS REPLACED IAW SRM SRM 53-20-15-0I-2, FIG. 1.Oct 11, 2017 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017101207447Seal Depressor · damagedAFT CARGO COMPARTMENT SEAL DEPRESSOR CRACKED AND WORN, ON THE AFT EDGE BETWEEN LONGERONS 24R TO 25R AND BS 994. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15-2R-4.Oct 11, 2017 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017101007414Frame Angle · crackedCRACKED FRAME ANGLE ON AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR FRAME, BETWEEN BS 1053 AND 12 O'CLOCK POSITION. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND 51-41-02-0G.Oct 9, 2017 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017101007392Angle · crackedCRACKED ANGLE AT 1152 BETWEEN LONGERONS 2 & 3L . THE ANGLE WAS REPLACED IAW SRM 51-41-05-0G, AND DWG 9911840, REV CR.Oct 9, 2017 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017100807371Web · crackedCRACKED WEB BS 715, BETWEEN LONGERONS 11 - 15R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 51-40-08-0G.Oct 7, 2017 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017100807370Floor Panel · crackedCABIN FLOOR PANEL 222ZF WAS FOUND CRACKED ON THE MID SECTION. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2.Oct 7, 2017 · N978AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017100807366Skin · crackedCRACKED SKIN AT BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIGINAL, AND ETI-17-17-172, REV 2.Oct 7, 2017 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017100807365Skin · crackedCRACKED FUSELAGE SKIN AT BS 1037 LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIG, AND ETI-17-17-178, REV 2.Oct 7, 2017 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017100807364Frame · crackedCRACKED FRAME CAP BS 1022, LONGERON 7L. THE DAMAGE FRAME CAP WAS REPAIRED IAW ER/A 560900-14, REV ORIGINAL AND ETI-17-17-176, REV ORIGINAL.Oct 7, 2017 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017100707362Skin · dentedDENT ON THE LT SIDE NEAR THE T/E OF THE RUDDER. THE RUDDER WAS REPAIRED IAW SRM 51-70-13-2R-1 PAR 4B.Oct 6, 2017 · N978AT · Boeing 717200 · Fuselage, Stabilizer Attach FittingsSDR DALA2017100707361Door Frame · crackedCRACKED RT NLG DOOR FRAME AT BS 47, LONGERON 27R. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Oct 6, 2017 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017100707360Door Frame · crackedCRACKED LEFT DOOR FRAME AT BS 47, LONGERON 27L OF NLG. THE LT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Oct 6, 2017 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017100707355Stop Fitting · crackedCRACKED STOP FITTINGS, LT LOWER AND MID POSITION, RT SIDE MID POSITION AT AFT EMERGENCY EXIT DOOR FRAME AREA BS 1053. HFEC INSPECTION WAS ACCOMPLISHED ON THE FITTING RT SIDE MID POSITION AND NO CRACKS WERE FOUND IAW NDT SPM, PART 6, 06-10-01.001. STOP FIOct 6, 2017 · N978AT · Boeing 717200 · Emergency ExitsSDR DALA2017100607323Longeron · crackedCRACKED LONGERON 2L, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05 2R-2.Oct 6, 2017 · N978AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
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