N980AT

Service difficulty reports · 245

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 = 'N980AT' 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 DALA2026102305844Spar Cap · crackedFOUND CRACK AT REAR SPAR LOWER CAP NEAR XRS 164, COMPLIED WITH ER/A 636450-14AD. (1879849) (AIRCRAFT GROUNDED).Oct 22, 2026 · N980AT · Boeing 717200 · Wing SparSDR DALA2026102305840Spar Cap · crackedFOUND CRACK NEAR XRS-158 AND 170 AT RT WING ERAR SPAR CAP SPLICE, COMPLIED WITH ER/A 636450-14AD. (1879441) (AIRCRAFT GROUNDED).Oct 22, 2026 · N980AT · Boeing 717200 · Wing SparSDR DALA2026102305839Spar Angle · crackedFOUND CRACK COMMON TO THE RT WING LOWER SPAR CAP, COMMON TO THE RT WING REAR SPAR INSTL AT AFT FLANGE NEAR XRS=164, COMPLIED WITH ER/A 636450-14AD. (1879433) (AIRCRAFT GROUNDED).Oct 22, 2026 · N980AT · Boeing 717200 · Wing SparSDR DALA2026102305838Spar Cap · crackedFOUND CRACK COMMON TO THE RT WING LOWER SPAR CAP, COMMON TO THE RH WING REAR SPAR INSTL AT AFT FLANGE NEAR XRS=164, CORRECTIVE ACTION: COMPLIED WITH ER/A 636450-14AD. (1879422) (AIRCRAFT GROUNDED).Oct 22, 2026 · N980AT · Boeing 717200 · Wing SparSDR DALA2026101905723Skin · damagedFOUND A DISCREPANT FASTENER HOLE WAS IDENTIFIED AT THE INTERSECTION OF FRAME Y503 AND LONGERON L1, AT THE FOURTH FASTENER LOCATION AFT OF THE FORWARD EDGE OF STC DOUBLER, CORRECTIVE ACTION: COMPLIED WITH ER/A 637350-14AD. (1871858) (AIRCRAFT GROUNDED).Oct 18, 2026 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026100205474Doubler · crackedRT WING UPPER MLG DOUBLER HAS TWO HOLES WITH CRACK INDICATIONS, COMPLIED WITH ER/A 636571-14AD. (1842799) (AIRCRAFT GROUNDED).Oct 1, 2026 · N980AT · Boeing 717200 · Wing, Landing Gear Attach FittingsSDR DALA2026020900914Bracket · damagedGIRT BAR BRACKETS DAMAGED. SECURED THE BRACKET FITTING, OPS CHECKED GOOD. (1430474)Feb 1, 2026 · N980AT · Boeing 717200 · Emergency EquipmentSDR DALA2025101707590Fuel Cell · leakingFUEL LEAK FOUND DURING INSPECTION OF THE L/H WING AFT LWR SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621176. (1243963).Oct 10, 2025 · N980AT · Boeing 717200 · Fuel StorageSDR DALA2025092306962Skin · damagedEXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED BEFORE FURTHER FLIGHT. RH WING XRS 14- XRS 177. REF. EA 619064-14AD REV. B SECT II. DVI OF AFT SIDE OF SPAR CAP AT STOP DRILL SHOWS NO DISCREPANCY. (1199238)Sep 14, 2025 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025090406566Sign · detachedEMERGENCY EXIT SIGN ON CEILING ABOVE ROW 1 DETACHING FROM CEILING. RESECURED EXIT SIGN PER B-717 AMM 33-51. (7354500)Aug 26, 2025 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2025090406560Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE ABOVE OVER WINGS EXITS. REMOVED AND REPLACED BATTERY PACK B5-121 REF AMM 33-51 (7280198)Aug 26, 2025 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2025082206254Elec Connector · dirtyAFT EMERGENCY LIGHT FLASHING. CLEANED CONNECTOR ON EMERGENCY LIGHT BATTERY PACK B5-260 AND OPS CHECKED IAW AMM 33-51, CHECKED GOOD (7280156).Aug 17, 2025 · N980AT · Boeing 717200 · Light System WiringSDR DALA2025081806158Battery Pack · no testEMER LIGHT ABOVE AFT FA JUMPSEAT STAYS ILLUMINATED WHEN IN ARM. T/S REF WDM 33-51. FOUND EMER LIGHT BATTERY PACK B5-260 WATER DAMAGED. R&R'D BATTERY PACK & BATTERY REF B717 AMM 33-51. OPS CHECK GOOD. (7280148)Aug 15, 2025 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2025070104878Sign · detachedSHIP 6546 EMERGENCY EXIT SIGN COVER HANGING LOOSE IN FIRST CLASS CABIN. CORRECTIVE ACTION: RE-SECURED EMERGENCY EXIT SIGN. OK FOR SVC (7552948)Jun 29, 2025 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2025062604790Doubler · leakingSHIP 9546 FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: FUEL LEAK REPAIRED ON ERA 621176-14AD REV C (1044305)Jun 25, 2025 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025062604794Angle · not reportedSHIP 9546 C/W LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ERA 626984-14 REV ORIG. CORRECTIVE ACTION: COMPLIED WITH LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ER/A 626894-14 REV A. (1043812)Jun 24, 2025 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025062504754Spar Cap · damagedC/W 621176-14AD REV B LH WING LOWER SPAR CAP LEAK REPAIR. DAMAGED AREA REPAIRED PER ERA 621176-14AD REV B PRI 621176-14AD (1043689).Jun 24, 2025 · N980AT · Boeing 717200 · Wing SparSDR DALA2025062504750Repair · no discrepancyEXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT (R/H WING). PER ENGINEERING C/W ERA 619064-14AD REV B SEC II STEP 3. NO ISSUES NOTED.Jun 24, 2025 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025060604328Repair · damagedSHIP 9546 EXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REPAIRED PER ERA 6190064-14AD (0984966)May 25, 2025 · N980AT · Boeing 717200 · Wing SparSDR DALA2025043003321Repair · not reported-AD- EXISTING REPAIR FOUND, CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FUTHER FLIGHT. FC 5720-01103-01A. OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC II OF ERA 621176-14AD REV A. (LP #7184928)Apr 28, 2025 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025043003314Repair · not reported-AD- EXISTING REPAIR FOUND, OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC I OF ERA 619064-14AD REV B. (LP #7184929)Apr 28, 2025 · N980AT · Boeing 717200 · Wing StructureSDR DALA2025041202831Fuel Cap · leaking-AD- WORKING PRI 621176-14AD REV "O" B717-200 LH WING REAR SPAR LOWER CAP FUEL LEAK. SUMMARY SEE NRC 004-0001:5720-01103-01A/004 00004: CMOR - COMPLIED WITH ER/A 621176-14 REV A, PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENApr 11, 2025 · N980AT · Boeing 717200 · Fuel StorageSDR DALA2025021201090None · noneIN REFERENCE NRC 00924: LEVEL AND SHORE AIRCRAFT IN ACORDANCE WITH AMM 07-11-00 AS WELL AS PER FIGURE 4 OF BOEING SERVICE SKETCH 3268E PER PRI 621176-14 REV 0 STEP 1 A) AND PERFORM DAILY CHECK UNTIL REMOVED. SUMMARY NRC 00981: SHORINGS WERE INSTALLED AND VERIFFeb 12, 2025 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025021201089Fitting · damagedPERFORM COLDWORK ON INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING. SUMMARY OF NRC 00924: INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING WAS REPAIRED PER PRI 621176-14 REV 10 AND ERA 621176-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. ALSO FAIRING WAS REFeb 11, 2025 · N980AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2025021001046Spar Cap · damaged-AD- AWR, AA, AD, IN REF TO AMDS 5720-01103-01B STEP 7: REPAIR IN PROGRESS AT RIGHT WING LOWER REAR SPAR CAP THATS INCLUDES LOWER WING SKIN AND DOUBLER BTW STA XRS 150 AND XRS 177. SUMMARY OF NRC 00918: THIS REPAIR PROVIDED WITH FAA AMOC APPROVAL AND INCLUDES Feb 8, 2025 · N980AT · Boeing 717200 · Wing SparSDR DALA2025020300801Spar Cap · crackedCRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARD DIRECTION. SUMMARY OF NRC 00347: CRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARDJan 31, 2025 · N980AT · Boeing 717200 · Wing SparSDR DALA2024100209615Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 13. SUMMARY NRC 00919: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 13 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024100209614Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 15 AND 16. SUMMARY NRC 00921: SEALANT WAS REMOVED AND APPLIED PER B717 AMM 20-60-01 PER AMDS 5720-01103-01A ALSO (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 16 AND BSep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024100209613Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 14. SUMMARY NRC 00920: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 14 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024091809135Fastener · shearedFASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCOSep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024091809134Fastener · shearedFASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCOSep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024091008882Lug · corrodedCORROSION ON OUTER/INNER LUGS (INNER PART) AND BUSHING OF LH FLAP OUTBOARD HINGE. SUMMARY OF NRC 00657: CORROSION LEVEL 2. LH FLAP OUTBOARD HINGE WAS REPAIRED PER PRI 619369-14 REV 4 & ER/A 619369-14 REV ORIG. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 29AUGSep 9, 2024 · N980AT · Boeing 717200 · Wing, Control Surface Attach FittingsSDR DALA2024082408418Fuel Cell · corrodedAIRCRAFT 9546, CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. CORRECTIVE ACTION: LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 WAS REPAIRED PER Aug 23, 2024 · N980AT · Boeing 717200 · Fuel StorageSDR DALA2024081608210Pan · crackedCRACK ON INNER PAN WAS FOUND ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00674: INNER PAN ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 619393-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 619393-14 REV 3. ASAug 15, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024081508167Pan · crackedCRACK (3 EA) ON OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00141: OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 619498-14 REV ORIGINAL. ASSOCIATED EAug 15, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024081208005Housing · crackedCRACK AT SETTLEMENT AREA OF HANDLE HOUSING WAS FOUND WHILE HOUSING REMOTION DOOR L1. SUMMARY OF NRC 00708: EXTERNAL SKIN ON SETTLEMENT AREA OF HANDLE HOUSING AT PASSENGER DOOR L1 WAS REPAIRED PER ER/A 619355-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI Aug 9, 2024 · N980AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024080907921Cap · corrodedCORROSION ON SEAT TRACK X=22 STA Y=197-225, -X=44.5 Y=200-237, AND FLOOR SUPPORT AT -X=54.5 Y=210. SUMMARY OF NRC 00719: CORROSION LEVEL 2. SEAT TRACK X=22 STA Y=197-225, AND SEAT TRACK -X=44.5 Y=200-237, WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 Aug 9, 2024 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024080807882Frame · crackedCRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. ASSOCAug 6, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024080707851Frame · crackedCRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. (LP #Aug 6, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024080607839Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE STA 565 X=- 59, STA 576 X=-58, STA 579-589 X=-60 AND X=-58 (UPPER AND UNDER), STA 589-617 X=-57 AND X=-59, STA 636 X=-49, STA 647 X=-58 AT PAX CAB. SUMMARY OF NRC 00491: CORROSION LEVEL 2. CUSP WEB MEMBRANE STA 565 X=-59, STA 579Aug 5, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024072907539Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE STA Y=794 TO Y=813, X=-44 X=-60, AND Y=832/Y=835 AND X=-57. ALSO, CORROSION ON THE REPAIR DOUBLER OF THE CUSP WEB MEMBRANE STA Y= 865 TO Y=870, X=-53 TO X=-60. CABIN PAX. SUMMARY OF NRC 00764: CORROSION LEVEL 2. CUSP WEB MEMBRANEJul 27, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024072607477Frame · crackedCRACK ON FRAME STA Y=1037 AND STR 17 RH AT C PAX. SUMMARY OF NRC 00360: FRAME STA Y=1037 AND STR 17 RH WAS REPAIRED PER B717 SRM 53-20-07-2R REP 4. (LP #0466007)Jul 25, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024072407442Door Frame · corrodedCORROSION ON DOOR JAMB BTW STA Y=387-408 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00079: CORROSION LEVEL 2. DOOR JAMB BTW STA Y=387-408 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #0462776)Jul 24, 2024 · N980AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024072407441Skin · crackedCRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE. SUMMARY OF NRC 00075: CRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 12. (LP #0461829)Jul 23, 2024 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024072307416Cusp Web · crackedCRACK ON CUSP WEB MEMBRANE STA 403 X=-58 AT PAX CAB. SUMMARY OF NRC 00498: CUSP WEB MEMBRANE STA 403 X=-58 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4, REPAIR 4, FIGURE 212. (LP #0460928)Jul 22, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024072307415Longeron · crackedCRACK ON RH LONGERONS 4 AND 6 STA Y=1022 AT C PAX. SUMMARY OF NRC 00363: CRACK ON RH LONGERONS 4 AND 6 STA Y=1022 AT C PAX WERE REPAIRED PER B 717-200 S.R.M. 53-00-05-2R REPAIR 2. (LP #0460780)Jul 22, 2024 · N980AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024072207314Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE BTW STA Y=483 AND X=55 AT CPAX. SUMMARY OF NRC 00488: CORROSION LEVEL 2. CUSP WEB MEMBRANE BTW STA Y=483 AND X=55 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 213. (LP #0457527)Jul 20, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024072207313Web · corrodedCORROSION ON WEB MEMBRANE STA Y=185-Y=200. SUMMARY OF NRC 00827: CORROSION LEVEL 2. WEB MEMBRANE STA Y=185-Y=200 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REP 2. (LP #0456066)Jul 19, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071707229Cusp Web · corrodedCORROSION OUT OF LIMITS ON RH CUSP WEB STA 896-904 X=-58 PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4.A. SUMMARY OF NRC S/N 00711: CORROSION LEVEL 2. RH CUSP WEB STA 896 -904 X=-58 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE Jul 17, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071707228Seat Track · corrodedCORROSION ON SEAT TRACK BTW STA Y=265-301 COORDINATE X=-22. SUMMARY OF NRC 00672: CORROSION LEVEL 2. SEAT TRACK BTW STA Y=265-301 COORDINATE X=-22 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5, PAR 4, FIG 201. (LP #0451567)Jul 17, 2024 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
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