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.
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
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 DALA2026102305844Spar Cap · crackedFOUND CRACK AT REAR SPAR LOWER CAP NEAR XRS 164, COMPLIED WITH ER/A 636450-14AD. (1879849) (AIRCRAFT GROUNDED).SDR 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).SDR 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).SDR 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).SDR 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).SDR DALA2026100205474Doubler · crackedRT WING UPPER MLG DOUBLER HAS TWO HOLES WITH CRACK INDICATIONS, COMPLIED WITH ER/A 636571-14AD. (1842799) (AIRCRAFT GROUNDED).SDR DALA2026020900914Bracket · damagedGIRT BAR BRACKETS DAMAGED. SECURED THE BRACKET FITTING, OPS CHECKED GOOD. (1430474)SDR 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).SDR 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)SDR DALA2025090406566Sign · detachedEMERGENCY EXIT SIGN ON CEILING ABOVE ROW 1 DETACHING FROM CEILING. RESECURED EXIT SIGN PER B-717 AMM 33-51. (7354500)SDR DALA2025090406560Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE ABOVE OVER WINGS EXITS. REMOVED AND REPLACED BATTERY PACK B5-121 REF AMM 33-51 (7280198)SDR 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).SDR 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)SDR DALA2025070104878Sign · detachedSHIP 6546 EMERGENCY EXIT SIGN COVER HANGING LOOSE IN FIRST CLASS CABIN. CORRECTIVE ACTION: RE-SECURED EMERGENCY EXIT SIGN. OK FOR SVC (7552948)SDR 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)SDR 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)SDR 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).SDR 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.SDR DALA2025060604328Repair · damagedSHIP 9546 EXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REPAIRED PER ERA 6190064-14AD (0984966)SDR 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)SDR 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)SDR 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. ENSDR 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 VERIFSDR 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 RESDR 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 SDR 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 INBOARDSDR 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 #0SDR 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 BSDR 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 #0SDR 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. ACCOSDR 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. ACCOSDR 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 29AUGSDR 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 SDR 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. ASSDR 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 ESDR 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 SDR 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 SDR 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. ASSOCSDR 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 #SDR 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 579SDR 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 MEMBRANESDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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 SDR 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)
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