N929AT
Service difficulty reports · 187
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 = 'N929AT' 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 = 'N929AT' 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 DALA2026102105785Spar Cap · crackedCRACK FOUND DURING INSPECTION OF LT WING REAR SPAR LOWER CAP AFT LEG, COMPLIED WITH ER/A 637410-14AD. (9540404) (AIRCRAFT GROUNDED).SDR DALA2026102105787Spar · crackedFOUND CRACK EXTENDING AFT FROM ONE OF THE IB BUTE DOOR ATTACH LOCATIONS IN THE AFT FLANGE OF THE LOWER REAR SPAR CHORD, COMPLIED WITH ER/A 637410-14AD. (1876126) (AIRCRAFT GROUNDED).SDR DALA2026102105786Spar · crackedFOUND CRACK AT LT WING REAR SPAR NEAR XRS = 164, COMPLIED WITH ER/A 637410-14AD. (1876109) (AIRCRAFT GROUNDED).SDR DALA2026041402368Unknown · smokeSMOKE/FUMES IN CABIN. R & R D1- 80 CABIN HIGH LIMIT TEMP ANTICIPATOR IAW AMM 21-62 (1541379) (AIRCRAFT GROUNDED)SDR DALA2026011600374Skin · crackedCRACK ON SKIN FUSELAGE BTW L15R, BS 037 AT AFT FUSELAGE AREA. DAMAGED FUSELAGE AREA WAS REPAIRED PER PRI 631355-14 REV. (1399353)SDR DALA2026011600376Skin · not reportedDTA ER/A 631355-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 11-JAN-26. CONTACT LIAISON ENGINEERING. REPAIRED PER ER/A 00-631355. (1398745)SDR DALA2026010500066Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)SDR DALA2026010500065Skin · corrodedCORROSION ON FUSELAGE SKIN( AREA UNDER FILLET PANELS) Y=590 BTW LONG 24RH, Y=615 BTW LONG 23RH-25RH, Y=901 BTW LONG 25LH-26LH , Y=586-590 LONG 24 RH , Y=588 TO Y=598 LONG 22RH-23RH. CORROSION WAS REMOVED PER BOEING 717 SRM 51- 10-04. (1378734)SDR DALA2025062504747Wire Splice · damagedEMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP AT 12C AND 27C CEILING. INSP AND FOUND DAMAGED SPLICES R5-6720 @ LIGHT L2-746 & R5-6722 @ LIGHT L2-771. REPLACED SPLICES PER B717 SWPM 20-10 & WDM 33-51 -12. MEL AND PLACARD REMOVED.SDR DALA2025041502919Door · unsecureSHIP 9570 -ATB/DE- AIRCRAFT HAD AN UNCOMMANDED HEAVY ROLL IN FLIGHT DURING CLIMB AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED THE AIRCRAFT BACK TO ATL, LANDING UNEVENTFULLY. CORRECTIVE ACTION: UPON ARRIVAL, MAINTENANCE FOUND THAT THE RIGSDR DALA2024120211376Light · inoperativeEMERGENCY LIGHTS ABOVE ROWS 24-27 ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY (B5-231) AND OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51. (LP #6585094)SDR DALA2024102910498Battery Pack · failedTHE EMERGENCY LIGHTS AT LOCATION SEAT ROW 20 ARE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK AT LOCATION B5-230 WAS BAD. THE BATTERY AT LOCATION B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6658874)SDR DALA2024092609433Connector · not seatedTHE AFT EMERGENCY CEILING LIGHT REMAINED ON IN THE ARM POSITION. MAINTENANCE RESEATED THE CANNON PLUG ON THE AFT CABIN EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. ALL LIGHTS OPERATE NORMALLY. OK FOR SESDR DALA2024061005955Battery Pack · inoperativeDURING SVC CHK FOUND R FWD AND L FWD OVERWING EXIT IDENTIFIER INOPERATIVE. T/S PER B717 WD 33-51-14, FOUND BATTERY PACK B5-118 INOPERATIVE. REPLACED BATTERY PACK PER B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #5958700)SDR DALA2024050604958Heater · inoperativeLT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)SDR DALA2024010800318Unknown · unknownCRACK ON WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00095: WEB (2 EA) X=11.5, Z=54 AND -X=11.5, Z=54 APPROX AT AFT CABIN BULKHEAD DOOR (CPAX) WAS REPLACED PER B717-200 SRM 51-41-02-0G PAR 4 AND 51-41-05-0SDR DALA2024022002334Hinge Fitting · corrodedCORROSION WAS FOUND ON BOLTS HOUSING AT FLAP HINGE FITTING #3 AND #2. (AI). SUMMARY OF NRC 00366: LH CENTER WING FLAP HINGE FITTING WAS REPLACED PER B717-200 AMM 57-55-25 AND LH INBD WING FLAP HINGE FITTING WAS REPLACED PER B 717-200 AMM 57-55-25 AND OUTBOARD SDR DALA2023120409898Unknown · unknownCRACK WAS FOUND ON OUTER AND INNER PAN IN LOWER AREA STA Y=974 AT AFT CARGO DOOR. SUMMARY OF NRC 00469 AFT CARGO DOOR WAS REMOVED PER B717-200 AMM 52-31-01 AND SERVICEABLE AFT DOOR WAS INSTALLED UNDER AMDS 5231-4004. (LP #0088352)SDR DALA2023112909799Unknown · unknownCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00053: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0085760)SDR DALA2023112809761Unknown · unknownCORROSION ON RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX. SUMMARY OF NRC 00308: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA 195 TO STA 205 AT CPAX WAS REPAIRED PER ER/A 613282-14 REV ORGINAL, SECTION 1 PERMANENT REPAIR. (LP #0084908)SDR DALA2023112809752Unknown · unknownCRACK ON WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1). SUMMARY OF NRC 00507: WEB STA Y=200 X=-44 AT PASSENGER CABIN (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2, REPAIR 2 AND SRM 51-41-08-0G PAR 7 A. (LP #0081861)SDR DALA2023112709725Unknown · unknownCORROSION WAS FOUND ON SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX. SUMMARY OF NRC 00483: CORROSION LEVEL 2. SEAT TRACK BTW STA 208 TO STA 218, X=-54 (RH) AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5, AND 51-41-01-0G. (LP #SDR DALA2023112709720Unknown · unknownCORROSION ON PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PREVIOUS REPAIR OF RH CUSP MEMBRANE BTW STA 200 TO STA 229 AT CPAX WAS REPLACED PER B717 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #007866SDR DALA2023112709718Unknown · unknownCRACK ON L2L STA 1144 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00192: LONGERON ON L2 STA 1144 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R, PROCEDURE 2. (LP #0077910)SDR DALA2023112209651Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00188: FRAME TAB OF THE OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-SDR DALA2023112209650Unknown · unknownCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH OF 1.500 IN (REF. CARD 5310-01436-01D). SUMMARY OF NRC 00189: FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G; TOGETSDR DALA2023112109573Unknown · unknownCRACK ON FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE. SUMMARY OF NRC 00252: FRAME BTW L7L AND STA Y1022 AT INTERNAL AFT FUSELAGE WAS REPAIRED PER ERA 613218-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #0074650)SDR DALA2023112009530Unknown · unknownCRACK ON FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT. SUMMARY OF NRC 00290: FLOOR SUPPORT OF ACCESS PANEL 211PF AT COCKPIT WAS REPAIRED PER B717 SRM 53-00-00-2R PROCEDURE 1. (LP #0073479)SDR DALA2023112009529Unknown · unknownCRACKS (2 EA) ON EXTERNAL FUSELAGE SKIN ON PREVIOUS REPAIR AREA, BTW STA 503-522 AND BTW LONG 27RH AND 29RH. SUMMARY OF NRC 00505: EXTERNAL FUSELAGE SKIN BTW STA 503-522 AND BTW LONG 27RH AND 29RH WAS REPAIRED PER B717-200 SRM 53-03-01-2R FIGURE 205 SHEET 1, 5SDR DALA2023112009518Unknown · unknownCRACK WAS FOUND ON THE CONTRAFRAME STRUCTURE OF THE AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00362: COUNTERFRAME STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1. (LP #0068675)SDR DALA2023111509404Unknown · unknownCRACKS ON PAN AFT UPPER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00130: PAN AFT UPPER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1.SDR DALA2023110809201Unknown · unknownCRACK ON FRAME STA 1037 L17L AT PAX CABIN. SUMMARY OF NRC 00201: FRAME STA 1037 L17L AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-41-05-0G PAR 8 AND 53-20-07-2R PROCEDURE 4. (LP #0054034)SDR DALA2023110709160Unknown · unknownCRACKS WERE GENERATED AROUND FASTENER HOLES OF REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APPROX, DURING REMOVAL OF FASTENERS. SUMMARY OF NRC 00372: REAR SPAR WEB ON INTERNAL FACE OF LEFT HORIZONTAL STABILIZER AT STA XHS 177 APSDR DALA2023051803950Unknown · unknownSHIP 9570 -ATO- THE PILOT ABORTED THE TAKEOFF AT 100 KTS DUE TO THE AIRCRAFT DRIFTING LEFT OF CENTER LINE. CORRECTIVE ACTION: MAINTENANCE PERFORMED A HIGH ENERGY STOP INSPECTION AND ACCOMPLISHED CHECKS OF ALL OF THE FLIGHT CONTROLS. NO DEFECTS WERE FOUND. (LP SDR DALA2023050203398Unknown · unknownFOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #4773170)SDR DALA2023030201550None · noneFOUND SKIN DAMAGE AT C-2 DOORWAY JAMB EDGE AT DOOR CUT OUT SURROUND AREA BELOW DOOR STOP #2. SUMMARY SEE NRC 003-0001:0514-2001/003 00003: COMPLIED WITH ER/A PRI 606111-14 REV'S "0","1","2","3" AND ALL REPAIR INSTRUCTIONAL STEPS ARE COMPLETED, ENSURED FINAL ERSDR DALA2023022201320None · noneLONGERON TEMPORARY REPAIR INSTALLED AT 25R BETWEEN STA 1022 AND STA 1042. COMPLIED WITH LONGERON SPLICE REPAIR PER B717 SRM 53-00-05-2R REPAIR 2 LONGERON REPAIR. A/C WAS DAMAGED BY BELTLOADER ON 13FEB22, REF LOG PAGE 9046786. (LP #2633018)SDR DALA2023021501182None · noneAIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOCIATED ER/A 14-605962 ADDED FOR AC 9570. (LP #9046786)SDR DALA2022110107062Unknown · faultedUPON LANDING GEAR EXTENSION, ALL OF THE EMERGENCY EXIT LIGHTS EXTINGUISHED (WENT INOPERATIVE). MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS. ALL LIGHTS CHECKED GOOD. (LP #9580236)SDR DALA2022080305324None · none---SUPPLEMENTAL INFORMATION: ATL 10AUG22 INSTALLED LEFT LOGO LIGHT PER B717 AMM 33-41. OPS CHECK GOOD. THIS CLEARS CDL. PLACARDS REMOVED. M PROCEDURES REVERSED. --- THE LEFT LOGO LIGHT IS MISSING FROM THE AIRCRAFT. *** CONTRACT MAINTENANCE EVENT - OCM: 250470 SDR DALA2022022401206None · noneTHE AFT EMERGENCY OVERWING DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51-04. OPERATIONAL CHECKS IS NOW GOOD. (LP #8542605)SDR DALA2021110406788None · noneCORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA). SUMMARY NRC #00213: CORROSION ON UPPER SKIN OF LH AILERON (INBOARD AREA) WAS TREATED. THE AREA REWORKED IS OUT OF LIMITS PER B717 SRM 57-00-00-1A. THE AILERON WAS REMOVED PER B717 AMM 27-10-01 AND A SERVICESDR DALA2021102606617None · noneCORROSION ON LOWER DOOR JAMB PAN BTW STA 954 -994 AT AFT CARGO COMPARMTENT. SUMMARY OF NRC 00067: CORROSION LEVEL 2, LOWER DOOR JAMB PAN BTW STA 954-994 AT AFT CARGO COMPARMTENT WAS REPAIRED PER B717 SRM 53-20-15-2R. PROCEDURE 7. REPAIR 7. (LP #1995219)SDR DALA2021102606616None · noneCORROSION ON FRAME AT STA Y=927 AND L-30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00222: CORROSION LEVEL 2, FRAME AT STA Y=927 AND L-30 WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/ A 594977-14 REV. ORIGINAL. ACCOMPLISH SECTION II INITIAL INSPECTIOSDR DALA2021102606615None · noneCORROSION ON FRAME AT STA Y=908 AND L-29L TO L-29R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2 FRAME AT STA Y=908 AND L-29L TO L-29R WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 3 AND ER/A 594972-14 REV. ORIGINAL. ACCOMPLISH SECTION IISDR DALA2021102606611None · noneLOOSE FASTENER ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00249: PERMANENT REPAIR WAS PERFORMED ON CLIP STA Y=1152 AND LONG 1L AT AFT ACCESSORY COMPARTMENT PER ETI-17-21- 017 REV. 2 AND ER/A 594962-14 REV. ORIGINAL, SECTION I. SDR DALA2021102606610None · noneCARGO DOOR JAMB WEB WAS FOUND CRACKED ON FRAME AT STA Y=954 AND BETWEEN L-29R TO L-27R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00220: FRAME AT STA Y=954 AND BETWEEN L-29R TO L- 27R, AFT CARGO COMPARTMENT WAS REPAIRED PER ETI-17-21-026 REV. ORIGINAL AND ERA 5949SDR DALA2021102606609None · noneCARGO DOOR JAMB WEB WAS FOUND CRACKED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00221: REPAIR WAS PERFOMED ON INTERCOSTAL AT STA Y=974 AND BETWEEN L-29R TO L-28R, AFT CARGO COMPARTMENT. PER B717 SRM 51-70-11-SDR DALA2023120710005Unknown · unknownFUSELAGE FRAMES STA 954.0 BETWEEN L- 28R & L-29R IS CRACKED. REPAIR PER SECTION I IS TIME LIMITED AND REQUIRES REPLACEMENT WITH SECTION II PERMANENT REPAIR. ACCOMPLISH ER/A 594963-14, SECTION II PERMANENT REPAIR WITHIN 24 MONTHS FROM 19OCT21. ASSOCIATED ER/A 0SDR DALA2021101806407None · noneCORROSION ON LONGERON L-29L AT STA Y=946 AND Y=954, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00244: CORROSION LEVEL 2, LONGERON L-29L AT STA Y=946 AND Y=954 AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #1986109)
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