N940AT
Service difficulty reports · 243
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 = 'N940AT' 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 = 'N940AT' 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 DALA2026102005747Engine · failedDECLARED AN EMERGENCY AND DIVERTED TO BNA DUE TO RIGHT ENGINE FAILURE. INSPECTED RIGHT ENGINE CHIP DETECTOR AND FOUND METAL DEBRIS. R & R ENGINE #2 IAW AMDS JIC 7100-9901-02. (9521740) (AIRCRAFT GROUNDED).SDR DALA2026101605699Wire · brokenDURING SVC CHK FOUND OVERHEAD EMERGENCY LIGHT AT ROW 27/28 INOPERATIVE, BROKEN WIRE. WIRE PULLED OUT OF CONTACT AT CONNECTOR, STRIPPED WIRE TO APPROPRIATE DIMS AND RE-TERMINATED WIRE IAW B717 SWPM 20-31-00 AND WDM 33- 51-12. (9521732) (AIRCRAFT GROUNDED).SDR DALA2026100605533Pump · faultedTHE FLIGHT RETURNED TO ATL DUE TO A RIGHT HYDRAULIC TEMP HIGH MESSAGE. MAINTENANCE REPLACED THE AUX PUMP, THE PTU, AND THE RUDDER HYDRAULIC SHUTOFF VALVE. ALSO REPLACED THE RUDDER HYDRAULIC ACTUATOR ASSEMBLY. SYSTEM OPERATES NORMAL AND PERFORMED ALL ADJUSTMESDR DALA2026092505348Skin · crackedCRACKS WERE FOUND ON FUSELAGE SKIN AND INNER DOUBLER -39, BS 1022 BETWEEN LONGERONS 13-14R, COMPLIED WITH ER/A 577210-14. (1830070) (AIRCRAFT GROUNDED).SDR DALA2026062903843Oxygen Mask · no testCAPT O2 MASK FAILED TEST. R & R FO'S CREW O2 MASK PER B717 AMM 35-23. (6545751) (AIRCRAFT GROUNDED).SDR DALA2026060203341Skin · damagedELONGATED HOLES ON EXTERNAL FUSELAGE SKIN BTW STA Y=813-832 AND LONG 26LH. PERMANENT REPAIR AND PRI 634243-14 (1621845) (AIRCRAFT GROUNDED)SDR DALA2026060203338Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BTW STA Y 813. FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-05 (1620108) (AIRCRAFT GROUNDED)SDR DALA2026051903062Pan · crackedCRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN. CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN WAS REPAIRED PER ER/ A 634007-14 REV ORIG. AND PRI 634007 REV 1. (1595786) (AIRCRAFT GROUNDSDR DALA2026051703031Support · corrodedCORROSION ON FILLET FAIRING SUPPORT ( UPPER/LOWER , FWD/AFT FACE) AT STA 832 BTW L29 AND L26 LH AND STA 832 BTW. CORROSION LEVEL 2, FILLET FAIRING SUPPORT (UPPER/LOWER , FWD/AFT FACE) AT STA 832 BTW L29 AND L26 LH AND STA 832 BTW L28 AND L26 RH AT AFT LOWER SDR DALA2026051703028Frame · crackedCRACK ON FRAME STA Y=1037 AND LONGERON 17L AT PASSENGER CABIN. CRACK ON FRAME STA Y=1037 AND LONGERON 17L WAS REPAIRED PER ER/A 633987-14 REV ORIG. AND PRI 633987-14 REV .1. (1590318) (AIRCRAFT GROUNDED)SDR DALA2026051102943Longeron Splice · corrodedCORROSION ON LONGERON SPLICE (LONG 30) AT Y= 1009 ON AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05 (1581979) (AIRCRAFT GROUNDED)SDR DALA2026050502820Fuel Tank · crackedCRACK ON WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK. REPAIRED PER ER/A 633561-14AD (1573556) (AIRCRAFT GROUNDED)SDR DALA2026050502819Pan · crackedCRACK ON OUTER PAN (UPPER EDGE) UNDER MID BRACKET (CUTOUT AREA STA Y972 APPROX) AT AFT CARGO COMPARTMENT DOOR. REPAIR PER ER/A 633588-14 (1573299) (AIRCRAFT GROUNDED)SDR DALA2026050502815Frame · crackedCRACK ON FRAME STA Y=1037 ON LONGERON 17R AT CPAX. REPAIRED PER SRM 53-20-07 (1569682) (AIRCRAFT GROUNDED)SDR DALA2026050502813Hinge · corrodedAFTER REMOVAL BOLT ON RH WING FLAP OUTBD HINGE PIVOT AREA BS 331.1 WAS FOUND CORROSION, TOOL MARKS, ELONGATED HOLES ON HOUSING ON INBD/OUTBD FACE AT RH WING. RT WING FLAP OTBD HINGE PIVOT AREA WAS REPAIRED PER PRI 633572-14 REV 1 AND ER/A 633572-14 (1569563)SDR DALA2026042302605Pan · crackedCRACK ON INNER PAN (AFT EDGE IN BEAM 2) AT FWD PASSENGER DOOR. REPAIRED PER B717-200 S.R.M. 52-10-02 (1557418) (AIRCRAFT GROUNDED)SDR DALA2026042202562Cusp Web · damagedLEFT FLOOR CUPS WEB AREA (UPPER/LOWER SURFACES) BTW STA 876 TO 884 WITH ORIGINAL THICKNESS IS 0.020 INCH AND MINIMUM REMAINING THICKNESS IS 0.008 INCH THEREFORE IT IS OUT LIMITS. REPAIRED PER B717- 200 SRM 53-00-55 (1554104) (AIRCRAFT GROUNDED)SDR DALA2026042102511Floor Support · crackedCRACKED INTERCOSTAL OF FLOOR STRUCTURE BTW STA Y= 1002 TO 1022 X=0 AT CPAX. REPAIRED PER B717-200 SRM 51-70-11 (1549483) (AIRCRAFT GROUNDED)SDR DALA2026042902731Hinge Fitting · damagedFWD HINGE FITTING #3, XW=-333.148 / INBD A OUTBD LUG / ELONGATED HOLES AND CORROSION. ASSOCIATED ER/A 00-633572 (1559456) (AIRCRAFT GROUNDED)SDR DALA2026042102509Skin · crackedCRACK ON EXTERNAL SKIN ON STA Y=1087 BTW LONG13L AND LONG14L AT AFT UPPER FUSELAGE. REPAIRED PER ER/A 633315- 14 (1548241) (AIRCRAFT GROUNDED)SDR DALA2026042902732Spar Cap · corrodedRH HORIZONTAL STABILIZER REAR SPAR LOWER CAP, HOLES #29 AND #30, XHR=-7.234 / CORROSION. RREPAIRED PER ER/A 00-633497. (1559543) (AIRCRAFT GROUNDED)SDR DALA2026041702448Cusp Web · crackedCRACK ON RH FLOOR CUPS WEB UNDER REPAIRED DOUBLER STA 343, X=-55.5 APROX AT PAX CABIN. DAMAGED AREA REMOVED AND INSTALLED PER B717-200 SRM 53-00-55. (1544260) (AIRCRAFT GROUNDED)SDR DALA2026041702446Cusp Web · corrodedCORROSION ON RH FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 229, BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED PER B717-200 SRM 53-00-55 (1542943) (AIRCRAFT GROUNDED)SDR DALA2026041402365Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX . CUSP WEB BTW STA Y= 715/719 AND BTW STA X= 44/46 WING BOX AREA AT C. PAX WAS REPAIRED PER SRM 53-00-55-2R REPAIR 4 FIGURE 221. (1541206) (AIRCRAFT GROUNDED)SDR DALA2026041402342Web · corrodedCORROSION ON RT FLOOR CUPS WEB AREA (UPPER/ LOWER SURFACES) STA 256 BTW-X =55.5 -X=44.5 APROX AT PAX CABIN. REPAIRED IAW SRM 53-00-55-2R (1536178) (AIRCRAFT GROUNDED)SDR DALA2026040802225Beam · crackedCRACK ON BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX.. BEAM NR 2 (AFT EDGE) ON L1 DOOR AT CPAX WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1531786) (AIRCRAFT GROUNDED)SDR DALA2025122309342Pressure Switch · faultedATB - RIGHT ENGINE SYSTEM FAIL MESSAGE ALONG WITH A RIGHT ENGINE FUEL FILTER MESSAGE ON CLIMB OUT. INSPECTED FILTERS WITH NO DEBRIS NOTED. BOTH HIGH AND LOW PRESSURE FILTERS REPLACED. FILTER DIFFERENTIAL PRESSURE SWITCH REPLACED. HIGH POWER RUN PERFORMED, OPSDR DALA2025111808419Pin · missingSPRING AND PIN MISSING FROM L1 GIRT BAR FLOOR FITTING (AFT ONE). REPLACED L1 CABIN EVACUATION SLIDE LATCH (AFT ONE) IAW CMM 25-60-02. (7585426)SDR DALA2025040902755Skin · crackedCRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R. SUMMARY OF NRC 00056: CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R WAS REPAIRED PER ER/A 625068-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND SDR DALA2025040802701Fastener · looseCRACK AND LOOSE FASTENERS (HI-LOCKS) ON EXTERNAL REPAIR DOUBLER ON STA Y=1022 AND BTW LONGERONS 13R/14R AT FUSELAGE WERE FOUND DURING REPETITIVE INSPECTION PER ER/A 577210-14 REV ORIGINAL SECTION II, STEP 1. SUMMARY OF NRC 00021: SKIN ON STA Y=1022 AND BTW LONSDR DALA2025100807324Lug · corrodedAFTER REMOVAL OF INBOARD AND OUTBOARD BUSHINGS OF HINGES LOCATED AT XE= 206 AND XE= 223, CORROSION WAS FOUND ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND OUTBOARD LUG OF HINGE XE= 206. CORRECTIVE ACTION: CORROSION ON INBOARD AND OUTBOARD LUGS OF HINGE XESDR DALA2025033102353Longeron · crackedCRACK LONGERON 4LH & STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00090: LONGERON 4LH BTW STA Y=1169 AND STA Y=1138 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0883561)SDR DALA2025033102347Skin · dentedSEVERAL DENTS ON EXTERNAL SKIN OF FWD CARGO DOOR. SUMMARY OF NRC 00025: EXTERNAL SKIN OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8. PERFORM AN EXTERNAL GVI OF THE REPAIR DOUBLERS ON FWD CARGO DOOR EVERY C-CHECK PER B717-200 SDR DALA2025040802695Release Mech · out of adjustTHE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00166: TAILCONE RELEASE MECSDR DALA2025032402185Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EA) AND INTERNAL DOUBLER BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT. SUMMARY OF NRC 00077: CORROSION LEVEL 2. REPAIR DOUBLER WAS REPLACED PER DWG 9923686-25 REV D, PER B717 SRM 51-41-02-0G AND 51-41-05-0G. CORROSDR DALA2024121011569Wire · damagedSHIP 9501 -ATB/FUME- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO AN ACRID BURNING SMELL IN THE CABIN. CORRECTIVE ACTION: MAINTENANCE REPAIRED DAMAGED WIRES AND RING TERMINALS AT THE SERVICE DOOR OVERHEAD LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (LSDR DALA2024120911540Power Supply · faultedSEVERAL EMERGENCY LIGHTS ARE INOPERATIVE NEAR FWD SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT AT CANNON PLUG P1-259 PER B717 AMM 22-51. OPERATIONAL CHECK WAS GOOD. (LP #6556658)SDR DALA2024120311396Service difficultySHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC GOING INTO ATL DUE TO "PSEU FAIL" MESSAGE AND THE RESULTANT FLAPS-UP LANDING AS PER THE QRH. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT SLAT A SENSOR WIRES TO BE SHORTED TO GROUND. THE WIRE SDR DALA2024120211377Sensor · inoperativeSHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED EMERGENCY WITH ATC INTO CHA DUE TO THE "PSEU FAIL" MESSAGE. A FLAPS-UP LANDING FOLLOWED PER THE QRH. CORRECTIVE ACTION: MAINTENANCE PERFORMED BITE OF THE PSEU WHICH RETURNED CODES 326029 (PSEU INTERNAL FAULT INTERMISDR DALA2024120911533None · none-AD- ACCOMPLISH ER/A 539703-14AD REV A SEC II. ACCOMPLISH ER/A 539703-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-539703 ADDED FOR AC 9501. **REDEFFESDR DALA2024100709735Battery Pack · inoperativeTHE OVERHEAD EMERGENCY EGRESS LIGHTS ARE INOPERATIVE FROM ROW 24 THROUGH TO ROW 29. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT 25DEF (B5-231) PER B717 AMM 33-51. CHECK IS GOOD. (LP #6103393)SDR DALA2024100709734Lens · missingTHE OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER IS MISSING AT 25/26DEF. DEFERRED 25/26DEF OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER PER NEF 33-51-02. DEFERRAL REMARKS NOTED. MAINTENANCE REPLACED THE MISSING COVER ASSEMBLY REF B717 AMM 33-51. THIS ACTION CLEARS NEF 33-SDR DALA2024071006987Skin · puncturedON WALKAROUND FOUND PUNCTURE IN SKIN AT STATION Y256 BETWEEN LONGERONS L18 AND L17. REMOVED THE PUNCTURED REPAIR SKIN AT FR 229-FR245 BETWEEN STGR L16L & L18L PER B717 SRM 51-40-02. C/W HFEC OF DAMAGED AREA. NO CRACK INDICATIONS. FABRICATED AND INSTALLED SKIN SDR DALA2024040203984Connector · dirtySHIP 9501 -MISC/DE- THE "TAILCONE UNLOCK" MASTER CAUTION ILLUMINATED THREE TIMES DURING FLIGHT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY ATC FOR THE CREW. EWR MAINTENANCE CLEANED THE CONNECTOR PLUGS OF BOTH THE INTERNAL AND EXTERNAL TAILCONE SDR DALA2024011000452Unknown · unknownSHIP 9501 -MISC/DE- AT 13K, THE F/A REPORTED A STRONG ELECTRICAL SMELL COMING FROM FORWARD GALLEY. COCKPIT FLIGHT CREW ALSO SMELLED IT AND DONNED O2 MASKS. SOON AFTER, IT WAS ALSO REPORTED TO BEING SMELLED IN THE TAIL AS WELL. ODOR WAS GONE BY 6K IN THE DECENTSDR DALA2023112809768Unknown · unknownTHE GATE AGENT COULD NOT OPEN THE MAIN CABIN DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE BRACKET, THAT THE DOOR HANDLE MOUNTS TO, WITH THREE BOLTS LOOSE AND ONE BOSDR DALA2023051603854Unknown · unknownCORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 27L AND 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00116: CORROSION LEVEL 2. CORROSION ON AFT PRESSURE BULKHEAD FORWARD FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 2SDR DALA2023051103712Unknown · unknownAFTER REMOVING DOUBLER, CORROSION WAS FOUND ON TEE CAP AFT PRESSURE GROUP BULKHEAD FORWARD FACE LOWER SECTION STA=1053 BTW LONGERON 25R AND 28R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00181: CORROSION LEVEL II. TEE PRESURE DOME ON STA 1053 WAS REPLACED PER B717-SDR DALA2023051003666Unknown · unknownCORROSION ON WEB AFT FACE LOWER SECTION STA Y=1053 BETWEEN LONGERON 28L AND 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00115: CORROSION LEVEL II. WEBS #9915561-53 AND #9915561-3 WERE REPLACED PER DOUGLAS DWG 9915561 REV CG AND B717-200 SRM 51-41-02-0G AND 51SDR DALA2023050903615Unknown · unknownCORROSION AT END LONGERON CLIPS STA 1032 (5 EA), 27RH, 28RH, 29RH, 28LH, AND 26RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00176: LEVEL CORROSION 2. END LONGERON CLIPS #26RH, #27RH, #28RH, AND #28LH WERE REPLACED PER B-717-200 SRM 51-40-08-0G AND END LONGERON
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