N942AT
Service difficulty reports · 250
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 = 'N942AT' 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 = 'N942AT' 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 DALA2026070904031Skin · crackedCRACK INNER SKIN OF SLAT NR 2 NEAR SLAT TRACK NR 5 STA XOS= 240 AT LEFT WING. REPAIRED INNER SKIN IAW SRM 57-00-00-2R. (1689281) (AIRCRAFT GROUNDED).SDR DALA2025090806623Battery · inoperativeBATTERY CHARGER FAIL MSG ANNUNCIATED SHORTLY AFTER TAKEOFF IN ATL IT CLEARED IN FLIGHT DURING PRE FLIGHT FOR RETURN LEG IT RE OCCURED CB WAS RESET AT MTC DIRECTION THERE WAS NO CHANGE THEN SMOKE WAS SEEN COMING FROM E AND E COMPARTMENT. REMOVED AND REPLACED SDR DALA2025070104879Eec · faultedSHIP 9505 -ATB- DUE TO LEFT ENGINE NOT MAKING EPR ON CLIMB OUT. CORRECTIVE ACTION: REPLACE EEC, FUEL FLOW TRANSMITTER, AND FMU. NO HELP, REPLACED FUEL PUMP AND FILTER. OPS CHECK NORMAL.(7479280)SDR DALA2025030101575Door · damagedTHE RIGHT SIDE OVERWING EXIT DOOR WAS FOUND DAMAGED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE RIGHT FWD OVERWING EMERGENCY EXIT DOOR PER B717 AMM 52-21. INSPECTIONSDR DALA2025030101573Engine · failedSHIP 9502 -ATB/IFSD/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO ATL DUE TO SMOKE IN THE CABIN. CREW REPORTED RIGHT ENGINE OIL QTY WENT TO ZERO WITH SMOKE IN CABIN. CREW SHUTDOWN RIGHT ENGINE PER QRH. AFTER LANDING PAX EVACUATED AIRCRAFT SDR DALA2025020500882Battery · no testTHERE ARE MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE AFT CABIN. MAINTENANCE REPLACED THE BATTERIES IN POWER SUPPLY B5-116 AND B5-260 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6411235)SDR DALA2025010500068Unknown · fumesSHIP 9502 -FUMES/DE- THE FLIGHT ATTENDANT REPORTED A "RUBBER SMELL" COMING FROM ROW 26 IN THE CABIN. SMELL STAYED FAIRLY CONTAINED BUT DID MIGRATE TO OTHER ROWS. THE SOURCE COULD NOT BE IDENTIFIED SO THE PILOT DECLARED AN EMERGENCY WITH ATC. A FOLLOW-UP LOG PASDR DALA2025010800167Blades · damagedSHIP 9502 -ATB- THE CREW RETURNED THE AIRCRAFT TO PHL DUE TO MULTIPLE COMPRESSOR STALLS DURING CLIMB OUT. CORRECTIVE ACTION: INSPECTION PERFORMED BORESCOPE INSPECTION AND FOUND NUMEROUS HPC STAGE 1 BLADES DAMAGED. THE POWERPLANT WAS REPLACED. (LP #6930842)SDR DALA2024121811802Battery Pack · inoperativeBOTH OF THE AFT EMERGENCY OVERWING EXIT DOOR LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (B5-230) PER B717 AMM 33-51-04. LIGHT OPERATIONS CHECK GOOD. OK FOR SERVICE. (LP #6930841)SDR DALA2024121711773Skin · damaged-AD- FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS=164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A. #FC5720-01103-01A. REFER TO NRC 0714281 FOR COMPLETION OF ERA 622950-14AD. NO LEAKS NOTED. OK FOR SESDR DALA2024121711772Skin · damaged-AD- REF TO LOG PAGE #6930830. ORIGINAL WRITE UP: FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS+164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A #FC5720-0110-01A. ALL WORK COMPLETED PER ERA 622950AD RESDR DALA2024121711771Tank · not reported-AD- STEP 16 OF ER/A 622950-14AD REV 0 PRI REV 2. C/W STEP 16 A&B PR1422A2 USED AT 1700 13DEC24. C/W STEP 16 STEP B PR1422B1/2 USED 0100 15DEC24. C/W STEP 16 STEP C UP TO LT TANK LEAK CHECK. LEAK CHECK COMPLETED. SENT TO REFUEL FOR LEAK CHECK. TANK FILLED WITHSDR DALA2024121711770Support Fitting · cracked-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #8 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC2013. REINSPECTED INBD FLAP HINGE SUPPORT FITTING #8 BHEC INSPECTION IAW NDTSPM PY6 06-10-01-003 NO CRACK INDICSDR DALA2024121711769Support Fitting · cracked-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #1 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC 2013. REINSPECTED FWD HINGE SUPPORT FITTING BHEC INSPECTION IAW PY6 06-10-01-003 WITH FS STANDARD NO CRACKS NOSDR DALA2024072907541Battery · inoperativeTHE OVERWING EMERGENCY EVACUATION LIGHT IS INOPERATIVE. OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. SATISFACTORY TEST. (LP #5841724)SDR DALA2024071607173Frame · crackedCRACK ON FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00468: FRAME AT STA Y=1133 & LONG 2R AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER ER/A 619238-14 REV ORIGINAL AND PRI REV 1. ASSOCIATED ER/A 14-619238 ADDED FOR AC 9502. (LP #SDR DALA2024071006984Finger Doubler · corrodedCORROSION ON FINGER DOUBLER BTW STA Y=867 TO STA Y=918 L26L, STA Y=946 TO STA Y=1002 L26L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FINGER DOUBLER BTW STA Y=867 TO STA Y=918 L26L, STA Y=946 TO STA Y=1002 WAS FABRICATED PER DWG 5911424 SDR DALA2024070806851Longeron · crackedCRACK ON LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT. LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2.SDR DALA2024070506802Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACKED ON CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-20SDR DALA2024070306743Frame · crackedCRACK ON CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT. CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.SDR DALA2024070306742Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK ON CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.SDR DALA2024070306741Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK AT FRAME STA 715 AND L27R CANTED KEEL AREA. CORRECTIVE ACTION: FRAME STA 715 AND L27R CANTED KEEL AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP 0425118)SDR DALA2024070206724Frame · crackedCRACKS ON FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 1 TABLE 203 FIG 201.SDR DALA2024062906602Skin · damagedAIRCRAFT 9502, INITIAL INSPECTION: ELONGATED HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR. CORRECTIVE ACTION: HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR WERE REPAIRED PER ERA 618743-14 REV. ORIGINAL. (LP 0417200)SDR DALA2024062906600Longeron · corrodedAIRCRAFT 9502, INITIAL INSPECTION: CORROSION ON LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1). CORRECTIVE ACTION: LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1) WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2, PAR 5, FIG 201. (LP 041654SDR DALA2024062706575Longeron · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK ON LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX. CORRECTIVE ACTION: LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURESDR DALA2024062706574Skin · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK (2EA) ON ANGLE AND INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH. CORRECTIVE ACTION: INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH WAS REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE SDR DALA2024062606514Skin · gougedGOUGE WAS FOUND ON SKIN BS 1013. THE SKIN WAS REPAIRED IAW SRM 53-02-01-2R REP 1 PAR 5.B(5)(C) FIG 202 SHEET 15. PERFORMED VISUAL INSPECTION, INITIAL AND REPETITIVE, EVERY 8,000 CYCLES PER B717-200 SRM 53-02-01-2R PROCEDURE 1, REPAIR 1, STEP 6.A, TABLE 202. MSDR DALA2024062506489Longeron · corrodedCRACK ON LONGERON 6L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00544: LONGERON 6L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 AND 51-41-05-0G. (LP #0411816)SDR DALA2024062406344Skin · crackedCRACK ON INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00307: INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R-1, CATEGORY A REPAIR. (LP #0409764SDR DALA2024062406342Floorbeam · crackedELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00701: ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #04SDR DALA2024062106297Longeron · crackedCRACK ON LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00543: LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404336)SDR DALA2024062106296Longeron · crackedCRACK ON LONGERON 13R STA Y=1032 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00545: LONGERON 13R STA Y=1032 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404102)SDR DALA2024062106295Web · crackedPUNCTURE ON MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00515: MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4 REPAIR 4 FIG 220. (LP #040401SDR DALA2024062006269Door Frame · corrodedCORROSION ON LOWER EDGE AND FWD EDGE DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00297: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0402912)SDR DALA2024061906216Window Frame · crackedCRACK ON UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW IN REF TO NRC 00027. SUMMARY OF NRC 00661: UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1 PROCEDURE 1, REPAIR 1. (LP #0400469)SDR DALA2024061606114Seat Track · corrodedCORROSION OUT OF LIMITS ON RH INBOARD SEAT TRACK X=-22 BTW STA Y=200-276 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00664: CORROSION LEVEL 2. SEAT TRACK X=-22 BTW STA Y=200-276 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0396078)SDR DALA2024061606113Window Frame · crackedDURING INSPECTION AFTER REMOVAL OF INTERNAL CAP UPPER AFT SIDE, A CRACK WAS FOUND ON THE UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW IN REF TO NRC 00024. SUMMARY OF NRC 00660: UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM SDR DALA2024061606111Web · crackedCORROSION ON WEB FROM STA 218 COORDINATE X=55 PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00695: CORROSION LEVEL 2. WEB FROM STA 218 COORDINATE X=55 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0394095)SDR DALA2024061406097Cusp Web · corrodedCORROSION ON CUSP MEMBRANE FROM STA Y=794 TO 813 BTW X=-55 TO -60 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00663: CORROSION LEVEL 2. REPAIR PARTS WERE FABRICATED PER B717-200 SRM 53-00-55 2R-4 FIG. 215 AND INSTALLED PER B717-200 SRM 51-41-02-0G. (LPSDR DALA2024061306055Beam · crackedCRACK ON BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00235: BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7 FIGURE 201. (LP #0390916)SDR DALA2024061306054Pan · crackedCRACK INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1). SUMMARY OF NRC 00227: INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1) WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0390698)SDR DALA2024011100474Unknown · unknownCAPTAIN WINDSHIELD ARCED AND OUTER PANEL CRACKED ON DESCENT. MAINTENANCE REPLACED THE CAPT LH WINDSHIELD IAW B717 AMM 56-11. MAINTENANCE REPLACWD THE LH WINDSHIELD TEMPERATURE CONTROLLER IAW B717 AMM 30-41. WINDSHIELD WAS WIPER REMOVED AND REINSTALLED IAW B717SDR DALA2023092707960Unknown · unknownCEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 1 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ACTIVATED. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHT BATTERY ASSY PER B-717 AMM 35-51. ALL LIGHTS OPERATE NORMAL NOW. AIRCRAFT OK FOR SERVICE. (LP #9986094)SDR DALA2023050803561Unknown · unknownSURFACE CORROSION ON SKIN CLIP STA 1022, BETWEEN STR 25-26L. - MARKED- SUMMARY NRC: 077-0001:0514-2001/010 00377 CLEANED AREA, EDGE SEALED, AND APPLIED CIC PER B717 SRM 53-00-06-2R PROCEDURE 2. (LP #2748010)SDR DALA2023052204050Unknown · unknownINNER LAP SKIN HAS SURFACE CORROSION. STA 1006-1047, JUST ABOVE STR 26L. -MARKED-. SUMMARY SEE NRC 077-0001:0514-2001/008 00375: REPLACED INNER SKIN SIN LAP FINGER DOUBLER REF DACDWG 5919707. (LP #2746141)SDR DALA2023051203745Unknown · unknownFOUND STR 27L AND 28L END CLIPS CORRODED AT STA 1053. SUMMARY SEE NRC 077-0001:0514-2001/006 00369: REPLACED END CLIPS AT STR 27L AND 28L STA 1053 PER B717 SRM 51-40-02. (LP #2746150)SDR DALA2023050203397Unknown · unknownORROSION ON STR 26L BETWEEN STA 1022-1043. -MARKED-. INSTALLED STRINGER 26L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746142)SDR DALA2023050203394Unknown · unknownAREAS OF CORROSION ON STR 27L, BETWEEN STA 1022-1050. -MARKED-. INSTALLED STRINGER 27L AND SPLICE IAW B717 SRM 53-00-05-2R PROCEDURE 2. (LP #2746146)SDR DALA2023042703286Unknown · unknownTASK CARD NUMBER: 001-0231:2520-1002/002 REF NR 00325. FOUND CORROSION ON SKIN UNDER FORWARD DRAIN MAST. CORROSION LEVEL 2. REPLACED DOUBLER AND INTERCOSTAL PER B717 DRAWING 9923686. (LP #2731615)
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