N951AT
Service difficulty reports · 209
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 = 'N951AT' 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 = 'N951AT' 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 DALA2026080604545Doubler · wornWEAR ON REPAIR DOUBLER ON FIXED LEADING EDGE STA XIS= 134, CUTOUT OF SLAT TRACK 2 AT RIGHT WING, COMPLIED WITH ER/A 635913-14. (1741054) (AIRCRAFT GROUNDED).SDR DALA2026080604544Doubler · wornWEAR ON REPAIR DOUBLER ON FIXED LEADING EDGE STA XIS= 134, CUTOUT OF SLAT TRACK 2 AT RIGHT WING, COMPLIED WITH ER/A 635913-14. (1741051) (AIRCRAFT GROUNDED).SDR DALA2026072804380Cusp Web · crackedCRACKS ON CUSP WEB WRE FOUND ON STA X= -58 AND STA Y= 674, Y= 696, AND Y= 715 AT CPAX, ALSO CORROSION ON CUSP WEB ON STA X= -58 AND STA Y= 713 AT CPAX. CUSP WEB BTW STA Y= 655 TO STA Y= 715 AT CPAX WAS REPLACED SRM 53-00-55-2R. (1723805) AIRCRAFT GROUNDED.SDR DALA2026071704222Skin · gougedLOWER LT WING SKIN UPPER SURFACE GOUGED AT WS 137 STRINGER 11 APPROX 2.4 LONG AND APPROX 0.017 DEEP, COMPLIED WITH ER/A 63340-14AD. (1702226) (AIRCRAFT GROUNDED).SDR DALA2026071704221Skin · crackedFOUND STR 11 LT CRACKED APPROX BS 160 AND 3 SKIN CRACKS , 2 AT HOLE S4 AND 1 EMANATING FROM HOLE S3, COMPLIED WITH ER/A 633840-14. (1702209) (AIRCRAFT GROUNDED).SDR DALA2026071304129Panel · no discrepancyREMOVE AND INSTALL LH I/B SPOILER PANEL TO FOM. REPAIRED LH I/B SPOILER PANEL REF B717 AMM 27-60-01. (1695364) (AIRCRAFT GROUNDED)SDR DALA2026070904036Doubler · crackedCRACK INDICATIONS IN THE LT MLG DOUBLER AREA AT UPPER AUX SPAR #1, #2 AND LOWER AUX SPAR #3, UNK #1,#2,#3, COMLIED WITH ER/A 634210-14. (1688524) (AIRCRAFT GROUNDED).SDR DALA2026070803994Skin · crackedFOUND CRACK AT INBOARD OF XSR 164 AND THE LOWER WING SKIN BETWEEN STRINGER S-11 AND THE REAR SPAR, COMPLIED WITH ER/A 634526-14AD. (1686898) (AIRCRAFT GROUNDED).SDR DALA2026070603942Skin · damagedSKIN DAMAGE LT VERT CAP FROM AIR GATE FAIRING. REPAIRED PER ER/A 635425-14. (1679920)(AIRCRAFT GROUNDED)SDR DALA2026070303897Spar · crackedCRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).SDR DALA2026070303896Spar · crackedCRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).SDR DALA2026070303895Skin · crackedCRACK FOUND AT LOWER WING SKIN BETWEEN S-11 AND THE REAR SPAR AND INBOARD SIDE OF XRS 164, COMPLIED WITH ER/A 633840-14AD. (1662158) (AIRCRAFT GROUNDED).SDR DALA2026042102508Skin · crackedCRACK INDICATION ON LOWER SKIN, INBD SIDE OF STA=164 BRACE DOUBLE 1.375" FROM INBD AFT EDGE. REF ERA 633599-14AD FOR ALL MAINT REPAIR. (1546137) (AIRCRAFT GROUNDED)SDR DALA2026042102515Skin · crackedLEFT WING INTERNAL LOWER SKIN HAS ONE CRACK 6 INCHES INBOARD OF XRS=164. RUNNING FWD AND AFT 1.0" FWD OF REAR SPAR CAP. VERIFIED WITH HFEC. IAW ERA 633599-14AD FOR ALL MAINT REPAIR. (1546124) (AIRCRAFT GROUNDED)SDR DALA2026031301750Unknown · odorFA'S REPORTED DIRTY SOCK SMELL IN CABIN ON APPROACH INTO BWI. NO SMOKE OR FUMES WERE NOTED, ODOR ONLY. COMPLETED W/C 0550-9001-B717 (8476228)SDR DALA2025042103070Warning Message · illuminatedSHIP 9510 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 110 KTS DUE TO RECEIVING AN AURAL "SLAT CONFIGURATION" MESSAGE. CORRECTIVE ACTION: MAINTENANCE (LP #7507750)SDR DALA2024100409700Barrel Nut · corrodedCORROSION ON BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH), AND 29 (LOWER RH) AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00544: CORROSION LEVEL 2. BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH) CLEANED PER DAL P.S. 900-1-2-1 NO 01 ANDSDR DALA2024100209618Skin · corroded-AD- CORROSION ON UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL. SUMMARY OF NRC 00216: CORROSION LEVEL 2. UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL WAS REPAIRED PER PRI 620162-14 REV 8 AND ER/A 620162-14AD REV ORIGINAL SECTION I: PERMSDR DALA2024100209616Skin · cracked-AD- CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH (FUS). SUMMARY OF NRC 00348: CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH WAS REPAIRED PER ER/A 619986-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 23-SESDR DALA2024091809138Skin · crackedCRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R. SUMMARY OF NRC 00047: CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R WAS REPAIRED PER ERA 619868-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II. ACCOMPLISH REPESDR DALA2024090508739Floorbeam · corrodedCORROSION ON FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00135: CORROSION LEVEL 2. FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT WAS REPLACED PER DWG 5971111 REV F AND PER B717-200 SRM 51-41-SDR DALA2024090408733Pan · corrodedCORROSION ON JAMB PAN (BTW LONG 25RH-29RH) LOWER EDGE AND AFT EDGE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2. JAMB PAN (BTW LONG 25RH-29RH) FWD CARGO DOOR COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. SDR DALA2024090308638Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00804: CORROSION LEVEL 2. INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT WAS REPLACED PER DRAWING 9923686 REV D AND NRC 00285. (LP #0535463)SDR DALA2024090308634Cusp Web · corrodedCORROSION ON LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN. SUMMARY OF NRC 00753: CORROSION LEVEL 2. LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR SDR DALA2024090308633Doubler · corrodedCORROSION ON DOUBLER PRODUCTION OF MASTER DRAIN BTW STA Y=199 AND Y=218, L28R, AND L29R. ALSO STA Y=163, Y= 183 BTW L29L AND L30 AT E/E COMPARTMENT. SUMMARY OF NRC 00295: CORROSION LEVEL 2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L2SDR DALA2024083008597Beam · crackedCRACK BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00225: BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 51-70-11-2R. PROCEDURE 2 REPAIR 2, FIG 201. (LP #0527465)SDR DALA2024083008595Window Frame · crackedCRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW. SUMMARY OF NRC 00693: FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0526479)SDR DALA2024082808523Web · crackedAIRCRAFT 9510, CRACK UNDER, INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX. CORRECTIVE ACTION: INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0525055)SDR DALA2024082808522Cusp Web · corrodedAIRCRAFT 9510, CORROSION OUT OF LIMITS WAS FOUND ON PASSENGER CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2- CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN WAS REPAIRED SDR DALA2024082708490Longeron · crackedAIRCRAFT 9510, CRACK ON LONGERON END (2EAS) FROM STA 1133 BTW LONG 2 LH TO LONG 2RH OF AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: LONGERON END FROM STA 1133 LONG 2RH OF AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B-717-200 SRM 53-00-05-2R PROCEDURE 2 FIG.201SDR DALA2024082708489Cusp Web · corrodedAIRCRAFT 9510, CORROSIONS ON CUSP MEMBRANE (WEB) RH ON SEVERAL LOCATIONS FROM STA Y=560 TO STA Y=579 AND STA Y=503 TO STA Y=522 AND STA Y=484 TO STA Y=503 AND STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH ON LOCATIONS FROM STA Y=560SDR DALA2024082708488Cusp Web · crackedAIRCRAFT 9510, INITIAL INSPECTION: CRACK ON CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R FIGURE 223. (LP 0523259)SDR DALA2024082708487Cusp Web · crackedAIRCRAFT 9510, AFTER BLEND OUT CRACKS WERE FOUND AT LH CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. WAS REPAIRED PER B717-200 SRM-53-00-55-2R-4. (LP 0523187SDR DALA2024082708486Window Frame · crackedAIRCRAFT 9510, HIDDEN DISCPRECANCY; AFTER BRACKET WAS REMOVED, CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW. CORRECTIVE ACTION: FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCSDR DALA2024082408420Cusp Web · corrodedAIRCRAFT 9510, CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0518607)SDR DALA2024082308415Cusp Web · crackedAIRCRAFT 9510, CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX. CORRECTIVE ACTION: CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP 0516683)SDR DALA2024082208361Floorbeam · corrodedAIRCRAFT 9510, CORROSION ON FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 AT PAX CABIN STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2, FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 WERE FABRICATED PER DWG SDR DALA2024082108331Cusp Web · corrodedAIRCRAFT 9510, INITIAL INSPECTION: CORROSION ON LH REPAIR DOUBLER OF CUSP WEB STA Y=841, Y=866 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2-LH CUSP WEB STA Y=866 AT PAX CABIN WAS REPAIR PER B717-200 SRM-53-00-55-2R-4 FIG. 214, LH CUSP WEB STA Y=841 WAS ASDR DALA2024081908280Beam · crackedCRACK ON BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR. SUMMARY OF NRC 00357: BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL SECTION I PERMANENT. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9510. (LP #0505999)SDR DALA2024081908241Skin · gougedGOUGE ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00704: EXTERNAL SKIN ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8 PAR 5 FIGURE 204. (LP #0506180)SDR DALA2024081608208Cusp Web · crackedCRACK ON INBD CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX. SUMMARY OF NRC 00389: CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIGURE 201. MAINTENANCE REQUIREMENTS VISUAL ISDR DALA2024081408113Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2). SUMMARY OF NRC 00670: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2) FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM 51-41-05-0G AND 51-4SDR DALA2024070106608Apu · fireSHIP 9510 -FIRE- WORKING APU MEL FOR NO START, TECHNICIANS REPLACED FCU AND START FUEL PURGE VALVE. APU WAS RUNNING FOR 15 MINUTES FOR LEAK AND OPS CHECKED WHEN FIRE WARNING ANNUNCIATION SOUNDED. FIRE WAS CONFIRMED, FIRE HANDLE PULLED, BOTTLE DISCHARGED. DUE TSDR DALA2024022002328Battery Pack · inoperativeTHE OVERWING EMERGENCY LIGHTS STAY ON. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY REF B717 AMM 33-51. BATTERY WAS CHARGED UP. OPERATIONAL CHECK IS GOOD. (LP #5478322)SDR DALA2023111309309Unknown · unknownBOTH THE LH & RH FWD OVERWING EXIT FLOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY AT STA 342R PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5070246)SDR DALA2023061504875Unknown · unknownWORKING AMDS AA CARD 5310-01436-03B. REPLACED RT SIDE FRAME AT STA 674 ON AMDS AA CARD 5310-01436-03B. (LP #4669550)SDR DALA2023060804665Unknown · unknownCRACK INDICATION AT OVERWING FRAME TAB STA 674 RT SIDE, MARKED (FLOOR LEVEL). SUMMARY SEE NRC 073-0004:5310-01436-01D/002 00055: REPLACED DAMAGED FRAME ON WC 5310-01436-03B. (LP #2804708)SDR DALA2023060704642Unknown · unknownLONGERON AT 11R FWD OF FRAME STA 674" REQUIRES REMOVAL FOR ACCESS TO MAKE FRAME REPLACEMENT AT STA. 674". SUMMARY SEE NRC 129-0002:5310-01436-03B/003 00293: COMPLIED WITH ERA 530437-14MA REV ORIG FOR REPAIR OF LONGERON AT 11R FWD OF FRAME STA 674". (LP #280181SDR DALA2023030701662None · noneTHE AISLE OVERHEAD EMERGENCY LIGHT COVER IS MISSING AT ROW 3. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE. (LP #9677521)SDR DALA2022120607805Access Panel · missingTHE LEFT WING INBOARD FLAP IS MISSING THE INSPECTION COVER. MAINTENANCE INSTALLED AN ACCESS COVER.
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