N965AT
Service difficulty reports · 196
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 = 'N965AT' 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 = 'N965AT' 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 DALA2026102205832Skin · damagedFOUND SEVERAL EXISTING LIGHTNING STRIKE DAMAGES COMMON TO STRINGER L2R IN THE KA1717 STC AREA, COMPLIED WITH ER/A 637562-14. (1877071) (AIRCRAFT GROUNDED).SDR DALA2026102205830Doubler · damagedFOUND LIGHTNING STRIKE DAMAGE LOCATED IN PCS ANTENNA DOUBLER AREA, COMPLIED WITH ER/A 637562-14AD. (1878172) (AIRCRAFT GROUNDED).SDR DALA2026102205829Doubler · damagedLIGHTNING STRIKE DAMAGE LOCATED IN ESA ANTENNA DOUBLER AREA, COMPLIED WITH ER/A 637560-14AD. (1878165) (AIRCRAFT GROUNDED).SDR DALA2026082704865Proximity Sensor · out of adjustATB- RETURNED TO LIT DUE TO LEFT GEAR UNSAFE ANNUNCIATION. MLG DOOR PROX SENSOR ADJUSTED TO BE WITHIN LIMITS IAW AMM 32-61. OPS CHECKS GOOD. R&R LEFT MLG DOOR PER B717 AMM 32-14. LEFT MLG DOOR NO LONGER HAS PLAY. (9206672) (AIRCRAFT GROUNDED).SDR DALA2026082104770Fmu · faultedABORTED TAKEOFF AT 110 KTS DUE TO LT ENGINE UNABLE TO MAKE TAKEOFF POWER. R & R NR 1 ENGINE FMU IAW AMM 73-21 AND R & R NR 1 ENGINE FUEL PUMP IAW AMM 73-12. (9206654) (AIRCRAFT GROUNDED).SDR DALA2026080704571Tab · damagedLIGHTNING STRIKE ON RH ELEVATOR CONTROL TAB UPPER SURFACE, R/R RH ELEVATOR CONTROL TAB PER B717 AMM 27-31-04-000-801. (1742126) (AIRCRAFT GROUNDED).SDR DALA2026080604543Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1087 BTW LONG 13L & 14L, COMPLIED WITH ER/A 635909-14. (1741062) (AIRCRAFT GROUNDED).SDR DALA2026080404488Skin · crackedCRACKS FUSELAGE SKIN STA Y=1087, L-13L TO L-14L. REPAIRED PER ERA 635909-14. (1735466) AIRCRAFT WAS GROUNDED.SDR DALA2026080304467Panel · corrodedCORROSION ON ATTACH POINTS OF SLAT PANEL NR 2 AT WING LT. REPLACED PER SERVICEABLE LT WING SLAT NR 2 PER AMDS 2780-4000-LH-2. (1731207) AIRCRAFT WAS GROUNDED.SDR DALA2026080304466Frame · crackedCRACK ON CAP OF FRAME STA Y# = 1,178 BTW LONG 14RH TO 15RH AT AFT ACCESORIES COMPARTMENT. REPAIRED PER ER/A 635890-14. (1731671) AIRCRAFT WAS GROUNDED.SDR DALA2026042302606Acoustic Liner · damagedDURING SERVICE CHECK FOUND DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER. REPAIRED DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER PER B717 SRM 54-10-01 (7985278) (AIRCRAFT GROUNDED)SDR DALA2025090406565Seal · dirtyTAILCONE DOOR NOT FULLY SEATING AND SEALING ON UPPER RT SIDE OF THE DOOR. NOISE OBSERVED FROM THE UNSEATED PORTION OF THE DOOR. CLEANED SEAL, CYCLED DOOR AND PRESSURIZED ACFT. DOOR OPS AND LEAK CKS GOOD IAW AMM 52-12. (7287760)SDR DALA2025022001287Lock Link Assy · damagedSHIP 9524 -IFSD/DE- THE CREW RECEIVED A "LEFT REVERSER UNLOCK" MESSAGE. THE QRH WAS COMPLIED WITH, WHICH INCLUDED SHUTTING DOWN THE LEFT ENGINE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE OUTBOARD UPPER AND LOWER LOCK LINK ASSEMBLY. THEY ALSO REPLACSDR DALA2024081608209Static Wick · damagedDURING LIGHTRING STRIKE INSPECTION FOUND LH ELEVATOR O/B STATIC DISCHARGER CONDUCTIVE DOUBLER DAMAGED. COMPLETED TEMP REPAIR PER ENGINEEREING CONCURRENCE EMAIL TOPP 40-60-05 PAR X.B.2 LH ELEVATOR O/B STATIC DISCHANGER CONDUCTIVE REPAIR BY ERA 618920-14 REV ORISDR DALA2024081508165Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LHSDR DALA2024081508164Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LHSDR DALA2024081508163Skin · crackedCORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE SDR DALA2024081208007Hinge · damagedELONGATED HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT). (PTAS). SUMMARY OF NRC 00106: HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT) WERE REPAIRED PER ERA 559577-14MA REV ORIGINAL, PER PRI 618954-14 REV 4, AND ERSDR DALA2024081208006Skin · crackedCRACKS WERE FOUND ON UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH. SUMMARY OF NRC 00701: UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH WAS REPAIRED PER ER/A 618920-14 REV ORIGINAL SECTION I: PERMANENT REPAIR ACCOMPLISH SECTION II REPETITIVE INSPECTION ISDR DALA2024080807887Skin · dentedDENTS (2EA) ON FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH. SUMMARY OF NRC 00669: FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH WAS REPAIRED PER ESDR DALA2024080807885Pan · crackedCRACK ON PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00402: PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER PRI 618569-14 REV 7 AND ERA 618569-14 REV ORIGINAL. SECTION I PERMANENT REPAIR. (LP #0489565)SDR DALA2024080707853Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW CUTOUT AREA WAS FOUND. SUMMARY OF NRC 00628: INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 PARAGRAPH 5 FIGURE 201.SDR DALA2024072907536Skin · corrodedSEVERAL SPOTS OF CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00346: CORROSION LEVEL 2. WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, YSDR DALA2024072207311Cusp Web · crackedCRACK WAS FOUND ON LH CUSP WEB STA 588 AT PAX CABIN. SUMMARY OF NRC 00798: LH CUSP WEB STA 588 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4. (LP #0454524)SDR DALA2024071707227Skin · wornWEAR ON EDGE SKIN AROUND HOOK AT L1 DOOR. SUMMARY OF NRC 00111: EDGE SKIN AROUND HOOK AT L1 DOOR WAS REPAIRED PER PRI 619136-14 REV 1 AND ERA 619136-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-619136 ADDED FOR AC 9524. (LP #0451426)SDR DALA2024071707226Longeron · corrodedCORROSION ON END LONGERONS 25R AND 26R STA Y=1004 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00783: CORROSION LEVEL 2. END LONGERONS 25R AND 26R STA Y=1004 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0451371)SDR DALA2024071507158Frame · cracked-AD- CRACK OF 1.00 IN LENGTH APPROX ON UPPER RADIUS OF THE LH OVERWING FRAME TAB STA Y=715.00 (IN REF. CARD 5310-01436-01B STEP 7). SUMMARY OF NRC 000333: THE LH OVERWING FRAME TAB STA Y=715.00 WAS REPLACED AMDS 5310-01436-03A JOB 165-0001. (LP #0444425)SDR DALA2024071107017Pan · crackedCRACK ON INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR. (PTAS) SUMMARY OF NRC 00099: INTERNAL PAN (BEAM #1 AREA) FWD EDGE AT FWD CARGO DOOR WAS REPAIRED PER PRI 618453-14 REV 1 AND ERA 618453-14 REV ORIGINAL SECTION I PERMANENT REPAIR. (LP #0439934)SDR DALA2024071006985Frame · crackedCRACK ON FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00499: FRAME STA Y=696 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROC 1 REPAIR 1. (LP #0438169)SDR DALA2024071006983Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00766: CORROSION LEVEL2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L29R AT E/E COMPARTMENT WAS FABRICATED AND INSSDR DALA2024071006982Cusp Web · corrodedCORROSION ON CUSP WEB STA 397-406 AND X=-59. ORIGINAL THICKNESS 0.020" AND MINIMUM REMAINING THICKNESS 0.003", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1. SUMMARY OF NRC 00690: CORROSION LEVEL 2. CUSP WEB STA 397-SDR DALA2024070806852Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1.SDR DALA2024070506803Seat Track · corrodedAIRCRAFT 9524, CORROSION ON INB SEAT TRACK X22 STA Y=200 TO STA Y= 218 AT PAX CABIN (W1). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK WERE REPAIRED ON X= 22 STA Y= 200 TO STA Y= 294 PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5. (LP 0428722)SDR DALA2024070306744Cusp Web · corrodedCORROSION ON PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN (CPAX). CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN(CPAX) WERE REPLACED PER B717-200 SRMSDR DALA2024062906604Seat Track · corrodedAIRCRAFT 9524, CORROSION ON SEAT TRACK AT STA Y=898 X=44.5 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK SECTION BTW STA Y=898 TO STA Y= 935 X=44.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R REPAIR 5. (LP 0418906)SDR DALA2024062906601Pan · corrodedAIRCRAFT 9524, CORROSION ON PAN DOOR JAMB STA Y=994 TO Y= 954 BTW LONG 24 AND 28 RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2, PAN DOOR JAMB STA Y=994 TO Y=954 BTW LONG 24 AND 28 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPSDR DALA2024062706573Fitting · corrodedAIRCRAFT 9524, CORROSION ON MAIN FRAME FITTING STAY=560 L18L AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. MAIN FRAME FITTING STAY= 560 L18L AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP 0414381)SDR DALA2024062506491Web · nickedNICK ON MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX. SUMMARY OF NRC 00434: MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 REPAIR 2. (LP #0411983)SDR DALA2024062506490Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN. SUMMARY OF NRC 00744: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 PAR 5 FIGUSDR DALA2024062406341Beam · crackedCRACK ON BEAM #2 STA Y=196 APROX IN PASSANGER DOOR (L1) AT CABIN PAX. SUMMARY OF NRC 00090: AREA ON BEAM #2 STA Y=196 IN PASSANGER DOOR L1 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0406350)SDR DALA2024062006270Frame · crackedCRACK ON MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN. SUMMARY OF NRC 00441: MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4, PAR 5A. (LP #0402943)SDR DALA2024040804186Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541841-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSSDR DALA2024040804185Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541845-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541845-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSSDR DALA2024031303283Pseu · failedSHIP 9524 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC APPROACHING ATL DUE TO THE LEFT AND RIGHT "GEAR UNSAFE" INDICATIONS WITH THE GEAR HANDLE UP. THE AIRCRAFT ALSO HAD A LOSS OF FLAP/SLAT INDICATION ON APPROACH. CORRECTIVE ACTION: MAINTENANCE CYCSDR DALA2024030803185Uplock Sensor · faultedSHIP 9524 -GEAR/DE- AFTER TAKEOFF AND LANDING GEAR SELECTED TO RETRACT, THE CREW RECEIVED A "LEFT GEAR UNSAFE" INDICATION AFTER RETRACTION. THE QRH WAS COMPLIED WITH AND THE GEAR WAS EXTENDED WITHOUT ANY PROBLEMS, UNTIL THE "PSEU FAIL" MESSAGE. THE QRH WAS COMSDR DALA2024010900329Unknown · unknownSHIP 9524 -GEAR/DE- THE NOSE GEAR DID NOT EXTEND NORMALLY WHEN HANDLE WAS MOVED TO THE DOWN POSITION DURING APPROACH FOR LANDING AT HSV. THE TOWER DECLARED AN EMERGENCY. THE CREW UTILIZE THE MANUAL GEAR EXTENSION PROCEDURES PER THE QRH AND LANDED UNEVENTFULLY.SDR DALA2024010200015Unknown · unknownSHIP 9524 -GEAR/DE- THE NOSE LANDING GEAR FAILED TO EXTEND NORMALLY AFTER TWO ATTEMPTS. THE FLIGHT CREW ACCOMPLISHED A GO-AROUND, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES PER THE QRH. THE LANDING WAS UNEVENTFUL. CORRSDR DALA2023112909805Unknown · unknownTHE COCKPIT EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (B5-123). OPERATIONAL CHECK WAS GOOD. (LP #5508919)SDR DALA2023112909804Unknown · unknownMULTIPLE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN AND TAIL. MAINTENANCE REPLACED THE BATTERY PACKS B5-118, B5-260, B5116, & B5-231. OPERATIONAL CHECK WAS GOOD. (LP #5508918)SDR DALA2023103008884Unknown · unknownTHE AISLE EXIT SIGN IS HANGING FREE. *** CONTRACT MAINTENANCE EVENT - OCM: 271717 *** COMPLIED WITH ERA 613272- 14 REV ORIG. TIME LIMITED REPAIR SECT I. DEFERED TO MONITOR FOR 1 FLT CYCLE. DTW MAINTENANCE REPLACED THE FORWARD CEILING MOUNTED EXIT LIGHT ASSEMBL
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