N953AT
Service difficulty reports · 137
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 = 'N953AT' 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 = 'N953AT' 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 DALA2026090905048Oxygen Mask · inoperativeFO'S OXYGEN MASK HARNESS DOES NOT INFLATE, R & R HARNESS PER AMM 35-12. (9096980) (AIRCRAFT GROUNDED).SDR DALA2025060604346Door · openSHIP 9512 -ATB/GEAR- RETURNED MSP DUE TO RUMBLING NOISE IN NOSE GEAR AREA AFTER GEAR RETRACTION. GEAR CYCLED BACK DOWN SHOWING LOCKED WITH 3 GREEN. NLG DOORS FOUND OPEN. NO DAMAGE NOTED. CLOSED DOORS, OPS CHECKS GOOD.SDR DALA2025060604343Battery Pack · inoperativeSHIP 9512 DURING SVC CHK FOUND ENERGENCY LIGHTS SEAT ROW 25 TO AFT OF CABIN INOP. T/S REF B717 SSM 33-51 REPLACED BATTERY PACK B5-231 REF B717 AMM 33-51. CHECKS GOOD (7262863)SDR DALA2024061105984Doubler · damagedRT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 3 SHT 1. PERFORMED HFEC IAW B717 PER B717 SRM 57-40-01-2R PROCEDURE 3 AND SDR DALA2024061005958Door · bentON ARRIVAL FOUND FUEL SELECTOR PANEL DOOR BENT OPEN. DAMAGE TO THE SLAT SEAL, DAMAGE TO FUEL SELECTOR PANEL, AND DAMAGE TO THE GUARDED SWITCHES. ALL REFUEL ASSOCIATED LATCHES WERE FOUND OPEN / UNLATCHED. REPLACED GUARDED SWITCHES IAW B717 AMM 28-21-14. REPAIRESDR DALA2024011500580Unknown · unknownDURING SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EXIT LIGHT AND ISLE OVERWING EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED 2 EACH BATTERIES, AT ROWS 18 & 19, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL LIGHTS ILLUMINATE. AIRCRAFT IS OSDR DALA2023061504881Unknown · unknownAT CRUISE, MULTIPLE SPARKS ON CENTER WINDSHIELD AND CRACK FORMED. TURNED ANTI-ICE OFF PER QRH PROCEDURE. REMOVED CENTER WINDSHIELD IAW B717 AMM 56-11-01. REPLACED CENTER WINDOW HEAT CONTROLLER IAW AMM 30-41-01 A2-10. REPLACED THE CENTER WINDOW PER B717 AMM 56-SDR DALA2023042003112Unknown · unknownSHIP 9512 -HYD/DE- THE RIGHT HYDRAULIC SYSTEM EXPERIENCED A COMPLETE LOSS OF FLUID WHILE ON APPROACH FOR LANDING. THE CREW DECLARED AN EMERGENCY WITH ATC AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE COMPLIED WITH. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE SDR DALA2023031802046Unknown · unknownSHIP 9512 - MISC/HYD - DECLARED EMERGENCY FOR THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. CORRECTIVE ACTION: FOUND RUDDER LIMITER ACTUATOR LINE LEAKING. FOUND LEAK ON PIPE ASSY CONNECTED TO RUDDER LIMITER CONTROL. PIPE WAS CHAFING AGAINST WORN ADEL CLAMP (91SDR DALA2023040402603Unknown · unknownSHIP 9512 -HYD/MISC- THE FLIGHT CREW DECLARED AN EMERGENCY FOLLOWING THE ILLUMINATION OF THE "RIGHT HYD LO" MESSAGE AND THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. THE QRH WAS COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUNDSDR DALA2023022001260None · noneSHIP 9512 -ATB/GEAR/DE- DURING CLIMB OUT AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR "UNSAFE" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED ANOTHER RETRACTION. WHEN IT WAS DETERMINED THAT THE RIGHT LANDING GEAR WSDR DALA2023011800364Structure · crackedDURING PRESSURE SEAL REMOVAL, CRACK WAS FOUND ON PASSENGER DOOR FWD UPPER CORNER. PASSENGER DOOR FWD WAS REPLACED FOR THE SERVICIABLE DOOR AND A NEW BRACKET WAS REPLACED PER AMM 52-11-01.SDR DALA2023011700313Skin · crackedCRACK ON FWD SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR (PTAS). SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 604439-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.SDR DALA2023011000171Frame · crackedCRACK ON FRAME STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00332: FRAMES ON STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2573068)SDR DALA2023011000169Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CPAX)(W1). SUMMARY OF NRC 00334: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 WAS REPLACED PER DWG 9936534 REV. BW AND B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-02-0G. (LP #2572323SDR DALA2023011000168Frame · crackedCRACK ON FRAME BS 674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00331: FRAMES ON STA Y=674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11 -2R, REPAIR 1. (LP #2571796)SDR DALA2023010308523Web · corrodedCORROSION ON WEB AT LWR SILL AREA BTW STA Y=946-954 PROJECTION LONG 28R-29R OF AFT CARGO COMPARTMENT. CORROSION LEVEL 2. WEB AT LWR SILL AREA BTW STA 946 TO STA 1002 PROJECTION LONG 28R-29R OF AFT CARGO WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-02-0G PAR 4,SDR DALA2022123008501Door Frame · corrodedCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 53-20-15- 2R REPAIR 7, SRM 51-40-02-0G, SRM 51-41-05-0G, AND SRM 51-41-01- 0G.SDR DALA2022123008500Seat Track · corrodedSEAT TRACK SECTION X=-56 BTW STA=479 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK SECTION X=-56 BTW STA=479 WAS REPAIRED IAW SRM 53-20-52-2R REP. 1 FIG. 201.SDR DALA2022122908460Seat Track · corrodedRIGHT SEAT TRACK SECTION X=-44 BTW STA Y=210 TO Y=275 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00503: CORROSION LEVEL 2. RH SEAT TRACK SECTION X =-44 BTW STA Y=218 TO Y=342 WAS REPAIRED PER B717-200 SRM 53-20 -52-2R PROCEDURE 5.SDR DALA2022122908459Seat Track · crackedAFTER REMOVAL RH SEAT TRACK SECTION X=-44 BTW STA Y= 218 TO Y=342 A CRACK WAS FOUND IN THE CUSP WEB AT STA Y=294 TO Y=300. SUMMARY OF NRC 00516: CUSP WEB STA Y=294 TO Y=300 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 222. (LP #2558235)SDR DALA2022122908458Seat Track · corrodedIN REF TO NRC 00325: SEAT TRACK SECTION X=-56 BTW STA=920 TO STA=922 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK SECTION X=- 56 BTW STA=920 TO STA=922 WAS REPAIRED PER ER/A 604805-14 SECTION I PERMANENT REPAIR REV ORIGINASDR DALA2022122908461Pan · wornWEAR ON SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00061: SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8. FIG. 206.SDR DALA2022122908457Longeron · crackedCRACK ON LOGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00469: LONGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2.SDR DALA2022122708378Web · corrodedCORROSION ON WEB BS 256, X=49. THE WEB WAS REPAIRED IAW SRM 53-00-55-2R-4R.SDR DALA2022122708377Cusp Web · crackedCRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.SDR DALA2022122708376Cusp Web · crackedCRACK IN RT CUSP WEB BTW BS 617-636, X=-53 TO X=-59 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4.SDR DALA2022122708375Seat Track · corrodedSEAT TRACK X=-22 BTW BS 200-266 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK REPLACED IAW SRM 51-41-01-0G & SRM 51-41-05-0G.SDR DALA2022122308316Angle · corrodedCORRODED OUT OF LIMITS AT CLIPS STA Y=829, Y=875, Y=912. ORIGINAL THICKNESS IS 0.032 IN AND MINIMUM REMAINING THICKNESS IS 0.10 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00376 AT PAX CABIN. CLIPS STA Y=829, Y=875, Y=912 AT PAX CABIN WERE REPLACED PER SDR DALA2022122308313Angle · crackedAFTER SEAL RETAINER REMOVAL, CRACKED INTERNAL ANGLE WAS FOUND ON APROX STA Y=390 AT FWD CARGO DOOR. INTERNAL ANGLE ON AFT LOWER EDGE APROX STA Y=390 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER DWG 9957664 REV N, B717-200 SRM 51-30-07-0G, SRM 51-41-05-0GSDR DALA2022122308312Fitting · crackedAFTER SEAL RETAINER REMOVAL, CRACK WAS FOUND ON FITTING. FITTING ON AFT LOWER EDGE AT FWD CARGO DOOR WAS REPLACED IAW SRM 51-41-01-0G AND SRM 51-41-02-0G.SDR DALA2022122208293Web · crackedCRACK ON LH CUSP WEB EDGE AT STA Y=717 AND X =56. SUMMARY OF NRC 00373: LH CUSP WEB EDGE AT STA Y=717 AND X=56 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 203. (LP #2548917)SDR DALA2022122208292Angle · crackedCRACK ON INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00048: INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02 -2R PROCEDURE 1 REPAIR 1. (LP #2548249)SDR DALA2022122108269Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=218 - X=0 (CPAX)(W1). SUMMARY OF NRC 00363: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=218 - X=0 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2547442)SDR DALA2022122108268Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CPAX)(W1). SUMMARY OF NRC 00335: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS FABRICATED AND REPLACED PER DWNG 936534 REV BW AND B717-200 SRM 51-41-02-0G. (LP #2547431)SDR DALA2022122108267Support · corrodedCORROSION ON GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 (CPAX)(W1). SUMMARY OF NRC 00361: CORROSION LEVEL 2. GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 WERE REPLACED PER B717-200 SRM 51-41-02- 0G. (LP #2547311)SDR DALA2022122008238Web · puncturedPUNCTURE ON WEB STA Y=217 - X=-11 WAS FOUND DURING REMOVAL OF GALLEY SUPPORT ON NRC 00361. (CPAX)( W1). SUMMARY OF NRC 00456: WEB STA Y=217 - X=-11 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. PAR 4 FIG. 201. (LP #2545920)SDR DALA2022122008237Floor Support · corrodedSECONDARY NRC, IN REF NRC 00364: AFTER REMOVAL PARTS TO ATTEND DISCREPANCY, CORROSION ON FLOOR SUPPORT STA Y=200 AND X=-55 WAS FOUND AT PASSENGER CABIN FLOOR AREA. SUMMARY OF NRC 00462: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 AND X=-55 WAS REPLACED PER B717SDR DALA2022121908173Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-42. CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G AND B717-200 SRM 51-41-05-0G.SDR DALA2022121908176Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1). SUMMARY OF NRC 00338: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1) WAS FABRICATED AND REPLACED PER DWG 9936534 -71 AND B717-200 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #SDR DALA2022121908175Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=160-195. ORIGINAL THICKNESS IS 0.071 IN AND MINIMUM REMAINING THICKNESS IS 0.025 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00352 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR SDR DALA2022122008236Doubler · corrodedCORROSION ON RH REPAIR DOUBLER BTWN STA 908 TO STA 927 AND FROM X=44 TO X=59 OF PASSENGER CABIN FLOOR. SUMMARY OF NRC 00333: CORROSION LEVEL 2. PREVIOS REPAIR DOUBLER BTW STA 908 TO STA 927 AND FROM X=-44 TO X=-59 OF FLOOR CABIN PASSENGER WAS REPLACED PER B-71SDR DALA2022082405714None · noneTHE EMERGENCY LIGHTS OVER THE EMERGENCY EXIT WINDOWS AND ALL OF THE CEILING LIGHTS AFT OF THE OVER WING EMERGENCY EXITS CAME ON IN FLIGHT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE SYSTEM WAS RESET AND THE OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51-0SDR DALA2022081605532None · noneSHIP 9512 -HYD/GEAR- AN EMERGENCY WAS DECLARED FOR THE APPROACH AND LANDING IN BTR FOLLOWING THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE NECESSARY AND UTILIZED. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTSDR DALA2022051603342None · noneTHE AFT LOWER OVERWING EMERGENCY EXIT LIGHTS WERE DISCOVERED AS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8505194)SDR DALA2022051603341None · noneTHE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. THE BATTERY POWER SUPPLY WAS REPLACED BY MAINTENANCE PER B717 AMM 33-51. OPERATIONAL WAS CHECK GOOD. (LP #8505193)SDR DALA2022051603340None · noneTHE AFT BULKHEAD EMERGENCY EXIT LIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8505192)SDR DALA2021113007344None · noneTAIL CONE EXTERNAL RELEASE CLAMP OUT OF RIG LEFT AND RIGHT CLAMPS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0113:5352-4002/003 00423: RIGGED CLAMPS PER B717 AMM 53-52-01. OSDR DALA2021112907291None · noneTHE AFT CABIN EMERGENCY EXIT DOOR FRAME HAS TWO LARGE CRACKS. RIGHT HAND MID AREA. -M- SUMMARY SEE NRC 001-0308:5212-2001/001 00084: REPAIRED DAMAGE TO AFT CABIN EMERGENCY EXIT DOOR FRAME IAW PRI 595460-14 REV 0 THROUGH REV 4, AND ER/A 595460-14 REV ORIGINAL. SDR DALA2021112407219None · noneTHE LEFT HAND FORWARD ENTRY DOOR SLIDE HAS THE PARACHUTE PIN ROUTED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0025:5211-4002/002 00405: THE LEFT HAND FORWARD EN
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