N978AT
Service difficulty reports · 226
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 = 'N978AT' 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 = 'N978AT' 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 DALA2026101305623Web · crackedCRACKS ON RT WEBS (2EAS) BTW STA Y= 645 TO 715 AT C PAX. REPAIRED PER B717-200 SRM 53-00-55-2R. (1858343) AIRCRAFT WAS GROUNDED.SDR DALA2026101305622Frame · crackedCRACK ON OVERWING FRAME STA Y= 674 RH SIDE. OVERWING FRAME STA Y= 674 RH SIDE WAS REPLACED PER CARD 5310-01436-03B. (1857798) AIRCRAFT WAS GROUNDED.SDR DALA2026101305625Skin · crackedDENT AND CRACK FUSELAGE SKIN STA Y=370-389, L-29R & L-30. REPAIRED PER ER/A 610692-14. (1857452) AIRCRAFT WAS GROUNDED.SDR DALA2026100905574Web · crackedFOUND CRACK AT RT WEB ON BS 655-715, R & R WEB IAW SRM 53-00-55-2R-4. (1855606) (AICRAFT GROUNDED).SDR DALA2026100605530Skin · dentedSEVERAL DENTS ON LOWER SKIN OF RT AFT MOVABLE VANE WAS FOUND AT RT WING. AREA AT RT AFT MOVABLE VANE RT WING WAS REPAIRED IAW ER/A 637238-14. (1850252) AIRCRAFT WAS GROUNDED.SDR DALA2026100605529Vane · dentedDENT ON LOWER SURFACE OF RT FWD MOVABLE VANE WAS FOUND AT RT WING. WD MOVABLE VANE AT RT WING WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1. AND SRM 51-70-02-0G. (1848375) AIRCRAFT WAS GROUNDED.SDR DALA2026100205472Slat Track · crackedCRACK PLATE OF SLAT TRACK 5 NEAR XOS 530 AT LT WING, COMPLIED WITH ER/A 540095-14MA. (1843372) (AIRCRAFT GROUNDED).SDR DALA2026100105449Repair · dentedDENTS ON PREVIOUS FLUSH REPAIR BTW BS 218-256 BTW LONG 17LT TO 18 LT, R & R FLUSH REPAIR PER SRM 53-00-01-2R. (1841666) (AIRCRAFT GROUNDED).SDR DALA2026100105451Roller · wornWEAR ON SIDE ROLLER STA XOS 136 UPPER INB/ OUTB AND LOWER OUTB (SLAT TRACK 2) ALSO SIDE ROLLER UPPER INBOARD AND LOWER OUTBOARD STA XOS 240 (SLAT TRACK 5) LH WING, CORRECTIVE ACTION: R/R UPPER AND LOWER ROLLERS PER B717 AMM 27-80-02. (1841097) (AIRCRAFT GROUNDSDR DALA2026091805218Circuit Breaker · faultedCOMM 1 EXTREMELY GIVING INTERFERENCE WHEN IN FLIGHT, RESET C/B REF AMM 23-12. (9488892) (AIRCRAFT GROUNDED).SDR DALA2026080604550Unknown · odorELECTRICAL RUBBER ODOR COMING FROM AFT FA JUMP SEAT AREA, T/S PER FIM 21-22-00-810-815. FOUND NO RUBBER ODOR, COULD NOT REPLICATE ISSUE. ACFT OK FOR SERVICE. (9093748) (AIRCRAFT GROUNDED).SDR DALA2026072104278Doubler · damagedDAMAGE TO AFT CARGO DOOR JAMB DOUBLER. REPAIRED PER B717 SRM 53-20-15-2R. (1707868) AIRCRAFT GROUNDED.SDR DALA2026072104277Skin · damagedDAMAGE TO FUSELAGE SKIN. REPAIRED PER B717 SRM 53-20-15-2R. (1708438) AIRCRAFT GROUNDED.SDR DALA2026060203344Battery Pack · no testSHIP 9543 DURING SVC CHECK, FOUND AFT EXIT DOOR EMERGENCY LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: R/R'D AFT EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. (8660314) (AIRCRAFT GROUNDED)SDR DALA2025122309344Pump · faultedTHE CREW REPORTED LT HYDRAULIC QTY LOW MESSAGE, FOLLOWED QRH AND LANDED WITH SYSTEM PRESSURE AND QUANTITY. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT RESERVOIR.(7954928)SDR DALA2025030401651Control Module · faultedSHIP 9543 -FCNT/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE TRAILING EDGE FLAPS BEIN INOPERATIVE ON APPROACH. A NORMAL LANDING WAS ACCOMPLISHED AND NO ISSUES WITH BREAKING DURING ROLLOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FLAP/SLAT SDR DALA2024122712032Pan · corrodedCORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH. SUMMARY OF NRC 00644: CORROSION LEVEL 2. CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH WAS REPAIRED PER ER/A 623018-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623018-14 RSDR DALA2024122311963Support · crackedCRACK ON LH TRACK SUPPORT STA Y=918-915, STA Y=879-876, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00252: LH TRACK SUPPORT STA Y=876 TO 1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R- PROCEDURE 4 REPAIR 4. (LP #0721119)SDR DALA2024122311960Structure · corrodedCORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH SDR DALA2024122311959Structure · corrodedCORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORRODED BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] ANDSDR DALA2024122311958Structure · wornFOUND WEAR ON BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER. SUMMARY OF NRC 00754: BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER WAS REPAIRED PER ER/A 622465-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHSSDR DALA2024121911827Bearing · wornWORN BEARING OF FLAP AND ELONGATED HOLES ON OUTB HINGE OF LH FLAP WERE FOUND. SUMMARY OF NRC 00684: OUTB HINGE OF LH FLAP WAS REPAIRED PER ER/A 622136-14 REV ORIG, SECTION I: PERMANENT REPAIR. "DTE" TIME CONTROLLED ITEM WITH LOG PAGE #0701683. ASSOCIATED ER/A SDR DALA2024121811801Skin · crackedCRACKS ON EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE. SUMMARY OF NRC 00050: EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE WAS REPAIRED PER ER/A 621926-14 REV ORIG SECTION I PERMANENSDR DALA2024121711768Skin · damaged-AD- WEAR AND ELONGATED COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE. SUMMARY OF NRC 00053: COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE WERE REPAIRED PER ERA 621994-14AD REV ORIGINAL. ASSOCIATED ER/A 14-6219SDR DALA2024121611734Skin · crackedELONGATED HOLES AND CRACKS ON COUNTERSINK OF PANEL 370CR. SUMMARY OF NRC 00658: PANEL 370CR WAS REPAIRED PER ERA 622046-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622046-14 REV 1. ASSOCIATED ER/A 14-622046.SDR DALA2024121311704Retainer · crackedCRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00663: CRACK ON INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED B717-200 SRM 56-10-SDR DALA2024121311702Frame · wornWEAR AT FRAME OF STA Y=598 LH SIDE WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00716: FRAME OF STA Y=598 LH SIDE WAS REPAIRED PER ER/A 622297-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622297-14 REV 4. ASSOCIATED ER/A 14-622297 ADDED FOR AC 9543. (LP SDR DALA2024121211664Skin · crackedCRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00774: CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, PROCEDURE 12, REPAIR 12, FIG 201. SDR DALA2024120911536Angle · corrodedCORROSION ON CUSP ANGLE OF FWD SERVICE DOOR JAMB AT FOUR POINTS; THE FIRST ONE, FORWARD OF STA Y=167; THE SECOND ONE, UNDER THE PAN AFT OF STA Y=167; THE THIRD ONE, ALSO UNDER THE PAN FORWARD OF STA Y=200; AND THE FOURTH ONE, AFT OF STA Y=200. SUMMARY OF NRC 0SDR DALA2024120911534Pan · corrodedCORROSION ON SEVERAL POINTS OF FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT. SUMMARY OF NRC 00224: CORROSION LEVEL 2. FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, RESDR DALA2024120911530Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (8 EA) X=-53.5, BTW STA Y=160 TO Y=200; STA X=44.5, BTW STA Y=160 TO Y=196; STA X=56, BTW STA Y=160 TO Y=196; STA Y=180.5, BTW STA X=13 TO X=38.25; STA Y=196, BTW STA X=15.5 TO X=44.5; STA Y=200, BTW STA X=-7 TO X=-44.5; STA Y=200, SDR DALA2024120911529Web · crackedCRACK WAS FOUND ON WEB IN STA Y=247 AND X-44.5 APPROX IN AREA OF X-44.5 (MEDIUM) AT STA Y=200 TO STA Y=266 RH SIDE. SUMMARY OF NRC 00671: CRACK ON WEB IN STA Y=247 AND X-44.5 APPROX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 215. (LP #0691502)SDR DALA2024120911528Seat Track · corrodedCORROSION ON LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00660: CORROSION LEVEL 2. LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0691470)SDR DALA2024120911527Fuel Tank · corroded-AD- CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL WELL AREA). SUMMARY OF NRC 00678: CORROSION LEVEL 2. CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL SDR DALA2024120911526Cusp Web · corrodedCORROSION ON CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX. SUMMARY OF NRC 00738: CORROSION LEVEL 2. CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2, REPAIR 2. (LP #0691024)SDR DALA2024120311395Cusp Web · corrodedCORROSION WAS FOUND ON LH CUSP ANGLE BTW STA Y=200-207 AT PASSENGER CABIN. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LH CUSP ANGLE BTW STA Y=200-207 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 3. (LP #0690306)SDR DALA2024120311394Cusp Web · crackedCRACKED IN FIVE PLACES OF THE CUSP WEB MEMBRANE AT STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y= 663, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56. SUMMARY OF NRC 00472: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ONLY ON STA Y=663, STA SDR DALA2024120311393Cusp Web · corrodedCORROSION ON CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX. SUMMARY OF NRC 00739: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR PARAGRAPH 5 B (14) FIG 216.SDR DALA2024121311700Cusp Web · crackedCUSP WEB LOCATED BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FOUND CRACKED. SUMMARY OF NRC 00647: DUE TO CRACKS, NEW CUSP WEB LOCATED AT BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG SDR DALA2024120211374Seat Track · corrodedCORROSION ON LH SEAT TRACK X=44 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00661: CORROSION LEVEL 2. LH SEAT TRACK X=44 STA Y=200 TO Y=304 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0685816)SDR DALA2024120211373Door Frame · corrodedCORROSION ON ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN (L1). SUMMARY OF NRC 00386: CORROSION LEVEL 2. ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (SDR DALA2024112711258Seat Track · corrodedCORROSION ON RH SEAT TRACK X=22 BTW STA Y=200-256 IN PASSENGER CABIN. SUMMARY OF NRC 00662: CORROSION LEVEL 2. SEAT TRACK RH X=22 STA Y=200 TO Y=266 WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5, 51-41-01-0G, AND 51-41-05-0G PAR 8. (LP #0679793)SDR DALA2024112611227Cusp Web · crackedFOUND RACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00737: CRACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0678225)SDR DALA2024112611226Longeron · crackedCRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX. SUMMARY OF NRC 0486: CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0678029)SDR DALA2024112511165Skin · dentedDENTS AND NICKS WERE FOUND ON THE EXTERNAL SKIN FLUSH REPAIR STA Y 237 AND BTW LONGERON 17L/18L. ALSO WRONG INSTALLED FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE. SUMMARY OF NRC 00343: PREVIOUS REPAIR ON STA Y 237 AND BTSDR DALA2024112511162Skin · dentedSEVERAL DENTS ON SKIN OF AFT MOVABLE FLAP VANE GUIDE AT RH WING. SUMMARY OF NRC 00196: AFT RH FLAP VANE WAS REPLACED PER AMDS 2750-4008. (LP #0670862)SDR DALA2024112211133Frame · dentedDENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 634: DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 2, REPAIR 2, FIG. 201. (LP #0670995)SDR DALA2024112111102Hinge Fitting · crackedCRACKED OUTBOARD LOWER BORE OF FLAP HINGE FITTING #3 AT RH WING. RH OUTBOARD WING FLAP HINGE FITTING WAS REMOVED PER B717-200 AMM 57-55-25 000-803 STEP A TO STEP E (2). RH OUTBOARD WING FLAP HINGE FITTING WAS REPLACED & INSTALLED PER B717-200 AMM 57-55-25 400-SDR DALA2024111911028Cusp Web · crackedCRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX. SUMMARY OF NRC 00406: CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0666517)SDR DALA2024111911026Cusp Web · crackedCRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX. SUMMARY OF NRC 00405: CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. PERFORM GVI EVERY C-CHECK PER B717 SRM 53-00-55-2R
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