N966AT
Service difficulty reports · 197
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 = 'N966AT' 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 = 'N966AT' 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 DALA2026092905408Doubler · installedFUSELAGE CROWN Y503 - Y522, L-1 - L-3R EXISTING DOUBLER NEAR STC INSTALL AREA. REPAIRED PER ER/A 637037-14. (1833976) AIRCRAFT WAS GROUNDED.SDR DALA2026081904728Transmitter · faultedCORROSION UNDER THE NR 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30, CORRECTIVE ACTION: COMPLIED WITH ER/A 631535-14. (1753411) (AIRCRAFT GROUNDED).SDR DALA2026012200497Uplock Sensor · faultedPERFORMED GO AROUND DUE TO RIGHT MLG UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. INDICATION RETURNED TO NORMAL AIRCRAFT LANDED SAFELY. CORRECTIVE ACTION: FOUND RIGHT MLG UPLOCK SENSOR OUT OF ADJUSTMENT. ADJUSTED SAME. SERVICED RIGHT MLG STRUT PER MCC REQSDR DALA2026011600381Skin · not reportedAIRCRAFT IS NOT TO BE RELEASE TO SERVICE UNTIL ERA 631535-14 HAS BEEN REVISED TO REFLECT FAA APPROVAL. REPAIRED PER ERA 631535-14. (1397287)SDR DALA2026011600380Skin · corrodedCORROSION UNDER NR 2 RECEIVE RADIO ALTIMETER ANTENNA. COMPLIED WITH ERA 631535-14 REV ORIG FUSELAGE SKIN REPAIR. (1397282)SDR DALA2026011600373Skin · corrodedENGINEERING 12-MONTH DTE LOG PAGE FOR CORROSION UNDER# 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30 PER ER/A 631535-14 REV A. REPAIRED PER ERA 631535-14. (1397118)SDR DALA2026010900240Seat Track · corrodedFOUND CORROSION ON RT INB SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52 (1383323)SDR DALA2026010500071Seat Track · corrodedFOUND CORROSION ON RH OTBD SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52. (1380043)SDR DALA2026010509566Web · corrodedAFTER REMOVAL OF INBOARD RT SEAT TRACK, SUB FLOOR SKIN IS CORRODED. REPAIRED SUB FLOOR MEMBRANE IAW SRM 53-00-55 (1375171)SDR DALA2024121611740Battery Pack · inoperativeTHE EMERGENCY LIGHTS POWERED BY BATTERIES B5-235 AND B5-118 ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS B5-235 AND B5-118 PER B717 AMM 33-51. OK FOR SERVICE. (LP #6519628)SDR DALA2024012901232Battery Pack · inoperativeFOUND THE FORWARD ENTRANCE EXIT PATHWAY SIGN GOING INTO COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. LIGHT OPERATION NOW CHECKS GOOD IAW B717 AMM 33-51-18. (LP #5448489)SDR DALA2023101608456Unknown · unknownTHE EMERGENCY LIGHTS DON'T OPERATE CORRECTLY DURING SERVICE CHECKS. SUMMARY OF NRC 00700: DURING CONTINUITY AND VOLTAGE CHECK TERMINAL 10, 11, AND 12 ON S3-559 WERE FOUND WITH CONTINUITY BETWEEN THEM. TERMINAL 10, 11, AND 12 ON S3-559 WERE INSTALLED CORRECTLY SDR DALA2023101608482Unknown · unknownIMPROPERLY INSTALLED TAIL-CONE KEVLAR LANYARD (CAT). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00703: TAIL-CONE KEVLAR LANYARD WAS INSTALLED CORRECTLY PER B717 AMM 53-52-01 400-8SDR DALA2023101408442Unknown · unknownELONGATED HOLES (2 EA) ON FAIRING PANEL 360AT. SUMMARY OF NRC 00511: ANGLE WAS FABRICATED AND REPLACED PER DWG 5912175 REV BR AND B717-200 SRM 51-41-02-0G AND FAIRING WAS REPAIRED PER ERA 612574-14 REV ORIGINAL, AND PRI 612574-14 REV 1. ASSOCIATED ER/A 14-6125SDR DALA2023100608221Unknown · unknownCORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA. SUMMARY OF NRC 00163: CORROSION LEVEL 2. CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA WAS REPAIRED PER PRI 611928-14 REV 3 AND ER/A 611928-14 REV ORIGINAL SECTION I: PERMANENT RESDR DALA2023100408160Unknown · unknownCRACK ON FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00649: FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIG 201 SHEET 1. (LP #0000432)SDR DALA2023100408156Unknown · unknownCORROSION ON SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO. SUMMARY OF NRC 00366: CORROSION LEVEL 2. SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO WAS REPAIRED PER ERA 612306-14 REV ORIGINAL SECTION I: PERMANENT SDR DALA2023100408159Unknown · unknownCRACK ON BRACKET AND SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR. SUMMARY OF NRC 00099: SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1, AND BRACKET (FITTING) INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPLASDR DALA2023100408155Unknown · unknownCORROSION ON STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT. (CCT) SUMMARY OF NRC 00622: CORROSION LEVEL 2. STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0000131)SDR DALA2023100408152Unknown · unknownCORROSION ON SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00336: CORROSION LEVEL 2. SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-SDR DALA2023100308096Unknown · unknownCORROSION ON FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00230: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R-2 REPAIR 2 & 53-20-06-2R-2 REPAIR 2. (LP #SDR DALA2023100308095Unknown · unknownCORROSION ON INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00203: CORROSION LEVEL 2. INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2996865)SDR DALA2023100308093Unknown · unknownCORROSION ON FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00197: CORROSION LEVEL 2. FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2. CORROSION ON FRAME WASSDR DALA2023100308089Unknown · unknownCORROSION ON FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00349: CORROSION LEVEL 2. FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND DWG 9912243 REV JSSDR DALA2023100308088Unknown · unknownCORROSION EXCESSIVE ON STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00643: CORROSION LEVEL 2. STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PER DWGSDR DALA2023100308085Unknown · unknownCORROSION ON FLOOR FITTING STA 200 TO 218 RBL=11 WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C, ORIGINAL THICKNESS IS 0.975IN AND MINIMUM REMAINING THICKNESS IS 0.850IN THEREFORE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERALSDR DALA2023100308083Unknown · unknownFITING AT STA 620 TO STA 636 L-30 HAD CORROSION FOUND ON SAME FITTING. CORROSION LEVEL 2. FITTING AT STA 620 TO STA 636 L-30 WAS FABRICATED PER DWG 5971577 REV D. FITTING OF STA 620 TO STA 636 L-30 WAS REPLACED PER DWG 5971577 REV D B717 SRM 51-41-05-0G ASDR DALA2023092908006Unknown · unknownCORROSION ON FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 0345: CORROSION LEVEL 2. FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 9958215 REV AM. (LP #2992309)SDR DALA2023092908005Unknown · unknownCRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116 WAS REPAIRED PER B717 SRM 53-00-05-2R REPAIR 2 FIG 201 SHEET 2. (LP #2992175)SDR DALA2023092908004Unknown · unknownCORROSION ON INTERCOSTAL STA Y=916 OVER STRG 28R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00328: CORROSION LEVEL 2. INTERCOSTAL ON STA Y=908 TO Y=927 STGR 28 RH WAS REPLACED PER DWG 9957704 REV M, B717 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2991968)SDR DALA2023092807971Unknown · unknownCORROSION ON WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00139: CORROSION LEVEL 2. WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (LP #2990111)SDR DALA2023092707953Unknown · unknownCRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00603: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2988599)SDR DALA2023092707952Unknown · unknownCORROSION ON CABIN FLOOR WEB DOUBLER BTW STA=641 TO 646 X=-58. CORROSION ON WEB DOUBLER BTW STA=476 TO STA=498 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00542: CORROSION LEVEL 1. CORROSION ON CABIN FLOOR WEB DOUBLER (SPLICE ANGLE) BTW STA=641 TO 646 X=-58 WAS REMOVSDR DALA2023092507867Unknown · unknownCORROSION OUT OF LIMITS ON CUSP WEB RBL=57 AND STA 266, 331, 926, 935, AND 944. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND REMAINING THICKNESS OF 0.007 INCHES, THE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, PAR 4 SDR DALA2023092507860Unknown · unknownCORROSION ON CUSP WEB STA Y=680 X=-50, AT CABIN PAX. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB BTW STA 655 TO STA 684 X=-50 AT CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 4 AND 5 FIGURE 223. (LP #2983819)SDR DALA2023092507859Unknown · unknownCORROSION ON CABIN FLOOR CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO X=-54, STA=636 TO 655 FROM X=-55 TO X=-46, AND BTW STA=655 TO STA=674 FROM X=-55 TO X=-46 RH SIDE ATSDR DALA2023092507857Unknown · unknownCRACK ON WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00093: WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PER DRAWING 9929480-49 REV BW, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G PAR 8. (LP #2982829)SDR DALA2023092507855Unknown · unknownCORROSION ON CUSP WEB STA FROM Y=860 TO Y=870 X=- 58, AT CABIN PAX. SUMMARY OF NRC 00621: CORROSION LEVEL 2. CUSP WEB STA FROM Y=860 TO Y=870 X=- 58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 216. (LP #2982286)SDR DALA2023092207783Unknown · unknownAFTER INNER SKIN REMOVAL, A CRACK WAS FOUND ON BEAM #1 AFT SECTION OF L1 DOOR. SUMMARY OF NRC 00647: BEAM #1 AFT SECTION OF L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2981121)SDR DALA2023092007728Unknown · unknownCORROSION ON CUSP WEB STA Y=256 X=-58. SUMMARY OF NRC 00618: CORROSION LEVEL 2. CUSP WEB STA 256 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 220. (LP #2978269)SDR DALA2023092107767Unknown · unknownCORROSION OUT OF LIMITS ON CABIN FLOOR CUSP WEB STA=377, STA=390, STA=417, AND STA=636 BTW -X=46 TO -X=59 RH SIDE AT PAX CABIN. ORIGINAL THICKNESS IS 0.020IN REMAINING THICKNESS IS 0.014IN THEREFORE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURSDR DALA2023092007724Unknown · unknownCORROSION OUT OF LIMITS ON CUSP WEB X=+57 STA 444, 517, 523, 544 TO 557, 608, 646 TO 660, AND 804 AT CPAX. WITH AN ORIGINAL THICKNESS=0.020 INCHES AND REMAINING THICKNESS=0.014 INCHES THEREFORE AREAS ARE OUT LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLSDR DALA2023091907686Unknown · unknownCRACK ON FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL. SUMMARY OF NRC 00381: FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976623)SDR DALA2023091907683Unknown · unknownCORROSION ON FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX. SUMMARY OF NRC 00301: CORROSION LEVEL 2. FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX WERE REPLACED PER B717 SRM 51-41-01-0G. (LP #2976176)SDR DALA2023091907682Unknown · unknownCRACK ON FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00388: FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976018)SDR DALA2023091907681Unknown · unknownCORROSION WAS FOUND AT FLOOR SUPPORT ON STA 200.0 LBL 12. SUMMARY OF NRC 00634: CORROSION LEVEL 2. FLOOR SUPPORT ON STA 200.0 LBL 12 WAS REPLACED PER B717 SRM 51-40-08-0G AND WITH NRC 00615. (LP #2976011)SDR DALA2023091907680Unknown · unknownCORROSION ON CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB. SUMMARY OF NRC 00628: CORROSION LEVEL 2. CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB WERE REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, FIG 215. (LP #2975964)SDR DALA2023091907679Unknown · unknownCORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA 200 AND LBL=5-10 AT FWD CPAX. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND MINIMUM REMAINING THICKNESS OF 0.013, THE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 C AND FISDR DALA2023091807631Unknown · unknownCRACK ON FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00389: FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2975043)SDR DALA2023091807630Unknown · unknownCORROSION OUT OF LIMITS WAS FOUND ON THE CUSP WEB STA 696 AND 715 X=-58, AT CABIN PAX. SUMMARY OF NRC 00620: CORROSION LEVEL 2. CUSP WEB STA 696 AND 715 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2974760)
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