N948AT
Service difficulty reports · 269
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 = 'N948AT' 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 = 'N948AT' 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 DALA2019070804075Splice · corrodedAWR IN REF MON/9508/049-MON, 95 REP, L.P. 2070042: CORROSION ON PREVIOUS REPAIR SPLICE LOWER AREA OF AFT CARGO COMPARTMENT. LEVEL 2. PREVIOUS REPAIR SPLICE LOWER AREA WERE REPLACED OF AFT CARGO COMPARTMENT PER SRM 53-20-15-2R-7, SRM 51-41-04-0G AND SRM 51-41-0SDR DALA2019070704062Cargo Track · corrodedINITIAL INSPECTION: CORROSION ON LT TIE TRACK, BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT. SUMMARY: OF NRC.00359 CORROSION LEVEL 2. LT TIE TRACK, WAS REPLACED BTW STA:915 TO STA:1020 AT AFT CARGO COMPARTMENT PER SRM 51-41-05-0G AND SRM 51-41-01-0G. (LP11SDR DALA2019070604056Frame · corrodedCORROSION ON FRAME STA:1022 BTW STGR:27L AND STGR:28R AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME WAS REPAIRED PER SRM 53-20-07-2R-3 REPAIR 3 CONFIGURATION -7005. PERFORM VISUAL INSPECTION INITIAL 25,000 CYCLES AND REPETITIVE 6,500 CYCLES PER SRM 53-20-SDR DALA2019070604059Cargo Track · corrodedINITIAL INSPECTION: CORROSION ON TIE TRACK BTW STA:994 TO STA: 1020 AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2.TIE TRACK RT BTW STA:994 TO STA:1020 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 53-20-51-0I-7 AND 51-41-01-0G. (LP1156952)SDR DALA2019070604053Cap · crackedINITIAL INSPECTION: CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7R. CRACK ON CAP AT BULKHEAD STA. 1022 LONGERON 7 RH WAS REPAIRED PER ETI-17-19-090 REV ORG. AND ERA 579434-14 REV. ORIG. (LP1156275)SDR DALA2019070604052Skin · crackedINITIAL INSPECTION: CRACK SKIN ON EXTERNAL AREA OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. SKIN ON EXTERNAL AREA OF OPENING LEVER WAS REPAIRED PER ER/A 579458-14 REV. ORIGINAL AND ETI-17-19-094 REV. 3. (LP1156212)SDR DALA2019070604051Intercostal · crackedINITIAL INSPECTION CRACKED INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 AT PASSENGER DOOR FWD ENTRANCE. INTERCOSTAL ON STA Y=184 BTW BEAM 4 AND 5 WAS REPLACED PER DWG 9955763 REVISION M, SRM 51-41-02- 0G AND 51-41-05-0G. (LP1156196)SDR DALA2019070604050Housing · wornAWR,HIDDEN WEAR: WEAR ON HOUSING OF HOLD LOCK AND OPENING LEVER AT PASSENGER DOOR FWD ENTRANCE. HOUSING OF HOLD LOCK AND OPENING LEVER WAS REPLACED PER SRM 51-41-02-0G. (LP1156264)SDR DALA2019070504043Pushrod · corrodedINITIAL INSPECTION: CORROSION ON PUSH ROD OF HOOK AT RUDDER THROW LIMITER. PUSH ROD OF HOOK AT RUDDER THROW LIMITER WAS REPLACED, ADJUSTED AND TESTED PER AMM 27-26-01-000-801, AMM 27-26-01-400-801 AND 2720-2003. (LP1154990)SDR DALA2019070504039Torque Tube · corrodedINITIAL INSPECTION: CORROSION ON RUDDER CONTROL TAB TORQUE TUBE IN REF 2720-2004 JOB #001-0259. RUDDER CONTROL TAB TORQUE TUBE WERE REPLACED FOR NEW P/N:3917927-1 AND WAS INSTALLED PER 2720-2004 JOB# 001-0259. (LP1155397)SDR DALA2019070504037Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1087 BTW LONG 13L TO 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY CSDR DALA2019070504024Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN AT STA Y=1073 LONG 14L. PERMANENT REPAIR WAS PERFORMED ON FUSELAGE SKIN AT STA Y=1073 LONG 14L PER ERA 579428-14 REV. ORG. SECTION I AND ETI 17-19-081 REV. 5. REPETITIVE INSPECTION WITHIN EVERY C CK (NOT TO EXCEED 24 SDR DALA2019070504023Skin · crackedINITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. 1087.060, LONGERON 14R SIDE. PERMANENT REPAIR FUSELAGE SKIN STA. 1087. LONGERON 14R WAS PERFORMED PER ERA 579432-14 REV. ORG. AND ETI 17-19-088 REV. 2 AND PERFORM A GVI WITHIN EVERY CCK (NOT TO EXCEED 24 MONTHS) SDR DALA2019070504042Bearing · corrodedINITIAL INSPECTION: RUSTED BEARING ON RUDDER DRIVE SECTOR AT AFT ACCESORIES COMPARTMENT IN REF 2720-2003. RUDDER DRIVE SECTOR AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER AMM 27-21-02. AND RUDDER CONTROL CABLES SYSTEM WAS ADJUSTED UNDER 2720-2004 JOB#001-02SDR DALA2019070404034Skin · crackedINITIAL INSPECTION CRACK ON SKIN AND CHANNEL MAIN LANDING GEAR DOOR RT. INNER SKIN AT RH MAIN LANDING GEAR DOOR WAS REPAIRED PER ER/A 579454-14 REVISION ORIGINAL SECTION I AND ETI-17-19-093 REVISION 3. REPETITIVE INSPECTION WITHIN EVERY 3,000 CYCLES AFTER SECTSDR DALA2019070404032Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME STA:889 AND STR:26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2, FRAME STA:889 AND STR: 26L WAS REPAIRED PER SRM 53-20-07-2R PROCEDURE 3, FIGURE 201 (SHEET 7). MAINTENANCE REQUIREMENTS ARE THE FOLLOWING. PERFORM VISUAL INSDR DALA2019070404030Doubler · corrodedINITIAL INSPECTION: CORROSION ON AFT BULKHEAD PRESSURE DOUBLER STA 1053 BTW STR 29L TO STR 29R AT AFT CARGO COMPARTMENT. OF NRC 00393 (CORROSION LEVEL 2) DOUBLER WAS REPLACED PER SRM 51-41-02-0G. (LP1153170)SDR DALA2019070304028Access Panel · corrodedPART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATE NBR 141AR (AD). FUEL ACCESS PLATE 141AR WAS REPLACED. (LP1152533)SDR DALA2019070304027Access Door · corrodedCORROSION IN COUNTERSUNK AREA AT FUEL ACCESSES PLATE NRS 620CT AND 520CT. CORROSION LEVEL 2, FUEL ACCESS DOORS 520CT AND 620CT WERE REPLACE PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III. AND PART NUMBER VERIFIED PER IPC 57-22-01-01 ITEM 065. (LP1152531)SDR DALA2019070304008Longeron · crackedCRACKED LONGERON ON STA 1133 STR 2L ON AFT ACCESSORY COMPARTMENT. (CAT). NRC 00405: LONGERON WAS REPAIRED PER SRM 53-00-05-2R. (LP #1152295)SDR DALA2019070203977Skin · corrodedCORROSION ON INNER SKIN BTW STA 1037 AND STA 1040, STGR 29L AND STGR 29R AT AFT CARGO COMPARTMENT. (CCT). NRC 00394: CORROSION LEVEL 2, AREA WAS REPAIRED PER SRM 53-02-01-2R-1 FIG. 202. (LP #1151051)SDR DALA2019070203979Longeron · crackedCRACK ON LONGERON 16R, STA 1022. (CPAX). NRC 00457: PERMANENT REPAIR WAS PERFORMED ON LONGERON 16R, STA 1022 PER SRM 53-00-05-2R. (LP #1151116)SDR DALA2019070203978Frame · crackedCRACKED FRAME ON STA Y=1037 BTW LONG 16R AND 17R (CPAX). NR 00703: FRAME ON STA Y=1037 BTW LONG 16R AND 17R WAS REPAIRED PER SRM 53-20-07-2R REP. 4. (LP #1151115)SDR DALA2019070203976Frame · corrodedCORROSION ON FRAME STA 1037 BTW STR 28L AND STR 28R AT AFT CARGO COMPARTMENT. (AMDS 5314-2001). (CCT). NRC 00371: CORROSION LEVEL 2, AREA WAS REPAIRED PER SRM 53-20-07-2R REPAIR 3 CONFIGURATION -7003. (LP #1150867)SDR DALA2019070103957Fitting · crackedCRACKED "L" FITTING ON STA Y=715, X=42-58 RT AT WING BOX AREA (CPAX). NRC 00184: "L" FITTING ON STA Y=715, X=42-58 RT AT WING BOX AREA WAS REPLACE PER SRM 51-41-05-0G, PAR. 8. AND DWG #5910464 REV: DE. (LP #1149523)SDR DALA2019063003952Seat Track · corrodedCORROSION ON SEAT TRACK RT, OF FIRST OFFICER'S SEAT, IN COCKPIT. (CPIL). NRC 00615: CORROSION LEVEL 2, SEAT TRACK RT OF FIRST OFFICER WAS REPLACED PER SRM 51-41-01-0G PAR. 6. (LP #1147833)SDR DALA2019062903942Longeron · crackedCRACK ON LONGERON #16 STA 1022 LT SIDE. (CPAX). NRC 00444: LONGERON #16 STA 1022 LT WAS REPIARED PER SRM 53-00-05-2R. (LP #1145916 )SDR DALA2019062803914Frame · crackedCRACK ON FRAME STA 1037 AND LONGERON 17 LH SIDE. (CPAX). NRC 00446: FRAME STA 1037 AND LONGERON 17 LH SIDE WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1144628)SDR DALA2019062803913Longeron · crackedCRACK ON LONGERON 17 RH STA 1022. NRC 00451: LONGERON 17 RH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 FIGURE 201 (SHEET 2). (LP #1144154)SDR DALA2019062703881Longeron · crackedCRACK ON LONGERON 4RH, STA 1022. (CPAX). NRC 00456: LONGERON 4RH, STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1142313)SDR DALA2019062703880Longeron · crackedCRACK ON LONGERON 13RH STA 1037. (CPAX). NRC 00453: LONGERON 13RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1142255)SDR DALA2019062703878Door Frame · crackedCRACK ON WEB OF FUSELAGE DOOR FRAME STA. 208, LONGERON 11 LH. (CPAX). NRC 00530: WEB OF FUSELAGE DOOR FRAME WAS REPAIRED PER B717-200 SRM 53-10-15-2R PAR. 4. (LP #1142067)SDR DALA2019062603865Longeron · crackedCRACKED LONGERON 13L, BS 1037. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2 FIG. 201 (SHEET 1).SDR DALA2019062603863Longeron · crackedCRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2, FIG. 201. (SHEET 2).SDR DALA2019062603862Floor Panel · crackedCRACKS ON FLOOR PANEL 211AKF AT FLIGHT COMPARTMENT. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, PROCEDURE 2, REPAIR 2.SDR DALA2019062543821Cusp Web · corrodedCORROSION ON RH CUSP WEB BTW STA Y=565-567 IS OUT OF LIMITS. CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.215.SDR DALA2019062433797Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE. (CPAX). NRC 00533: CRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433796Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE. (CPAX). NRC 00534: CRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE WAS REPAIRED PER B717-200 SRM 56SDR DALA2019062433795Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE. (CPAX). NRC 00535: CRACK ON RINGPAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433794Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE. (CPAX). NRC.00536: CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (SDR DALA2019062433793Pan · crackedCRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN. CRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433792Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927, RH SIDE. CRACK ON RING PAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927 RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433790Pan · crackedCRACKS ON PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R REPAIR 4 FIG. 201.SDR DALA2019062423789Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE. RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062423788Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE. (CPAX). NRC 00539: RINGPAN OF PASSENGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1135004)SDR DALA2019062423787Pan · crackedCRACKED RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN. RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062423786Pan · crackedCRACKED RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN. RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.SDR DALA2019062423785Pan · crackedCRACKED LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN. LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.SDR DALA2019062423784Pan · crackedCRACKED RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN (CPAX). NRC 00627: RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1134973)SDR DALA2019062423783Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 145 BETWEEN X=- 44 TO X=-53 RH SIDE. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-40-05 AND DWG #9936533 REV CM.
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