N970AT
Service difficulty reports · 201
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 = 'N970AT' 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 = 'N970AT' 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 DALA2021031801529Former · corrodedFORMER AT FS 889 CORRODED AT BL0. PER NRC 001-0291:2550-2003/018 00336 TASK COMPLETE. REPLACE FORMER PER DWG #9923486 AND REF B717 SRM 53-20- 07-2R PROCEDURE 3. (LP #1757932)SDR DALA2021031801528Door Frame · corrodedCORROSION AT MULTIPLE SPOTS AFT CARGO DOOR CUT OUT. (MARKED) PER NRC 00173 001-0371:5230-2002/002, MAINTENANCE APPLIED TOP COAT OF POLY. TASK COMPLETE PER B717 SRM 53-20-15-2R-7. (LP #1757922)SDR DALA2021040101922Trunnion · corrodedRT MLG TRUNNION FITTING ATTACH LUG FOR FIXED SIDE STRUT AFT FACE PITTED AND CORRODED. NRC 005-0001:08-5740-9- 0052/002 00009: REPAIRED PER PRI 590053-14 REV 0, 1, AND 2 AND ER/A 590053-14 REV ORIGINAL. (LP #1733182)SDR DALA2021040101921Trunnion · gougedLMLG TRUNNION FITTING FIXED SIDE BRACE ATTACH LUG BORE HAS STRAIGHT LINE GOUGE FROM FRONT TO BACK AT BOTTOM OF BORE. NRC 006-0001:08-5740-9- 0051/005 00020 REWORKED FITTING IAW B717 OHM 57-40-1, PRI 590055-14, AND ER/A 590055-14 REV ORIGINAL. (LP #1729599)SDR DALA2019122703561Panel · missingDURING B-CHECK, MAINTENANCE FOUND THAT PANEL 330KB WAS MISSING. MAINTENANCE INSTALLED A NEW PANEL (MPN 5910412-151) IAW AMM 06-33.SDR DALA2018112606793Skin · pulledMETAL PULLED AWAY FROM FWD CARGO DOOR FWD EDGE DOOR CUTOUT. MID SPAN APPROX 7" LONG X .027 WIDE. IN ACCORDANCE WITH R/I REFORMED SKIN AND REMOVED FASTENERS PERFORMED DVI AND FOUND NO FURTHER DAMAGE TO SEAL DEPRESSOR OR UNDERLYING STRUCTURE. ACCOMPLISHED SERFACSDR DALA2018032101821Light · unsecureSEAT MOUNTED EMERGENCY LIGHTING IS DAMAGED / INOPERATIVE AT 26C. MAINTENANCE RESECURED THE EMERGENCY LIGHT PER AMM 33-51. SYSTEM IS NOW OK FOR SERVICE.SDR DALA2021031901566Structure · damagedA/C DAMAGED 22 IN AFT OF R-1 DOOR. PREFORMED TIME LIMITED REPAIR PER B717 SRM 53-02-01 PARA 5.A(3) REPAIR 1. TEMP REPAIR IS LOCATED AT STA 208 STR 16R, VISUAL INSPECTED PER B717 SRM 53-02-01, NO DEFECTS FOUND, O.K. TO CONTINUE ON QC DEFERRAL. REMOVED EXTERNAL SDR DALA2017041903184Cover · detachedEMERGENCY LIGHT COVER CAME OFF FROM CEILING. SECURED EMERGENCY LIGHT COVER IAW AMM 33-51. CHECKED NORMAL.SDR DALA2016092306786Angle · damagedDAMAGE LOWER ANGLE AT LT CUSP WEB BETWEEN STA Y=889 AND STA Y=908 AND STA X=54 AND X=60 AT PASSENGER CABIN. DUCT OF ANTI-ICE SYS WAS REMOVED IAW AMM 30-10-07, PAGE BLOCK 401. SPLICE WAS REMOVED IAW SRM 51-41-05, SPLICE WAS FABRICATED IAW SRM 53-20-01, FIG 1,SDR DALA2016092306782Frame · crackedCRACKED FRAME STA 1225 CANT AND 7 HRS POSITION AT AFT ACCESSORY COMPARTMENT, SM, SN 00519. HFEC WAS ACCOMPLISHED, 01 CRACK WERE FOUND OF 1.65" IAW MD NDT SPM 06-10-01.001. VISUAL INSPECTION WAS PERFORMED NOT DISCREPANCIES WERE FOUND HFEC INSPECTION WAS ACCOMPSDR DALA2016092306779Window Frame · crackedCRACK ON UPPER OUTER RT CUTOUT OF RT WINDSHIELD, SETTLEMENT AREA, AYP, SERIAL 00620. WINDSHIELD RETAINER WAS REPLACED IAW AMM 20-60-01 914-801, SRM 51-41-02, SRM 51-40-08, DWG 9966436, REV ORIGINAL, DWG NR 5911356, REV DJ.SDR DALA2016092006724Structure · crackedCRACK ON SETTLEMENT AREA HOLES OF T/E FIXED STA XW=530 AT RT WING. T/E FIXED STA XW=530 AT RT WING WAS REPAIRED IAW ETI-17-16-122 REV 1 AND ER/A 550301-14, REV ORIGINAL, ASSOCIATED ER/A 00-550301.SDR DALA2016091906720Cargo Track · corrodedCORROSION ON LT CARGO TRACK BS 820 - 1022 BETWEEN LONGERONS 27 AND 28L AT AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.SDR DALA2016091906719Skin · crackedCRACK AT FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2 AND 3R. REPAIRED IAW ETI-17-16-115 REV. 2 AND ER/A 549302-14AD REV. ORIGINAL.SDR DALA2016091606669Channel · crackedCRACKED FWD CHANNEL ON RIGHT MLG WW CUTOUT DOOR AREA. REPLACED THE CHANNEL IAW SRM 51-41-01, 51-41-02, 51-41-05, 51-40-08, 51-10-04 PARAGRAPH 15, 21, AND AMM 20-50-02-917-801.SDR DALA2016091506637Tab · damagedLIGHTNING STRIKE AT RT GEARED ELEVATOR TAB (BROKEN FIBERS). REPAIRED IAW SRM 51-70-09 REP 5, REMOVED AND INSTALLED IAW AMM 27-31-05.SDR DALA2016091506635Channel · crackedCRACKED RT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE CHANNEL WAS REPAIRED IAW SRM 53-10-14 FIG 201.SDR DALA2016091506634Door Frame · crackedCRACKED LEFT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14 FIG 201.SDR DALA2016091506632Floor Panel · corrodedCORROSION, CRACKED, LOOSE FASTENERS ON FLOOR PANEL. CORROSION REMOVED IAW SRM 51-10-04 PAR 26SDR DALA2016091406589Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PLATE 620CB, NRC 00624. CORROSION WAS REMOVED IAW SRM 51-10-04, PAR 26. COUNTERSINK AREAS WERE MEASURED MAXIMUM COUNTERSINK DIAMETER, ALLOWABLE DOOR, PN ARB0975, IS 0.532" MAXIMUM DIAMETER MEASURED IS 0.610. THEREFORESDR DALA2016091406588Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN STA Y=994 AND Y=905 AT AFT CARGO COMPARTMENT. LONGERON 30, FRAME CLIPS, AND SPLICES BETWEEN STA Y=897 AND Y=1012 WERE REMOVED IAW SRM 51-41-05, 51-41-02, AND 53-20-05, REPAIR 1, FIG 201. NEW LONGERON 30 BETWEEN STA Y=897 AND SDR DALA2016091106509Support · crackedCRACKED RT NLG DOOR SUPPORT STA 64, SM, SN 00590. SUPPORT WAS REPLACED IAW SRM 51-41-05 AND DWG 9910088, REV LP 2675427.SDR DALA2016090906475Intercostal · crackedCRACK ON INTERCOSTAL STA Y=1076 X=-19 Z=5 AT AFT CABIN PRESSURE BULKHEAD. INTERCOSTAL WAS REPLACED IAW DWG 5917579, REV, ED ITEM -325, SRM 51-41-05 AND SRM 51-41-02.SDR DALA2016090906474Frame · crackedCRACK ON FRAMES STA Y=674 AND Y=696 AT LT KEELBEAM AREA, SM NRC 00306. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES STA Y=674 AND Y=696 AT LEFT KEELBEAM AREA. NO CSDR DALA2016090906473Frame · crackedCRACK ON FRAMES STA Y=674 AND Y=696 AT RT KEELBEAM AREA, SM NRC 308. FRAMES WERE REPAIRED IAW SRM 51-70-11, 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, 26, AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAMES, STA Y=674 AND Y=696 AT RT KEELBEAM AREA. NO CRACSDR DALA2016090906472Frame · crackedCRACKED FRAME 715 BETWEEN LONGERON 27/28 AT KEELBEAM AREA, SM, NRC 00552. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02, 51-41-05, AND 51-10-04, PAR 15,21,26 AND 37. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME STA Y=715 BETWEEN LONGERON 27/28 AT KEEL SDR DALA2016090806454Channel · crackedCRACK ON GENERATION FLOOR CHANNEL NR 221, TF, SM, NRC 00226. CRACK WAS STOP DRILLED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-41-02, SRM 51-20-09, AND SRM 53-20-50, REPAIR 5, FIG 202. HFEC INSPECTION WAS PERFORMED AT END OF CRACK. NO CRACKS WERE FOUSDR DALA2016110208150Cusp Web · corrodedEXCESIVE CORROSION ON CUSP WEB BS 911-913 AND X -54 TO -60 . DAMAGE WAS REMOVED AND A REPAIR WAS FABRICATED IAW SRM 53-00-55 RAPAIR 4 FIG 216.SDR DALA2016090706401Access Panel · damagedELONGATED HOLE ON FUEL ACCESS PLATE 520LB, SN 575. HOLE WAS REWORKED IAW SRM 57-10-01, PAR 5, CONDITION II, 3. HOLE AND COUNTERSINK WERE MEASURED WITH ID 0.3435" AND COUNTERSINK 0.613" THEREFORE WITHIN LIMITS OF REPAIR IAW SRM 57-10-01, PAR 5 CONDITION II. SDR DALA2016090706400Web · wornWEAR ON LOWER WEB LT SIDE INTERNAL STRUCTURE AT AFT CABIN BULKHEAD VENTRAL DOOR, SN 594, DUE TO EXCESSIVE DAMAGE, WEAR ON LOWER WEB LT SIDE INTERNAL WILL BE REPAIRED. RETAINERS WERE REMOVED IAW SRM 51-41-01, LOWER WEB ON LT SIDE. INTERNAL STRUCTURE WAS MEASUSDR DALA2016090506384Cusp Web · corrodedEXCESSIVE CORROSION ON CUSP WEB BETWEEN STA 478-STA 481 BETWEEN X-54--60 ON REF SN CARD 300, SN 00548. DAMAGE WAS REMOVED IAW SRM 53-00-55, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT, SPM 06-10-01.001 ALONG TRIM LINE AND NO CRACKS WERE FOUND. REPAIR PARTS WAS SDR DALA2016090506383Angle · damagedDAMAGED ON LOWER ANGLE AT RT CUSP WEB BETWEEN STA Y=579 AND STA Y=598 AND X=-54 AND X=-60 AT PASSENGER CAB, SN 00300. SPLICE WAS REMOVED DUE TO EXCESSIVE CORROSION IAW SRM 51-41-05, AND NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-20-01, FIG 51-20-09 ANSDR DALA2016090406378Pan · crackedCRACK ON RT RING PAN AFT UPPER CORNER, STA Y= 832 AT CABIN PASSENGER RT SIDE, SN 00206. DAMAGE WAS REMOVED IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=832 CABIN PASSENGER RT SIDE. NO CRACKS WERE FOUND. REPAIR PASDR DALA2016090406377Pan · crackedCRACK ON LT RING PAN FWD LOWER CORNER, STA Y= 598 AND Y= 889 AT CABIN PASSENGER LEFT SIDE, S/N 00207. DAMAGE WAS REMOVED IAW SRM 56-20-02 REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=598 AND 889 AT CABIN PASSENGER LT SIDE. NO CRACKSDR DALA2016090406376Pan · crackedCRACK ON RT RING PAN FORWARD UPPER CORNER, STA Y= 636 AND Y= 696 AT CABIN PASSENGER RT SIDE, SN 00203. DAMAGE WAS REMOVED, IAW SRM 56-20-02, REPAIR 1, FIG 202, SHEET 3 AND INSPECTION NDT CHECK FOR CRACKS ON STA Y=636 AND 696 AT CABIN PASSENGER RT SIDE, NO CRASDR DALA2016090206349Beam · crackedCRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE ON STA 389, UPPER EDGE OF BEAM 5, SN 00529. PAN UPPER EDGE ON STA 389 UPPER EDGE OF BEAM 5 WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.100".SDR DALA2016090206348Beam · crackedCRACK AT FWD CARGO COMPARTMENT DOOR PAN UPPER EDGE STA 408 UP OF BEAM 5 SN 00530. PAN UPPER EDGE ON STA 408 UP OF BEAM 5 WAS REPAIRED SRM 52-30-02, REPAIR 1, FIG 201, LENGTH CRACK: 2.400".SDR DALA2016090106318Frame · crackedCRACKED FRAME BS 1474 AND X -20. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 2, 51-30-2 AND 51-30-5.SDR DALA2016081906088Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FORWARD CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2015052803484Bulb · inoperativeDURING LINE CHECK, FOUND BULBS OUT IN L1 DOOR EXIT SIGN, RT AFT OVERWING EXIT SIGN AND LT FORWARD OVERWING EXIT SIGN. REPLACED BULBS AND OPS CHECKED GOOD.SDR DALA2015051103189Lamp · inoperativeDURING LINE CHECK, THE LEFT NR 1 OVERWING EXIT EMERGENCY SIGN LIGHT WAS INOPERATIVE. THE SIGN WAS REPLACED THE LAMP AND CHECKED NORMALLY.SDR DALA2015033102517Battery Pack · inoperativeLEFT OVER WING EMERGENCY BATTERY PACK FAILED OPS CK. REPLACED EMERGENCY LIGHT BATTERY PACK PN AD803949-1, SN ON 152426, SN OFF 136813, OPS CHECKED GOOD IAW AMM 33-51-06.SDR DALA2015033002484Frame · crackedDURING FRAME BS 674 LT INSPECTION, NOTED CRACK IN UPPER RADIUS OF THE FRAME TAB, OVER WING FRAME. REPAIRED IAW ER/A 534641-14AD.SDR DALA2014120106296Power Supply · inoperativeDURING LINE CHECK, NOTED COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY B5-123 AND CHECKED NORMAL.SDR SWAA2014090831639Light · inoperativeRIGHT AFT OVERWING EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.SDR SWAA2014090831638Light · inoperativeCATWALK 3RD AFT EMER LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.SDR SWAA2014082131085Lens · crackedMAIN CABIN FWD CEILING EMER EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.SDR SWAA2014081830925Cusp Web · crackedRIGHT CUSP WEB CRACKED BETWEEN BS 218 TO 220. R & R CUSP WEB IAW SRM & DWG.SDR SWAA2014081530876Support · corrodedBLOCK SUPPORT CORRODED AT BS 200, LBL 22. R & R SUPPORT IAW SRM & DWG.
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