N936AT
Service difficulty reports · 206
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 = 'N936AT' 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 = 'N936AT' 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 DALA2019061103517Frame Angle · crackedCRACK ON CLIP FRAME LONG 5LH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00393: FRAME CLIP LONG 5LH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #1117079)SDR DALA2019061103499Cusp Web · corrodedRH CORROSION CUSP MEMBRANE BTW STA Y=936 TO Y=942 AT CPAX IN REFERENCE NRC #341 IS OUT OF LIMITS. NRC 00613: CORROSION LEVEL 2, CUSP MEMBRANE BTW STA Y=936 TO Y=942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215.SDR DALA2019061103498Access Door · corrodedCORROSION ON FUEL TANK ACCESS DOOR #520CT AND #620CT OF WING LEFT -RIGHT. (AI) (AD). NRC 00609: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND #620CT WERE REPLACED AND PART NUMBER WAS VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 065.SDR DALA2019061103497Longeron · crackedCRACK ON LONGERON 5LH STA 1022 (CPAX). NRC 00387: SECTION LONGERON 5LH FROM STA 986 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1116805)SDR DALA2019061103496Floorbeam · corrodedCORROSION ON FLOOR SUPPORT AT STA 148 FROM X=-31/-44 (CPIL). NRC 00560: LEVEL CORROSION 2, FLOOR SUPPORT AT STA 148 FROM X=-31/-44 WAS REPLACED PER B717-200 SRM 51-41-02-0G. ORIGINAL THICKNESS WAS 0.040" REMAINING THICKNESS IS 0.019", THEREFORE IT IS OUT OF LISDR DALA2019061103494Longeron · crackedCRACK ON LONGERON 3RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00394: SECTION OF LONGERON 3RH FROM STA 1010 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1115922)SDR DALA201906113493Longeron · crackedCRACK ON LONGERON 5RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00395: SECTION OF LONGERON 5RH BTW STA 1010 TO 1053 WAS REPAIRED PER SRM 53-00-05-2R. (LP #1115229)SDR DALA201906113492Longeron · crackedCRACK ON LONGERON 6LH STA 1022 (CPAX). NRC 00386: SECTION LONGERON WAS REPLACED PER B717-200 SRM 53-00-05-2R-2. (ET) HFEC INSPECTION WAS PERFORMED ON LONGERON 6LH STA 1022 (CPAX) ON TRIM OUT. NO CRACKS WERE FOUND PER B717 NDT SPM PART 6. 06-10-01.001. (EQ. NORSDR DALA201906113491Cusp Web · corrodedCORROSION CUSP MEMBRANE BTW STA Y=559 TO Y=562 AT CPAX IN REFERENCE NRC #338 IS OUT OF LIMITS. NRC 00612: CUSP MEMBRANE BTW STA Y=559 TO Y=562 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114952)SDR DALA201906113490Cusp Web · crackedCRACK AT CUSP WEB STA 660 RH X=-44/-60 (FUS). NRC 00366: CRACK AT CUSP WEB STA 660 RH X=-44/-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114893)SDR DALA2019060903459Floor Panel · crackedCRACK ON FLOOR PANEL #223GF PAX CABIN. FLOOR PANEL #223GF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1113427)SDR DALA2019060503399Beam · crackedCRACKED BEAM #4 FWD EDGE AT FWD GALLEY SERVICE DOOR (R1) (PTAS). NRC 00342: BEAM #4 AT FWD GALLEY SERVICE DOOR WAS REPLACED PER B717-200 SRM 51-41-01-0G , 51-41-02-0G, AND 51-41- 05-0G. (LP #1106564)SDR DALA2019060323371Floorbeam · corrodedCORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 (CPAX). NRC 00433: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 WAS REMOVED PER B717-200 SRM 51-10-04 PAR 26 DUE TO BEING OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG 103. FLOOR SUPSDR DALA2018102206191Battery Pack · dischargedBOTH FORWARD OVERWING FLOOR EXIT IDENTIFIER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE B5-118 BATTERY PACK AND OPERATION OF THE LIGHTS RETURNED TO NORMAL REF AMM 33-51. (LP 5114264)SDR DALA2018092505735Flange · crackedSTAB INSPECTION 5530-01048-01 FOUND CRACK INDICATION IN 1 EA HOLE OF THE RT VERT STAB FWD FLANGE JUST BELOW THE LEADING EDGE SKIN SPLICE AT STA ZFS 52.267. REPAIRED PER ER/A 571712-14AD REV ORIG.SDR DALA2016110208154Seal Depressor · corrodedAFT CARGO LOWER SEAL DEPRESSORS CORRODED. REPAIRED IAW RI 551356-14 REV A SEC IV.SDR DALA2016110208153Door Sill · corrodedAFT CARGO LOWER DOOR SILL DOUBLERS CORRODED.SDR DALA2016091206510Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.SDR DALA2016090706457Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT EXIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY AND THE OPS CHECK WAS GOOD.SDR DALA2016081706043Battery Pack · dischargedDURING PRE-FLIGHT CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT EXIT ROW 19E WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.SDR DALA2016072805625Control Unit · faultyFLIGHT CREW DIVERTED THE AIRCRAFT AFTER THE NR 1 ENGINE FIRE INDICATION ILLUMINATED, ACCOMPANIED WITH AURAL WARNINGS. THE QRH PROCEDURE WAS COMPLIED WITH AND THE NR 1 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND NO EVIDENCE OF ANY ACTUAL FIRE AND REPLACED THE NR 1SDR DALA2016072605548Control Unit · faultyCREW DIVERTED THE ACFT TO RDU WITH THE NR 1 ENGINE SHUTDOWN FOLLOWING A FIRE WARNING INDICATION. DURING CRUISE AT FL330, THE EAD DISPLAYED NR 1 ENGINE FIRE AND IT WAS ACCOMPANIED BY THE AUDIBLE ALERT. CREW STATES THAT THE NR 1 ENGINE FIRE HANDLE WAS NOT ILLUSDR DALA2016041202795Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT BOTH FORWARD DOORS, L1 & R1, AND THE COCKPIT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.SDR SWAA2015111045931Light · inoperativeTAIL COMPARTMENT CATWALK, AFT EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.SDR SWAA2015110945912Battery Pack · dischargedFLIGHT STATION EMER LIGHT INOPERATIVE AT BS 123. RECONNECTED BATTERY PACK IAW AMM.SDR SWAA2015110345688Battery Pack · dischargedFORWARD OVERWING EXIT IDENTIFIERS INOPERATIVE. R & R BATTERY PACK IAW AMM.SDR SWAA2015110245603Intercostal · crackedINTERCOSTAL CRACKED AT BS 954, LONGERON 30R. R & R INTERCOSTAL IAW DWG.SDR SWAA2015110445715Sign · inoperativeEXIT IDENTIFIER SIGNS, LIGHT INOPERATIVE. R & R SIGN IAW AMM.SDR SWAA2015102345256Floor Support · brokenMAIN CABIN FLOOR SUPPORT BROKEN AT BS 256, BETWEEN RBL 22 - 44. R & R SUPPORT IAW SRM.SDR SWAA2015102045158Former · crackedCANTED KEEL FORMER CRACKED AT BS 679 RT SIDE. REPAIRED FORMER IAW EA.SDR SWAA2015101544913Doubler · corrodedFORWARD WET AREA MEMBRANE DOUBLER CORRODED, BETWEEN BS 160 - 180 & RBL 41 - 60. R & R DOUBLER IAW DWG.SDR SWAA2015101945061Membrane · crackedFORWARD WET AREA MEMBRANE CRACKED, BETWEEN BS 157 - 200, BETWEEN RBL 41 - 60. REPAIRED MEMBRANE IAW SRM.SDR SWAA2015102645368Cusp Web · corrodedRIGHT CUSP ANGLE CORRODED AT BS 218, RBL 59. REPAIRED CUSP IAW SRM & DWG.SDR SWAA2015102145190Cusp Web · corrodedCUSP MEMBRANE AT BS 218, RBL 54.5. REPAIRED MEMBRANE IAW SRM.SDR SWAA2015102045106Floorbeam · corrodedFLOORBEAM CORRODED AT BS 218, RBL 55. REPAIRED FLOORBEAM IAW EA.SDR SWAA2015102045159Cusp Web · crackedRIGHT CUSP WEB CRACKED BETWEEN BS 218 - 237. R & R CUSP WEB IAW SRM & DWG.SDR SWAA2015101444891Angle · corrodedWING TO BODY T ANGLE CLIP, CORRODED AT BS 820, LONGERON 30. R & R ANGLE CLIP IAW SRM & DWG.SDR SWAA2015101444890Angle · corrodedWING TO BODY T ANGLE CLIP, CORRODED AT BS 807, LONGERON 30. R & R ANGLE CLIP IAW SRM & DWG.SDR SWAA2015100844688Fitting · corrodedWING TO BODY ANGLE CLIP CORRODED AT BS 832, LONGERON 30. R & R CLIP IAW DWG & SRM.SDR SWAA2015102245214Former · crackedCANTED KEEL BEAM FORMER CRACKED AT BS 678, LONGERON 25L. REPAIRED FORMER IAW EA.SDR SWAA2015102245213Former · crackedLEFT CANTED KEEL BEAM FORMER CRACKED AT BS 695, LONGERON 26L. REPAIRED FORMER IAW EA.SDR SWAA2015101644998Attach Angle · crackedFRAME ATTACH ANGLE CRACKED AT BS 1174, AFT FACE LONGERON 2L. R & R ANGLE IAW SRM & DWG.SDR SWAA2015101544914Former · crackedFORMER CRACKED AT BS 695, LONGERON 30. R & R FORMER IAW DWG.SDR SWAA2015101244776Attach Angle · crackedFRAME ATTACH ANGLE CRACKED AT BS 1116, LONGERON 15R. REPAIRED ANGLE IAW SRM & DWG.SDR SWAA2015102045107Longeron · crackedLONGERON CRACKED AT BS 1133, LONGERON 2L. REPAIRED LONGERON IAW SRM.SDR SWAA2015110545763Longeron · corrodedAFT CARGO BILGE AREA LONGERON CORRODED AT BS 954, LONGERON 30. REPAIRED LONGERON IAW SRM & DWG.SDR SWAA2015102045108Former · corrodedFORMER CORRODED AT BS 946, BETWEEN LONGERON 30R - 29R. R & R FORMER IAW DWG.SDR SWAA2015101645000Seat Track · corrodedLEFT OTBD SEAT TRACK CORRODED, BETWEEN BS 218 - 588, LBL 55. R & R SEAT TRACK IAW DWG.SDR SWAA2015101644999Seat Track · corrodedLEFT OTBD SEAT TRACK CORRODED, BETWEEN BS 588 - 890, LBL 55. R & R SEAT TRACK IAW DWG.SDR SWAA2015101544916Seat Track · corrodedLEFT INBD SEAT TRACK CORRODED, BETWEEN BS 588 - 890, LBL 22. R & R SEAT TRACK IAW DWG.
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