N961AT
Service difficulty reports · 199
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 = 'N961AT' 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 = 'N961AT' 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 DALA2023091907689Unknown · unknownMISSING RELEASE CABLE AND CLIP RETAINERS (2 EA) ON TAILCONE SLIDE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00130: NEW DEPLOYMENT CABLE WAS INSTALLED PER B717-200 AMM 25-61-02 4SDR DALA2023091807627Unknown · unknownCRACK ON FRAME 17LH STA Y=1037LH (INNER STRUCTURE) AT CPAX. SUMMARY: FRAME 17LH STA Y=1037LH (INNER STRUCTURE) WAS REPAIRED PER B717-200 SRM 53-20-07-02-4, PAR 5(A)(4) TO (7) AND 51-41-05-0G PAR 8. (LP #2974201)SDR DALA2023091807626Unknown · unknownCORROSION ON LONGERON END (2 EA) STA 1053 L- 28L AND L-27L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY: NEW END LONGERON WAS INSTALLED PER B717 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #2972954)SDR DALA2023091807625Unknown · unknownCORROSION ON CUSP WEB LH SIDE STA Y=920 IN REF NRC 00402 CPAX. SUMMARY OF NRC 00594: CORROSION LEVEL 2. CUSP WEB LH SIDE STA Y=920 WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4. (LP #2972822)SDR DALA2023092107774Unknown · unknownWEAR ON CAM ASSY OF TAIL CONE RELEASE MECHANISM AT THE 10:00 0'CLOCK POSITION. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC #00025: BASE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52SDR DALA2023091407540Unknown · unknownA HOLE WAS FOUND AT LOWER SURFACE OF LH INBOARD SLAT (CLOSE TO ATTACHING POINT OF SLAT TRACK 1). SUMMARY OF NRC 00546: LOWER SURFACE OF LH INBOARD SLAT (CLOSE TO ATTACHING POINT OF SLAT TRACK 1) WAS REPAIRED PER B717-200 SRM 57-00-00-2R PROCEDURE 2 REPAIR 2. (SDR DALA2023091407539Unknown · unknownCORROSION ON PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 X=10 TO X=-10 AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00409: CORROSION LEVEL 2. PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 X=10 TO X=-10 AT AFT PRESSURE SDR DALA2023091407530Unknown · unknownCRACK ON EXTERNAL FUSELAGE NEAR RH AFT HINGE AT NOSE LANDING DOOR. SUMMARY OF NRC 00407: EXTERNAL SKIN WAS REPAIRED PER B717-200 SRM 53-10-01-2R-11 PAR. (K). (LP #2964851)SDR DALA2023091107390Unknown · unknownA CRACK WAS FOUND ON THE OUTER PAN STA 389 ON FWD CARGO COMPARTMENT DOOR (UPPER EDGE). SUMMARY OF NRC 00522: AREA ON OUTER PAN STA 389 ON FWD CARGO COMPARTMENT DOOR (UPPER EDGE) WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2962737)SDR DALA2020011000184Battery · dischargedTHE CEILING PANELS 1-8, 11-13, AND OVERWING EXIT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AT B5-227, B5-120, B5-231, AND REPLACED THE POWER SUPPLY UNIT B5 -227 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6727999)SDR DALA2019081904854Power Supply · malfunctionedTHE AFT CABIN EMERGENCY LIGHTS ARE FLASHING IN THE ARMED POSITION. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY AND POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL. (LP #6142124)SDR DALA2019081204731Battery Pack · failedROW 26C EMERGENCY LIGHT IS NOT ILLUMINATING. MAINTENANCE SUSPECTS A BAD EMERGENCY BATTERY POWER SUPPLY PACK, REPLACED THE BATTERY PACK IAW AMM 33-51-03. EEPL SYSTEM NOW OK FOR SERVICE.SDR DALA2019060903460Charger · inoperativeFOUND AFT WING EMERGENCY EXIT DOOR LOWER LIGHTS INOPERATIVE ON BOTH THE LEFT AND RIGHT SIDES. MAINTENANCE REPLACED THE BATTERY CHARGER B5-119 PER B717 AMM 33-51. NO HELP. NO POWER AT TERMINAL BLOCK 53-388 PIN 1. FOUND NEW BATTERY CHARGER BAD FROM STOCK. REPLACSDR DALA2019022531193Battery Pack · inoperativeTHE EMERGENCY LIGHTS AT ROW 20 AFT TO LAVS AND AFT OVERWING UPPER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PACKS AT STA 726 (ROW 20), STA 803 (ROW 22), AND STA 879 (ROW 25) PER B717 AMM 33-51. OPERATIONAL CHECK IS GSDR DALA2018062504175Power Supply · inoperativeEMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROW 19AB UPPER AND LOWER EXIT, SIGN, AND 19CDE LOWER EXIT SIGN. MAINTENANCE FOUND BOTH LOWER LIGHT ASSEMBLIES AT 40 OHMS AND REPLACED THE RIGHT SIDE. INSTALLED POWER SUPPLY IAW SSM 33-51. OPS CHECKED GOOD. THE AIRCRSDR DALA2018061103925Frame · corrodedAFT CARGO FRAME WAS CORRODED AT BS 1022, STRINGER 30. REMOVED THE DAMAGE SECTION OF FRAME AND INSTALLED A NEW SECTION OF FRAME, IAW SRM 53-20-07-2R 4.SDR DALA2018032001815Warning Light · false activationDECLARED AN EMERGENCY ON APPROACH, DUE TO THE TAIL TEMP HIGH WARNING INDICATION REPEATEDLY. FOLLOWING THE FIRST INDICATION THE CREW COMPLIED WITH THE QRH AND SECURED THE LEFT PACK AND BLEED. THE MESSAGE INITIALLY WENT OUT, BUT CAME BACK WITHIN 2 MINUTES. TSDR DALA2018021901003Light · missingDURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHT AT SEAT 19AB MISSING. INSTALLED A NEW LIGHT SECTION. CHECKED OK.SDR DALA2017121008489Power Supply · inoperativeLEFT & RIGHT AFT OVERWING EXIT IDENTIFIERS FOUND TO BE INOPERATIVE. (5 LTS). MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-119) PER B717 AMM 33-51. ALL OPERATIONAL CHECKS WERE NORMAL. (LP #3885940)SDR DALA2017102307732Battery Pack · inoperativeEMERGENCY LIGHTS AT ROWS 24-28 INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-03. CHECKED GOOD.SDR DALA2017091006811Intercostal · crackedCRACKED INTERCOSTAL BS 636, BL 0 ON CEILING AREA AT FWD CARGO COMPARTMENT. THE INTERCOSTLE WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.SDR DALA2017012000527Taper Pin · not reportedTAPER PINS FAIL INSPECTION FORECAST 95-0532-8-0010. REPLACED NLG DRAG BRACE REF AMM 32-22-05.SDR DALA2016111308745Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEATS 1B & 1C IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016102107426Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 20BCD IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPERATIONAL CHECK WAS GOOD.SDR DALA2016061704728Skin · corrodedCORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE. RIGHT WHEEL WELL AREA, ZONE 144, CARD 1. REPAIR WAS ACCOMPLISHED IAW ER/A 546499-14, REV ORIGINAL, HFEC ON BLENDED AREAS WAS PERFORMED AND NO ADDITIONAL DAMAGE WAS FOUND.SDR DALA2016061704727Skin · corrodedCORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE LT WHEEL WELL AREA, ZONE 145, CARD 1. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED IAW ER/A 546499-14, REV ORIGINAL. HFEC BLENDED AREA AND NO ADDITIONAL DAMAGE WAS FOUND. ASSOCIATED ER/ASDR DALA2016061504663Doubler · crackedCRACK ON PRODUCTION DOUBLER BS 1178 CANT BETWEEN LONGERON NR 1 AND NR 2 LT AT AFT ACCESSORY COMPARTMENT, SM. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 546495-14, REV ORIGINAL, PERFORM REPETITIVE INSPECTIONS AT EVERY, C-CHECK OR 3000 CYCLES WHICHEVER COME FIRSTSDR DALA2016061504661Cusp Web · corrodedCORROSION ON CUSP WEB UPPER/LOWER SURFACE AT BS 157 TO 187 BETWEEN X=-54 AND X=-60 LOWER AREA OF R1 DOOR JAMB. W1, SM, CARD 87, ZONE 200. SERVICE DOOR JAMB PAN AND CUSP ANGLE WERE REPAIRED IAW ER/A 546506-14, REV ORIGINAL.SDR DALA2016103107962Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620KB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.SDR DALA2016103107961Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620HB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.SDR DALA2016103107960Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL. THE ACCESS PANEL WAS REPLACED AND A. LEAK CHECK WAS PERFORMED.SDR DALA2016103107959Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620QB. ACCESS PANEL WAS REPLACED AND LEAK CHECKED.SDR DALA2016061404598Cargo Track · corrodedCORROSION ON LT CARGO TRACK BETWEEN BS 900 TO 1022. THE CARGO TRACK WAS REWORKED IAW SRM 51-10-04 PAR. 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-41-05 AND 51-41-01.SDR DALA2016061404597Cargo Track · corrodedCORROSION ON LEFT CARGO TRACK FROM BS 817 TO 900. CARGO TRACK WAS REPLACED IAW SRM 53-20-52, 51-41-05 AND 51-41-01.SDR DALA2016061404596Skin · damagedENLONGATED HOLES ON FUSELAGE SKIN AND LONGERON 26 LT FROM BS 1004 TO 1045. SKIN REPAIRED IAW ETI-17-16-060, REV. 2 AND ER/A 546557-14, REV. ORIGINAL.SDR DALA2016061404595Skin · crackedCRACK ON SKIN BS 1133 BETWEEN LONGERON 2-3R AT OUTER FUSELAGE SKIN AREA. SKIN WAS REPAIRED IAW ETI-17-16-035, ER/A 546487-14AD, REV. ORIGINAL. ASSOCIATED ER/A 00-546487 ADDED FOR AC 9520.SDR DALA2016061304545Finger Doubler · corrodedCORROSION ON INTERNAL STRUCTURE BETWEEN BS 1002 TO 1022, LONGERON 26L AT AFT CARGO COMPARTMENT. FINGER DOUBLER WAS REPLACED BY EXCESSIVE CORROSION IAW SRM 53-03-07, FIG 212 AND 51-41-02.SDR DALA2016061204543Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF WING ACCESS PLATE NR 520CB. CARD 38, ZONE 500. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.SDR DALA2016061204542Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 620LB. ZONE 600, CARD 35. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.SDR DALA2016061204541Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620CT. ZONE 600, DUE TO CORROSION FOUND ON ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.SDR DALA2016061204540Access Panel · corrodedCORROSION ON WING ACCESS PLATE 520CT AT SETTLEMENT AND COUNTERSKIN AREA. ZONE 500, DUE TO CORROSION FOUND ON ACCESS PLATE NR 520CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.SDR DALA2016061204539Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF WING ACCESS PLATE 520HB. ZONE 500. CORROSION ON COUNTERSKIN AT FUEL ACCESS PLATE 520HB WAS REMOVED, AND MAX DIAMETER ALLOWABLE IS 0.532 AND MAX DIAMETER MEASURED IS 0.565 IN AND WERE FOUND 3 HOLES ADJACENT OUT SDR DALA2016061204538Longeron · corrodedCORROSION ON LONGERON 29LT AND SPLICE FROM BS Y=929 TO 1022 AT AFT CARGO COMPARTMENT, C2, SM. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED, MEASURED, ORIGINAL THICKNESS: 0.125" REMAINING THICKNESS 0.110" THEREFORE IT'S WITHIN LIMITS IAW SRM 51-10SDR DALA2016061004507Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE NR 520MB. SM, CARD 40, ZONE 500. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520 MB WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUSDR DALA2016061004506Longeron · corrodedCORROSION ON LONG 28 LT AND SPLICE FROM BS Y=927 TO Y=1037 AT AFT CARGO COMPARTMENT C2, SM, ZONE 180, CARD 5. CORROSION ON LONG 28 LT FROM BS Y=927 TO BS 1037 AT AFT CARGO COMPARTMENT WAS REMOVED IAW SRM 51-10-04, PAR. 26, 21, AND 15. MEASURE: ORIGINAL THICKSDR DALA2016061004505Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE 520EB. SM, CARD 34, ZONE 500. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED ON ACCESS PLATE 520EB AND WAS MEASURED MAX. DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND MORE 2 ADJACENTSDR DALA2016060904485Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSKIN AREA OF WING ACCESS PLATE NR 620CB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSKIN WERE REMOVED IAW SRM 57-10-01, MAX DIAMETER ALLOWABLE ON COUNTERSKIN IS 0.532", MAX DIAMETER MESURED IS 0.545" AND WERE FOUND 3 ASDR DALA2016060904484Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF FUEL ACCESS PLATE NR 620MB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 620MB WAS REMOVED IAW SRM 57-10-01 MAX DIAMETER ALLOWABLE ON COUNTERSINK IS 0.532" MAX DIAMETER MEASURED SDR DALA2016060904481Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK OF WING ACCESS PLATE NR 620DT. RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED, MAX DIMENSION ALLOWABLE 0.660" MAX DIAMETER MESURED ARE 0.675" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SSDR DALA2016060904480Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620EB. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED MAX DIAM ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS 0.565" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SRM
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