N964AT

Service difficulty reports · 264

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 = 'N964AT' 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.

SDR DALA2022052703685Diffuser · missingEMERGENCY EXIT COVER DIFFUSER MISSING. MAINTENANCE RE-INSTALLED 1L DOOR EXIT SIGN COVER. (LP #8625158)May 26, 2022 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2022011300257None · noneMAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS, FROM ROW 15-19, WERE INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AT STA 645 WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8121299)Jan 13, 2022 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021120607527None · noneFOUND FORWARD CARGO DOOR SKIN LEAKING AT LOWER EDGE APPROXIMATELY STA Y 408. - M - SUMMARY SEE NRC 001-0050:5230-2004/003 00364: REPLACED FWD CARGO DOOR REF B717 AMM 52-31-01. (LP #2041378)Dec 5, 2021 · N964AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2021120607526None · noneTHE TAIL CONE RELEASE CABLE TURNBUCKLE IS BENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/001 00349: REPLACED BENT TURNBUCKLE REF B717 AMM 53-52- 01. (LP #203Dec 1, 2021 · N964AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2021120107381None · noneLEFT HAND AFT EMERGENCY DOOR JAMB HAS DAMAGE AT BOTTOM. POSSIBLE CRACK. REFER TO NRC 98: W/O P324720220210922, COMPLIED WITH ER/A 595511-14 TO REPAIR DAMAGE IN DOOR JAMB. (LP #2036011)Nov 30, 2021 · N964AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2021113007343None · noneFWD CARGO DOOR JAMB: 6 AREAS OF CORROSION LOCATED ON DOOR JAMB. -M- SUMMARY SEE NRC 001-0371:5230-2001/011 00187: CORROSION LEVEL 2, BLENDED AND CHECKED LIMITS REF B717 SRM 51-10-06. INSTALLED A NEW FWD CARGO LOWER DOOR JAM PAN, LOWER SCUFF PLATE, FWD AND AFT Nov 24, 2021 · N964AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2021111907131None · none1R DOOR AFT GIRT BAR FITTING HAS CORROSION. SUMMARY SEE NRC 042-0023:5310-2005/006 00274: 1R DOOR AFT GIRT BAR FITTING CORROSION FOUND TO BE BEYOND LIMITS PER B717 SRM 53-00-00-1A FIG 103. 1R DOOR AFT GIRT BAR FITTING WAS REPLACED WITH NEW PART REF BOEING DWG Nov 18, 2021 · N964AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2021111707084None · noneERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. ACCOMPLISH SECTION III WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 2400 FC THEREAFTER. ASSOCIATED ER/A 95-590337 ADDED FOR AC 95Nov 15, 2021 · N964AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2021111707085None · noneERA 590337-14AD SECTION I ISSUED FOR CRACK FINDINGS DURING EM5530-01048. ERA REVISED TO REV 'A' FOLLOWING DTE STAGE III. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II WITHIN 3000 FC OF SECTION I (28FEB21) AND REPEAT EVERY 3000 FC THEREAFTER. ACCOMPLISH SECTNov 15, 2021 · N964AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2021091405453Cover · detachedTHE EXIT SIGN COVER FELL OFF. MAINTENANCE REINSTALLED THE EXIT LIGHT SIGN IAW B717 AMM 33-51. (LP #7366767)Sep 13, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021083105136Hydraulic System · leakingSHIP 9514 - THE FLIGHT CREW DECLARED AN EMERGENCY WHILE ON APPROACH DUE TO THE LEFT HYDRAULIC SYSTEM LOSS OF PRESSURE FROM EITHER THE LT ENGINE DRIVEN PUMP OR THE TRANSFER PUMP. CORRECTIVE ACTION: MAINTENANCE BLED THE LT HYDRAULIC SYSTEM AND ALSO REPLACED BOTHAug 28, 2021 · N964AT · Boeing 717200 · Hydraulic System, MainSDR DALA2021081604687Power Supply · inoperativeTHE L&R AFT OVERWING EXIT UPPER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-230 AND BATTERY PER B717 AMM 33-51. TESTS GOOD. (LP #7807523)Aug 13, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021072304154Power Supply · inoperativeBOTH OF THE OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCR REPLACED THE AFT CARGO EMERGENCY BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7336449)Jul 23, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021052102838Switch · no testDURING SERVICE CHECK, FOUND F/A EMERGENCY LIGHT SWITCH NOT TESTING. MAINTENANCE REPLACED THE F/A PANEL SWITCH, NO HELP REF B717 WDM 33-51. REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK 5-125 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #May 21, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021031801530Battery Pack · no testTHE EMERGENCY LIGHTS WOULD NOT TEST FROM F/A SWITCH. MAINTENANCE FOUND THE OVERWING BATTERY PACK LOW AND REPLACED IT. THE EMERGENCY LIGHTS NOW CHECK GOOD FROM BOTH THE F/A AND COCKPIT POSITIONS. (LP #7577565)Mar 16, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021031201419Power Supply · inoperativeBOTH LEFT & RIGHT EXTERIOR EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMEGRENCY EVACUATION LIGHT BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7577552)Mar 12, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021030101128Skin · crackedCRACK DETECTED ON OPEN HOLE BY HFEC ROUTINE CARD 5530-01048-02, STEP 14, VERT STAB L/E SKIN AND FRONT SPAR CAP. CRACK INDICATION IS FIRST HOLE GOING UP R/H SIDE SKIN SPLICE L/E ZFS 52.267. MAINTENANCE REMOVED VOR #1 RH / LH AND VOR #2 RH / LH PER B717 AMM 34-3Mar 1, 2021 · N964AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2021022200992Battery Pack · inoperativeTHE OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHTS BATTERY PER B717 AMM 33-51. THE OPERATIONAL CHECK IS NOW GOOD. (LP #7543697)Feb 22, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2021021800932Switch · inoperativeTHE EMERGENCY LIGHT SWITCH AT THE ATTENDANT PANEL IS INOPERATIVE. LIGHTS WILL NOT TURN ON WHEN SWITCHED TO ARM (ON). TROUBLE SHOT PER B717 SDS 33-51-00-003 & WDM 33-51-11 AND SUSPECT B5-125 BATTERY PACK. REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY PAFeb 17, 2021 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2020120904033Slide · detachedMAINTENANCE FOUND THAT THE AFT TAIL COMPARTMENT EMERGENCY ESCAPE SLIDE WAS DETACHED FROM THE AIRCRAFT. THE TAIL CONE SLIDE WAS REPLACED, PER AMDS WORKCARD 2561-9006. RII INSPECTION OF TAILCONE SLIDE INSTALL WAS COMPLIED WITH (QC 5158) 598514. AIRCRAFT IS OKDec 4, 2020 · N964AT · Boeing 717200 · Escape SlideSDR DALA2024012401103Skin · damagedFUSELAGE GOUGE AND DENT AT STA 237 BETWEEN STRINGERS 19L AND 20L AT 8 O CLOCK POSITION STRAIGHT BELOW L/E OF SECOND WINDOW PLUG. BLENDED GOUGE. DENT DAMAGE WITHIN LIMITS PER B717 SRM 53-01-01 CONDITION 1B. ACTUAL DENT LOCATION IS BETWEEN L18L AND L19L. INTERNAMay 24, 2020 · N964AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020032301984Module · inoperativeDURING EMERGENCY LIGHT BATTERY PACK REPLACEMENT, FOUND BATTERY POWER SUPPLY MODULE FOR SEATS 10-12 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY MODULE PER B717 AMM REF 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7161872)Mar 21, 2020 · N964AT · Boeing 717200 · Emergency LightingSDR DALA2020020300781Longeron · corrodedLONGERON L28RT FROM FS 946 TO FS 898 NEEDS REPLACED DUE TO CORROSION. INSTALLED 28RT LONGERON PER B717 SRM 51-41. INSTALL COMPLETE. (LP #1467794)Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020013000725Stringer · corrodedSTRINGER 28L END FITTING AT F.S. 1053 IS CORRODED. FITTINGS INSTALLED PER B717 SRM 51-40. RII COMPLETED QC1988. (LP #1467826)Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020013000724Stringer Splice · corrodedSTRINGER 28L HAS TWO CORRODED SPLICE FITTINGS LOCATED BETWEEN F.S. 898 AND F.S. 1053. AND LONGERON 28L FROM F.S. 898 TO F.S. 1053 NEEDS REPLACED. REPLACED STRINGER 28L QC2037 REPLACED 28L LONGERON AND SPLICE FITTINGS FROM F.S. 898-1053 IAW B717 SRM 51-40.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020013000723Shear Tie · corrodedFRAME Y946 BETWEEN 23-24L FRAME FORMER FOOT CORRODED. BHEC INSPECTION OF AREA SHOWED NO DEFECT NOTED PER B717 NDT SPM PART 06-10- 01.003 DETLA QC 1991. INSTALLED FABRICATED FRAME FORMER FOOT IAW SRM 53-20 -06-2R. SKIN FASTENERS IN FORMER FOOT INSTALLED.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2020013000698Doubler · corrodedAT STRINGERS 29R TO 30R BETWEEN BS 946 TO 974, THERE IS CORROSION ON THE INTERNAL DOUBLER. REPAIRED PER ER/A 584183-14 REV O.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020013000695Doubler · corrodedREMOVED DOUBLER ON LOWER INBD OF PRESSURE BULK HEAD DUE TO CORROSION. REQUIRES OPEN HOLE INSP BHEC. NO CRACKS NOTED QC1988. REPLACED WITH NEW DOUBLER TO AFT PRESSURE BULKHEAD PER SRM 51-40.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2020013000694Stringer · corrodedSTRINGER 27L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS1053. REPLACED STRINGER 27L BETWEEN FS 898-1053 IAW B717 SRM 51-40.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020013000693Stringer · corrodedSTRINGER 24L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS 1053. REPLACED FWD PART OF LONGERON SPLICE PER SRM 51-41. REPLACED AFT SHOVEL FITTING AT FS 1053 AND LONGERON. REPLACED LONGERON 24L FS 1022 TO FS 898 PER SRM 51-41.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020013000692Intercostal · corrodedINTERCOSTAL AT STRINGER 26L AND LOCATED BETWEEN FS994 AND FS 1022 IS CORRODED. REPLACED INTERCOSTAL PER B717 SRM 51-40. RII COMPLETED QC 1988. (LP #1467731)Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2020013000691Tee Fitting · corrodedAFT PRESSURE BULKHEAD T-CORD HAS CORROSION Y1053 R29-L27. BHEC REQUIRED. NO CRACKS NOTED QC 1988. REPLACED THE AFT PRESSURE BULKHEAD T-CORD PER B717 SRM 51-40. RII COMPLETE ON T-CORD INSTALL QC 5137. (LP #1467725)Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2020013000690Skin · corrodedFUSELAGE SKIN HAS MULTIPLE AREAS OF CORROSION AND FASTENERS PULLING THROUGH FRAME Y898-Y1053 R29-L26. REPLACED SKIN PANEL IAW SRM 51-40. RII COMPLETED.Jan 30, 2020 · N964AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020012410547Former · corrodedFORMER AT FRAME 1002 AND FRAME 1002 CUT AND REMOVED DUE TO CORROSION. REPLACED FRAME 1002 BETEEN STRINGER L21-30 AND SPLICE AT L21 IAW B717 SRM 53-20-07-2R-3. RII COMPLETED BY QC2037. (LP #1455181)Jan 21, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020012210486Longeron · corrodedLONGERON 25L HAD MULTIPLE AREAS OF CORROSION BETWEEN BS. 898 AND 1053. REPLACED THE LONGERON SPLICE IAW SRM 53-00-05-02 R2, AND ER/A 584398-14, REV ORG.Jan 21, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020012210485Longeron · corrodedLONGERON 26L HAS MULTIPLE AREAS OF CORROSION BETWEEN BS 898 AND 1053. REPLACED THE LONGERON IAW SRM 53-00-05-02-R2 AND ER/A 584398-14, REV ORG.Jan 21, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020012210484Intercostal · corrodedINTERCOSTAL HAS CORROSION ON FRAMES 1022-1037 AT L25. REPLACED THE INTERCOSTAL IAW SRM 51-41.Jan 21, 2020 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2020012210483Frame Angle · damagedAT BS 1002 BETWEEN STRINGER 29 AND 30L, THERE IS A FRAME SPLICE ANGLE WITH DAMAGE BEYOND LIMITS. REPLACED FRAME ANGLE IAW SRM 51-41.Jan 21, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020011700372Frame · corrodedFRAME FORMER CORRODED Y946 R29-L26. REPLACED FRAME FORMER AT Y946 R29-L26 PER SRM 51-41-05. RII COMPLETED.Jan 16, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020011700371Frame · corrodedFRAME FORMER Y954 R29-L24 CORRODED. REMOVED FRAME FORMER AT Y954 R29-L24. CORROSION LEVEL 2, INSTALLED FRAME FORMERS PER SRM 51-41. RII COMPLETED.Jan 16, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020011700370Frame · corrodedFRAME FORMER Y974 CORRODED. REPLACED 2 EA FORMERS FROM FRAME AT Y974 FROM L23R-L29L PER SRM 51-41. RII BYBACK C/W.Jan 16, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020011700369Frame · corrodedFRAME FORMER Y927 R29-L23 IS CORRODED. ALSO FRAME 927 IS CORRODED. REMOVED FRAME FORMER AND FRAME AT SPLICE. APPLIED TREAT / SURFACE PROTECTION IAW SRM 51-10. COMPLETED FRAME FORMER & FRAME / SPLICE WAS INSTALLED IAW SRM 53-20-07 & 51-41-05. RII COMPLETED. OK Jan 16, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020011400241Stringer · corrodedSTRINGER 30 HAS THREE STRINGER FITTING WITH CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER 30 BUT ONLY ONE SPLICE REQUIRED. INSTALLED STRINGER SPLICE FITTING BETWEEN FS 898-FS1053 IAW SRM 51-40. RII COMPLETE.Jan 12, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020011300238Stringer · corrodedSTRINGER 30 HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER #30 IAW SRM 51-40. RII COMPLETE.Jan 12, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020011400240Stringer Splice · corrodedSTRINGER 29L HAS TWO CORRODED SPLICE FITTINGS LOCATED BETWEEN FS898 AND FS1053. REPLACED SPLICE FITTINGS PER SRM 51-41. INSTALLATION COMPLETE. RII COMPLETE.Jan 11, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020011300237Longeron · corrodedSTRINGER "LONGERON" 29L IS CORRODED FROM STA 1002 TO 898. REPLACED LONGERON 29L PER SRM 51-41. INSTALLATION FROM FS 898 TO FS 1053 COMPLETE. RII COMPLETE.Jan 11, 2020 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020010900142Former · corrodedFRAME FORMER Y994 L29-L23 CORRODED. REMOVED FORMER FROM Y994 L20-25, DRILLED, TREATED, AND FITTED FORMER Y994 L20-L25. OK TO INSTALL FORMER. INSTALLED FRAME FORMER ON Y994 FROM L20-L25 PER SRM B717 51-41. RII COMPLETE. (LP #1436253)Jan 8, 2020 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020010600059Doubler · corrodedINTERNAL SKIN DOUBLER LOCATED BETWEEN STRINGER 22L AND STRINGER 26L AND BETWEEN FS 994 AND FS 1053 HAS MULTIPLE AREAS OF CORROSION ON DOUBLER. REMOVED CORROSION, COMPLIED WITH PRI ER/A 584182-14 REV O STEP 7. C/W STEPS 8 AND 9 OF ER/A 584182-14 REV O. RII COMPJan 2, 2020 · N964AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2020010600058Floor Support · crackedFLOOR SUPPORT AT FR908 FROM L-L27 THRU L-L23 IS CRACKED. BHEC REQUIRED PRIOR TO INSTALLING NEW PART. NO CRACK NOTED BUT INSTALLED NEW FLOOR SUPPORT PER SRM 51-41. OK FOR SVC. (LP #1427718)Jan 2, 2020 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019040602252Bolt · frozenRT WING, OUTBD FLAP HINGE PIVOT BOLT FROZEN, SEALER BROKEN INDICATING FROZEN RUSTED BOLT. REMOVED MIDDLE AND OUTBOARD HINGE BOLTS REF B717 AMM 27-50-01. REMOVED SEALER AND FOUND I/B FITTING LEG BOLT HOLE ELONGATED REF B717 AMM 27-50-01. MACHINED O/B LUG OUTER Apr 5, 2019 · N964AT · Boeing 717200 · Trailing Edge Flaps
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