N966AT

Service difficulty reports · 197

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 = 'N966AT' 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 DALA2023091807629Unknown · unknownCORROSION ON ANGLE OF LOWER BEAM APPROX STA 185 AT L1 DOOR. SUMMARY: CORROSION LEVEL 2. ANGLE OF LOWER BEAM APPROX STA 185 AT L1 DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-04-0G. (LP #2974532)Sep 17, 2023 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023091507591Unknown · unknownCRACK ON CUSP WEB STA 717-723 AND RBL=44 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA 717-723 AND RBL=44 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR. 4 AND 5, FIGURE 221. (LP #2970366)Sep 15, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023091507590Unknown · unknownCRACK ON CUSP WEB STA 717-723 AND RBL=44 AT CPAX. SUMMARY OF NRC 00397: CUSP WEB STA 717-723 AND RBL=44 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 4 AND 5, FIGURE 221. (LP #2970302)Sep 15, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023091507589Unknown · unknownCORROSION OUT OF LIMITS. CORROSION ON FLOOR FITTINGS STA 200 RBL=9 TO 44 AND STA 196 LBL=9 TO 44. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.035IN AREA, THUS IT IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERASep 15, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023091507588Unknown · unknownCORROSION ON FLOOR FITTING BWT STA 148 TO STA 200 AND LBL/RBL=7 (2 EA), STA 148 AND LBL=10 (1 EA), ALSO STA 198 AND LBL=44 (1 EA) AT FWD CPAX. SUMMARY OF NRC 00302: CORROSION LEVEL 2. FLOOR FITTING ON STA 198 LBL=44 WAS REPLACED PER B717 SRM 51-41-05-0G & FLOOSep 15, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092607923Unknown · unknownCORROSION ON FERRULES OF FLOOR PANELS 9936601- 351, 121VF, AND 121RF. SUMMARY OF NRC 00539: FLOORS PANELS 9936601-351, 121VF, AND 121RF WERE FABRICATED PER B717-200 AMM 25-58-01 350-801C2 PAR A AND ER/A 591778-14TR REV ORIGINAL SECTION I: PERMANENT REPAIR. FLOSep 13, 2023 · N966AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023091207456Unknown · unknownCORROSION ON SPLICE BTW STA Y=895 TO STA Y=901 L18R (BELOW THE CABIN FLOOR) AT CABIN PAX. SUMMARY OF NRC 00273: CORROSION LEVEL 2. SPLICE ON BTW STA Y=895 TO STA Y=901 L18R WAS REPLACED PER DWG 9930612 REV CB AND B717 SRM 51-41-05-0G. (LP #2964582)Sep 11, 2023 · N966AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023070405376Unknown · unknownTHE PILOT NOTICED A LOOSE PART NEAR 1R DOOR GIRT BAR. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED 1R DOOR SLIDE DEPLOY MECHANISM. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #4Jul 2, 2023 · N966AT · Boeing 717200 · Emergency EquipmentSDR DALA2023032602320Unknown · unknownAIRCRAFT 9525, ROWS 1-13 EMERGENCY LTS INOP. CORRECTIVE ACTION: REPLACED 2 EMERGENCY BATTERY PACK AT LOCATION 342R, AND 398R. (LP 4112094)Mar 25, 2023 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2023040402600Unknown · unknownA TRAY TABLE WAS DISCOVERED TO BE INSTALLED IN THE EMERGENCY EXIT ROW ON SEAT 21B. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED TRAY TABLE ASSEMBLY FROM THE SEAT BACK. THE AIRCMar 16, 2023 · N966AT · Boeing 717200 · Passenger Compartment EquipmentSDR DALA2023011900388Steering Sys · out of alignmentDURING THE TAKEOFF ROLL, FROM 80 KNOTS TO V1, THE AIRCRAFT YAWED LEFT. YAW ENOUGH TO REQUIRE HALF RUDDER TO MAINTAIN CENTERLINE. AIRCRAFT ALSO MOVED, YAW LT ON LANDING, AGAIN ENOUGH TO REQUIRE HALF RUDDER CORRECTION. MX IAW FIM 32-50-00 810-801, FOUND LT NLGJan 13, 2023 · N966AT · Boeing 717200 · Landing Gear Steering SystemSDR DALA2023012540046Actuator · failedTHE FLIGHT CREW REPORTED AN IMMEDIATE LOSS OF RIGHT HYDRAULIC QUANTITY UPON GEAR EXTENSION DURING APPROACH FOR LANDING. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES. THE LANDING WAS UNEVENDec 30, 2022 · N966AT · Boeing 717200 · Landing Gear ActuatorSDR DALA2023011140046Actuator · failedTHE FLIGHT CREW REPORTED AN IMMEDIATE LOSS OF RIGHT HYDRAULIC QUANTITY UPON GEAR EXTENSION DURING APPROACH FOR LANDING. THE CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY WITH ATC, AND UTILIZED THE ALTERNATE GEAR EXTENSION PROCEDURES. THAT LANDING WAS UNEVEDec 30, 2022 · N966AT · Boeing 717200 · Landing Gear ActuatorSDR DALA2022112207497Lanyard · brokenTHE FLIGHT CREW DICOVERED THAT THE METAL CABLE FROM 1L DOOR SLIDE TO GIRT BAR WAS BROKEN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. *** CONTRACT MAINTENANCE REPLACED THE L1 DOOR SLIDE RELEASE LNov 21, 2022 · N966AT · Boeing 717200 · Emergency EquipmentSDR DALA2022102706966None · noneTAIL COMPARTMENT EMERGENCY CEILING LIGHTS AND TAIL CONE SLIDE EMERGENCY LIGHTS INOP LOG-PAGE UPDATED @ 27OCT22 0620 UTC 02 CORR BY HOLDEN 00466094 CLT 27OCT22 ATA 3352 RII: N ENTR 00466094 W R/R EMERGENCY LIGHT BATTERY ASSY PER B717 AMM 33-51. P/N OFF 803949-1Oct 27, 2022 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2022061704242Cover · looseTHE AFT SIDE COVER IS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE SECURED THE SLIDE COVER AND REPLACED THE TAIL CONE SLIDE PER JIC B717 CARD 2561-7006. INSPECTED PER B717 CARD Jun 17, 2022 · N966AT · Boeing 717200 · Escape SlideSDR DALA2022032902082Circuit Breaker · trippedSHIP 9525 - THE CREW DIVERTED THE AIRCRAFT TO CLT AFTER THE LOSS OF THE RT DC BUSS AT CRUISING ALTITUDE. THE #4 AND #5 SCREENS WENT BLANK AND AP DISENGAGED. THE QRH WAS COMPLIED WITH AND THEN DUE TO WEATHER AT THE SCHEDULED DESTINATION THE DECISION WAS MADE TOMar 29, 2022 · N966AT · Boeing 717200 · DC Power Distribution SystemSDR DALA2021070503703Structure · corrodedCORROSION ON UPPER CENTER TANK SKIN AT PULLEY SUPPORT ANGLE AT STA. 745 LBL 25-34. BLENDED AND REMOVED ALL CORROSION REF B717 SRM 57-10-01-1A. UT THICKNESS INSPECTED AND MAPPED ON 1/2" GRID PER NDTSPM PART 04-00-00 TO 04-00-09. ORIGINAL THICKNESS IS .252. LOWEJul 4, 2021 · N966AT · Boeing 717200 · Hydraulic System, MainSDR DALA2021070503702Structure · corrodedCORROSION ON UPPER CENTER TANK SKIN AT PULLEY SUPPORT ANGLE AT STA. 745 RBL 48-53. SUMMARY NRC 001-0284:5310-2003/015 00415: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863524)Jul 4, 2021 · N966AT · Boeing 717200 · Fuel StorageSDR DALA2021070503701Structure · corrodedCORROSION ON UPPER CENTER TANK SKIN AT STA. 705 RBL 53. SUMMARY NRC 001-0284:5310-2003/014 00414: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863519)Jul 4, 2021 · N966AT · Boeing 717200 · Fuel StorageSDR DALA2021070503700Structure · corrodedCORROSION ON UPPER CENTER TANK SKIN AT STA. 745, RBL 23- RBL33. SUMMARY NRC 001-0284:5310-2003/012 00412: REPAIRED PER ERA 592454-14 REV. ORIG. AND PRI 592454-14 REV. 0 AND REV. 1. MATCHES ERA 592454-14 REV. ORIG. (LP #1863517)Jul 4, 2021 · N966AT · Boeing 717200 · Fuel StorageSDR DALA2021070503697Floor Support · corrodedON OK TO CIC R1 SUBFLOOR AREA: CORROSION WAS FOUND ON SUBFLOOR AND FLOOR PANEL SUPPORT. ALSO AREAS OF BARE METAL. (MARKED). SUMMARY NRC 001-0024:2040-0024/002 00454: REMOVED CORROSION AND CHECKED LIMITS REF B717 SRM 53-00-00-1A. REPLACED FLOOR SUPPORTS AS REQUJul 2, 2021 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2021070203650Skin Splice · corrodedAFT CARGO INTERNAL SKIN SPLICE CORRODED AT STA 900 BETWEEN STR 30 AND 29LT. SUMMARY SEE NRC 061-0008:5331-2001/005 00304: REPAIRED PER ER/A 592326-14 REV A ASSOCIATED ER/A 00-592326 ADDED FOR AC 9525. (LP #1860302)Jul 1, 2021 · N966AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021070703760Skin · corrodedLT WING UPPER SURFACE HAS CORROSION AT FASTENERS AFT EDGE OF UPPER SURFACE FWD OF INBOARD CORNER OF OUTBOARD SPOILER (MKD). COMPLIED WITH PRI 592282-14 REV. 0 AND 1. FINAL ERA AND PRI MATCH. REMOVED CORROSION AT STATION XRS267 AT STRINGER 1 AND CHECKED LIMITS Jun 27, 2021 · N966AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2021062903514Release Mech · failedTAIL-CONE RELEASE SYSTEM. FAILED STEP 2.G.(5). CLAMP (ITEM 28) TO CONDUIT (ITEM 29) CLEARANCE WAS BELOW 0.5 IN. WITH LATCH LEVERS IN FULL OPEN POSITION. TASK CARD 5352-2001, FIG. 5, SHEET 4. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT Jun 27, 2021 · N966AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2021062803478Stringer · corrodedIN THE AFT CARGO, STRINGER 30 IS CORRODED AT FS 908. MARKED. REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1.Jun 26, 2021 · N966AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021062903512Frame · corrodedCORROSION ON FRAME ATTACH AT STA 974 BETWEEN STRINGER 27 AND 28L. REPLACED ATTACH CLIP PER LONG BEACH DRAWING #9958215. (LP #1853038)Jun 25, 2021 · N966AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2021062903511Frame · corrodedCORROSION ON FRAME ATTACH POINT FRAME STATION 954 AFT SIDE. REPLACED ATTACH POINT PER LONG BEACH DRAWING #9958214. (LP #1852991)Jun 25, 2021 · N966AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019060903461Battery Pack · inoperativeTHE LEFT ENTRY DOOR EMERGENCY LIGHT WENT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51-03.Jun 8, 2019 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2018060503811Frame · crackedCRACK IN FRAME AT STATION 737 RT IN RADIUS AT FLOOR LEVEL. CRACK GREATER THAN 125", CONDITION 3, REF AA5310-01439-01D. NRC 075-0004:5310-01439-01D/001 00172 FRAME REPLACED ON ROUTINE CARD 083-0002:5310-01439-02B.Jun 4, 2018 · N966AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018060203783Skin · dentedFOUND DENT 13 INCHES AFT OF L1 DOOR UPPER RIGHT HAND CORNER. CUT OUT DAMAGE SKIN UPPER AFT SIDE OF L1 DOOR REF SRM 53-02-01 REPAIR 1. FABRICATED FINGER DOUBLER REF SRM 53-02-01 REPAIR 1. TREATED AND PRIMED FINGER DOUBLER AND FILLERS REF SRM 53-02-01 REPAIR 1. Oct 26, 2017 · N966AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017092207033Lens · detachedEMERGENCY EXIT SIGN LENS FELL OFF. REINSTALLED THE LENS ON THE EMERGENCY EXIT SIGN AT ROW 20. OPS NORMAL IAW AMM 33-51.Sep 21, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017091206829Battery Pack · dischargedON SERVICE CHECK MAINTENANCE FOUND THAT THE EXIT SIGN OVER BOTH LT AND RT AFT OVERWING EXITS DO NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUPPLY B5-230 PER AMM 33-51. THE OPERATIONAL CHECK WAS GOOD.Sep 12, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017081506257Sign · detachedEMERGENCY EXT SIGN HAS BEEN KNOCKED OFF. MAINTENANCE REINSTALLED THE SIGN AND OPERATIONAL CHECKS ARE GOOD.Aug 14, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017080105933Lens · missingEMERGENCY EXIT COVER DIFFUSER LENS MISSING. REINSTALLED THE SIGN COVER. OK FOR SERVICE.Jul 31, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017072305671Sign · detachedMID CENTER EXIT SIGN. BACKSIDE COVER HAS FALLEN OFF. INSTALLED THE COVER.Jul 22, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017051503868Cover · looseEMERGENCY EXIT SIGN COVER LOOSE, LOCATION 604. ADJUSTED EXIT SIGN, OK FOR SVC.May 12, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017050103483Lens · missingEMERGENCY EXIT SIGN LENS MISSING OVER R1 DOOR. INSTALLED A NEW LENS, OPS CHECKED GOOD.Apr 29, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017032402374Door · dentedAPU DOOR HAS DENTS INCURRENCE PER TOPP 40-60-05, PARAGRAPH XBZ THAT THIS CONDITION IS ACCEPTABLE FOR A SINGLE NON-REVENUE FERRY FLIGHT FROM SLC TO VQQ PROVIDED LEFT HAND APU DOOR IS CLOSED. REPLACED LEFT APU ACCESS DOOR IAW SRM 51-41-01 AND DRAWING 5915081 REVMar 23, 2017 · N966AT · Boeing 717200 · Auxiliary Power Unit (APU) DoorsSDR DALA2017032202280Frame · corrodedCORROSION TO THE LOWER FRAME TEE CAP AT BS 1095.87 NEAR LONGERON 28R. FOUND OUT OF LIMITS IAW SRM 53-00-00 AND DRAWING S4923323 REV -. REPAIRED AREA IAW ER/A 553860-14 REV. ORIGINAL.Mar 21, 2017 · N966AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016092706849Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Sep 26, 2016 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2016061604670Skin · crackedVERTICAL STABILIZER L/E HAS A 3" CRACK & FASTENERS PULLED INTO THE SKIN & ELONGATED HOLES BY LWR VOR ACCESS PANELS, REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS USING 7075-0 HEAT TREATED TO 7075-T6 2090. INSTALLED REPAIR PARTS IAW ER/A 545681-14AD REPETITIJun 14, 2016 · N966AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016061504668Longeron · corrodedLONGERON 30 AND SPLICE CORRODED FROM BS 927-946. BLENDED CORROSION ON L30 SPLICE AT BS 927 TO BS 946 ORIGINAL THICKNESS .250 REMAINING .245 FOUND TO BE WITHIN LIMITS IAW 53-00-00 AND 53-00-05, REPAIR 2, FIG 201, TAG 1768. BLENDED L30 BETWEEN BS 927 AND BS 94Jun 14, 2016 · N966AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016061504669Door Frame · corrodedR1 DOOR JAMB HAS CORROSION VISIBLE IN FWD AND AFT LOWER CORNER POCKETS OF JAMB AND IN LOWER POCKET OF AFT DOOR FRAME MARKED WITH ARROW. REMOVED CORROSION FROM LWR AND AFT LWER POCKETS AT R1 DOOR JAMB AREA AND LOWER POCKET OF AFT DOOR FRAME. INSTALLED REPLACEMJun 13, 2016 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016061404592Support · crackedLOWER FUSELAGE, UNDER WING BARREL KEELBEAM BS 606 CRACKED KEELBEAM SUPPORT, MARKED. REMOVED DAMAGED FORMER LT KEEL BS 606. REPAIRED FORMER IAW ER/A 545683-14MA. REINSTALLED FORMER IAW ER/A 545683-14MA, STEPS 1 THRU 10.Jun 13, 2016 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061404594Skin · crackedRIGHT FUSELAGE BS 1095 SKIN CRACKED FROM FASTENER HOLE APPROXIMATELY .75" JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE BS 1095 CRACKED SKIN FROM FASTENER HOLE JUST ABOVE LONGERON 14-R IAW ER/A 545684-14, REV. OR. ASSOCIATED ER/A 00Jun 10, 2016 · N966AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061404593Structure · crackedCRACK ON LT SIDE OF VERITCAL STABILIZER AT MATING SURFACE OF EMPENNAGE AT BS 116. REPAIRED CRACK ON LT SIDE OF VERTICAL STABILIZER AT MATING SURFACE OF EMPENNAGE BS 1116 IAW SRM 55-30-01, FIG 201, REPAIR 5.Jun 9, 2016 · N966AT · Boeing 717200 · Vertical StabilizerSDR DALA2016060904486Support · crackedRIGHT WING, KEEL BEAM, BS 680, CRACKED LONGERON SUPPORT INSIDE BOX. REPLACED CRACKED LONGERON SUPPORT ON RT WING KEEL BEAM BS-680 REPAIR DOUBLER ON FORMER IAW ER/A 545683-14MA-O, STEP 8. WORK COMPLETE ASSOCIATED ER/A 00-545683 ADDED FOR AC 9525.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060804422Stop Fitting · crackedBS 1053 VENTRAL DOOR LOWER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED. REPLACED DOOR STOP IAW SRM 51-41-02, PAR. 4.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060804421Stop Fitting · crackedBS 1053, VENTRAL DOOR UPPER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED, REPLACED DOOR STOP FITTING IAW SRM 51-41-02, PAR 4.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Main, Structure
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