N965AT

Service difficulty reports · 196

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 = 'N965AT' 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 DALA2023041102799Unknown · unknownFUSELAGE EDGE SKIN DAMAGE. LOWER FORWARD CORNER OF AFT CARGO DOOR CUT OUT. COMPLIED WITH PRI 607567-14-AD- REV 0 AND REV 1. (LP #2700709)Apr 2, 2023 · N965AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023040502673Unknown · unknownFOWARD L/H MOUNT FOR G-7 GALLEY CORRODED. FOUND AFTER GALLEY DISPLACEMENT. SUMMARY SEE NRC 089-0001:0591-2001/002 00355: REPLACED FWD L/H MOUNT AT G-7 GALLEY PER B717 AMM 25-31-70. (LP #2698677)Apr 1, 2023 · N965AT · Boeing 717200 · Fuselage Floor PanelSDR DALA202303094717DDisc · cracked1 AXIAL CRACK IN AIR SEAL F AREA (ABOVE DIA 15-2) MEASURING ~0.340 INCH 1 CIRCUMFERENTIAL CRACK IN AIR SEAL F AREA (BELOW DIA 15-2) MEASURING ~0.100 INCHMar 8, 2023 · N965AT · Boeing 717200 · Turbine SectionSDR DALA2022032802028Power Supply · inoperativeFOUND WING EMERGENCY EXIT DOOR LOWER LIGHTS INOPERATIVE. MAINTEANACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY AT ROW 22 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #8751621)Mar 26, 2022 · N965AT · Boeing 717200 · Emergency LightingSDR DALA2022031401643None · noneLIGHTNING STRIKE F.S. 60 BETWEEN 2ND AND 3RD FRAME FWD OF POWER RECEPTECLE L/H. REPAIRED REF B717 SRM 53-01-01-01A-2. (LP #2150411)Mar 9, 2022 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022031001554None · noneLIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150523)Mar 9, 2022 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022031001553None · noneLIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150535)Mar 9, 2022 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022031001552None · noneLIGHTNING STRIKE F.S. 149 ON SKIN BETWEEN S7R &S-8R. REPAIRED PER B717 SRM 53-01-01-1A-2. (LP #2150520)Mar 9, 2022 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021041302152Handle · malfunctionedSHIP 9524 - THE CREW RETURNED THE AIRCRAFT BACK TO ATL FOLLOWING THE "TAILCONE UNLOCK" INDICATION ILLUMINATING. CORRECTIVE ACTION: MAINTENANCE FOUND THE AFT INSIDE RELEASE HANDLE LOWER BALL OUT OF THE SWITCH. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PApr 12, 2021 · N965AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2021041302151Battery Pack · inoperativeBOTH THE LEFT AND RIGHT OVER-WING EMERGENCY EXIT LIGHT ARE INOPERATIVE. MAINTENANCE REPLACED THE OVER-WING EMERGENCY EXIT LIGHT BATTERY REF B717 AMM 33-51-06. (LP #1778268)Apr 10, 2021 · N965AT · Boeing 717200 · Emergency LightingSDR DALA2021041202109Stringer · corrodedAFT CARGO COMPARTMENT, STRINGER #30 CORRODED FROM STA 908 TO 974. NRC 057-0022:5310-2014/007 00211: MAINTENANCE REPLACED LONGERON 30 FROM STATION 906 TO 1012 PER DWG #5919707 AND INSTALLED REPAIR SPLICE AT STA 964 PER B717 SRM 53-20-05-2R PROCEDURE 1 REPAIR 1.Apr 10, 2021 · N965AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021040902103Retainer · missingTHE RETAINING CLIP IS MISSING FROM THE COVER OF THE TAIL SLIDE REF STEP 9A AND FIG 4 SHEET 13. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. NRC 000-0002:2561-9006/002 00310: MAINTENANCE REPLACED TApr 7, 2021 · N965AT · Boeing 717200 · Escape SlideSDR DALA2019011800336Battery Pack · dischargedTHE OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVER WING EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-54. OPERATIONAL CHECK WAS GOOD. (LP #4842898)Jan 18, 2019 · N965AT · Boeing 717200 · Emergency LightingSDR DALA2017052604310Skin · corrodedCORROSION SKIN BS 629, LONGERON 28L - 30L. REPAIRED IAW SRM 51-40-08, 51-44-02 PARA 4, AND 51-41-05 PARA 8.May 25, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052404207Seat Track · corrodedSEAT TRACK AT BS 587 TO 656, LBL 17 HAS CORROSION IN SCREW HOLES. MECHANICALLY BLENDED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52-1A, FIG 101. THE SEAT TRACK WAS REPLACED WITH NEW.May 23, 2017 · N965AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017052304107Cusp Web · crackedON REMOVAL OF THE FIRST OFFICER`S OTBD SEAT TRACK, FOUND A CRACKED CUSP WEB FROM ATTACH FASTENER HOLE. REPAIRED THE CUSP WEB IAW SRM 53-00-00-2R, EX B, AND 51-41-02.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017052304106Skin · crackedLEFT FUSELAGE SKIN CRACKED, BS 1022, LONGERON 14L. REPAIRED SKIN IAW ER/A 555612-14, REV O.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052304105Skin · crackedRIGHT FUSELAGE SKIN CRACKED, BS 1087, ABOVE LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557984-14, REV OR.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052304104Skin · crackedRIGHT FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 557983-14, REV OR.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052304103Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT BS 1037, LONGERON 14R. REPAIRED THE SKIN IAW ER/A 555611-14, REV OR.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052304102Door Frame · damagedFWD LOWER FUSELAGE, FWD CARGO DOOR FRAME, BS 408 TO 434.5, LONGERON 18R, UPPER SILL, LOWER CUSP WEB PANEL. REPAIRED IAW SRM 53-00-55-2R-4 .May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017052304101Frame · corrodedCORROSION AT BS 974 FRAME FWD SIDE LONGERON 29L - 29R. PERFORMED FRAME REPAIR IAW SRM 53-20-07-2R-2.May 22, 2017 · N965AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017051303864Cusp Web · corrodedRT STA 389 UNDERSIDE OF CUSP WEB HAS CORROSION. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREAT, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-00-55-2R-4, AND AMM 51-10-00-370-803.May 11, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051303863Cusp Web · corrodedRT STA 434 CUSP WEB HAS CORROSION ON TOP AND BOTTOM. REPAIRED DAMAGED CUSP WEB IAW SRM 53-00-55-2R-4. TREATED, PRIMED, TOPCOATED, AND INSTALLED REPAIR DOUBLERS IAW SRM 51-41-05, 53-055-2R-4, AND AMM 51-10-00 370-803.May 11, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051303862Cusp Web · corrodedTHE RT CUSP WEB AT STA 737-756, RBL 55 HAS CORROSION AROUND THE UNDERSIDE OF LIGHTENING HOLE(S). BLENDED CUSP WEB AT STA 737-756 ORIGINAL THICKNESS .040 REMAINING THICKNESS .028. FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW SRM 53-00-55 REPAIR 4.May 11, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051103808Floor Support · corrodedAFT WET AREA STA 1022-1053, LBL 46 FLOOR SUPPORT HAS CORROSION IN MULTIPLE AREAS INCLUDING OUTBD FLANGE. REMOVED CORROSION BY BLENDING ON FLOOR SUPPORT AT LBL46 STA 1041 .025" MATERIAL REMOVED .055" REMAINING .080" ORIGINAL THICKNESS OUT OF LIMITS IAW SRM 53-0May 10, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051103807Seat Track · corrodedRIGHT INBOARD SEAT TRACK RBL 22, BS 200 - 256, HAS AREAS OF CORROSION. BLENDED THE SEAT TRACK, AND FOUND AREAS OUT OF LIMITS. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-20-52-2R.May 10, 2017 · N965AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017051103806Longeron Splice · corrodedCORROSION AT BS 891 - 906, LONGERON 30 SPLICE FITTING. REMOVED AND REPLACED THE DAMAGED LONGERON SPLICE IAW SRM 51-41-01, 51-41-05, AND DRAWING 5924878.May 10, 2017 · N965AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017051103761Bulkhead · gougedAFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR INTERNAL STRUCTURE IS GOUGED IN SEVERAL AREAS AT LOWER RT SECTION WHERE FLIGHT ATTNANTS SEAT IS MOUNTED. REPAIRED IAW SRM 52-10-02-2R, OPTION 2.May 10, 2017 · N965AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2017051103760Cusp Web · corrodedCORROSION ON TOP AND BOTTOM SIDE OF LEFT CUSP WEB BETWEEN BS 737-756, LBL 60. REPAIRED THE CUSP WEB IAW SRM 53-00-55-4R-2, REPAIR 4.May 10, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051103759Longeron · corrodedCORROSION AT BS 954 - 908, L30. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS AT STA 931. REPAIR THE AREA. TREATED, PRIMED, TOP COATED, INSTALLED FASTENERS, IAW SRM 51-41-02, 53-00-00, FIG 103, 53-00-05-2R-3, AND AMM 51-10-00-370-803.May 10, 2017 · N965AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017051103758Cusp Web · crackedCRACKS AROUND RIVET HEADS ON LT SIDE CUSP WEB BS 716, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R4, REPAIR 4.May 10, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051203810Frame · crackedFWD LT STA 1022 FRAME FORMER CRACKED BETWEEN LONGERON 5L-6L. REPAIRED FWD LT STA 1022 FRAME FORMER BETWEEN 5L-6L IAW SRM 53-00-06-2R REPAIR 3.May 9, 2017 · N965AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017051203861Cusp Web · corrodedCUSP WEB LT AT STA 427-446 CORRODED. REPAIRED LT CUSP WEB AT STA 427-446 IAW SRM 53-00-55-2R-4. BLENDED CORROSION ON WEB. NOMINAL .020 REMOVED .005 REMAINING .015. OUT OF LIMITS IAW SRM 53-00-55-1A-1.May 8, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017051103762Seat Track · corrodedCORROSION ON THE F/O'S OTBD SEAT TRACK. CORROSION ON SEAT TRACK FOUND TO BE BEYOND DWG TOLERANCE OF .015 WITH 50% MATERIAL LOSS IAW BOEING DWG 5971207. REPLACED THE SEAT TRACK IAW AMM 53-22-01.May 8, 2017 · N965AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017051203812Seat Track · gougedRT I/B SEAT TRACK GOUGED STA 890. GOUGED AREA ON SEAT TRACK WAS OUT OF LIMITS ORIG 0.115" REMAINING 0.090" IAW SRM 53-20-52-1A. REPLACED RT IB SEAT TRACK FROM STA 822 TO 897 IAW SRM 53-20-52-2R-5 FIG 201.May 5, 2017 · N965AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017050903725Cargo Track · corrodedCORROSION BS 995 - 1022, RT CARGO TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, FIG 103. REPLACED THE CARGO TRACK IAW SRM 51-41-01.May 5, 2017 · N965AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017051503894Skin · crackedFWD CARGO DOOR SKIN CRACKED AT FWD LWR CORNER UNDER DOOR LATCH HOOK. FWD CARGO DOOR FOUND TO BE OUT OF LIMITS. REMOVED UNSERVICEABLE. SERVICEABLE DOOR TO BE INSTALLED ON JOB CARD 5231-4003.May 4, 2017 · N965AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017050403548Cusp Web · corrodedCUSP WEB AT BS 446 - 465 CORRODED. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R, REPAIR 4, FIGURE 205.May 3, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017050403547Cusp Web · corrodedTHE RT CUSP WEB AT BS 532, RBL 55 HAS CORROSION AROUND THE UNDERSIDE OF LIGHTENING HOLES. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.May 3, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017050403546Cusp Web · corrodedLEFT CABIN FLOOR CUSP WEB IS CORRODED AROUND SEVERAL FASTENERS FROM BS 408 - 465. COMPLETED A CUSP WEB REPAIR IAW SRM 53-00-55-2R-4, REPAIR 4, FIGURE 204.May 3, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017050403549Skin · damagedLOWER LEFT EDGE OF RUDDER IS DAMAGED. REMOVED DAMAGED SECTION OF THE RUDDER SKIN. FABRICATED & INSTALLED A REPAIR DOUBLER & FILLER IAW SRM 51-70-13-2R-2.May 2, 2017 · N965AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2017051203811Cusp Web · corrodedLT CABIN FLOOR CUSP WEB IS CORRODED AROUND SEVERAL FASTENERS FROM STATION 541 TO 617. BLENDED AREAS LT CABIN FLOOR CUSP THAT WAS CORRODED BETWEEN STA 541-617, ALL AREAS WERE FOUND TO BE WITHIN ALLOWABLE LIMITS; EXCEPT STA 580. TREATED, PRIMED ALL AFFECTED AREAApr 30, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042903476Angle · crackedFORWARD CARGO BS 636, BL 0 AFT SIDE OF INTERCOSTAL ANGLE IS CRACKED IN CEILING. REPAIRED THE ANGLE IAW SRM 51-70-11-2R-1. CRACK FOUND TO BE 2 INCHES IN LENGTH.Apr 28, 2017 · N965AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110708319Doubler · damaged2 EA 3/16TH DOUBLER ATTACHMENT FASTENER HOLES DAMAGED. COMPLIED WITH PRI 552498-14 REV 0 IAW ER/A 552498-14 REV ORG.Nov 7, 2016 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA20160720152Skin · delaminatedDURING NON ROUTINE LINE CHECK, R/H I/B SPOILER FOUND DELAMINATED.Jul 20, 2016 · N965AT · Boeing 717200 · SpoilersSDR DALA2015123007778Battery Pack · inoperativeMAINTENACE FOUND THE MID CABIN OVERHEAD EMERGENCY EXIT SIGNS INOPERATIVE. THE BP120 BATTERY PACK WAS REPLACED. THE EMERGENCY EXIT SIGNS CHECKED OK.Dec 30, 2015 · N965AT · Boeing 717200 · Emergency LightingSDR DALA2015102306368Battery Pack · inoperativeDURING SERVICE CHECK, CEILING EMERGENCY LIGHTS ROW 22-29 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES AND CHECKS OK.Oct 23, 2015 · N965AT · Boeing 717200 · Emergency LightingSDR DALA2015090305401Control Unit · faultedON T/O THE ACFT ROLLED LEFT BUT WAS CONTROLLABLE. AT 2,000FT ACFT NORMAL WITH RIGHT STEERING , BUT TO THE LEFT WAS VERY STIFF, LIKE SOMETHING WAS BINDING. RETURNED TO DEPARTURE. COMPLIED WITH FIM 27-10-00-810-803. AILERON RTS CHECKS GOOD ON BOTH FCCS. LUBRICASep 2, 2015 · N965AT · Boeing 717200 · Aileron Tab Control SystemSDR SWAA2015052740068Light · inoperativeAFT LT OVERWING DOOR EMER LIGHT BULB INOPERATIVE. R & R LIGHT IAW AMM.May 26, 2015 · N965AT · Boeing 717200 · Emergency Lighting
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