N980AT

Service difficulty reports · 245

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 = 'N980AT' 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 DALA2018040504206Door · damagedLEFT NR 1 SLAT OUTBOARD TRACK DOOR DAMAGED. REMOVED DOOR AND FORWARD TO CDL 57-47-01. MCC NOTIFIED. MCC PLACARD INSTALLED. EA 5929781-2.Apr 4, 2018 · N980AT · Boeing 717200 · Leading Edge DevicesSDR DALA2017111308077Battery Pack · inoperativeFOUND AFT EXIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 24-34. OPS CHECKED GOOD.Nov 11, 2017 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2017101507527Light · malfunctionedEXIT LIGHT OVER AFTL EXIT, FLICKERED SEVERAL TIMES IN-FLIGHT THEN REMAINED ON. ALL OTHER CABIN EMERGENCY LIGHTS REMAINED OFF. F/A TRIED RESET, BUT WAS UNSUCCESSFUL. COULD NOT DUPLICATE, INSPECTED AND TESTED EMERGENCY LIGHTS IAW AMM 33-51, NO DEFECTS NOTED Oct 14, 2017 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2017080406015Battery Pack · inoperativeEXTERIOR EMERGENCY ILLUMINATION SYSTEM MALFUNCTIONED. ON ARRIVAL FOUND OVERWING EMERGENCY LIGHTS ON. REPLACED BATTERY PACK AND POWER SUPPLY, B5-125, IAW AMM 33-51-06. EMERGENCY LIGHT SYS OPS NORMAL.Aug 3, 2017 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2017071205364Spar · crackedDURING REMOVAL OF OUTBD FLIGHT SPOILER LOCKED TOOL ONE CRACK WAS MADE TO RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355. RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355 WAS REPAIRED PER ETI -17-17-097 REV 2 AND ER/A 559526-14 REV ORIG.Jul 11, 2017 · N980AT · Boeing 717200 · Wing SparSDR DALA2017071005294Bellcrank · wornWEAR ON BELLCRANK AT THE RT SLAT DRIVE MECHANISM. THE BELLCRANK WAS REPAIRED IAW ETI-17-17-075, REV 1, AND ER/A 559492-14, REV ORIG.Jul 9, 2017 · N980AT · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2017071005293Fitting · corrodedCORROSION ON FWD STAIRWAY DOOR MECHANISM FITTING. THE DAMAGED FITTING WAS REPLACED IAW AMM 20-50-01-201.Jul 9, 2017 · N980AT · Boeing 717200 · Entrance StairsSDR DALA2017071005291Skin · corrodedCORROSION ON RT WING UPPER SKIN XRS 375. ONE INCH FROM FRONT SPAR. THE SKIN WAS REPAIRED IAW ETI-17-17-094, REV 1, AND ER/A 559516-14, REV ORIG.Jul 9, 2017 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017070905289Cargo Track · corrodedCORROSION OUT OF LIMITS ON THE RT CARGO TRACK BETWEEN BS 892 & 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51-01-7, AND 51-41-01.Jul 8, 2017 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017070905287Cargo Track · corrodedCORROSION OUT OF LIMITS ON THE LT CARGO TRACK BETWEEN BS 813 - 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51-01-7, AND 51-41-01.Jul 8, 2017 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017070705278Frame · corrodedCORROSION ON FRAME ANGLE BS 927 BETWEEN LONGERONS 29L AND 29R. REPAIRED IAW SRM 53-00-06-2R, FIG 201, AND 53-20-07-01.Jul 6, 2017 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017070705277Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 620MB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01-2R, PROCEDURE 2, REPAIR 2, FIGURE 201, SHEET 1.Jul 6, 2017 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017070705276Skin · corrodedCORROSION ON WING BOX UPPER SKIN BETWEEN BS 737 - 751 RBL 22 - 60. REPAIRED IAW ETI-17-17-079, REV 1 AND ER/A 559498-14, REV ORIGINAL.Jul 6, 2017 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017070705275Panel · out of limitsSEVERAL COUNTERSINK OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV) WAS REPAIRED IAW DRAWING SG95550001, REV ORIGINAL, AND JIC CARD 5530-01048-03.Jul 6, 2017 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017070605216Floor Panel · crackedCRACK FLOOR PANEL 121NF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R.Jul 5, 2017 · N980AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017070405178Panel · corrodedSEVERAL COUNTERSINKS OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER. REPAIRED IAW SERVICE GENERAL REPAIR DRAWING SG 95550001 REV ORIGINAL.Jul 3, 2017 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017070305154Access Panel · corrodedCORROSION ON SETTLEMENT AREA AT FUEL ACCESS PANEL. THE FUEL ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.Jul 2, 2017 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017070305153Access Panel · corrodedCORROSION ON COUNTERSINK HOLES ON FUEL ACCESS PANEL. REPLACED THE ACCESS PANEL IAW SRM 57-10-01, PAR 5, CONDITION II.Jul 2, 2017 · N980AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017070205114Skin · damagedLOOSE FASTENERS ON LT/RT SIDE AT VERTICAL STABILIZER LEADING EDGE STRUCTURE (REPAIR DOUBLER) AND REMOVABLE LEADING EDGE, STA ZFS=52.267. SEVERAL COUNTERSINK ON REMOVABLE LEADING EDGE STRUCTURE WERE MEASURED ABOVE 0.540" WERE LIMIT IS 0.517" AND ABOVE 0.420" WEJul 1, 2017 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017063005080Skin · crackedCRACK ON FUSELAGE SKIN Y=1087 BTW LONG 13L-14L. FUSELAGE SKIN WAS REPAIRED PER ETI -17-17-072 REV 2 AND ER/A 558145-14 REV ORIG.Jun 29, 2017 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017063005078Attach Angle · corrodedCORROSION ON ANGLE THAT ATTACH FUSELAGE TO CUSP ANGLE BTW LONGS 18L-19L, BTW STA Y=889-908. ANGLE WAS REPLACED PER SRM 53-20-51-01 AND DWG 9910151 ITEM -117. MEASURED (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2. THE ORIGINAL THICKNESS Jun 29, 2017 · N980AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017062905043Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE UPPER LWR SURFACE BTW X=-54 TO X=-60 AND STAY=552 TO STAY=553 AT CAB PAX RT SIDE. DAMAGE WAS REMOVED PER SRM 53-00-55-2R REPAIR 4. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS WERE FOUND PER NDTSPM PART 6, 06-10-01.0Jun 28, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062805021Skin · crackedCRACK ON EXTERNAL SKIN, BS 1087 BETWEEN LONGERONS 13 AND 14R. THE SKIN WAS REPAIRED IAW ETI -17-17-074, REV ORIGINAL AND ER/A 558173-14, REV ORIGINAL,Jun 27, 2017 · N980AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017062805019Skin · damagedPROTUBERANCE ON LOWER SKIN FOR THE RT WING AFT FLAP MOVEABLE VANE. THE SKIN WAS REPAIRED IAW SRM 57-53-01.Jun 27, 2017 · N980AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017062704996Beam · crackedCRACK ON FWD LOWER CORNER RETAINER AT THE FWD RT SERVICE DOOR. THE NR 4 BEAM WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.Jun 26, 2017 · N980AT · Boeing 717200 · Service DoorsSDR DALA2017062604956Former · crackedCRACK ON FORMER BS 694, RBL 34. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R, 51-70-11, 51-41-02-0G, AND 51-41-05-0G.Jun 26, 2017 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017062605017Floor Support · corrodedCORROSION AND CRACKED FLOOR PANEL 221AG. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9957828, REV Y.Jun 25, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062604994Cusp Web · corrodedCORROSION ON CUSP WEB UPPER & LOWER SURFACES BETWEEN RBL 54 TO 60, BS 622 TO 624 AND BS 629 TO 630. THE DAMAGE WAS REMOVED IAW SRM 53-00-55-2R, FIG 216. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE DAMAGED WAS REMOVED IAW NDT SPM 06-10Jun 25, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062604954Channel · crackedCRACKS ON CHANNEL OF PAX CABIN FLOOR PANEL 222ADF. THE CHANNEL WAS REPLACED IAW SRM 51-41-01-0G.Jun 25, 2017 · N980AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017062504946Tee Fitting · crackedCRACKED TEE FITTING ON THE AFT LOWER STOP OF THE FWD CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND DRAWING 3926046, REV. B.Jun 24, 2017 · N980AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017062504945Membrane · corrodedCORROSION ON MEMBRANE BS 200 BETWEEN LONGERONS 17 &18L. THE MEMBRANE WAS REPAIRED IAW SRM 51-70-10-2R, FIG 201.Jun 24, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404944Cusp Web · corrodedCORROSION ON CUSP WEB BETWEEN RBL 54 TO 60 OUT OF LIMITS AT BS 655 - 663. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404943Cusp Web · corrodedCORROSION ON LT CUSP WEB BETWEEN BS 602 - 603, LBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG. 216.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404942Cusp Web · corrodedCORROSION ON CUSP WEB RBL 54 TO 60, BS 487 TO 490. THE DAMAGE WAS REMOVED IAW SRM 53-00-55 2R, REPAIR 4, FIG 215. HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVED AND NO CRACK INDICATIONS WERE FOUND IAW NDT SPM 06-10-01.001. THE REPAIR WAS FABRICATED IAJun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404941Beam · crackedCRACK ON BELOW DOOR STOP PAN AFT EDGE BEAM 3 OF FWD CARGO DOORWAY. REPAIRED IAW SRM 52-30-02, REPAIR 3.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017062304895Seat Track · corrodedCORROSION ON SEAT TRACK X=-44.5 STA Y=429-430 AT CAB PAX. SEAT TRACK X=-44.5 STA Y=429-430 AT CAB PAX WAS REPAIR PER SRM 53-20-52-2R REPAIR 1.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017062304894Retaining Clip · wornWORN ON LOWER LT DOUBLER RETAINER CLIP AT AFT CABIN BULKHEAD DOOR (DOORS). LT LOWER DOUBLER RETAINER CLIP WAS REPLACED PER SRM 51-41-01 AND 51-41-02.Jun 22, 2017 · N980AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017062304893Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y=544 TO Y=555 X54 TO X60 AT PAX CABIN IN REF NRC 195. DAMAGE WAS REMOVED PER SRM 53-00-55-2R-4 FIG 216 HFEC INSPECTION WAS ACCOMPLISHED ON CUSP WEB BTW STA Y=544 TO Y=555 X54 TO X60 AT PAX CABIN NO CRACKS WERE FOUND AFTER DAMAGE Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304891Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=148 TO Y=168 AND X=-6 AT COCKPIT. FLOOR SUPPORT BTW STA Y=148 TO Y=168 AND X=-6 AT COCKPIT WAS REPLACED PER SRM 51-40-08-0G AND 51-41-01.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304890Cusp Web · corrodedCORROSION ON LT CUSP WEB STA Y-855 BTW X54 TO X60 AT PAX CABIN IN REF NRC 198. REPAIR PART WAS FABRICATED AND INSTALLED PER SRM 53-00-55-2R FIG 215 AND 51-41-02. CIC WAS APPLIED PER SRM 51-10-04 PAR 37.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062204885Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 200 BETWEEN RBL 54 TO 44 IN THE PAX CABIN. THE FLOORBEAM WAS REPLACED SRM 51-41-02, 51-10-4, PAR 26, AND 51-40-08.Jun 21, 2017 · N980AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017062004838Pan · crackedCRACKED RING PAN ON STA Y=832 AND Y=870 AFT UPPER CORNER ALSO ON STA Y=579 LOWER FWD CORNER AT PAX CABIN LT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.Jun 19, 2017 · N980AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017062004835Pan · crackedCRACKED RING PAN ON STA Y=908 AFT LOWER CORNER AT PAX CABIN RT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.Jun 19, 2017 · N980AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017061904803Floorbeam · corrodedCORROSION ON FLOORBEAM BS 200 LBL 6 TO RBL 6. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02.Jun 18, 2017 · N980AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017041002851Power Supply · no testDURING CHECK, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED GOOD.Apr 10, 2017 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2016101207173Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.Oct 11, 2016 · N980AT · Boeing 717200 · Emergency LightingSDR SWAA2015071341860Charger · inoperativeCEILING EMER LIGHTS INOPERATIVE. R & R CHARGER IAW AMM.Jul 10, 2015 · N980AT · Boeing 717200 · Emergency LightingSDR SWAA2015071341859Charger · inoperativeRIGHT AFT UPPER OVERWING EMER EXIT SIGN INOPERATIVE. R & R CHARGER ASSEMBLY IAW AMM.Jul 10, 2015 · N980AT · Boeing 717200 · Emergency LightingSDR SWAA2015070141278Membrane · corrodedWEB MEMBRANE CORRODED BETWEEN BS 200 TO 218, BETWEEN RBL 35 TO RBL 56. R & R WEB IAW SRM & DWG.Jun 16, 2015 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2015070941603Lens · crackedOVERHEAD CEILING EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.Jun 9, 2015 · N980AT · Boeing 717200 · Emergency Lighting
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