N943AT

Service difficulty reports · 213

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 = 'N943AT' 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 DALA2019070103953Door Frame · crackedBENT ON AFT COMPARMENT CARGO DOOR JAMB STA 992 BTW L25R TO L24R (FUS). NRC 00089: A CRACK OF 0.500" IN LENGTH, WAS FOUND AFTER FORMING. CRACK ON AFT COMPARMENT CARGO DOOR JAMB STA 992 BTW L25R TO L24R WAS REPAIRED PER SRM 53-20-15-2R-4 PAR. 4. (LP #1148784)Jun 30, 2019 · N943AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062903948Vane · wornWEAR ON TRAILING EDGE OF AFT MOVABLE FLAP VANE AT LT WING. NRC 00241: TRAILING EDGE TIP OF AFT MOVABLE FLAP VANE AT LT WING WAS REPLACED PER DWG. #5910040 REV. BN AND SRM 51-41-02. (LP #1146810)Jun 29, 2019 · N943AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019062903947Frame · crackedCRACKED ON CUT OUT FRAME AT STA 47 X=11, X=-11 LH NOSE LANDING GEAR. NRC 00159: AREA WAS REPAIRED PER SRM 53-10-14-2R-2 FIG 201. (LP #1146437)Jun 29, 2019 · N943AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062903946Frame · crackedCRACKED ON CUT OUT FRAME AT STA 47 X=11, X=-11 RH NOSE LANDING GEAR. NRC 00161: AREA WAS REPAIRED PER SRM 53- 10-14-2R-2 FIG 201. (LP #1146419)Jun 29, 2019 · N943AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019062903945Longeron Splice · corrodedCORROCION SPLICES (4 EA) ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARMENT (REF NRC SN 146)(C2). NRC 00497: CORROSION LEVEL 2, CORROSION ON SPLICES (4EAS) ON LONGERON L30 FROM STA 889 TO STA 1053 AT AFT CARGO COMPARMENT WERE REMOVED PER SRM 51-1Jun 28, 2019 · N943AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019062903943Finger Doubler · corrodedCORROSION ON INTERNAL FINGER DOUBLER BTW STA Y=927 TO Y=954 AND LONG 30 TO 29L AT AFT CARGO COMPARTMENT. (C2). NRC 00497: CORROSION LEVEL 2, INTERNAL FINGER DOUBLER BTW STA Y=927 TO Y=954 AND LONG 30 TO 29L AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-41-0Jun 28, 2019 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062903940Cusp Web · corrodedCORROSION ON CUSP MEMBRANE (WEB) FROM Y= 965 TO Y=986 RT SIDE (PAX CAB). NRC 00510: CORROSION LEVEL 2, CORROSION WAS REMOVED ON STA Y=979 TO Y=981 PER SRM 51-10-04-0G PAR 26, A10X MAGNIFIED INSPECTION WAS PERFORMED AND A CRACK OF 0.380" LENGTH WAS FOUND AND REJun 28, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062703885Floor Panel · debondedDISBONDED FLOOR PANEL #211ANF COCKPIT (CPIL). NRC 00401: FLOOR PANEL #211ANF WAS REPLACED AND IDENTIFIED BY A FABRICATED PANEL PER B-717-200 SRM 53-20-50-2R-3. (LP #1143068)Jun 26, 2019 · N943AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019062703882Access Panel · corrodedCORROSION IN ACCESS 620CT SETTLEMENT AREA AND COUNTERSINK HOLES. AT FUEL TANK (AD). NRC 00502: CORROSION LEVEL 2, THE UPPER WING ACCESS DOOR 620CT WAS REPLACED PER B717-200 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION 3. (LP #1142552)Jun 26, 2019 · N943AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019062703879Floor Panel · puncturedPUNCTURE AT PAX CABIN FLOOR PANEL #223EF. (CPAX). NRC 00488: PUNCTURE IN FLOOR PANEL #223EF WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #1142188)Jun 26, 2019 · N943AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019062603861Cusp Web · crackedCRACKED CUSP WEB BS 560 - 579 RT SIDE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G PAR 8.Jun 25, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062503827Cusp Web · crackedCRACK ON CUSP MEMBRANE (WEB) AT Y=813 RH SIDE. AREA WAS CLEANED PER PS 900-1-2-1NO. GVI WAS PERFORMED AND NO CORROSION WAS FOUND PER B717-200 AMM 05-21-02-210-802. CRACK WAS REPAIRED PER B717-200 SRM 53-00-00-2R AND 51-41-02-0G.Jun 24, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062543824Cusp Web · corrodedCORROSION ON REPAIR OF CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE (PAX CAB). NRC 00308: CORROSION LEVEL 2, MAINTENANCE FOUND CORROSION ON THE EXISITING REPAIR OF THE CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE: SO THIS REPAIR WAS REPLACED PER B717-200Jun 23, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062543823Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=20 AT CABIN PAX. (CPAX). NRC 00351: CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. MINIMUM REMAINING THICKNESS IS 0.028 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-Jun 23, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062543822Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=-20 AT CABIN PAX. CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. REMAINING THICKNESS IS ONLY 0.025 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGJun 23, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062433798Beam · crackedCRACKED BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE (L1) (PTAS). NRC 00080: BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE WERE REPAIRED PER B717-200 SRM 52-10-02-2R-13, 52-10-02-2R-8, AND 52-10-02-2R-7.Jun 22, 2019 · N943AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019062423777Channel · crackedCRACKED CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE. (L1) (PTAS). CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE WAS REPAIRED IAW SRM 52-10-02- 2R REPAIR 3.Jun 21, 2019 · N943AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019070304026Housing · corrodedCORROSION ON RUDDER YOKE BEARING SUPPORT HOUSING (AMDS 2720-2004). NRC 00379: CORROSION LEVEL 2, BEARING SUPPORT HOUSING WAS REPLACED PER SRM 51-41-02-0G AND 51-41-01- 0G. (LP #1132426)Jun 20, 2019 · N943AT · Boeing 717200 · Rudder Miscellaneous StructureSDR DALA2019062003669Floor Panel · debondedDEBONDED FLOOR PANEL #221LF PAX CABIN (CPAX). NRC 00403: FLOOR PANEL #221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1131537)Jun 19, 2019 · N943AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019061803621Frame · crackedCRACK ON RH WINDOW RING PAN STA Y=889 AT PAX CABIN. NRC 00197: CRACK ON RH WINDOW RING PAN STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.Jun 17, 2019 · N943AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703616Web · crackedCRACK ON WEB FROM STA 161 BTW X=-42 TO X=-44 (FUS). NRC 0366: WEB FROM STA 161 BTW X=-42 TO X=-44 WAS REPAIRED PER B717 SRM 53-00-00-2R-1 FIG. 201. (LP #1126059)Jun 16, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019F00147Spoiler · debondedLARGE DISBOND.Mar 8, 2019 · N943AT · Boeing 717200 · SpoilersSDR DALA2019022761256Battery · inoperativeB5-235 BATTERY WILL NOT ILLUMINATE THE EXIT SIGN OVER FWD FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACED THE BATTERY ASSEMBLY. CHECK WAS NORMAL REF B717 AMM 33-51. (LP #5513762)Feb 26, 2019 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2018121007116Battery Pack · inoperativeON THE SERVICE CHECK, MAINTENANCE FOUND THAT THE AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE DETERMINED THAT THE EMERGENCY LIGHT BATTERY PACK, B5-230, WAS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE OPERATIONAL CHECK WAS GOOD REF B717 AMDec 10, 2018 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2018061854044Power Supply · inoperativeDURING A SERVICE CHECK, FOUND THE LOWER WING EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE DISCOVERED A BAD POWER SUPPLY B5-119 AND REPLACED IT. OPS CHECKED GOOD IAW AMM 33-51-03, AND WDM 33-51-12.Jun 15, 2018 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2018032001814Seat Track · corrodedSEAT TRACK CORRODED. SPLICED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-20-52-2R, PRO 5.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031501735Attach Fitting · corrodedTHE FWD GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE FITTING DWG 3936190.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2018031501734Attach Fitting · corrodedTHE AFT GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE IAW DWG 3936190.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017090406574Lamp · inoperativeSEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE ON AFT CATWALK. MAINTENANCE REPLACED THE LAMPS IAW AMM 33-52. OPS CHECKED GOOD.Sep 3, 2017 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2017071405422Antenna · erodedL/E OF FWD TCAS ANTENNA ERODED. REPLACED THE TCAS ANTENNA IAW AMM 34-46-03.Jul 13, 2017 · N943AT · Boeing 717200 · Independent Position Determining SystemSDR DALA2017071205363Skin · crackedSKIN CRACK AT FASTENER AT STA 1095, 4" ABOVE L14R ABOVE RT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.Jul 11, 2017 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017071205362Fastener · looseFOUND NUMEROUS LOOSE FASTENERS ON VERTICAL STABILIZER REMOVABLE LEADING EDGE AT STA ZFS 52. REPAIRED REF PRI 560042-14 REV 0 AND ER/A 560042-14 REV A.Jul 11, 2017 · N943AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017071205361Skin · cracked2 SKIN CRACKS AT FASTENERS AT STA 1095, 4" ABOVE L14R ABOVE LT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.Jul 11, 2017 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017071205360Fastener · looseVERTICAL STAB LEADING EDGE LOWER FASTENERS ARE LOOSE AT STA ZFS 52. COMPLIED WITH PRI 560026-14 REV 0 AND REV 1. REPAIRED REF ER/A 560026-14 REV ORIG.Jul 11, 2017 · N943AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017071005331Door Sill · corrodedCORROSION ALONG THRESHOLD SILL FROM STA 370 TO 427. REPAIRED PER SRM 53-20-15-2R PROCEDURE 6.Jul 8, 2017 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017041903181Skin · damagedSKIN WRINKLED BETWEEN BS 813 AND 899 LT SIDE ABOVE WING AND BELOW WINDOW.Apr 18, 2017 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017041903180Skin · damagedSKIN DAMAGED BS 813 - 898. LONGERON 15 - 18L. REMOVED, FABRICATED, AND REPLACED THE SKIN PANEL IAW ER/A 557708-14, AND SRM 51-41-02 / 51-41-05.Apr 18, 2017 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016103107952Battery Pack · inoperativeTHE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS DAMAGED. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.Oct 30, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016100607104Battery Pack · inoperativeDURING LINE CHECK, THE PILOT FOUND HE COULD NOT CONTROL THE EMERGENCY LIGHTS IN THE CABIN AT THE L1 DOOR. IT WOULD REACT WHEN CONTROLLING CABIN LIGHTING. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.Oct 5, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016100607103Power Supply · failedDURING LINE CHECK, THE PILOT FOUND HE COULD NOT CONTROL THE EMERGENCY LIGHTS IN THE CABIN AT THE L1 DOOR, IT WOULD REACT WHEN CONTROLLING CABIN LIGHTING. MAINTENANCE REPLACED THE POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.Oct 5, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016061004508Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jun 9, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016051603931Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.May 13, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016042103127Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Apr 19, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016022501398Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES AND AT THE AFT CABIN DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Feb 25, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2018011000175Skin · damagedSKIN DAMAGED AT BS 210, STRINGER 25R. REPAIRED THE SKIN IAW PRI 544069-14, REV 0, 1, & 2.Feb 17, 2016 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019071104152Skin · dentedDENT INSPECTION RT AILERON CONTROL TAB, LOWER SKIN - QTY 3, 1) 6" FROM I/B, 5.5" FROM T/E, 2) 7" FROM I/B, 5" FROM T/E, 3) APPROX 8" FROM I/B, 4" FROM T/E. AREA TO DENTS ON RT AILERON CONTROL TAB LOWER SKIN WERE REPAIRED PER SRM 51-70-02-2R PROCEDURE 6 REPAIR Sep 2, 2015 · N943AT · Boeing 717200 · AileronsSDR SWAA2015090143408Mount Bracket · crackedOVERHEAD EMER EXIT LIGHT MOUNT BRACKET CRACKED AT ROW 1. R & R LIGHT IAW AMM.Aug 29, 2015 · N943AT · Boeing 717200 · Emergency LightingSDR SWAA2015083143335Cover · looseR2 DOOR EMER EXIT SIGN COVER LOOSE. R & R COVER IAW AMM.Aug 29, 2015 · N943AT · Boeing 717200 · Emergency LightingSDR SWAA2015083143334Light · inoperativeAFT OTBD EMER LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.Aug 29, 2015 · N943AT · Boeing 717200 · Emergency LightingSDR SWAA2015082643215Battery · dischargedR1 LOWER EMER EXIT IDENTIFIERS INOPERATIVE. R & R BATTERY IAW AMM.Aug 25, 2015 · N943AT · Boeing 717200 · Emergency Lighting
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