N926AT

Service difficulty reports · 180

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 = 'N926AT' 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 DALA2017081606258Cover · looseEMERGENCY EXIT SIGN COVER LOOSE. SECURED THE SIGN, CHECKED OK.Aug 15, 2017 · N926AT · Boeing 717200 · Emergency LightingSDR DALA2017050103484Lens · missingR1 DOOR EXIT LIGHT LENS MISSING. REINSTALLED THE LENS.Apr 30, 2017 · N926AT · Boeing 717200 · Emergency LightingSDR DALA2016050403609Skin · damagedDURING RUDDER INSTALL LOWER LT SKIN WAS CRACKED AND BENT. LOWER LT SKIN WAS REPAIRED IAW SRM 51-70-13, REPAIR 1.May 3, 2016 · N926AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2016050303561Skin · corrodedCORROSION ON UPPER WING SKIN AFT EDGE FROM BS XCW=16 TO XCW=50 AT RT MLG WHEEL WELL. DAMAGE WAS REPAIRED IAW ER/A 545128-14, REV ORIGINAL, AND ETI 17-16-013, REV 2. RII COMPLETED.May 2, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050303560Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. FUEL ACCESS DOOR REPLACED IAW IPC 57-23-01.May 2, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050303559Web · puncturedPUNCTURE AT FLOOR WEB, UNDER FLOOR PANEL. WEB WAS REPAIRED IAW 53-00-00, FIG 102.May 2, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016050303558Access Panel · corrodedCORROSION OUT OF LIMITS IN COUNTERSINK, 3 HOLES NON ADJACENT AT FUEL ACCESS DOOR 620JB. FUEL ACCESS DOOR WAS REPAIRED IAW SRM 57-10-01, CONDITION II.May 2, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050303557Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620AT. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.May 2, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050303556Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 520CB. FUEL ACCESS DOOR WAS REPAIRED IAW AMM 51-10-01, CONDITION II.May 2, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050203473Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620DT. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 620DT WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 4 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPAIRED IAW SRM 51-10-01 AND TREAMay 1, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016050203472Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 620MB. CORROSION WAS REMOVED. COUNTERSINK WERE MEASURED AND WERE FOUND 3 COUNTERSINK OUT OF LIMITS IAW SRM 57-10-01. ACCESS WAS REPAIRED IAW SRM 51-10-01 AND TREATED IAW SRM 51-10-04.May 1, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016103107955Cargo Track · corrodedCORROSION ON CARGO TRACK FROM BS 994 - 1022, BETWEEN LONGERONS 27 TO 28R. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-40-08, AND 51-10-04 PAR 15 AND 21.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042903432Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14 REV ORIGINAL.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042903431Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620GB. DUE TO EXCESSIVE CORROSION FUEL ACCESS PLATE NR 620GB WAS REPLACED IAW SRM 57-10-01 CONDITION III.Apr 28, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042903429Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV. ORIGINAL.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042903428Cargo Track · corrodedCORROSION ON RT CARGO TRACK FROM BS 816 TO 889. RT CARGO TRACK WAS REPLACED IAW SRM 51-41-01.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042903427Cargo Track · corrodedCORROSION ON RT CARGO TRACK FROM BS 900 TO 954. CARGO TRACK WAS REPLACED IAW SRM 51-41-01.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042903426Cargo Track · corrodedCORROSION ON LT CARGO TRACK FROM BS 816 TO 889. CARGO TRACK WAS REPLACED IAW SRM 51-40-08, 51-41-01, 51-10-4.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042803394Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW 10 TO XCW=50 AT LT MLG WHEEL WELL FWD BULKHEAD, SM, CARD 3, ZONE 140. CORROSION WAS REMOVED, MEASURE NDT SPM 04.00.07 PAR 5, FIG 3, SH 1-2, ORIGINAL THICKNESS 0.177" REMAINING THICKNESS 0.157" WITHIN LIApr 27, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042803393Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. OUT OF LIMITS FUEL ACCESS PLATE WAS REPLACED IAW SRM 57-10-01.Apr 27, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042803392Angle · crackedCRACKED ZEE ON LOWER LT CORNER AT AFT CABIN BULKHEAD DOOR. DAMAGE ZEE WAS REPLACED FOR NEW 1 IAW SRM 51-41-02.Apr 27, 2016 · N926AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016042803391Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV ORIGINAL SECTION I.Apr 27, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042703390Access Panel · corrodedCORROSION OUT OF LIMITS ON FUEL ACCESS PANEL 520CT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 AND IPC 57-22-01-01.Apr 26, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042703389Doubler · corrodedCORROSION AT PRODUCTION DOUBLER UNDER LONGERON 30, BS 969. REPAIRED IAW ER/A 5451-04-14, REV ORIGINAL.Apr 26, 2016 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042603269Pan · crackedCRACKED UPPER PAN AT RT, FWD OVERWING EMERGENCY EXIT DOOR JAMB. CRACK WAS STOPPED IAW 53-20-15, FIG 201, REP 8. NEW DOUBLER WAS DRILLED IAW 51-40-08. NEW DOUBLER WAS INSTALLED IAW 51-40-02. LENGTH CRACK .265".Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042603268Longeron · corrodedCORROSION ON LONGERON 30 FROM BS 889 TO 927 AT AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042603267Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 927 - 1000 ON AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042503195Skin · crackedCRACK ON FUSELAGE SKIN BS 1086.5, LONGERON 14L. SKIN WAS REPAIRED IAW ETI-17-16-002, REV 2 AND ER/A 545090-14, REV ORIGINAL.Apr 24, 2016 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042403190Frame · corrodedCORROSION ON FRAME BS 1022 BETWEEN LONGERON 20 RT TO 26 RT AT AFT CARGO COMPARTMENT, C2,SM, CARD 10, ZONE 180. CORROSION WAS REMOVED, REWORKED AREA WAS MEASURED, TREATED, AND PAINTED IAW SRM 51-10-04, PAR 26, 21 AND 5. ORIGINAL THICKNESS: 0.063", REMAINING THApr 23, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042403188Frame · crackedCRACKED FRAME BS 679, LONGERONSS 25 AND 26R AT KEEL BEAM AREA. FRAME REPAIRED IAW SRM 51-70-11, REP 1.Apr 23, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042303187Rub Strip · brokenBROKEN RUBSTRIP ON FLOOR PANEL NR 223. NEW SECTIONS OF RUB STRIPS WERE INSTALLED IAW SRM 51-20-05, 51-10-04 PAR 15 DWG NR 9956320, REV G AND SRM 51-40-08.Apr 22, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042203168Seat Track · corrodedCORROSION ON SEAT TRACK X -54.5 BETWEEN BS 1022 AND 1065,. SEAT TRACK WAS REPLACED IAW SRM 51-41-05.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042203167Door Frame · corrodedCORROSION ON AFTER CARGO DOOR FRAME LOWER AREA. DOOR JAMB WAS REPAIRED IAW SRM 53-20-15, REP 7.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042203166Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 889-908. DAMAGE WAS REPAIRED IAW SRM 53.00.05, REPAIR 3, 2.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042203163Floor Panel · damagedDISBONDED AND CRACKED CHANNEL ON FLOOR PANEL NR 222AJF7. CHANNEL ON FLOOR PANEL REPAIRED AND BONDED IAW SRM 53-20-50 FIG 202, 51-20-09, 51-30-08, AND 51-10-4 PAR 15/21.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042203162Cusp Web · corrodedCORROSION ON LT CUSP WEB BS 851 TO BS 870 BETWEEN X=44 AND X=60 AT CPAX IN REF CARD 22, ZONE 000, CARD 87, ZONE 200. CORROSION ON CUSP WEB WAS ATTENDED IAW SRM 51-41-02, 51-41-03, 51-41-05, 5141-01, 51-10-04 PAR 15, 21 AND 37, AND 53-00-55, FIG 215, SHEET 1 OApr 21, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042103125Seat Track · corrodedCORROSION ON RT SEAT TRACK X=54 FROM BS 256 TO BS 340 IN REF CARD 14, ZONE 200. CARD 88 ZONE 200. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201, REPAIR 5 CONFIGURATION -7005.Apr 20, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042003046Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW SRM 53-20-50.Apr 19, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042003044Fitting · crackedCRACKED FWD INNER FITTINGS ON BEAM NR 1 AT AFT CARGO DOOR. FITTING WAS REPLACED IAW SRM 51-41-05, 51-40-08, 51-10-04, PAR 15/21.Apr 19, 2016 · N926AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016041903019Seat Track · corrodedCORROSION ON SPLICE OF SEAT TRACK X=-56, BS 218. SEAT TRACK SPLICE, X=-56, BS 218 WAS REPLACED IAW SRM 51-40-08 AND DWG 5953059, REV H, SRM 51-40-01.Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041903018Frame · crackedCRACKED FRAME BS 694, LONGERON 26 LT AT KEELBEAM AREA. SM, CARD 24, ZONE 140. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02 AND 51-41-05 CRACK LENGTH 0.650".Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041903017Frame · crackedCRACKED FRAME BS 679, LONGERON 25 LT AT KEEL BEAM AREA. FRAME WAS REPAIRED IAW 51-70-11, FIG 201. CRACK LENGTH 0.500".Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041702961Seat Track · corrodedCORROSION ON RT SEAT TRACK BS 952-988, SEAT TRACK WAS REPLACED IAW SRM 53-20-52, FIG 201, REPAIR 5 AND 51-41-01.Apr 16, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041602954Beam · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER IN BEAM BS 427 BETWEEN LONGERONS 26-27R IN FWD CARGO COMPARTMENT. NEW REPAIR DOUBLERS WERE REPLACED IAW SRM 53-20-15, REA 6, 51-41-02, 51-10-04 PAR 15 AND 21, AND 51-20-09.Apr 15, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016041502925Cusp Web · damagedDAMAGE OUT OF LIMITS CUSP WEB, BS 551 X=56 - 60 AT LT AREA OF CABIN PAX. DAMAGE WAS REMOVED IAW IAW SRM 53-00-55, FIG 125. REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 125.Apr 14, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041402892Seat Track · corrodedCORROSION ON SEAT TRACK X=44.5 BETWEEN BS 1022 AND BS 1065. SEAT TRACK WAS REPLACED IAW SRM 53-20-50, FIG 1, 51-41-05, 51-40-08, AND 51-10-04, PAR 15/21.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402891Seat Track · not reportedLT SEAT TRACK X=56 FROM BS 817 TO 818 AND 868 TO 870 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402890Seat Track · not reportedSEAT TRACK X=56 AND BS 578 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402889Beam · crackedCRACK ON BEAM AFT EDGE AND FWD EDGE AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND 202, 51-40-02, 51-40-05, AND 51-10-04. PAR 15 AND 21.Apr 13, 2016 · N926AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016041302859Angle · crackedMAINTENANCE DISCOVERED THAT THE RT FORWARD EMERGENCY ESCAPE DOOR HAD A CRACKED CLIP BEHIND THE DOOR STOP. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR CLIP WAS REPLACED IAW SRM 51-41-05 ANApr 12, 2016 · N926AT · Boeing 717200 · Emergency Exits
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