N925AT

Service difficulty reports · 182

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 = 'N925AT' 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 DALA2021022501093Power Supply · inoperativeON THE SERVICE CHECK, MAINTENANCE FOUND THE OVER WING WALL EXIT LIGHT TO BE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED THE POWER SUPPLY LOCATED AT B5-119. THE EMERGENCY LIGHTS NOW OPERATE NORMALLY REF B717 AMM 33-51. (LP 7596098)Feb 25, 2021 · N925AT · Boeing 717200 · Emergency LightingSDR DALA2021021200817Slide · no testTHE L1 DOOR SLIDE FAILED THE DEPLOYMENT TEST FORECAST #95-0525-0111 DUE TO THE LANYARD NOT ATTACHED TO GIRT BAR. PN- D29982-225 SN-2678 MFR DATE- 11/09. MAINTENANCE REPLACED THE SLIDE PER W/C 2561-9001. (LP #1728645)Feb 12, 2021 · N925AT · Boeing 717200 · Escape SlideSDR DALA2020021801203Door Frame · corrodedAFT CARGO DOOR JAMB INTERNAL FACTORY ALUMINUM DOUBLER IS CORRODED FOR APPROXIMATELY 6 INCHES FWD AND AFT OF CENTERLINE. NRC 001-0304:5231-2002/002 00218: COMPILED WITH ER/A 585336-14 ORIGINAL. (LP #1494200)Feb 17, 2020 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2020021801202Door Frame · corrodedAFT CARGO DOOR JAMB HAS CORROSION. NRC 001-0304:5231-2002/001 00013: REPAIRED REF B717 SRM 53-20-15-2R PROC 7. (LP #1493931)Feb 17, 2020 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019041102393Battery Pack · inoperativeTHE EMERGENCY LIGHTS IN ROW 5, 6, & 7 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW B717 AMM 33-55. ALL CHECKS ARE GOOD. (LP #5531007)Apr 11, 2019 · N925AT · Boeing 717200 · Emergency LightingSDR DALA2018032701941Frame · corrodedCORROSION ON FRAME BS 1022, BETWEEN LONGERONS 20R - 22R. REPAIRED IAW SRM 53-20-07-2R, REPAIR 3.Mar 26, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018032701940Frame · crackedCRACKED FRAME BS 1162, BETWEEN LONGERONS 1L AND 2L. REPAIRED IAW ETI-17-18-061, REV 1, AND ER/A 567141-14, REV ORIGINAL.Mar 26, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018032601901Angle · crackedCRACKED ANGLE BS 1162 LONGERON 2L. REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.Mar 25, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018032501888Shear Tie · corrodedCORROSION ON THE FRAME SHEAR TIE BS 1022 BETWEEN LONGERONS 29L - 29R. THE FRAME SHEAR TIE WAS REPLACED IAW DWG 9958214, REV BW, SRM 51-41-02, AND 51-41-05.Mar 24, 2018 · N925AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2018032401885Intercostal · corrodedCORROSION THE ON THE INTERCOSTAL, LONGERON 30 BETWEEN BS 1022 - 1037. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05.Mar 23, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018032301850Floor Panel · corrodedCORROSION ON FLOOR PANEL 221NF. THE FLOOR PANEL WAS REPLACED IAW AMM 53-21-01.Mar 22, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018032301849Hinge Fitting · wornFREE PLAY AT THE LT WING OTBD FLAP HINGE FITTING. OTBD FLAP HINGE WAS REPAIRED IAW ETI-17-18-056, REV 3, AND ER/A 566913-14, REV ORIGINAL.Mar 22, 2018 · N925AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018032301884Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 954 BETWEEN LONGERON 27L TO 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06-2R, REPAIR 2, AND DWG 9958214, REV BW.Mar 21, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018032201834Angle · corrodedCORROSION TYPE EXFOLIATION AT RT CUSP ANGLE STA 200. CORROSION LEVEL 2, RT CUSP ANGLE STA 200 WAS REPAIRED PER ETI-17-18-045 REV 1 AND ER/A 566866-14 REV ORIGINAL.Mar 21, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018032201833Fitting · crackedCRACK ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870. FRAME CLIP WAS REPAIRED PER SRM 53-00-06-2R REPAIR 2. HFEC INSPECTION WAS ACCOMPLISHED ON CLIP FRAME BTW LONG 25R TO 26R STA Y=870 AFTER TRIM OUT. NO CRACKS WERE FOUND PER NDT SPM PART 6, 06-10-01.001.Mar 21, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018032101820Gusset · crackedCRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROTECTION LONG 7R AT PAX CABIN. GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R WAS REPAIRED PER ETI-17-18-043 REV 1 AND ER/A 566865-14 REV ORIGINAL.Mar 20, 2018 · N925AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2018031901764Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF AT PAX CAB (CPAX). NRC 00560: FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031901767Longeron · corrodedCORROSION OUT OF LIMITS ON LONGERON 30, BS 934 TO 1002. CORROSION OUT OF LIMITS. THE LONGERON WAS REPLACED IAW SRM 53-20-05-01-3, FIG 1.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031901766Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 1022 - 1037. THE LONGERON SECTION WAS REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031901765Longeron · corrodedCORROSION ON LONGERON 27L BETWEEN BS 990 TO 1022. THE LONGERON SECTION WAS REPLACED SRM 53-20-05-01-3, FIG 1, AND 51-40-08.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031801760Floor Panel · brokenBROKEN CHANNEL ON GEN FLOOR PANELS #221GF, 222AJF, AND 222EF. NRC 00536: GEN FLOOR PANELS #221GF, 222AJF, AND 222EF WERE REPAIRED PER B717 SRM 53-20-50-2R REPAIR 5 FIG. 202. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON GEN FLOOR PANELS #222AJF AND 222EF AFTER STOPMar 17, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031801763Floorbeam · crackedCRACKED FLOORBEAM BS 645. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 5971111, REV F.Mar 17, 2018 · N925AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018031801762Skin Splice · corrodedCORROSION ON SKIN SPLICE BS 898, BETWEEN LONGERONS 26L TO 30L. THE SKIN SPLICE WAS REPLACED IAW SRM 53-20-01-0I-3, FIG 1. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND OUT LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE PAR 4, FIMar 17, 2018 · N925AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031901813Pan · crackedCRACK FOUND ON THE FWD EDGE OUTER PAN BELOW THE NR 2 STOP FITTING AT THE FWD CARGO DOOR. REPAIRED IAW ETI-17-18-055, REV 1, AND ER/A 566780-14, REV ORIG.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031701759Longeron Splice · corrodedCORROSION ON THE LONGERON 30 SPLICE BETWEEN BS 927 TO 946. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031701758Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 27L BETWEEN BS 973 TO 994 IN THE AFT CARGO BAY. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031701756Strap · corrodedCORROSION ON STRAP AT LONGERON 25L BETWEEN BS 1002 TO 1022. THE STRAP WAS REPLACED IAW SRM 51-41-05, AND DWG 5936021, REV EG.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031701750Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022, BETWEEN LONGERONS 7L - 8L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05 AND DWG 9912243, REV JS. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01.001.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031501713Membrane · corrodedCORROSION ON MEMBRANE STA Y=200 X=-54 5300-2010. CORROSION LEVEL 2, MEMBRANE WAS REPAIRED PER SRM 51-70-10-2R. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=200 X=-54, NO CRACKS WERE FOUND AFTER CUT OUT PER NDTSPM 06-10-01.001.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031501709Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 REF 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 WERE REPLACED PER SRM 51-41-02.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031501708Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 REF AMDS 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 WERE REPLACED PER SRM 51-41-02.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031401687Seat Track · corrodedCORROSION ON THE SEAT TRACK LBL 54, BETWEEN BS 240 TO 247. THE SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R-5.Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031401684Cusp Web · corrodedCORROSION ON THE CUSP WEB, BS 902 TO 904, LBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031301683Cusp Web · crackedCRACK ON THE RT CUSP WEB, BS 674, RBL 46: THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R-2. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS FOUND IAW NDT SPM PART 6, 06-10-01.001,Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031301626None · noneEXCESSIVE CORROSION ON FUEL ACCSESS PLATE #620CT, 520CT, AND 520DT AT SETTLEMENT AND COUNTERSINK AREA RH/LH WING IN REFERENCE NRCS 00549, 00553, AND 00554. NRC 00603: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR Mar 12, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018031301625Floor Panel · corrodedCORRODED FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED, AND REPLACED IAW DWG 9957828, REV AB.Mar 12, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031201620Floor Panel · crackedCRACKS ON FLOOR PANELS #221EF, 211ANF, AND 223GF AT PAX CAB (CPAX). NRC 00556: FLOOR PANELS #221EF, 211ANF, AND 223GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50. FLOOR PANELS WERE INTALLED WITH JIC CARD 2040-0024. (LP #0460121)Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031201623Access Panel · corrodedCORROSION OUT OF LIMITS ON ACCESS PANEL 620AT. THE ACCES PANEL WAS REPLACED IAW SRM 57-10-01-2R-2, PAR 5.Mar 11, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018031201622Door Frame · crackedCRACKED NLG DOOR FRAME, RT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018031201621Door Frame · crackedCRACKED DOOR FRAME AT THE NLG LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018031201619Web · crackedCRACKED WEB BS 208, LONGERON 15L. THE WEB WAS REPAIRED IAW SRM 53-10-15-2R, PR 4. HFEC INSPECTION PERFORMED AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM 06-10-01.001.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031201618Cusp Web · crackedCRACKED CUSP WEB BS 219, LBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R. HFEC INSPECTION WAS PERFORMED AT THE TRIMMED OUT AREA. NO CRACKS WERE FOUND IAW NDT SPM PART 6 06-10-01.001.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031201617Angle · crackedCRACKED ANGLE AT THE RT FWD EMERGENCY EXIT DOOR UPPER BEAM FWD EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957735, REV G.Mar 11, 2018 · N925AT · Boeing 717200 · Emergency ExitsSDR DALA2018031201616Angle · crackedCRACKED ANGLE AT THE FWD CARGO DOOR BETWEEN THE UPPER EDGE AND BEAM 1 AND NEXT TO AFT HINGE. THE ANGLE WAS REPLACED SRM 51-41-02, 51-41-05, AND DWG 9957664, REV N.Mar 11, 2018 · N925AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018031201615Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R -2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ON TRIMMED OUT AREA IAW NDT SPM 06-10-01.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031201614Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT BETWEEN BS 120 TO 148, RBL 50 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031101612Rub Strip · corrodedCORROSION ON RUBSTRIPS OF THE FUEL ACCESS PANELS 520GB AND 520MB ON THE LT WING THE RUBSTRIPS WERE REPLACED IAW SRM 57-10-01-2R, REP 3, PAR 6.Mar 10, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018031101611Skin · puncturedPUNCTURE ON AFT EDGE INTERNAL SKIN OF LT MLG DOOR. THE DOOR SKIN WAS REPAIRED IAW SRM 52-82-02-2R-1, FIG 201, SHEET 5.Mar 10, 2018 · N925AT · Boeing 717200 · Landing Gear DoorsSDR DALA2018031101610Frame Angle · crackedCRACKED FRAME ANGLE AFT FACE, BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DRAWING 9912243, REV JS.Mar 10, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031101609Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, AND SRM 51-20-09.Mar 10, 2018 · N925AT · Boeing 717200 · Fuselage Main, Frame
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