N975AT, cancelled Nov 19, 2025

Service difficulty reports · 122

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 = 'N975AT' AND deregistration_id = 'N975AT-2025-11-19'
  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 DALA2019040800000Skin · delaminatedSPOILER SKIN, UNSCHEDULED REMOVAL. FOUND DELAMINATED.Apr 8, 2019 · N975AT · Boeing 717200 · SpoilersSDR DALA2018070204300Relay · faultyOVERWING EMERGENCY LIGHTS WON'T EXTINGUISH AFTER SETTING EMERGENCY LIGHT SWITCH TO OFF AS REPORTED BY 2ND SHIFT (WILL ONLY SWITCH OFF ON 'ARM' POSITION). T/S PER FIM 33-51-00-802. REMOVED AND REPLACED OVERWING EMER EVAC LIGHTS BATTERY PACK RELAY R2-273 IAW AJul 2, 2018 · N975AT · Boeing 717200 · Emergency LightingSDR DALA2017090306564Cusp Web · corrodedCORROSION ON THE CUSP WEB, RBL 54 AND 60, BS 416 TO 417, OUT OF LIMITS. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.Sep 2, 2017 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122310056Hinge · damagedELONGATED HOLE ON LT WING OUTBOARD FLAP FWD OUTBOARD HINGE IAW NRTC 00456. THE HINGE WAS REMOVED IAW AMM 20-50-01 AND AMM 27-50-01. THE BEARING WAS REPLACED, AND THE HINGE WAS REPAIRED IAW ER/A 552872-14 REV ORIGINALDec 22, 2016 · N975AT · Boeing 717200 · Leading Edge DevicesSDR DALA2016122109992Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN STA 1021 BTW LONG 13/14 LT. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ETI-17-16-183 REV. ORIGINAL AND ER/A 552865-14 REV ORIGINAL SECTION I. PERFORM REPETITIVE EXTERNAL GENERAL VISUAL INSPECTION OF THE REPAIR EVERY C-CHECK OR 24 MODec 20, 2016 · N975AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016122009962Stiffener · crackedAFT ACCESSORY COMPARTMENT HAS A CRACK ON STIFFENER STA Y=1200 CANT LONG PROJECTION 2L. STIFFENER WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201 IN REF ORNRC 00394.Dec 19, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122009961Support · crackedAFT CARGO COMPARTMENT HAS A CRACK ON VERTICAL SUPPORT STA Y=816 LONG 30 (AMDS 5331-2001). CRACK DIMENSION IS .650". CRACK IN VERTICAL SUPPORT WAS STOP DRILLED PER SRM 53-00-00 FIG 201, HFEC WAS ACCOMPLISHED. NO CRACK WERE FOUND AFTER STOP DRILL PER NDT SPM 06-Dec 19, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121809948Support · crackedFWD CARGO COMPARTMENT HAS A CRACKED SUPPORT ON STA Y=655 BTW LONGS 23R AND 24R. SUPPORT WAS REPAIRED PER SRM 53-00-00 FIG 201 SHEET 1 REF ONNRC 363.Dec 17, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121809945Angle · crackedFWD CARGO DOOR: CRACK ON ANGLE UPPER EDGE OF DOOR BETWEEN BS 408-410. DAMAGE AREA WAS REPAIRED IAW SRM 52-00-00 REPAIR 2, AND DWG 9957663 REV W.Dec 17, 2016 · N975AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016121709943Longeron · crackedIN THE AFT ACCESORY COMPARTMENT THERE IS A CRACK ON LONGERON 4L, BS 1152. THE LONGERON WAS REPAIRED IAW SRM 53-00-05, REPAIR 2, FIGURE 201, 51-40-08, AND 51-41-05.Dec 16, 2016 · N975AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016121709942Bulkhead Web · crackedFWD CARGO COMPARTMENT HAS CRACKED WEB OF FWD BULKHEAD BS 218, 15 INCHES ABOVE LONGERON 27. THE BULKHEAD WAS REPAIRED BS SRM 53-00-00 REPAIR 1.Dec 16, 2016 · N975AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016121609905Longeron · crackedAFT ACCESORIES COMPARTMENT HAS A CRACK ON LONGERON 3L BS 1152. REPAIRD IAW SRM 53-00-05 REPAIR 2 FIGURE 201 AND 51-41-02.Dec 15, 2016 · N975AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016121609904Frame · crackedCRACK ON FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07 REPAIR 4, 51-41-01, AND 51-41-05.Dec 15, 2016 · N975AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016121409840Support · crackedFWD CARGO COMPARTMENT: CRACKED RT SUPPORT ON STA Y=664 LONG PROJECTION 23R AND 24R. FITTING WAS REPLACED PER SRM 51-41-02.Dec 13, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121409839Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 620DT. CORROSION WAS REMOVED ON COUNTERSINK AREA AND SETTLEMENT SURFACE ON ACCESS PLATE 620DT PER SRM 51-10-04 PAR 26, COUNTERSINK AREA WAS MEASURED MAXIMUM COUNTERSINK DIAMETER ALLOWABLE IS 0.660", MAX DIAMETER MEASURED IS 0.705Dec 13, 2016 · N975AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016121409832Frame · crackedBARREL KEEL BEAMS; CRACKS ON RT/LT FRAMES KEEL AREA FROM STA Y=655 TO Y=737. FRAMES WERE REPAIRED PER SRM 51-70-11 REPAIR 1, SRM 51-41-02, 51-41-05, AND 51-10-04 PAR 15, 21, AND 37. CRACK FRAME DIMENSIONS, STA 679LH 0.656 IN , 694RH 0.906 IN, AND 715R 0.406 INDec 13, 2016 · N975AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016121409831Fitting · crackedCRACK ON FRAME CLIP AT STA Y=1022 BTW LONG 16L AND LONG 17L. FRAME CLIP WAS REPLACED PER DWG 9912243 REV JS, SRM 51-41-02 AND 51-41-05.Dec 13, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121309810Cusp Web · crackedCRACK ON LT CUSP WEB LBL 54 - 60, BS 656 - 674 . REPAIRED IAW SRM 53-00-55 FIG 215.Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121309809Beam · crackedL1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 7. REPAIRED IAW SRM 52-10-02 REPAIR 13 FIGURE 201.Dec 12, 2016 · N975AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016121309808Beam · crackedL1 DOOR HAS A CRACKED AFT EDGE ON BEAM NR 1. REPAIRED IAW SRM 52-10-02 REPAIR 7 FIGURE 201.Dec 12, 2016 · N975AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016121309807Frame · crackedCRACKED FRAME ANGLE ON BS 1022, LONGERONS 13 - 14L. REPLACED IAW DWG 9912243 REV. JS, SRM 51-41-02 AND 51-41-05.Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016121309806Door Frame · crackedCRACKED DOOR FRAME WEB BS 207 LONGERON 11 AND 15L. REPAIRED IAW SRM 53-10-15.Dec 12, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016121209753Skin · delaminatedDELAMINATON ON RUDDER TAB SKIN. THE RUDDER TAB SKIN WAS REPAIRED IAW SRM 55-41-01 REPAIR 1, AND 51-70-02 REPAIR 3 PAR 5.Dec 11, 2016 · N975AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2016121209752Cusp Web · crackedCRACKED RT CUSP WEB BS 671 - 674, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 203.Dec 11, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121209751Cusp Web · crackedCRACKED CUSP WEB BS 652 - 655, RBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 211.Dec 11, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016121009803Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211ALF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.Dec 9, 2016 · N975AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016121009802Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.Dec 9, 2016 · N975AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120909746Pan · crackedCRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909745Pan · crackedCRACKED RT RING PAN UPPER FWD CORNER BS 696. REPAIRED THE RING PAN WAS REPAIRED IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909744Pan · crackedCRACKED RT RING PAN LOWER FWD CORNER BS 889. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909743Pan · crackedCRACKED RT RING PAN UPPER & LOWER AFT CORNERS BS 851. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909742Pan · crackedCRACKED RT RING PAN LOWER FWD CORNER BS 794. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909722Pan · crackedCRACK ON LOWER FWD CORNER AT RING PAN WINDOW LT SIDE BTW STA Y 598-617. CRACKED RING PAN LOWER FWR CORNER BTW STA Y=598-617 LT, WAS REPAIRED PER SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016120909721Cusp Web · puncturedPUNCTURES ON RT CUSP WEB BTW STA Y=974 TO Y=975 AND BTW Y=989 TO Y=990, X=49R. PUNCTURE WAS DRILLED, DAMAGE WAS REMOVED PER SRM 53-00-00 PAR 2, AND FASTENERS WERE INSTALLED PER SRM 51-41-02.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 2016F00131Skin · delaminatedDURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE LOWER AND UPPER SURFACE. SUP: P/N 5940974-1.May 31, 2016 · N975AT · Boeing 717200 · SpoilersSDR 2016F00128Skin · delaminatedDURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.May 31, 2016 · N975AT · Boeing 717200 · SpoilersSDR DALA2017033003179Skin · damagedDURING ATG4 MODIFICATION, MAINTENANCE NOTED THAT ALL FIVE HOLES COMMON TO THE SKIN OF THE SHEAR TIE WERE DAMAGED AND DID NOT PASS NDT INSPECTION. REPAIRED IAW ER/A 00-545433.Mar 29, 2016 · N975AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016101007123Skin · crackedSKIN CRACKED AT BS 1076 LONGERON 14R. REPAIRED THE SKIN IAW PRI 542271-14 REV. 0 AND ER/A 542271-14 REV. ORIGINAL.Dec 14, 2015 · N975AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2015051103188Cable · frayedDURING SERVICE CHECK, FOUND TAILCONE SLIDE KEVLAR DEPLOYMENT CABLE FRAYED. REPLACED AFT TAILCONE SLIDE DEPLOYMENT CABLE IAW AMM 25-61. LP 7277097.May 10, 2015 · N975AT · Boeing 717200 · Escape SlideSDR DALA2014110606004Battery Pack · inoperativeDURING LINE CHECK, NOTED CEILING EXIT LIGHTS IN FIRST CLASS AND 2 ROWS OF COACH EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK, BS-227 IAW AMM 33-51.Nov 6, 2014 · N975AT · Boeing 717200 · Light System WiringSDR SWAA2014010223703Lens · crackedR1 DOOR EXIT LIGHT LENS CRACKED. R & R LENS ASSEMBLY IAW AMM.Dec 29, 2013 · N975AT · Boeing 717200 · Emergency LightingSDR SWAA2014010823898Wire · looseRT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.Dec 27, 2013 · N975AT · Boeing 717200 · Light System WiringSDR SWAA2014010823897Wire · looseLT OVERWING EMERGENCY EXIT LIGHT WIRE LOOSE. SECURED WIRE IAW AMM.Dec 27, 2013 · N975AT · Boeing 717200 · Light System WiringSDR SWAA2014010223698Wire · disconnectedLT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED WIRE IAW WDM.Dec 27, 2013 · N975AT · Boeing 717200 · Light System WiringSDR SWAA2013122723652Battery Pack · dischargedOVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R OVERWING EMERGENCY LIGHTS BATTERY PACK IAW MM.Dec 21, 2013 · N975AT · Boeing 717200 · Emergency LightingSDR SWAA2013122623635Light · inoperativeAFT CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.Dec 21, 2013 · N975AT · Boeing 717200 · Emergency LightingSDR SWAA2013121823493Intercostal · crackedINTERCOSTAL CRACKED BETWEEN STATION 619 & 636, BL 0. R & R INTERCOSTAL IAW SRM.Dec 9, 2013 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2013112522752Stringer Splice · crackedSTRINGER SPLICE 6R DAMAGED & CRACKED AT BS 246. R & R STRINGER SPLICE IAW SRM.Nov 13, 2013 · N975AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2013120222832Crease Beam · corrodedCREASE BEAM WEB CORRODED BETWEEN STATION 598 TO STATION 617, STRINGER 18L. REPAIRED WEB IAW SRM.Nov 8, 2013 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR SWAA2013121223247Longeron · crackedLONGERON CRACKED AT STATION 1133, LONGERON 2R. R & R LONGERON IAW SRM.Oct 28, 2013 · N975AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
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