N969AT, cancelled Jun 28, 2025

Service difficulty reports · 144

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 = 'N969AT' AND deregistration_id = 'N969AT-2025-06-28'
  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 2019F00226Spoiler · delaminatedSPOILER HAD DELAMINATION.Jun 20, 2019 · N969AT · Boeing 717200 · SpoilersSDR DALA2018071604493Light · damagedTHE EMERGENCY SEAT MOUNTED LIGHTING IS DAMAGED AND INOPERATIVE AT SEAT 27C. MAINTENANCE RESECURED THE PANEL. OK FOR SERVICE.Jul 15, 2018 · N969AT · Boeing 717200 · Emergency LightingSDR DALA2018071604492Sign · looseTHE EMERGENCY EXIT SIGN COVER AT DOOR 1L IS LOOSE. MAINTENANCE RESECURED EXIT THE EEPL SIGN AT 1L DOOR. AIRCRAT IS OK FOR SERVICE.Jul 15, 2018 · N969AT · Boeing 717200 · Emergency LightingSDR DALA2017122108917Engine · odorODOR PREVALENT AFTER TAKEOFF AND THROUGHOUT FLIGHT. ODOR STRONGEST FROM RT PACK ON THE NR 2 ENGINE BLEED. NO CONTAMINATION WAS FOUND. FOUND TURBINE OIL ODOR ISOLATED TO THE NR 2 ENGINE. SUSPECT ISSUE WITH BUFFER AIR VALVE. REPLACED NR 2 ENGINE BUFFER AIR VDec 20, 2017 · N969AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2016120509588Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=-52 BTW STA Y=132 TO Y=-148. AT COCKPIT FLOOR STRUCTURE. FLOOR SUPPORT WAS REPLACED PER DRAWING 9936533 ITEM 35 REV CM AND SRM 51-41-02.Dec 3, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111708911Window Frame · crackedCRACK ON LWR FWD SECTION OF RT SLIDE WINDOW COUNTER FRAME AT COCKPIT. DAMAGE AREA WAS REPAIRED PER ETI -17-16-170 REV 1 AND ER/A 551770-14 REV ORIG.Nov 16, 2016 · N969AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016111608812Pan · crackedCRACK ON INBD AND OUTBD PAN LOWER EDGE BS 388 AT FWD CARGO DOOR. INBD & OUTBD PAN LOWER EDGE WAS REPAIRED IAW ETI-17-16-161 REV 1 AND ER/A 551739-14 REV ORIGINAL.Nov 15, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111208742Vane · dentedSEVERAL DENTS ON AFT MOVABLE FLAP VANE ON THE LT WING. THE FLAP VANE WAS REPAIRED IAW SRM 57-53-01 REP.1 PARAGRAPH 4.Nov 12, 2016 · N969AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2016111208741Skin · crackedCRACKED FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2-3L. THE SKIN WAS REPAIRED IAW ETI-17-16-139 REV. 3 AND ER/A 551722-14AD REV. ORIGINAL.Nov 11, 2016 · N969AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016111108739Cargo Track · corrodedCORROSION ON LT CARGO TRACK BETWEEN BS 899 TO 813 AT AFT CARGO BAY. THE DAMAGE SECTION WAS REPLACED IAW SRM 53-20-51 FIG 1.Nov 10, 2016 · N969AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016111108707Fitting · crackedCRACKED FRAME CLIP STA Y 1037 BTW LONG 16-17R AT RT AFT LAVATORY AREA. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.Nov 10, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111108706Fitting · crackedCRACKED FRAME CLIP STA Y=1037 LONG 16L TO 17L AT W2. CLIP WAS REPAIRED PER ETI-17-16-145 REV 1 AND ER/A 551734-14 REV ORIG.Nov 10, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111008442Cargo Track · corrodedCORROSION ON RT CARGO TRACK BS 899 - 1022 IN AFT CARGO BAY . THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.Nov 9, 2016 · N969AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016111008441Cargo Track · corrodedCORROSION ON THE LEFT CARGO TRACK BS 899 - 1022. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51 FIG 1.Nov 9, 2016 · N969AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016111008436Frame · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERON 13 & 14L, REPLACED IAW SRM 51-41-02, 51-41-05 AND DRAWING 9912243 REV JS.Nov 9, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016111008435Frame · crackedCRACKED FRAME BS 1037 LONGERON 17L. THE FRAME WAS REPAIRED IAW SRM 53-20-07 FIG 201 REPAIR 4.Nov 9, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110908365Access Panel · crackedRIGHT WING FUEL ACCESS PANEL 620MB FOUND CRACKED. THE ACCESS PANEL WAS REPLACED, NO LEAK WAS FOUND.Nov 8, 2016 · N969AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110808337Structure · crackedCRACK ON GROUND CONDITIONED AIR ACCESS CUT OUT. REPLACED PER ETI-17-16-147 REV ORIGINAL, ER/A 551737-14 REV ORIGINAL, AND SRM 51-41-02 AND 51-41-08.Nov 7, 2016 · N969AT · Boeing 717200 · Air Distribution SystemSDR DALA2016110808336Longeron · corrodedCORROSION ON LONGERON 30 FROM STA Y=908-Y=993 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=905-993 WAS REPLACED PER SRM 51-41-01, SRM 51-41-02, SRM 51-41-05, AND SRM 53-20-05 FIG 201 REPAIR 1.Nov 7, 2016 · N969AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016110808335Longeron · corrodedCORROSION ON LONGERON 30 FROM STA Y=988 TO Y=1009 AT AFT CARGO COMPARTMENT. SECTION LONGERON 30 FROM STA Y=900 TO Y=1012 WAS REPLACED PER SRM 51-41-01, SRM 51-41-02, SRM 51-41-05, AND SRM 53-20-05 FIG 201 REPAIR 1.Nov 7, 2016 · N969AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016110808334Pan · crackedHIDDEN DAMAGE, CRACK ON INNER PAN STA Y=370 BTW BEAMS 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. HFEC WAS ACCOMPLISHED ON CONFIRMED CRACK NDT SPM 06-10-01.001 IS 1.593". CRACK WAS STOPPED PER SRM 51-00-07 PAR 5-16 HFEC OK NO CRACKS AFTER STOP DRILL PER SRM 51-00Nov 7, 2016 · N969AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016110808333Angle · corrodedCORROSION ON ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB PAN AT FWD CARGO COMPARTMENT. ANGLES (2EA) STA Y=383 AND Y=415 FRONT OF LOWER DOOR JAMB PAN AT FWD CARGO COMPARTMENT WERE REPLACED PER SRM 51-41-02 AND DWG 5910142 REV DJ.Nov 7, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110708313Pan · wornWEAR ON INNER PAN OF AFT CARGO DOOR AT BS 994 BETWEEN BEAMS 1 AND 2. THE PAN WAS REPAIRED IAW SRM 52-30-02 REP 5 FIG 201.Nov 6, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110608312Frame · crackedCRACKED FRAME BS 715 RBL-LBL 44. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1.Nov 5, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110608311Frame · crackedCRACKED FRAME BS 674 LBL TO RBL 42. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1.Nov 5, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110608310Frame · corrodedCRACKED LH/RH FRAMES BS 696 RBL 32 AND LBL-32 AT KEEL BEAM. THE FRAME WAS REPAIRED IAW SRM 51-70-11 FIG 201 REP 1 .Nov 5, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110608307Angle · wornWEAR ON LOWER RT ANGLE AT THE AFT CABIN BULKHEAD DOOR. THE DAMAGED AREA WAS REPAIRED IAW SRM 52-10-02-2R REPAIR 16 PARAGRAPH 4 B (2).Nov 5, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110608306Angle · crackedCRACKED ANGLE ON FWD & AFT ENDS OF NR 1 BEAM AT RH FWD OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 9957735 REV G.Nov 5, 2016 · N969AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016110508305Floor Panel · crackedCRACKED COCKPIT FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00 FIG 201.Nov 4, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016110508304Access Panel · corrodedCORROSION ON CENTER TANK FUEL ACCESS PANEL 141AL. THE CORROSION WAS REMOVED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.Nov 4, 2016 · N969AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110508303Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 620AT RT WING. THE CORROSION WAS REMOVED. FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-10-01.Nov 4, 2016 · N969AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016110408242Angle · crackedCRACKED ANGLE ON FWD END OF BEAM NR 1, AT THE LT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02 AND 51-41-05.Nov 3, 2016 · N969AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016110408241Floorbeam · crackedCRACKED FLOORBEAM LBL 54.5 AND BS 737. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-41-05.Nov 3, 2016 · N969AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2016110408240Pan · crackedCRACKED PAN BS 427 BETWEE BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED ON PAN BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR, 2 CRACKS WERE FOUND AS FOLLOW 1) 0.875" 2) 1.062 PER DC/MD BOEING NDTSPM 06-10-01 .001. EQUIPMENT: PHASEC Nov 3, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110408239Angle · crackedCRACKED ANGLE ON BEAM NR 1 FWD END, AT RT AFT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735 REV. G, SRM 51-41-02 AND 51-41-05.Nov 3, 2016 · N969AT · Boeing 717200 · Emergency ExitsSDR DALA2016110308232Floor Panel · delaminatedDELAMINATED FLOOR PANEL 223CF IN THE PAX CABIN. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50 AND REPLACED IAW SRM 53-20-50.Nov 2, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016110308181Pan · crackedCRACK ON INNER PAN STA Y=370 IN BEAM 3 (FWD EDGE) AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR ,ONE CRACK OF 2.125" WAS FOUND PER NDTSPM 06-10-01.001. STOP DRILL WAS PERFORMED ON INNER PAN STA Y=370 Nov 2, 2016 · N969AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016110308180Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222KF AT PASSENGER CABIN. FLOOR PANEL 222KF AT PASSENGER CABIN WAS REPLACED PER SRM 53- 20-50.Nov 2, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016110308179Fitting · crackedCRACK FRAME CLIP 2 EA, STA Y=1152 PROJECTION LONG 2R AND 2L AT AFT ACCESSORY COMPARTMENT. REPLACED CLIPS PER DRAWING 9911860 REV L AND SRM 51-40-02 AND 51-40-05.Nov 2, 2016 · N969AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016110208141Beam · crackedCRACKED BEYOND STOP DRILL ON BEAM NR 1 AT PASSENGER ENTRANCE DOOR (L1). BEAM NR 1 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B-717 SRM 52-10-2 REPAIR 7 FIG 201 SHEET 3.Nov 1, 2016 · N969AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016103107949Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BETWEEN BS 579 - 598 X -60. THE DOUBLER WAS REPLACED IAW SRM 53-20-51 FIG. 1 ITEM 25 AND 51-41-05.Oct 30, 2016 · N969AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016103107948Splice · corrodedCORROSION ON SPLICE FROM BS 579 TO 598 BETWEEN LONGERONS 17 - 18R. REPAIRED IAW SRM 53-20-51 FIG.1 AND 51-41-05.Oct 30, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107947Cusp Web · corrodedCORROSION ON RT CUSP WEB BETWEEN X -54 TO X -60 BS 638. DAMAGED AREA WAS TRIMMED AND REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG 216, HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINE IAW NDT SPM 06-10-01.001, NO CRACKS WERE FOUND.Oct 30, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107946Seat Track · corrodedCORROSION ON RT SEAT TRACK X -22 AND X -44.5 BS 200 - 256. THE SEAT TRACK WAS REPLACED IAW SRM 53-20-52 REPAIR 5 FIGURE 201.Oct 30, 2016 · N969AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016103107945Cusp Web · crackedCORROSION ON RT CUSP WEB X 14 TO X 60 BS 420. CORROSION WAS REMOVED IAW SRM 53-00-00 FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01. REPAIRED IAW SRM 53-000-00 FIG 201.Oct 30, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500103Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=200-208 AND X=-56 AT PAX CABIN (CS) (SM). DUE TO EXCESSIVE DAMAGE SUPPORT WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201.Oct 29, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103008231Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL IN COCKPIT. THE FLOOR PANEL WAS REPAIRED IAW AMM 20-60-10 340-801 SUBTASK 390-002.Oct 29, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016103007944Channel · crackedCRACKED HAT CHANNEL. REPAIRED IAW SRM 53-20-50 REP. 5.Oct 29, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016102907942Cusp Web · crackedCRACKED RT CUSP WEB BELOW SEAT TRACK X 44 BS 219. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55 FIG 219 AND 51-41-02.Oct 28, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102907941Stop Fitting · crackedCRACKED STOP FITTINGS ON FWD EDGE OF AFT CARGO DOOR. THE STOP FITTINGS WERE REPLACED IAW SRM 51-41-01 AND 51-41-05.Oct 28, 2016 · N969AT · Boeing 717200 · Cargo/Baggage Doors
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