N995AT

Service difficulty reports · 158

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 = 'N995AT' 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 DALA2017112308320Skin · wornWEAR ON INTERNAL FACE OF SLAT SKIN SS 119, RT WING NR 1 SLAT. REPAIRED IAW ETI-17-17-240, REVISION 2, AND ER/A 562401-14, REVISION ORIGINAL.Nov 22, 2017 · N995AT · Boeing 717200 · Leading Edge DevicesSDR DALA2017112308319Door Frame · corrodedCORROSION ON DOOR FRAME BS 954 TO 994 IN THE AFT CARGO BAY. THE DOOR FRAME WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-05.Nov 22, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017112308318Fitting · crackedCRACK ON FITTING, LONGERON 22R, BS 661. REPAIRED IAW ETI-17-17-236, REV 2, AND ER/A 562397-14, REV ORIGINAL.Nov 22, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017112208317Torque Tube · corrodedCORROSION WAS FOUND ON THE RUDDER TORQUE TUBE ASSY. THE RUDDER TORQUE TUBE WAS REPAIRED IAW ER/A 562416-14, REV ORIGINAL.Nov 22, 2017 · N995AT · Boeing 717200 · Rudder StructureSDR DALA2017112208316Structure · corrodedCORROSION ON BARREL NUTS WAS FOUND. THE BARREL NUT HOLES WERE REPAIRED IAW ETI-17-17-231, REV 5, AND ER/A 562391-14, REV ORIG. BOLTS AND NUTS WERE REPLACED IAW AMM 20-20-22.Nov 22, 2017 · N995AT · Boeing 717200 · Empennage StructureSDR DALA2017112108241Gusset · crackedCRACKED GUSSET AT LONGERON 7R AT BULKHEAD BS 1022. THE GUSSET WAS REPAIRED IAW ER/A 562380-14, REV ORIGINAL, AND ETI-17-17-226, REV ORIGINAL.Nov 20, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017112108240Skin · corrodedCORROSION ON UPPER SURFACE OF THE SKIN BETWEEN BS 737 & 756, RBL 44 - 60. CORROSION OUT OF LIMITS AND WAS REPAIRED IAW ER/A 562387-14 REV. ORIGINAL. AND ETI-17-17-228 REV 1.Nov 20, 2017 · N995AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017111908212Frame Angle · crackedCRACKED FRAME ANGLE BS 408 AT FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-01-0G AND 51-41-05-0G.Nov 18, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017111808211Frame · crackedCRACK ON RT OVERWING FRAME AT BS 674, BETWEEN LONGERONS 9R TO 19R. THE FRAME WAS REPLACED IAW DWG SR95530013, REV A, & SRM 51-41-05.Nov 17, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017111808209Cusp Web · crackedSEVERAL CRACKS IN THE RT CUSP WEB BS 674 - 725. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 226 AND FIG 223.Nov 17, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111808208Cusp Web · crackedSEVERAL CRACKS IN THE RT CUSP WEB BS 725. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG.215.Nov 17, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111608162Cusp Web · crackedCRACK ON THE CUSP WEB BETWEEN BS 715 - 737, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.Nov 15, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111608161Cusp Web · crackedCRACK ON THE LEFT CUSP WEB BS 807, LBL 44 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4 CONFIGURATION 7037.Nov 15, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111508133Longeron · crackedCRACKED LONGERON 5R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Nov 15, 2017 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017111508132Longeron · crackedCRACKED LONGERON 4R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Nov 15, 2017 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017111508129Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERONS 6R TO 7R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, SRM 51-41-05, AND DWG 9912243, REV. HF.Nov 14, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017111508128Cusp Web · crackedCRACKED CUSP WEB BS 657, LBL 5. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 209.Nov 14, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111508127Longeron · crackedCRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Nov 14, 2017 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017111508126Longeron · crackedCRACK ON LONGERON 6L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Nov 14, 2017 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017111308075Pan · crackedCRACK ON LOWER EDGE INNER PAN, BELOW PRESSURE SEAL OF THE FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R, REPAIR 1, FIG 201.Nov 12, 2017 · N995AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017111308074Intercostal · crackedCRACKED INTERCOSTAL UPPER EDGE BS 380 AT THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Nov 12, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111208071Intercostal · crackedCRACKED INTERCOSTAL AND ANGLE BETWEEN LOWER EDGE AND BEAM 1 BS 408 AT THE FWD CARGO DOOR. THE INTERCOSTAL AND ANGLE WERE REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Nov 11, 2017 · N995AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017111208070Angle · crackedCRACKED ANGLE ON THE LOWER EDGE BS 408 AT FWD CARGO DOOR. THE CARGO DOOR TEE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Nov 11, 2017 · N995AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017111108068Access Panel · crackedCRACK ON THE RT ACCESS PANEL 620KB. THE ACCESS PANEL WAS REPLACED IAW SRM 51-41-01, AND SERVICEABLE MAGNETIC DRIPLESS FUEL MEASURING HOUSING WAS INSTALLED ON THE NEW ACCESS PANEL IAW AMM 28-42-01.Nov 10, 2017 · N995AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017111108067Frame · crackedCRACKED FRAME BS BS 1037, LONGERON 17L. HFEC INSPECTION WAS ACCOMPLISHED ON THE FRAME. NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW SRM 53-20-07-2R, PROCEDURE 4, PARA. 5.A.(2), AND NDT SPM 06-10-01.001. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R.Nov 10, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017111108066Frame · crackedCRACKED FRAME BS 1037, LONGERON 17R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R. HFEC INSPECTION WAS ACCOMPLISHED ON THE FRAME, NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW SRM 53-20-07-2R, PROCEDURE 4, PARA. 5.A.(2). AND NDT SPM 06-10-01.001.Nov 10, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017111108065Floor Panel · corrodedCORROSION ON FLOOR PANEL 211AMF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, FIG 201, SHEET 2.Nov 10, 2017 · N995AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017111008034Longeron · crackedCRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Nov 9, 2017 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017110908019Pan · crackedCRACKED LEFT PAN UPPER AFT CORNER BS 851 - 870 AND 813-832. REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 202.Nov 9, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110908018Pan · crackedCRACKED PAN UPPER FWD CORNER BS 908 - 889. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 202.Nov 9, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110908031Seat Track · corrodedEXCESSIVE CORROSION ON SEAT TRACK SUPPORT BS 110 TO 140, RBL 22. A NEW SEAT TRACK SUPPORT WAS INSTALLED IAW SRM 51-41-01.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017110908017Floorbeam · corrodedEXCESSIVE CORROSION ON THE FLOORBEAM BS 200, LBL 8 TO LBL 14. REMOVED AND REPLACED IAW SRM 51-41-02.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017110908016Floorbeam · corrodedCORROSION ON FLOORBEAM BS 200 BETWEEN RBL 8 TO LBL 8. THE CORROSION WAS REMOVED IAW SRM 51-10-04, PAR 26. ACCOMPLISHED NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE FIG 103. REMOVED AND RENov 8, 2017 · N995AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017110908015Cusp Web · crackedCRACKED CUSP WEB BS 413 & 419, RBL 56. THE CRACKS WERE FOUND WHEN CORROSION WAS REMOVE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 207. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW NDT SPM 06-10-01-01.001.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110908014Floor Panel · brokenBROKEN FLIGHT DECK FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED, AND REPLACED IAW 2040-0024.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017110807999Floor Support · corrodedEXCESSIVE CORROSION ON THE FLOOR SUPPORT BS 140, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05-0G AND 51-41-08-0G.Nov 7, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110807998Vane · debondedDISBOND OF 2.300" X 3.500" AT 9.00" FROM OUTBOARD EDGE AND 9.00" FROM AFT EDGE ON THE RT AFT MOVABLE FLAP VANE, REPAIRED IAW SRM 57-53-01-2R-1.Nov 7, 2017 · N995AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017110807997Floor Panel · brokenBROKEN FLOOR PANEL 221LF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R, REP 3.Nov 7, 2017 · N995AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017110707975Frame · crackedCRACK FOUND ON THE BS 851 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110707974Frame · crackedCRACK ON THE BS 756 FRAME UPPER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110707973Frame · crackedCRACK ON THE BS 617 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110507947Rub Strip · corrodedCORROSION ON THE RT WING ACCESS PANEL RUBSTRIP 620D. THE RUBSTRIP #620DT WAS REPLACED IAW SRM 57-10-01, REP 3.Nov 5, 2017 · N995AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017110507944Door Frame · crackedCRACK ON NLG LT DOOR FRAME AT BS 46. REPAIRED IAW SRM 53-10-14-2R. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.001.Nov 5, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507943Door Frame · crackedCRACK ON NLG RT DOOR FRAME AT BS 46. CRACK ON NLG RH DOOR JAMB AT STA 46 APPROX WAS REPAIRED IAW SRM 53-10-14-2R. NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.Nov 5, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507948Rub Strip · corrodedCORROSION POINTS ON THE RIGHT WING FUEL ACCESS PANEL RUB STRIP 620CT. THE RUBSTRIP WAS REPLACED IAW SRM 57-10-01, REP 3.Nov 4, 2017 · N995AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2017110507941Retainer · corrodedCORROSION ON THE R1 DOOR SEAL RETAINER. THE RETAINER WAS REPLACED IAW SRM 51-41-01 AND DWG 5910084, REV EP.Nov 4, 2017 · N995AT · Boeing 717200 · Service DoorsSDR DALA2017110507940Tab · delaminatedDELAMINATED RUDDER TRIM TAB. THE TRIM TAB WAS REPAIRED IAW SRM 51-70-02-2R, PROCEDURE 7, PARAGRAPH 4 B.Nov 4, 2017 · N995AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2017051503867Battery Pack · dischargedEMERG ESCAPE LIGHT INOP BY C1 DOOR. REPLACED BATTERY PACK B5-235 REF AMM 33-51. OPS CHECK GOOD. OK FOR SERVICE.May 14, 2017 · N995AT · Boeing 717200 · Emergency LightingSDR DALA2017072305663Skin · damagedDURING C CHECK, MAINTENANCE REPORTED DAMAGE TO THE UPPER EDGE OF THE LOWER FIXED LEADING EDGE PANEL COMMON TO THE ZFS=52 SPLICE STRAP. ON THE PANEL, ALL FASTENER LOCATIONS WERE BADLY OVERSIZED AND SKIN WASHERS HAD WORN INTO THE SURFACE ON THE LT UPPER AND LOWJan 12, 2016 · N995AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016102607664Fitting · not reportedGIRT BAR FITTING MOUNT. SEE NR FOR ADDITIONAL INFORMATION 027-0015:5310-2005/004 00112. REPLACED FITTINGS PER DWG 3936190.Jan 9, 2016 · N995AT · Boeing 717200 · Fuselage Miscellaneous Structure
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