N929AT

Service difficulty reports · 188

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 = 'N929AT' 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 DALA2021101806407None · noneCORROSION ON LONGERON L-29L AT STA Y=946 AND Y=954, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00244: CORROSION LEVEL 2, LONGERON L-29L AT STA Y=946 AND Y=954 AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #1986109)Oct 17, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021101806406None · noneCORROSION ON LOWER SPLICE OF AFT PRESSURE BULKHEAD ON STA Y=1053 AND L-30, AFT CARGO COMPARTMENT. SUMMARY, CORROSION LEVEL 2: LOWER SPLICE OF AFT PRESSURE BULKHEAD ON STA Y=1053 AND L-30 AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-08-0I, PROCEDURE 2 Oct 16, 2021 · N929AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2021101806405None · noneCORROSION ON LONGERON 30 AND BTW STA Y=954 TO Y=964 UNDER REPAIR SPLICE, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00180: LONGERON 30 OF STA 935 TO 1010 WAS REPAIRED PER B717 SRM 53-20-05-2R. (LP #1981483)Oct 13, 2021 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023051203744Unknown · unknownSOME DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING (AD). ADDL TIME RLTD MON 1972923 ADDED. SUMMARY OF NRC 00161: 57 DENTS ON RIGHT FLAP MOVEABLE AFT VANE RH WING WERE MEASURED WITH A LARGER DIMENSION: DEPTH: 0.015 IN, DIAMETER: 0.599 IN, DIAMETER/DEPTH: 0.599 Oct 5, 2021 · N929AT · Boeing 717200 · Trailing Edge FlapsSDR DALA202012150489Tab · delaminatedTAB WAS DELAMINATED.Dec 15, 2020 · N929AT · Boeing 717200 · Aileron TabsSDR DALA2020081302787Power Supply · inoperativeTHE ENTRY DOOR EMERGENCY LIGHTS WERE NOTICED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IAW B717 AMM 33-51-03. (LP #6964715)Aug 12, 2020 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2020050402339Cable · out of positionMAINTENANCE FOUND THE TAILCONE DEPLOYMENT KEVLAR CABLE TO BE INSTALLED/ROUTED INCORRECTLY. THE CABLE WAS RE-INSTALLED AND ROUTED CORRECTLY IN ACCORDANCE WITH B717 AMM 53-52. THE REQUIRED INSPECTION IS COMPLETE. (LP #6898954)May 2, 2020 · N929AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2024012401105Pan · unknownSRM REPAIR INSPECTION AFT CARGO DOOR JAMB LOWER PAN SPLICE STA 954-994, L-27R LOG-PAGE UPDATED AT 15JAN14. REMOVED AND INSTALLED AFT CARGO DOOR JAMB LOWER PAN THRESHOLD PER B717 SRM 53-20-15-2R PROC 7 PER NRC 107 ON 19FEB19. OK FOR SERVICE. AFT CARGO DOOR JAMBJan 15, 2020 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 2020F00044Tab · delaminatedNON-ROUTINE CHECK UNSCHEDNov 15, 2019 · N929AT · Boeing 717200 · Wing StructureSDR DALA2019081704852Skin · damagedFUSELAGE SKIN DAMAGE AT STA 256, 2 INCHES BELOW L17LT. NRC 011-0001:0514-2001/001 00001: COMPLIED WITH ER/A 580474-14 REV O. ASSOCIATED ER/A 14-580474 ADDED FOR AC 9570. NRC 16: COMPLIED WITH ER/A 580474-14 REV ORIG. PRI 580474-14 REV 0 MATCHES ER/A 580474-14 Aug 16, 2019 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 2019F00175Panel · delaminatedRIGHT INBOARD SPOILER PANEL IS DELAMINATED ON THE LOWER INBOARD PORTION OF THE PANEL.Mar 29, 2019 · N929AT · Boeing 717200 · SpoilersSDR DALA2019022101079Seat Track · corrodedFORWARD GALLEY FLOOR - RIGHT INBOARD SEAT TRACK HAS CORROSION. NRC 001-0213:2561-1001/001 00245: REPLACED PER B717 SRM 53-20-52-2R-5 FIG 201. (LP #0952566)Feb 20, 2019 · N929AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019021901023Threshold · corrodedCORROSION FOUND AT AFT CARGO DOOR THRESHOLD. REPLACED AFT CARGO DOOR JAMB REF SRM 53-20-15-2R PROC 7.Feb 18, 2019 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017073105924Guard · brokenFOUND EMERGENCY LIGHT GUARD SWITCH BROKEN. REPLACED TOGGLE SWITCH GUARD. LP# 3434126Jul 31, 2017 · N929AT · Boeing 717200 · Emergency LightingSDR DALA2017030501766Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA 755 Z=-9 FROM X=O TO X=-53. AS VIEWED FROM RT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI 17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.Mar 4, 2017 · N929AT · Boeing 717200 · Fuel StorageSDR DALA2017030501764Frame · corrodedCORROSION ON FRAME Y=1022 BTW LONG 28L AND 27R AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER SRM 53-20-07 2R-3. HFEC INSPECTION WAS PERFORMED PER NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND ALONG TRIM LINE.Mar 4, 2017 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017030501763Cargo Track · corrodedAFT CARGO COMPARTMENT HAS CORROSION ON RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022. RT TIE TRACK FROM Y=813 TO Y=954, Y=994 TO Y=1022 WAS REPLACED PER SRM 51-41-01 0G.Mar 4, 2017 · N929AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017030501767Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA STA 755 Z=-9 FROM X=O TO X=-53. AS VIEW FROM LT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI-17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.Mar 2, 2017 · N929AT · Boeing 717200 · Fuel StorageSDR DALA2017030301721Rub Strip · corrodedCORROSION ON LEFT UPPER RUBTRIPS BETWEEN BS 775 TO 813 AND BETWEEN BS 579 TO 696. THE RUB STRIPS WERE REPLACED IAW SRM 51-20-05 0G.Mar 2, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017030201699Seat Track · corrodedCORROSION ON INBD & OTBD F.O. SEAT TRACK , ALSO ON FLOOR SUPPORT RBL 54 BTW BS 140 TO 110. REPAIRED IAW ETI-17-17-034 REV. 1 AND ER/A 555629-14 REV.ORIGINAL.Mar 1, 2017 · N929AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017030201687Skin · corrodedCORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BETWEEN BS 760 - 800. CORROSION REMOVED IAW SRM 51-10-04 0G PAR. 26, 21, AND 15. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2.Mar 1, 2017 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017030201686Angle · crackedANGLE CRACKED ON REPAIR ON FWD CARGO BAY BULKHEAD BS 674, LONGERON 24L. REPLACED IAW SRM 51-41-05 AND SRM 51-40-08 0G.Mar 1, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017030101649Angle · corrodedCORROSION ON CUSP ANGLE FROM BS 465 - 470, LONGERON 18R. THE CUSP ANGLE WAS REPAIRED IAW ETI-17-17-028 REV.2, AND ER/A 555636-14 REV. ORIGINAL.Feb 28, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017030101640Door Frame · crackedCRACK IN WEB OF THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB AT 2 HRS POSITION (CPAX). REPAIR WAS ACCOMPLISHED PER INSTRUCTIONS OF ETI 17-17-023 REV 3 AND ER/A 554168-14 REV ORIGINAL.Feb 28, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017030101639Skin · corrodedTO ACCOMPLISH REMOVAL OF CORROSION ON CENTER TANK UPPER SKIN, CUT/REPAIR WEB/ANGLE AS REQUIRED FROM STA Y=727, 737, AND X=0. AREA WAS REPAIRED ON CENTER TANK UPPER SKIN (WEB/ANGLE) FROM STA Y=726, 755, AND X=0 PER 51-70-11 2R, 51-40-02, AND 51-40-05.Feb 28, 2017 · N929AT · Boeing 717200 · Fuel StorageSDR DALA2017030101638Floor Panel · damagedCORROSION ON FLOOR PANELS 222XF AND 222AQF (SM). DUE TO EXCESSIVE DAMAGE FLOOR PANELS WERE REPLACED PER SRM 51-40-08 06 AND DWG 9952521 REV BB.Feb 28, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022801610Beam · crackedFWD R1 DOOR AREA HAS A CRACKED NR 4 BEAM AT FWD EDGE. A NEW BEAM WAS FABRICATED AND REPLACED IAW SRM 51-41-02, 51-41-05,AND DWG 911582 REV T.Feb 27, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017022701570Beam · crackedCRACKED LATERAL BEAM LBL 60- 18 AND RBL 18 IN THE NOSE LANDING GEAR WHEEL WELL. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 53-10-14-2R PROCEDURE 2.Feb 26, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017022701569Seal Depressor · crackedCRACK ON AFT CARGO DOOR FRAME SEAL DEPRESSOR BS 994 BETWEEN LONGERONS 24 AND 25R. THE SEAL DEPRESSOR WAS REPAIRED IAW SRM 53-20-15 2R.Feb 26, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017022701607Rub Strip · corrodedCORROSION ON ACCESS PANEL CUT OUT RUB STRIPS ON THE LT WING THE RUB STRIPS WERE REPLACED IAW SRM 57-10-01 2R PROCEDURE 3.Feb 25, 2017 · N929AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2017022601567Access Panel · corrodedCORROSION ON THE SETTLEMENT AREA OF THE UPPER FUEL ACCESS PANEL OF THE LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 AND SRM 51-22-2A COND. III.Feb 25, 2017 · N929AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017022601566Channel · crackedCRACK ON FLOOR PANEL CHANNEL. REPAIRED IAW SRM 53-20-50 2R-5.Feb 25, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022601564Floorbeam · crackedCRACKED FLOORBEAM, BS 737 RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-01 0G , SRM 51-41-02 0G, AND SRM 51-41-05 0G.Feb 25, 2017 · N929AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017022601563Floor Support · crackedCRACKED FITTING BS 715 LBL 44 FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05 0G.Feb 25, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022501561Intercostal · crackedAFT CARGO DOOR HAD A CRACKED INTERCOSTAL AT AFT CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05 AND DWG 9957665 REV. R.Feb 24, 2017 · N929AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017022501559Intercostal · crackedFWD CARGO BAY HAD A CRACKED INTERCOSTAL BS 636 - 617, BL 0. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00 2, FIGURE 201, AND INSTALLED IAW SRM 51-41-05.Feb 24, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022501558Frame · crackedCRACKED FRAME ANGLE BS 715. THE FRAME WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1.Feb 24, 2017 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017022501557Frame · crackedCRACKED FRAME ANGLE BS 674. THE FRAME ANGLE WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR. 1.Feb 24, 2017 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017022501556Frame · crackedCRACKED FRAME ANGLE BS 696. THE FRAME ANGLE WAS REPAIRED IAW SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1.Feb 24, 2017 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017022501552Pan · crackedCRACKED OTBD PAN IN BEAM NR 5 AT AFT CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02, REPAIR 6, FIG. 201.Feb 24, 2017 · N929AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017022401553Floorbeam · crackedCRACK ON FLOORBEAM BS 715 BETWEEN LBL 22 TO RBL 22. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02.Feb 23, 2017 · N929AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017022401517Intercostal · crackedCRACKED ON LOWER CENTER INTERCOSTALS OF AFT CARGO DOOR. LOWER CENTER INTERCOSTALS WERE REPLACED PER SRM 51-41-02 0G AND 51-41-05 0G.Feb 23, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022401516Floor Panel · crackedCRACK ON COCKPIT FLOOR PANEL 211EF. FLOOR PANEL WAS REPAIRED PER SRM 53-00-00 2R-1.Feb 23, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022401515Floor Panel · crackedCRACKED ON SIDES FLOOR PANELS OF COCKPIT (CAB PILOT). FLOOR PANEL WAS REPAIRED PER SRM 53-00-00 2R-1.Feb 23, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022401514Angle · corrodedCORROSION ON ANGLE AT LWR FWD EDGE. ANGLE WAS REPLACED PER SRM 51-41-02, 51-41-05, AND DWG 9911578 REV H.Feb 23, 2017 · N929AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017022301484Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 160 - 200 BETWEEN LBL 44 AND 54. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-1A, AND 51-30-07-0G FIG 9.J. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08 0G AND SRM 51-30-07 0G FIG. 9(J) AND 19.Feb 22, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022201480Floor Panel · crackedFLOOR PANEL CRACKED. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R.Feb 21, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022201479Floor Support · out of limitsFLOOR SUPPORT BS 160 TO 200, RBL 44 , FOUND OUT OF LIMITS. REPLACED IAW SRM 51-30-07-0G FIG 9.J.Feb 21, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022201478Floor Panel · delaminatedDELAMINATED FLOOR PANEL. REPLACED IAW SRM 53-20-50 2R.Feb 21, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022201476Floorbeam · out of limitsFLOORBEAM BS 180, RBL 7 - 44 WAS FOUND OUT LIMITS. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-07 0G, FIG 9.J, 51-40-08 OG, 51-10-04 0G PAR 21 AND 15, 51-41-02 0G, AND 51-41-05 0G.Feb 21, 2017 · N929AT · Boeing 717200 · Fuselage Main, Floor Beam
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