N712US

Service difficulty reports · 341

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 = 'N712US' 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 AALA201706089048Bolt · corrodedCORROSION ON RIGHT WING SLAT TRACK NR 11 ECCENTRIC BOLT. REPLACED SLAT TRACK BOLT IAW AMM 27-84-67.Jun 3, 2017 · N712US · Airbus A319112 · Leading Edge DevicesSDR AALA201706089047Bolt · corrodedCORROSION ON RIGHT WING SLAT TRACK NR 10 UPPER FORWARD BOLT AT RIB 21. REPLACED SLAT TRACK BOLT IAW AMM 27-84-66.Jun 3, 2017 · N712US · Airbus A319112 · Leading Edge DevicesSDR AALA201706029007Seal · tornTORN EMERGENCY EXIT DOOR SEAL. REPLACED EMERGENCY EXIT DOOR SEAL.Jun 1, 2017 · N712US · Airbus A319112 · Emergency ExitsSDR AALA201706029006Door · damagedTORN SEAL EMERGENCY EXIT DOOR. REPLACED EMERGENCY EXIT DOOR.Jun 1, 2017 · N712US · Airbus A319112 · Emergency ExitsSDR AALA201706019026Attach Fitting · wornWEAR ON THE PAX DOOR ON SLIDE RAFT FITTING AT FOWARD GALLEY AREA. REPLACED FITTINGS.May 31, 2017 · N712US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201706279014Slat · not reportedAIRCRAFT IN BASE MAINTENANCE. REPAIR NEEDED ON RIGHT HAND WING INBOARD LEADING EDGE ON SLAT NR 3 AT RIB 7 MINUS 24 INCHES. REPAIRED SLAT NR 3 PER SRM 57-40-00-300-091 FIGURE 20106.May 30, 2017 · N712US · Airbus A319112 · Leading Edge DevicesSDR AALA201706159025Fitting · corrodedCORROSION ON R1 DOOR SILL UNDER BOTH FORWARD AND AFT GIRT BAR FITTINGS AT STRINGER 23R BETWEEN FRAMES 16 AND 20. REPLACED THE FITTINGS IAW SRM 51-72-11, AND DRAWING D53110339.May 30, 2017 · N712US · Airbus A319112 · Fuselage Main, Attach FittingsSDR AALA201706159013Door Sill · corrodedCORROSION ON L1 DOOR SILL PLATE IN TWO SPOTS UNDER FORWARD GIRT BAR FITTING PLATE. REPLACED SILL PER SRM A319 51-72-11.May 30, 2017 · N712US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201706069034Skin · damagedWHILE REPLACING A BLIND FASTENER ON FUSELAGE SKIN, MAINTENANCE FOUND FASTENER HOLE WAS DRILLED INTO CENTER FLANGE OF STRINGER 23L, BETWEEN FRAMES 65 AND 66. REPAIRED THE SKIN IAW EA #111496C.May 30, 2017 · N712US · Airbus A319112 · Fuselage Main, Plate/SkinSDR AALA201706069030Floor Support · corrodedCORROSION ON AFT GALLEY FLOOR SUPPORT Y1450, STRINGER 23L, BETWEEN FRAME 65 AND 66. REPLACED THE FLOOR SUPPORT SRM 51-42-11, AND DRAWING D53472035.May 30, 2017 · N712US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201706089044Fitting · corrodedCORROSION ON AFT GALLEY CORNER FITTING, STRINGER 23L, FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11 AND DRAWING D53480505.May 28, 2017 · N712US · Airbus A319112 · Fuselage Main, Longeron/StringerSDR AALA201706089046Bearing · wornAIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON RIGHT ELEVATOR HINGE ARM NR 6 BEARING AT RIB 13. REPLACED HINGE FITTING ASSEMBLY PER AMM 55-16-42.May 27, 2017 · N712US · Airbus A319112 · Elevator StructureSDR AALA201706269002Attach Fitting · crackedAIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON FORWARD POSITION KEELBEAM RIGHT HAND MAIN LANDING GEAR DOOR FORWARD ATTACH FITTINGS IN MAIN WHEEL WELL AT FR 43 AND -Y251. REPLACED DOOR ATTACHMENT FITTING PER SRM 51-72-11 AND EA 270816.May 26, 2017 · N712US · Airbus A319112 · Main Landing Gear Attach SectionSDR AALA201706269004Attach Fitting · damagedELONGATED HOLES ON LEFT MAIN LANDING GEAR DOOR FORWARD ATTACH FITTINGS IN MAIN WHEEL WELL AT STRINGER 41L, FRAME 42, AND Y254. REPLACED THE ATTACH FITTING IAW SRM A319 51-72-11, AND EA 270816.May 26, 2017 · N712US · Airbus A319112 · Landing Gear DoorsSDR AALA201706159023Shear Tie · corrodedCORROSION ON FORWARD CARGO BAY SHEAR TIE AT FRAME 27, STRINGER 43L. REPLACED THE SHEAR TIE IAW SRM , AND DRAWING D53233523.May 25, 2017 · N712US · Airbus A319112 · Fuselage Internal Mounting StructureSDR AALA201706269024Door Frame · crackedCRACKED ON DOOR FRAME, REMOVED AND REPLACED IAW SRM A319-51-72-11 AND EO 5210Y228.May 23, 2017 · N712US · Airbus A319112 · Fuselage Main, StructureSDR AALA201706269008Beam · crackedCRACK ON PASSENGER CABIN, EMERGENCY EXIT DOOR BEAM 1 BETWEEN FRAMES 40 AND 41. REPAIRED IAW EO 5210Y228.May 23, 2017 · N712US · Airbus A319112 · Fuselage Main, StructureSDR AALA201706269007Structure · crackedCRACK ON PASSENGER CABIN EMERGENCY EXIT DOOR SEGMENT BETWEEN BEAMS 1 AND 3 AT FR 40, REPAIRD IAW EO 5210Y228.May 23, 2017 · N712US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201706269006Beam · crackedCRACK ON EMERGENCY EXIT DOOR BEAM 2 AT FRAME 40, LOCATED AT RIGHT LOAD TRANSMITTING PROFILE. REPAIRED IAW EO # 5210Y228.May 23, 2017 · N712US · Airbus A319112 · Emergency ExitsSDR AALA201706269005Beam · crackedCRACK ON PASSENGER CABIN, INTERNAL STRUCTURE, EMERGENCY EXIT DOOR BEAM 2 AT FRAME 41, LOCATED AT RIGHT LOAD TRANSMITTING PROFILE. REPAIRED IAW EO 5210Y228.May 23, 2017 · N712US · Airbus A319112 · Emergency ExitsSDR AALA201706219012Floor Panel · crackedA CRACK WAS FOUND ON THE PASSENGER CABIN FLOOR PANEL 241HF, BETWEEN Y1292 AND Y1732, FRAMES 36 AND 41. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.May 23, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706199010Floor Panel · delaminatedDELAMINATION FOUND ON THE PASSENGER CABIN FLOOR PANEL 241MF BETWEEN FRAMES 42 AND 47. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701, REVISION G.May 23, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706199009Floor Panel · crackedCRACK ON THE PASSENGER CABIN FLOOR PANEL 232AH, -Y129 AND -Y1732, BETWEEN FRAMES 28 AND 35. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, AND IRM 9701 REVISION G.May 23, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706199007Door Frame · crackedA CRACK INDICATION ON AFT GALLEY DOOR FRAME 68, BETWEEN STRINGERS 22L AND 23L. REPAIRED THE DOOR FRAME IAW SRM 53-41-12-300-010.May 23, 2017 · N712US · Airbus A319112 · Fuselage Main, StructureSDR AALA201706159022Bolt · corrodedCORROSION ON LEFT WING SLAT TRACK 11 FORWARD BOLT BETWEEN RIBS 23 AND 24. REPLACED THE BOLT IAW AMM 27-84-67.May 23, 2017 · N712US · Airbus A319112 · Leading Edge DevicesSDR AALA201706099022Floor Panel · delaminatedDELAMINATION ON PASSENGER CABIN FLOOR PANEL 252HG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.May 23, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706069024Slat Track · damagedMISSING MATERIAL ON SLAT TRACK NR 9 AT INBOARD LUG ON LEFT WING. REPAIRED THE SLAT TRACK IAW SRM 57-40-00.May 23, 2017 · N712US · Airbus A319112 · Leading Edge DevicesSDR AALA201706279017Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 232DF. REPLACED FLOOR PANEL PER EA 270826 AND AMM 53-12-12-400-001-A.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706279015Flap · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION IS ON LEFT HAND OUTBOARD FLAP, INTERNAL AREA, BETWEEN RIB 9 AND 22. REPLACED FLAP PER JOB CARD 26L00027009.May 21, 2017 · N712US · Airbus A319112 · Trailing Edge FlapsSDR AALA201706199011Floor Panel · delaminatedDELAMINATION FOUND ON THE FORWARD GALLEY FLOOR PANEL 231CF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00, AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706199008Seat Track · corrodedCORROSION ON THE FORWARD GALLEY SEAT TRACK AT -Y1292 AND FRAME 20. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWING D53112782, AND D53112812-D53110984.May 21, 2017 · N712US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201706199006Splice · corrodedCORROSION ON FORWARD GALLEY SPLICE AT -Y765 AND FRAME 24. REPLACED SPLICE IAW SRM 51-42-11 AND DRAWING D53112812.May 21, 2017 · N712US · Airbus A319112 · Fuselage Main, StructureSDR AALA201706199005Seat Track · corrodedCORROSION ON FORWARD GALLEY SEAT TRACK AT -Y765 BETWEEN FRAMES 20 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING D53112812.May 21, 2017 · N712US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201706199003Floor Panel · delaminatedDELAMINATION ON THE FORWARD GALLEY FLOOR PANEL 221EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706199002Floor Panel · delaminatedDELAMINATION ON THE AFT GALLEY FLOOR PANEL 261DF. REPLACED THE FLOOR PANEL IAW AMM 53-42-12-400-002-A.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706159015Skin · damagedTRAPPED WATER INDICATION ON ELEVATOR UPPER SKIN OF RIGHT HORIZONTAL STABILIZER BETWEEN RIB 5 AND 6, AT 7.60 INCHES INBOARD FROM RIB 5 AND 4.0 INCHES FROM TRAILING EDGE. REPAIRED THE UPPER SKIN IAW SRM 55-21-11-300-004.May 21, 2017 · N712US · Airbus A319112 · Elevator, Plate/SkinSDR AALA201706159012Floor Panel · delaminatedDELAMINATION FOUND ON THE AFT GALLEY FLOOR PANEL 262HG. REPLACED THE FLOOR PANEL IAW AMM 53-42-12-400-002.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706099024Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 221PF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706099023Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 221DF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706099021Floor Panel · delaminatedDELAMINATION ON AFT GALLEY FLOOR PANEL 261AG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706099020Insert · delaminatedDELAMINATION ON AFT GALLEY FLOOR PANEL INSERT OF FLOOR PANEL 261BG. REPLACED FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706089049Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 221LF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706089045Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706089043Floor Panel · delaminatedDETERIORATED AND DELAMINATED TOP LAYER OF FORWARD GALLEY FLOOR PANEL 232FF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706089042Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 232EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706089041Seat Track · corrodedCORROSION ON FORWARD GALLEY SEAT TRACK AT Y1292, FRAME 15 PLUS 10 INCHES. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53112812.May 21, 2017 · N712US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201706069033Floor Panel · delaminatedDELAMINATION ON AFT GALLEY FLOOR PANEL 261PF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00 AND IRM 9701 REVISION G.May 21, 2017 · N712US · Airbus A319112 · Fuselage Floor PanelSDR AALA201706069031Web · corrodedCORROSION ON FORWARD GALLEY WEB AT STRINGER 23R, FRAME 20. REPLACED THE WEB IAW SRM 51-72-11, AND DRAWING D53114392.May 21, 2017 · N712US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201706029021Floor Support · corrodedCORROSION ON FORWARD GALLEY SEAT TRACK AT Y765 BETWEEN FRAMES 12 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS D53112813, D53110984, AND D53112812.May 21, 2017 · N712US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201706279016Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY SHEAR PLATE AT STRINGER 23L BETWEEN FR 69 AND FR 70. REPLACED SHEAR PLATE PER SRM 51-42-11 AND 51-72-11, DWG 53474180.May 20, 2017 · N712US · Airbus A319112 · Fuselage Miscellaneous Structure
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