N730US

Service difficulty reports · 285

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 = 'N730US' 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 AALA201709299016Fitting · wornWEAR ON LOWER CUTOUT FORWARD CARGO BAY LOCK FITTING AT FRAME 25 PLUS 10 INCHES. REPLACED THE LOCK FITTING IAW SRM 51-72-11 AND DRAWING D53231685.Sep 22, 2017 · N730US · Airbus A319112 · Fuselage Main, Attach FittingsSDR AALA201710019010Pin · wornWEAR ON MAIN LANDING GEAR RETRACTION ACTUATOR PIN AT RIB 5. REPLACED RETRACTION ACTUATOR PIN IAW AMM 32-31-46-400-002-A.Sep 21, 2017 · N730US · Airbus A319112 · Landing Gear ActuatorSDR AALA201709299020Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND DURING AN 2S CHECK. REPLACED THE SEAT TRACK AT Y1292 BETWEEN FRAMES 36 - 41 IAW SRM 51-72-11, DRAWINGS D53370382 AND D57133491.Sep 21, 2017 · N730US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201709299019Seat Track · corrodedCORROSION FOUND DURING AN 2S CHECK IAW 3-15-12. REPLACED THE SEAT TRACK.Sep 21, 2017 · N730US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201709229009Slide · deterioratedDETERIORATED RT OVERWING ESCAPE SLIDE ENCLOSURE COMPOUND. REMOVED AND REPLACED ESCAPE SLIDE IAW AMM.Sep 21, 2017 · N730US · Airbus A319112 · Escape SlideSDR AALA201709219010Mechanism · out of adjustOUT OF ADJUSTMENT PASSENGER CREW DOOR. BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM AT FWD GALLEY AREA PERFORMED ADJUSTMENT OF THE PAX DOOR IAW AMM.Sep 20, 2017 · N730US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201709199010Control Handle · out of toleranceWEAR ON HOOK INNER CONTROL HANDLE OF DOOR AT FWD GALLEY AREA. REPLACED INNER CONTROL HANDLE IAW AMM.Sep 14, 2017 · N730US · Airbus A319112 · DoorsSDR AALA201709149003Bellcrank · out of adjustOUT OF ADJUSTMENT TORSION BAR BELLCRANK ON THE PAX DOOR. ADJUSTED THE TORSION BAR BELLCRANK IAW AMM.Sep 13, 2017 · N730US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201709149002Bellcrank · out of adjustOUT OF ADJUSTMENT TORSION BAR BELLCRANK ON THE PASSENGER CREW DOOR.Sep 13, 2017 · N730US · Airbus A319112 · Passenger/Crew DoorsSDR AALA201710019004Hinge Pin · wornAIRCRAFT IN BASE MAINTENANCE. WEAR ON RIGHT HAND WING SPOILER NR 1 CENTER FITTING OUTBOARD HINGE PIN (BOLT). REPLACED HINGE PIN (BOLT) ASSEMBLY PER AMM 27-64-41.Sep 12, 2017 · N730US · Airbus A319112 · SpoilersSDR AALA201710019002Hinge Pin · wornAIRCRAFT IN BASE MAINTENANCE. WEAR ON RIGHT HAND WING SPOILER #1 CENTER FITTING INBOARD HINGE PIN (BOLT). REPLACED HINGE PIN (BOLT) ASSEMBLY PER AMM 27-64-41.Sep 12, 2017 · N730US · Airbus A319112 · SpoilersSDR AALA201709129017Hook · wornWEAR ON HOOK INNER CONTROL HANDLE PASSENGER CREW DOOR 831. REPLACED HOOK INNER CONTROL HANDLE.Sep 11, 2017 · N730US · Airbus A319112 · Emergency ExitsSDR AALA201710099026Hinge Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE. WEAR ON NOSE LANDING GEAR LEFT HAND AFT DOOR, AFT HINGE FITTING AT YT449 AND FRAME 20. REPLACED THE HINGE FITTING IAW CMM 52-82-32-400-802, AND 51-72-11.Sep 10, 2017 · N730US · Airbus A319112 · Fuselage, Door HingeSDR AALA201710099024Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. WEAR ON NOSE LANDING GEAR LEFT AFT DOOR FORWARD HINGE FITTING AT YT499 AND FRAME 18. REPLACED THE HINGE FITTING IAW CMM 52-82-32-400-805, AND SRM 51-72-11.Sep 10, 2017 · N730US · Airbus A319112 · Fuselage, Door HingeSDR AALA201709249002Bolt · corrodedCORROSION ON THE LEFT WING MID FORWARD SLAT TRACK NR 2 BOLT BETWEEN RIBS 2 AND 3. REPLACED SLAT TRACK BOLT IAW AMM 27-84-63.Sep 10, 2017 · N730US · Airbus A319112 · Leading Edge DevicesSDR AALA201710019005Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING SLAT NR 4 SLAT TRACK NR 9 UPPER BOLT. REPLACED UPPER BOLT PER AMM 27-84-66.Sep 9, 2017 · N730US · Airbus A319112 · Leading Edge DevicesSDR AALA201709299022Floor Panel · delaminatedDELAMINATION ON THE COCKPIT FLOOR PANEL 212EF. REPLACED THE FLOOR PANEL.Sep 9, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709289017Bolt · corrodedCORROSION ON THE RIGHT WING NR 4 SLAT TRACK BOLT. REPLACED LOWER BOLT IAW AMM 27-84-66.Sep 9, 2017 · N730US · Airbus A319112 · Leading Edge DevicesSDR AALA201709249003Floor Panel · delaminatedDELAMINATION ON COCKPIT FLOOR PANEL 211EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.Sep 9, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709289014Hinge Pin · corrodedCORROSION ON THE RIGHT WING AILERON HINGE PIN BETWEEN RIBS 23 AND 24. REPLACED THE HINGE PIN NR 2 IAW AMM 27-14-41.Sep 8, 2017 · N730US · Airbus A319112 · AileronsSDR AALA201709249008Floor Panel · delaminatedDELAMINATION ON PASSENGER CABIN FLOOR PANEL 241GF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011 AND IRM 9701 REVISION G.Sep 8, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709249007Floor Panel · delaminatedDELAMINATION ON FWD CARGO BAY FLOOR PANEL 131AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.Sep 8, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709249006Floor Panel · delaminatedDELAMINATION ON PASSENGER CABIN FLOOR PANEL 241AF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.Sep 8, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709249005Floor Panel · delaminatedDELAMINATION ON PASSENGER CABIN FLOOR PANEL 241JF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.Sep 8, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201710019006Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD GALLEY DUMMY RAIL AT Y503.2 AND FR 16. REPLACED DUMMY RAIL PER SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201710019003Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND AFT GALLEY FLOOR BEAM AT -Y465 AND FR 65 PLUS 18 INCHES. REPLACED BEAM ASSEMBLY PER SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA201710019008Fitting · corrodedCORROSION ON AFT GALLEY CORNER FITTING AT STRINGER 23R AND FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Main, Attach FittingsSDR AALA201710019007Support · corrodedCORROSION ON LEFT AFT GALLEY LOWER SUPPORT AT STRINGER 23L AND FRAME 68. REPLACED THE SUPPORT SRM 51-72-11, DRAWING D53480505 AND D 53-41-14.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Main, StructureSDR AALA201710019014Splice · corrodedCORROSION ON AFT GALLEY OUTBOARD UPPER SPLICE AT STRINGER 23L AMD FRAME 66. REPLACED THE SPLICE SRM SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201710019013Splice · corrodedCORROSION ON INBOARD UPPER SPLICE AT STRINGER 23L, FRAME 66. REPLACED THE SPLICE IAW SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201710019012Support · corrodedCORROSION ON AFT GALLEY LOWER SUPPORT AT STRINGER 23L AND FRAME 68. REPLACED LOWER SUPPORT IAW SRM 51-72-11.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201709299021Floor Panel · delaminatedDELAMINATION ON THE AFT GALLEY FLOOR PANEL 261BG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709289016Floor Support · corrodedCORROSION ON AFT GALLEY FLOOR SUPPORT AT Y765 AND FRAME 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53472780.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201709289015Floor Support · corrodedCORROSION FOUND ON THE AFT GALLEY FLOOR SUPPORT FRAME 66 PLUS 15.5 INCHES. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472780.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201709289013Floor Support · corrodedCORROSION ON AFT GALLEY FLOOR SUPPORT AT STRINGER 23L AND Y765, FRAME 64 PLUS 9 INCHES. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472815.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201709249009Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 221PF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709249004Floor Panel · delaminatedDELAMINATION ON FORWARD GALLEY FLOOR PANEL 231BF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201709249001Floor Panel · delaminatedDELAMINATION ON THE FORWARD GALLEY FLOOR PANEL 231EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701, REVISION G.Sep 7, 2017 · N730US · Airbus A319112 · Fuselage Floor PanelSDR AALA201710099035Frame · crackedA CRACK INDICATION ON AFT GALLEY FRAME 68 AT STRINGER 8R, AFT FACE BEND RADIUS . REPAIRED THE FRAME IAW EA 273276A.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage Main, FrameSDR AALA201710099034Frame · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON AFT GALLEY FRAME 68 AT STRINGER 8L, AFT FACE BEND RADIUS. REPAIRED THE FRAME IAW EA 273274.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage Main, FrameSDR AALA201710099032Window Frame · crackedA CRACK INDICATION ON COCKPIT WINDSHIELD CUTOUT CENTER POST LEFT FITTING. REPAIRED IAW EA 273392.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage Main, StructureSDR AALA201710049028Seat Track · corrodedCORROSION ON FORWARD GALLEY SEAT TRACK -Y1292, BETWEEN FRAMES 17 AND 24. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53112812.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201710019001Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY FLOORBEAM AT -Y765 AND FR 68 PLUS 1 INCH. REPLACED FLOORBEAM PER SRM 51-72-11 AND DRAWING D53472093.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA201710039026Hinge Fitting · wornEXCESSIVE PLAY ON HINGE ARM NR 5 FORK END FITTING ON VERTICAL STABILIZER AT RIB 8. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Vertical StabilizerSDR AALA201710039025Hinge Fitting · wornEXCESSIVE PLAY ON HINGE ARM NR 2 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 3. REPLACED THE HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Vertical StabilizerSDR AALA201710039024Hinge Fitting · wornEXCESSIVE PLAY, LOOSE BEARING, HINGE ARM NR 4 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 6. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-400-001-A, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Vertical StabilizerSDR AALA201710039023Hinge Fitting · wornEXCESSIVE PLAY, LOOSE BEARING ON HINGE ARM NR 1 FITTING ASSEMBLY FORK END ON VERTICAL STABILIZER AT RIB 2. REPLACED HINGE ARM FITTING AMM 55-36-41-0401, AND SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Vertical StabilizerSDR AALA201710019009Web · corrodedCORROSION ON FORWARD GALLEY WEB AT FRAME 20 AND STRINGER 23R. REPLACED THE WEB IAW SRM 51-72-11, AND DRAWING D53114332.Sep 6, 2017 · N730US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA201710019011Hinge Arm · wornEXCESSIVE PLAY ON FITTING ASSEMBLY FORKED END LOOSE BEARING HINGE ARM 7. REPLACED HINGE ARM PER AMM 55-36-41-0401 AND SRM A319 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Wing StructureSDR AALA201709299023Structure · crackedCRACK ON SECTION CONNECTION, RIGHT AFT POSITION ON BELLY FAIRING AT STRINGER 42R, BETWEEN FRAME 40 AND 42. REPLACED SECTION CONNECTION IAW SRM 51-72-11.Sep 6, 2017 · N730US · Airbus A319112 · Aerodynamic Fairings
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