N124US

Service difficulty reports · 344

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 = 'N124US' 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 AALA202003309019Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR #5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309018Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #6 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309017Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #5 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309016Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #4 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309015Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #3 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309014Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #2 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA202003309013Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE LEFT HAND THRUST REVERSER AFT HINGE ATTACHMENT POINT ON THE PYLON HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ATTACHMENT FITTING PER AMM 54-57-17.Mar 13, 2020 · N124US · Airbus A320214 · Nacelle/Pylon, Attach FittingsSDR AALA202003309012Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE LEFT HAND THRUST REVERSER MIDDLE HINGE ATTACHMENT POINT ON THE PYLON HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE ATTACHMENT FITTING PER AMM 54-57-17.Mar 13, 2020 · N124US · Airbus A320214 · Nacelle/Pylon, Attach FittingsSDR AALA2020033099003Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR #6 HINGE HAS EXCESSIVE PLAY / WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA2020033099002Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42 AND EA 302984.Mar 13, 2020 · N124US · Airbus A320214 · Elevator StructureSDR AALA2020030329007Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL 241KF HAS BUBBLES / DELAMINATED ON UPPER SURFACE. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-002.Mar 1, 2020 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA2020030329006Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL #241FF HAS BUBBLES / DELAMINATION ON UPPER SURFACE. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-002.Mar 1, 2020 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA2020030319018Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR FITTING CRACKED AT FR 28 AND BL 0. REPLACED FLOOR FITTING PER SRM 51-40-02.Feb 29, 2020 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2019122319012O-Ring · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS HYD "G'" RSVR LO LEVEL "G" ECAM. PUMP TURNED OFF WITHIN 5 MINUTES OF ECAM, PUMP RAN APPROX 10 MIN LATER FOR GEAR EXT UNTIL LO LVL MSG REAPPEARED. EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED #1 HYD PUMP DELIVERYDec 20, 2019 · N124US · Airbus A320214 · Hydraulic System, MainSDR AALA2019112759033Apu · leakingAIRCRAFT WAS GROUNDED: PILOT REPORTS CABIN ODOR PERSISTENT FROM TAKE-OFF TO LANDING. MAINTENANCE FOUND OIL LEAK ON APU GEARBOX. SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU IAW JOB CARD 26L31049003. (CLOSED)Nov 24, 2019 · N124US · Airbus A320214 · APU Core EngineSDR AALA201907249011Warning System · false activationAIRCRAFT WAS GROUNDED: PILOT REPORTS MATER CAUTION CAME ON DURING TACKOFF PRIOR TO 80 KNOTS, REJECTED TAKEOFF AND WARNING DISAPPEARED MAX SPEED LESS THAN 90 KNOTS FO REPORTS SEEING ECAM CAUTION MESSAGE SAYING "MAN THR" IN AMBER. MAINTENANCE ACCOMPLISHED REJECTJul 23, 2019 · N124US · Airbus A320214 · Central WarningSDR AALA2019041189003Limiter · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS ON TAKE OFF A SIGNIFICANT RUDDER KICK WAS FELT NOT CAUSED BY WIND GUST, WAKE TURB OR RUDDER INPUT. AFTER LANDING RUD TRL LIMT 1ECAS MSG DISPLAYED. MAINTENANCE REPLACED THE RUDDER TRAVEL LIMITER IAW CARD 26L32527002.Apr 7, 2019 · N124US · Airbus A320214 · Rudder Control SystemSDR AALA201808219014Lens · looseEMERGENCY LIGHT INOPERATIVE. SECURED THE LENS. OPS CHECKED GOOD, OK FOR SERVICE.Aug 20, 2018 · N124US · Airbus A320214 · Emergency LightingSDR AALA201806119056Cylinder · damagedAIRCRAFT IN BASE MAINTENANCE. DURING OPERATIONAL TEST OF PASSENGER CREW DOOR 841 HARD IMPACT BETWEEN THE BUFFER DOOR AND FUSELAGE AT FORWARD GALLEY AREA. REPLACED DOOR DAMPER/CYLINDER ON PASSENGER CREW DOOR 841 PER AMM 52-11-14-400-001-B AND AMM 52-11-14-000-0Jun 8, 2018 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201806069022Slide · deformedDEFORMED SLIDE ON THE PASSENGER DOOR. REPLACED THE SLIDE IAW AMM 25-62-44-400-803-A, AND OPS TESTED OK.Jun 5, 2018 · N124US · Airbus A320214 · Escape SlideSDR AALA2018060869014Slide · deformedDEFORMED SLIDE ON THE PASSENGER DOOR. REPLACED THE SLIDE IAW AMM 25-62-44-400-803-A AND OPERATIONAL TEST OF THE EMERGENCY LIGHTS WAS OK.Jun 5, 2018 · N124US · Airbus A320214 · Escape SlideSDR AALA201806059025Strut · corrodedCORROSION FOUND ON THE INBOARD FLAP HOUSING OF THE INTERCONNECTING STRUT, RIGHT WING. REPLACED THE INTERCONNECTING STRUT.Jun 1, 2018 · N124US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018053089009Strut · corrodedCORROSION ON THE INBOARD FLAP HOUSING OF THE INTERCONNECTING STRUT ON THE LEFT WING. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-400-001, AND OPS TESTED IAW AMM 27-54-00-710-001A. ADJUSTMENT AND OPS TESTED OK.May 25, 2018 · N124US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018053089011Window · scratchedSCRATCH FOUND ON THE PASSENGER DOOR INNER PANE WINDOW. REPLACED THE INNER AND OUTER WINDOW PANE IAW AMM 56-31-13-400-002-A.May 25, 2018 · N124US · Airbus A320214 · Door WindowsSDR AALA2018052989016Seal · cutCUT ON PASSENGER DOOR LINING SEAL AT THE CONTROL HANDLE. REPLACED THE DOOR LINING SEAL IAW AMM 25-23-46-400-002-A, STEPS 3.May 24, 2018 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201805249005Floor Panel · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION FOUND ON FLOOR PANEL 242FF, BETWEEN FR 36 TO FR 42, AND -Y254 TO -Y765. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 FIG 20109; IRM 9701 REV H.May 17, 2018 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018052109002Damper · out of adjustOUT OF ADJUSTMENT DAMPER ON THE PASSENGER DOOR. PERFORMED AN ADJUSTMENT ON THE DAMPER IAW AMM 52-13-14-820-002-A. ADJUSTMENT OK.May 17, 2018 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201806129005Fitting · wornCONTINUITY FITTING BETWEEN FRAMES 1 & 2, Y0 FOUND WORN.May 16, 2018 · N124US · Airbus A320214 · Fuselage Main, StructureSDR AALA201806129004Fitting · wornCONTINUITY FITTING BETWEEN FRAMES 1 TO 2, BL Y0 FOUND WORN.May 16, 2018 · N124US · Airbus A320214 · Fuselage Main, StructureSDR AALA2018051759032Liner · cutCUT ON LINING COVER PASSENGER CREW DOOR SEAL OF THE EMERGENCY CONTROL HANDLE. REPLACED THE LINING IAW AMM 25-23-46-400-001-A STEP 4.A.May 11, 2018 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR AALA2018051759008Liner · cutCUT ON COVER LINING OF THE PASSENGER DOOR SEAL, EMERGENCY CONTROL HANDLE. REPLACED THE COVER LINING IAW AMM 25-23-46-400-001-A STEP 4.A.May 11, 2018 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201806129007Window Frame · crackedCRACK INDICATION ON THE LEFT SIDE WINDSHIELD FRAME CENTER POST AT FRAME 1, Y0. REPLACED THE WINSHIELD FRAME IAW EA 270378.May 8, 2018 · N124US · Airbus A320214 · Fuselage Main, StructureSDR AALA201805249025Slat Track · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON SLAT TRACK 12 LOWER MID BOLT ON RIGHT HAND WING. REPLACED LOWER MID SLAT BOLT ON TRACK 12 PER AMM 27-84-67.May 7, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA201805189008Bolt · corrodedCORROSION FOUND ON AFT LOWER SLAT TRACK 11 BOLT, RT WING RWS 12277 TO 12870, BETWEEN RIBS 23 TO 24. REPLACED THE BOLT IAW AMM 27-84-67-000-001-A, AND AMM 27-84-67-400-001-A.May 7, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA201806119011Access Panel · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON THE FUEL ACCESS PANEL 640EB LOCATED BETWEEN STA 5512 - 6132. REPLACED ACCESS PANEL PER AMM 57-27-11.May 5, 2018 · N124US · Airbus A320214 · Wing, Plate/SkinSDR AALA201806119010Access Panel · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON FUEL ACCESS PANEL 640AB BTW STA 700 TO STA 1957 AND BETWEEN RIB 2 TO RIB 4. REPLACED ACCESS PANEL PER AMM 57-27-11.May 5, 2018 · N124US · Airbus A320214 · Wing, Plate/SkinSDR AALA201806119009Access Panel · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON FUEL ACCESS PANEL 640CB LOCATED BETWEEN STA 4067- 4862 AND BETWEEN RIB 8- 19. REPLACED ACCESS PANEL PER AMM 57-27-11.May 5, 2018 · N124US · Airbus A320214 · Wing, Plate/SkinSDR AALA2018052989006Bolt · corrodedCORROSION FOUND ON LOWER SLAT TRACK BOLT 7, LEFT WING. REPLACED THE SLAT BOLT IAW AMM 27-84-65.May 5, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA201805189009Bolt · corrodedCORROSION FOUND ON THE AFT LOWER SLAT TRACK 4 BOLT, RWS 2580 - 3059, BETWEEN RIBS 5 TO 6. REPLACED THE BOLT IAW AMM 27-84-63-000-001-A, AND AMM 27-84-63-400-001-A.May 5, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA2018051749012Bolt · corrodedCORROSION FOUND ON THE SLAT TRACK NR 9 FORWARD BOLT ON LEFT WING. REPLACED THE BOLT IAW AMM 27-84-66.May 5, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA2018051649023Bolt · corrodedCORROSION FOUND ON SLAT TRACK NR 12, LOWER FORWARD BOLT ON THE LEFT WING. REPLACED THE BOLT IAW AMM 27-84-67-000-001-A, AND AMM 27-84-67-400-001.May 5, 2018 · N124US · Airbus A320214 · Leading Edge DevicesSDR AALA2018051749026Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 211FF IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, PARA 2A, FIGURE 20106, AND IRM 9701.May 4, 2018 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA201805149051Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 211EF BETWEEN FR 6 TO FR 9, LBL Y254 TO LBL Y765 IN COCKPIT. REPLACED FLOOR PANEL 211EF PER SRM 53-12-00-300-006 FIGURE 20106 AND IRM 9701 REVISION H.May 4, 2018 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA201805289002Seat Track · wornAIRCRAFT IN BASE MAINTENANCE. WEAR ON SEAT TRACK BETWEEN FR 32 TO FR 33, LBL Y765 IN PASSENGER CABIN. REPAIRED SEAT TRACK PER SRM 51-72-11 AND DRAWING D53231730.May 3, 2018 · N124US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201806059008Stop Fitting · crackedA CRACK WAS INDICATED ON THE STOP FITTING NR 7 AT FRAME 20. REPLACED THE STOP FITTING IAW SRM 51-72-11, AND DRAWING D53112331.May 2, 2018 · N124US · Airbus A320214 · Fuselage Main, StructureSDR AALA201806059014Intercostal · crackedA CRACK INDICATION WAS FOUND ON THE INTERCOSTAL, FRAME 16, FROM LOWER INBOARD HOLE OF DOOR STOP FITTING NR 7. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11, AND DRAWING 53112300.May 2, 2018 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201805249023Support · corrodedCORROSION FOUND ON THE LOWER SUPPORT, STRINGER 23L, FRAME 66. REPAIRED THE SUPPORT IAW SRM 53-41-14-300-001.May 2, 2018 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201805249027Stringer · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 56-57 IN AFT CARGO COMPARTMENT. REPLACED STRINGER 43L PER SRM 51-72-11 AND DRAWING D53470345.Apr 29, 2018 · N124US · Airbus A320214 · Fuselage Main, Longeron/StringerSDR AALA201805189010Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK LOCATED BETWEEN FRAMES 12 TO 24, -Y765. REPLACED THE SEAT TRACK IAW IAW SRM 51-72-11 AND DRAWING 53112812.Apr 29, 2018 · N124US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201806119008Plate · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CRACK FOUND ON PLATE LOCATED FR 69 AND 23R. REPLACED PLATE PER SRM A320 51-42-11 DWG D53474180.Apr 28, 2018 · N124US · Airbus A320214 · Fuselage Miscellaneous Structure
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