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 AALA201604229007Fan · defectiveAIRCRAFT WAS GNDED. ON FINAL DESCENT, A STRONG SMOKE & BURNING PLASTIC SMELL IN THE COCKPIT WAS REPORTED BY THE FLIGHT CREW. FOUND THAT THE AVIONICS BLOWER FAN 20HQ HAD AN ELEC SMELL & WAS VERY NOISY RESULTING IN THE REPLACEMENT OF THE FAN IAW AMM 21-26-51-0Apr 21, 2016 · N124US · Airbus A320214 · Air Distribution FanSDR AALA201511169014Skin · saturatedC11 CHECK, LEFT ELEVATOR HAS EVIDENCE OF WATER INGRESS IN 3 AREAS, BETWEEN 15" & 25" FROM THE INBD EDGE & 7" & 13" FROM THE TE.Nov 14, 2015 · N124US · Airbus A320214 · Elevator, Plate/SkinSDR AALA201511119008Skin · saturatedC11 CHECK, LT ELEVATOR UPPER SURFACE SKIN HAS AREA WITH WATER INGRESS, 20" FWD OR THE TE & 99.5" FROM THE INBD END. REPAIRED IAW SRM 55-21-11-201 PARAGRAPH 5E.Nov 10, 2015 · N124US · Airbus A320214 · Elevator, Plate/SkinSDR AALA201510029011Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 151GF HAS DELAMINATION. REPLACED FLOORBOARD IAW AMM 53-42-14-400-001-A.Oct 1, 2015 · N124US · Airbus A320214 · Fuselage Floor PanelSDR AALA201507089004Brake Assy · brokenNUMBER 1 BRAKE ASSEMBLY BROKEN APART. MAIN WHEEL STUCK ON BRAKE. R & R NR 1 BRAKE ASSEMBLY IAW AMM 32-42-27.Jul 7, 2015 · N124US · Airbus A320214 · BrakeSDR USAA2015021500004Girt Bar · lack of lubeFLIGHT ATTENDANT REPORTS 2R SLIDE DISARM & ARM. CLEANED & LUBED 2R DOOR SLIDE GIRT BAR & FLOOR FITTINGS IAW AMM 52-13-22.Feb 13, 2015 · N124US · Airbus A320214 · Emergency EquipmentSDR USAA2014111800004Arming Lever · dirtyFLIGHT ATTENDANT REPORTS ARMING LEVER AT 2R DOOR HARD TO OPERATE. CLEAN & LUBE ARMING LEVER ON 2R DOOR. OPERATES GOOD, OK TO SERVICE IAW AMM 52-13-22 PAGE 501.Nov 17, 2014 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2014111200002Cover · missingCOVER MISSING ON EMER EXIT LIGHT ON SEAT RAIL 1C. REPLACED MISSING COVER. OK FOR SERVICE.Nov 11, 2014 · N124US · Airbus A320214 · Emergency LightingSDR USAA2014091100010Lens · missingLENS COVER MISSING FROM SEAT 1C EMER LIGHT. INSTALLED EMER LIGHT LENS AT SEAT 1C.Sep 10, 2014 · N124US · Airbus A320214 · Emergency LightingSDR USAA2014071000003Battery · dischargedFLASHLIGHT UNDER FWD FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. REPLACED FLASHLIGHT BATTERY AT FWD FLIGHT ATTENDANT JUMP SEAT.Jul 9, 2014 · N124US · Airbus A320214 · Emergency EquipmentSDR USAA2014061900011Slide Raft · bulgedPERFORMING ENGINEERING ORDER 2514Y110 FOUND CONTACT BETWEEN THE SLIDE RAFT COVER AT DOOR L2 & THE FUSELAGE. NO DAMAGE FOUND. PLACED ON MONITOR, INSPECT EVERY 100 HRS, REPLACED SLIDE AT NEXT HEAVY CHECK. REPLACED DOOR L2 ESCAPE SLIDE & RAFT IAW JOB CARD 26L0Jun 18, 2014 · N124US · Airbus A320214 · Escape SlideSDR USAA2014061600035Reservoir · brokenLEFT SLIDE RESERVOIR CABLE END BROKE OFF. R & R LT SLIDE RESERVOIR IAW AMM 25-62-46.Jun 16, 2014 · N124US · Airbus A320214 · Emergency EquipmentSDR USAA2014052700041Battery · dischargedAFT LT FLASHLIGHT INOPERATIVE. REPLACED AFT LT FLASHLIGHT BATTERY.May 26, 2014 · N124US · Airbus A320214 · Emergency EquipmentSDR USAA2014042800001Door · dirtyAFT RT DOOR WILL NOT ARM. REMOVED DEBRIS FORM UNDER AFT RT DOOR.Apr 27, 2014 · N124US · Airbus A320214 · Service DoorsSDR USAA2014041100009Generator · inoperativeRETURN TO FIELD AFTER APU GENERATOR DROPPED OFF LINE IN FLIGHT, IDG WAS ALREADY ON MEL. REPLACED APU GENERATOR IAW AMM 24-33-51. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD.Apr 9, 2014 · N124US · Airbus A320214 · AC Generator-AlternatorSDR USAA2014032600006Power Supply · inoperativeEMERGENCY LIGHT MOUNTED ON SEATS ROW 3, 7, 15, 20, 24 & 26 ARE NOT ILLUMINATING WHEN TESTED. REPLACED EPSU 11WL, OPERATIONS CHECKED NORMAL IAW AMM 33-51-38-000-001-A.Mar 25, 2014 · N124US · Airbus A320214 · Emergency LightingSDR USAA2014020300028Wire Harness · damagedAUTO BRAKE FAILED DURING LANDING ROLLOUT, BRAKE RELEASED. NR 4 TACH WIRING FOUND DAMAGED. REPLACED DAMAGED CONDUIT SUB ASSEMBLY, BRAKE FAN, & NR 4 TACHOMETER WIRING IN RLG HARNESS IAW CMM 32-12-28, WDM 32-11-02, & ESPM 20-52-21 22.Feb 1, 2014 · N124US · Airbus A320214 · Landing Gear System WiringSDR USAA2014012100001Door · obstructedDOOR 2R INDICATES OPEN WHEN DOOR CLOSED. REMOVED TRASH FROM DOOR 2R SILL, OPERATIONS CHECKED GOOD.Jan 20, 2014 · N124US · Airbus A320214 · Passenger/Crew DoorsSDR USAA2014010700009Attach Fitting · dirtyDOOR 2R IS DIFFICULT TO ARM & DISARM, ARMING LEVER IS STIFF. CLEANED & LUBRICATED GIRT BAR FITTINGS IAW A320 AMM 25-62-44.Jan 6, 2014 · N124US · Airbus A320214 · Emergency EquipmentSDR USAA2013121300008Proximity Switch · out of adjust1L DOOR SLIDE DOES NOT SHOW ARMED IN COCKPIT WHEN ARMED AT THE DOOR. ADJUSTED 1L DOOR SLIDE ARMING & DISARMING PROXIMITY SWITCH IAW A320 AMM 52-71-00-820-002.Dec 12, 2013 · N124US · Airbus A320214 · Door Warning SystemSDR USAA2013012800015Power Supply · inoperativeROW 1 LEFT SIDE AISLE SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-001-A.Jan 25, 2013 · N124US · Airbus A320214 · Emergency LightingSDR USAA2012121000013Slide Raft · defectiveTHE 2R DOOR HARD TO ARM. REMOVED AND REPLACED R2 DOOR SLIDE RAFT PER JOBCARD 26L00025011.Dec 9, 2012 · N124US · Airbus A320214 · Escape SlideSDR USAA2012073000006Wire · inoperative2S CHECK - DURING OPERATIONAL CHECK OF THE EMERGENCY GENERATING SYSTEM FAILED TEST. PERFORMED CONTINUITY CHECK AND FOUND OPEN CIRCUIT IN WIRING 2424-7902. REPLACED WIRE 2424-7902 IAW A320 AWM 24-24-03 , ESPM 20-48-14 , ESPM 20-53-22 AND PERFORM OPERATIONAL Jul 27, 2012 · N124US · Airbus A320214 · Electrical Power System WiringSDR USAA2012072600008Mechanism · damaged2S CHECK - BEND PAWL AND PIN OF HATCH CONTROL MECHANISM AT RIGHT OVERWING EMERGENCY EXIT DOOR 843. REPLACED HATCH LOCKING MECHANISM OF DOOR 843 IAW AMM 52-21-11-400-002-A STEP 18 ITEM B (1).Jul 25, 2012 · N124US · Airbus A320214 · Emergency ExitsSDR USAA2012072600005Connector · damaged2S CHECK - DAMAGED CONNECTOR ( 7532VCA ) ON RIGHT WING ESCAPE SLIDE. REPLACED ELECTRICAL CONNECTOR 7532VCA ON RIGHT WING ESCAPE SLIDE IAW A320 AMM 33-51-04, ESPM 20-44-11 AND PERFORMED OPERATIONAL TEST IAW A320 SMM 33-51-00-710-001-A, TEST IS OK OF EMERGENCY Jul 25, 2012 · N124US · Airbus A320214 · Light System WiringSDR USAA2012072600004Connector · broken2S CHECK - BROKEN BACKSHELL ON ELECTRICAL WIRING ON CABIN OVERHEAD COMPARTMENT AT FR42. REPLACED BACKSHELL OF ELECTRICAL CONNECTOR 203WL-A IAW A320 AWM 33-51-02, ESPM 20-33-45 AND PERFORMED OPERATIONAL TEST IAW A320 AMM 33-51-00-710-001-A OF EMERGENCY LIGHT, Jul 25, 2012 · N124US · Airbus A320214 · Light System WiringSDR USAA2012072400015Cleat · corroded2S CHECK - CORROSION ON SHEAR TIE CLEAT AT FR28 BETWEEN S43L TO S43R. REPLACED SHEAR TIE CLEAT AT FR28 BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.Jul 18, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071600011Strut · corroded2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTBOARD FLAP. REPLACED RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTBOARD FLAP IAW A320 AMM 27-51-44.Jul 12, 2012 · N124US · Airbus A320214 · Wing Miscellaneous StructureSDR USAA2012072300039Access Panel · corroded2S CHECK - CORROSION ON INTERNAL SIDE OF FUEL PANEL 640FB BETWEEN WS 670 TO WS 732, STR 8 TO STR 11, RIB 12 TO RIB 15. REPLACED FUEL PANEL 640FB IAW A320 AMM 57-27-11-400-001A AND SRM 51-72-11.Jul 11, 2012 · N124US · Airbus A320214 · Wing, Plate/SkinSDR USAA2012071200013Floor Panel · corroded2S CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL 222FF IAW A320 SRM 51-72-11.Jul 11, 2012 · N124US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012073100005Skin · corroded2S CHECK - CORROSION ON SKIN PLATE BETWEEN FR63 TO FR64, S41L TO S42L. REPAIRED SKIN PLATE BETWEEN FR63 TO FR64, S41L TO S42L IAW A320 SRM 53-00-11 FIGURE 203 AND EA 502034.Jul 4, 2012 · N124US · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA2012073000044Skin Panel · corroded2S CHECK - CORROSION ON SKIN PANEL BETWEEN FR63 TO FR64, BETWEEN S41R TO S42R. REPAIRED SKIN PANEL BETWEEN FR63 TO FR64, BETWEEN S40R TO S43R IAW EA 502043.Jul 4, 2012 · N124US · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA2012072300038Access Panel · damagedS2 CHECK - ELONGATED HOLE ON FUEL PANEL 640KB BETWEEN WS 827 TO WS 824, STR 8 TO STR 11, RIB 15 TO RIB 16. REPLACED FUEL PANEL 640KB IAW A320 AMM 57-27-11.Jul 3, 2012 · N124US · Airbus A320214 · Wing, Plate/SkinSDR USAA2012071800013Cleat · corroded2S CHECK - CORROSION ON SHEAR TIE CLEAT AT FR29 BETWEEN S43L TO S43R. REPLACED SHEAR TIE CLEAT AT FR29 BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712 & D53231535.Jul 3, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071700015Cleat · corroded2S CHECK - CORROSION ON CLEAT AT FR29 BETWEEN S42L TO S43L. REPLACED CLEAT AT FR29 BETWEEN S42L TO S43L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.Jul 3, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012070900032Hinge Fitting · excess play2S CHECK - EXCESSIVE PLAY ON BEARING OF LEFT HORIZONTAL STABILIZER 6 HINGE FITTING ASSEMBLY. REPLACED 6 HINGE FITTING ASSEMBLY IAW A320 AMM 55-16-42-400-001.Jul 3, 2012 · N124US · Airbus A320214 · Horizontal Stabilizer StructureSDR USAA2012071900009Support Frame · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53474180.Jul 2, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071800012Support Frame · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474180.Jul 2, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071200019Support Fitting · corroded2S CHECK - CORROSION ON PENDULUM ASSEMBLY (MACHINED FITTING) ON RIGHT OUTBOARD FLAP OUTBOARD POSITION AT RIB 15. REPLACED PENDULUM ASSEMBLY (MACHINED FITTING) ON RIGHT OUTBOARD FLAP OUTBOARD POSITION IAW A320 SRM 51-72-11 & CMM 57-53-21.Jul 2, 2012 · N124US · Airbus A320214 · Trailing Edge FlapsSDR USAA2012070900007Fitting · cracked2S CHECK - CRACK ON FITTING AT FR66, -Y1400. REPLACED FITTING AT FR66, -Y1400 IAW A320 SRM 51-72-11.Jul 2, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012072000007Cleat · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE CLEAT AT FR32 BETWEEN S43L TO S43R. REPLACED SHEAR TIE CLEAT AT FR32 BETWEEN S43L TO S43R IAW A320 SRM 51-72-11 & AIRBUS DRAWINGS D53231712 & D53231534.Jun 30, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071200018Cleat · corroded2S CHECK - CORROSION ON CLEAT AT FR33 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR33 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231586 & D53231535.Jun 30, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012071200005Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 241EF BETWEEN FR36 TO FR42 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 241EF IAW A320 SRM 53-02-00 & IRM 9701 REV G.Jun 30, 2012 · N124US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012071100014Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232YF BETWEEN FR32 TO FR35 & BETWEEN -Y1732 TO Y1292. REPLACED FLOOR PANEL 232YF IAW A320 SRM 53-02-00 & IRM 9701 REV G.Jun 30, 2012 · N124US · Airbus A320214 · Fuselage Floor PanelSDR USAA2012072700004Door Frame · cracked2S CHECK - CRACK ON FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT OF EMERGENCY EXIT DOOR 833 IAW EO 5210Y228.Jun 29, 2012 · N124US · Airbus A320214 · Emergency ExitsSDR USAA2012072700003Door Frame · cracked2S CHECK - CRACK ON FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.Jun 29, 2012 · N124US · Airbus A320214 · Emergency ExitsSDR USAA2012072700002Door Frame · cracked2S CHECK - CRACK ON FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED FRAME SEGMENT OF EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.Jun 29, 2012 · N124US · Airbus A320214 · Emergency ExitsSDR USAA2012072600019Door Frame · cracked2S CHECK - CRACK ON EMERGENCY EXIT DOOR 843 INNER FRAME SEGMENT BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT DOOR 843 INNER FRAME SEGMENT IAW EO 5210Y228.Jun 29, 2012 · N124US · Airbus A320214 · Emergency ExitsSDR USAA2012072300044Seat Track · corroded2S CHECK - GALVANIC CORROSION ON SEAT TRACK AT FR25 PLUS 4 INCHES, Y1292. REPLACED SEAT TRACK AT FR25 PLUS 4 INCHES, Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53231730.Jun 29, 2012 · N124US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012072300043Splice · damaged2S CHECK - ELONGATED HOLE ON OUTBOARD SPLICE AT FR24, Y1292. REPLACED OUTBOARD SPLICE AT FR24, Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53110920.Jun 29, 2012 · N124US · Airbus A320214 · Fuselage Miscellaneous Structure
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