Airbus A318-111
Service difficulty reports · 353
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'A318111' 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.
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 aircraft_model_key = 'A318111' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA2009121100256Sill · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION AT THE NUT CLIP HOLE AT FRAME 66 AND STA -Y1732. MX PERFORMED MAJOR REPAIR TO THE DOOR SEAL IAW SRM 53-41-14, SRM 51-75-12 AND SRM 51-42-11.SDR F3LA2009120800248Floor Support · corrodedREF NON ROUTINE C075821. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUT PLATE HOLES LOCATED AT FRAMES 68 TO 69 AND STA -Y1292. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-23-11.SDR F3LA2009120800247Seat Track · corrodedREF NON ROUTINE C075806. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE SEAT TRACK LOCATED AT FRAMES 64 TO 66 AND STA Y1292. MX REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 53-41-14, SRM 51-44-11, SRM 51-21-00, SRM 51-75-00 AND SRM 51-72-11.SDR F3LA2009120800246Floorbeam · corrodedREF NON ROUTINE C075818. DURING DEN C4/S1 C-CHECK, INSP NOTED CORRODED NUT PLATE HOLES ON THE FLOORBEAM LOCATED AT FRAME 68 AND STA Y1292. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-72-11.SDR F3LA2009112800238Floorbeam · corrodedDURING C4 S1 C-CHECK, INSP NOTED CORROSION AT NUT PLATE HOLES ON Y1292 LT AT FRAME 68. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-72-11.SDR F3LA2009120800242Profile · corrodedREF NON ROUTINE C075679. DURING DEN C4/S1 C-CHECK, INSP NOTED CORRODED FASTENERS ON THE FLOORBEAM LOCATED AT FRAME 61 AND STR 40R. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11.SDR F3LA2009121100257Rib · corrodedDURING C4/S1 C-CHECK, INSP NOTED THE LT SIDE HORIZONTAL STABILIZER OTBD L/E RIB WHERE THE HORIZONTAL STABILIZER SECURES TO, HAS SURFACE CORROSION. MX REPAIRED RIB IAW EA A8-55R-31516 AND IAW SRM 51-74-00, NTM 51-10-04-270-801-A-01, NTM 51-10-08-250-803-A-01, SSDR F3LA2009120900254Profile · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM LOCATED IN THE AFT CARGO COMPARTMENT AT FRAME 60 AND STRINGER 40R. MX PERFORMED REPAIR IAW SRM 51-42-11, SRM 51-44-00, SRM 51-21-11, SRM 51-75-12 AND EA A8-53R-31553.SDR F3LA2009120800245Profile · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED THE LT SUPPORT PROFILE AT FRAMES 57-60 IN THE AFT CARGO PIT HAS CORROSION ON THE UPPER SURFACE. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND SRM 51-44-11.SDR F3LA2009112500240Fitting · corrodedREF NON ROUTINE C075703. DURING C4 S1 CHECK, INSP NOTED THE SUPPORT FITTING IN THE AFT CARGO COMPARTMENT AT FRAME 60 STR 43 RT HAS CORROSION AT THE NUT PLATE HOLE. MX REMOVED AND REPLACED THE FITTING IAW SRM 51-74-00, SRM 51-74-00, SRM 51-42-11 AND SRM 51-44SDR F3LA2009120900253Strut · chafedDURING DEN C4/S1 C-CHECK, INSP NOTED WIRING CONDUIT CHAFING THE RT SIDE OF THE NLG BARREL. MX PERFORMED MAJOR REPAIR, REFERENCE EA A8-32R-31531, REV A.SDR F3LA2009080300123Support · chafedDURING C-CHECK, INSP NOTED DAMAGE ON THE LT AND RT NLG UPPER SUPPORT. MX BLENDED CHAFED AREA IAW SRM 51-73-00, PERFORMED FLUORESCENT PENETRANT INSP IAW NTM 51-80-00 PB1, AND FLAP PEENED, TREATED AND PAINTED AREA IAW EA NR A8-32R-31224.SDR F3LA2009080300122Strut · chafedDURING C4 C-CHECK, INSP NOTED THE NLG BARREL IS CHAFED ON THE RT SIDE AT THE STEERING LOCKOUT WIRING CONDUIT. MX BLENDED THE CHAFED AREA IAW SRM 51-73-00, PERFORMED FLUORESCENT PENETRANT INSP IAW NTM 51-80-00 PB1, AND FLAP PEENED, TREATED AND PAINTED AREA IAWSDR F3LA2009080300121Buffer · out of adjustREFERENCE NON ROUTINE C065693. DURING C4 C-CHECK, INSP NOTED THE R-1 DOOR PUSHBUTTON SWITCH FAILED THE FUNCTIONAL LOAD TEST. MX ADJUSTED TO R-1 DOOR BUFFER ASSY IAW AMM 52-13-00-820-059 AND PERFORMED OPS TEST.SDR F3LA2009080300120Hook · inoperativeREFERENCE NON ROUTINE C065692. DURING C4 C-CHECK, INSP NOTED THAT THE R-2 DOOR, INSIDE DOOR HANDLE DOES NOT LOCK OPEN. MX REMOVED AND REPLACED THE DOOR GEAR BOX ASSY HOOK AND PERFORMED OPS CHECK IAW AMM 52-13-21-000-001 AND 52-13-21-400-001.SDR F3LA2009080300119Hook · inoperativeREFERENCE NON ROUTINE C065691. DURING C4 C-CHECK, INSP NOTED THAT THE L-2 DOOR INSIDE DOOR HANDLE DOES NOT LOCK OPEN. MX REMOVED AND REPLACED DOOR GEAR BOX ASSY HOOK AND PERFORMED OPS CHECK IAW AMM 52-13-21-000-001 AND 52-13-21-400-001.SDR F3LA2009062200092Transponder · no testDURING DEN-RON SCHEDULED MAINTENANCE TASK CARD TC34210-07, ATC TRANSPONDER NR 2 FAILED FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 ATC TRANSPONDER AND PERFORMED BITE TEST, REFERENCE AMM 34-52-33 PB 401.SDR F3LA2009042400079Servo Control · faultedAIR TURN BACK DUE TO NOSE WHEEL STEERING FAULT. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 32-51-00-810 FAILURE OF NOSE WHEEL STEERING AND FOUND STEERING SERVO VALVE FAULTED PER TROUBLESHOOTING DATA FAULT CODE 745. MAINTENANCE REMOVED AND REPLACED THE NOSSDR F3LA2009042100078Computer · inoperativePILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCRAFT TRIMMED NOSE UP IF NO STICK INPUT RUNAWAY NOSE UP. MAINTENANCE REMOVED AND REPLACED THE NR 2 SDR F3LA2009041700076Switch · malfunctionedAIR TURN BACK DUE TO BLUE HYDRAULIC RESERVOIR LOW INDICATION ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SYSTEM. MAINTENANCE APPLIED MEL 29-30-04F FOR THE RESERVOIR LOW LEVEL SWITCH, COMPLIED WITH FOLLOW-UP ACTION TO VERIFY THE BLUE HYDRAULIC RESERVOIR SDR F3LA2009032400066Lug · gougedREFERENCE NON-ROUTINE C035636. DURING C3/S1 C-CHECK, INSPECTION NOTED THE LEFT WING NR 5 SPOILER ANTI-ROTATION LUG FOR ACTUATOR BOLT IS DAMAGED. MAINTENANCE REMOVED GOUGE DAMAGE AND PERFORMED REPAIR IAW ENGINEERING AUTHORIZATION A8-57R-12382.SDR F3LA2009032300065Transmitter · inoperativeAIR TURN BACK, PILOT REPORTED THAT AFTER TAKEOFF, ENGINE NR 2 OIL PRESSURE GAUGE INDICATED ZERO PRESSURE. INDICATION ALTERNATED BETWEEN RED 0 AND AMBER XX. ALL OTHER INDICATIONS WERE NORMAL, NO ELECTRONIC CENTRALIZED AIRCRAFT MONITORING WARNING. MAINTENANCESDR F3LA2009021600027Cable · lack of lubeDURING C3 C-CHECK, INSPECTION NOTED THAT THE RIGHT OVERWING EMERGENCY SLIDE CABLE FAILED THE FUNCTIONAL TEST OF THE SLIDE RELEASE SIGNAL AND OPERATIONAL TEST OF THE UNLOCKING AND OPENING FROM THE OUTER SIDE IN THE ARMED MODE. MAINTENANCE INSPECTED AND LUBED CSDR F3LA2009021600026Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED CORROSION AT THE FASTENER HOLE OF THE AFT GIRT BAR FITTING, L2 DOOR THRESHOLD. MAINTENANCE REMOVED THE CORROSION. FABRICATED REPAIR DOUBLER AND FILLER AND COMPLETED THE REPAIR PER ENGINEERING AUTHORIZATION A8-53R-30930.SDR F3LA2009021300025Floorbeam · corrodedREFERENCE NON-ROUTINE C057562. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68 IN REFERENCE TO SRM 51-42-11 PARAGRAPHS 5 AND 7.SDR F3LA2009020500020Light · inoperativeEMERGENCY PATH LIGHT PARTIALLY BURNED OUT AT SEAT ROWS 9 AND 13. MAINTENANCE REMOVED AND REPLACED EMERGENCY PATH LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK, REFERENCE AMM 33-51-19 PB401.SDR F3LA2008121600727Connector · looseDURING C4 C-CHECK, INSPECTION NOTED THE EMERGENCY PATH LIGHTING AT SEAT 7 ABC INOPERATIVE. MAINTENANCE FOUND PUSHED BACK PIN ON ROW 7 SEAT CONNECTOR, LOCKED PIN IN PLACE AND PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH AMM 33-51-00-710-009.SDR F3LA2008121600726Isolation Valve · crackedENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY DEPLETED. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE THRUST REVERSER ISOLATION VALVE HYDRAUSDR F3LA2008111900718Fitting · out of adjustDURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTED THE R2 GIRT BAR FITTING AND PERFORMED OPERATION CHECK IN ACCORDANCE WITH A318 AMM 52-13-00-820-001.SDR F3LA2008111800717Battery · failedDURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN ACCORDANCE WITH AMM 33-51-38-000-001.SDR F3LA2008111900719Warning Light · failedPILOT REPORTED THAT THE LEFT OVERWING EXIT SLIDE ARMED LIGHT IS ILLUMINATED WHEN ON MAINTENANCE BUS. EMERGENCY EXIT OPEN ECAM INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING SLIDE ARMED INDICATOR LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE SDR F3LA2008111800716Hook · wornDURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INTO THE CLOSED POSITION BEFORE THE DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED THE DOOR HOOK IN ACCORDANCE WITH AMM 52-13-21-420-052.SDR F3LA2008111700715Control Panel · failedPILOT REPORTED THE LEFT OVERWING EXIT SHOWS OPEN ON LOWER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND LEFT OVERWING LIGHT TO BE AT FAULT. THE WARNING LIGHT PANEL WAS REMOVED, REPLACED AND CHECKED IN ACCORDANCE WITH A318 AMM 52-73-21 PB 401.SDR F3LA2008111700714Lamp · inoperativeLINE MAINTENANCE NOTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 5ABC WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH A318 AMM 33-51-19 PB 401.SDR F3LA2008111700713Hinge Fitting · gougedDURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.SDR F3LA2008111700712Hinge Fitting · gougedDURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.SDR F3LA2008111000710Solenoid · failedREFERENCE NON-ROUTINE 104853. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE TWELFTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN SDR F3LA2008111000709Solenoid · failedREFERENCE NON-ROUTINE 104852. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE FIFTEENTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGESDR F3LA2008111000708Solenoid · failedREFERENCE NON-ROUTINE 104851. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE SECOND ROW OF SEATS ON THE RIGHT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN SDR F3LA200800624Floor Panel · debondedDURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151DH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OFSDR F3LA200800625Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY TRANSITION PANEL 132EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00 PARA 8F AND EO A0-53F-12307. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCSDR F3LA200800626Floor Panel · debondedDURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151BH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OFSDR F3LA200800627Floor Panel · debondedDURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151CH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OFSDR F3LA200800619Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131CG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.SDR F3LA200800620Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131AF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.SDR F3LA200800621Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.SDR F3LA200800622Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131DG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.SDR F3LA200800623Floor Panel · damagedDURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131BF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.SDR F3LA200800558Blanking Plate · corrodedDURING C-CHECK, INSP NOTED L2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)SDR F3LA200800557Blanking Plate · corrodedDURING C-CHECK, INSP NOTED L2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)
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