Airbus A318-111

Service difficulty reports · 353

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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.

SDR EE4Y20110087Fitting · wornAFT AND FWD CARGO DOORS LOWER CUTOUT SECTION CAM- CENTRAL FITTINGS WITH WEAR.Feb 4, 2011 · N592EL · Airbus A318111 · Fuselage Main, StructureSDR EE4Y20110078Floor Support · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT AT FR 29 +Y 28, FLOOR CHANNEL CRACKED.Feb 4, 2011 · N592EL · Airbus A318111 · Fuselage Miscellaneous StructureSDR EE4Y20110079Floor Support · corrodedUPPER FUSELAGE, PAX CABIN BETWEEN FR 69 AND FR 70 -Y 1200 FLOOR CHANNEL WITH CORROSION.Feb 4, 2011 · N592EL · Airbus A318111 · Fuselage Miscellaneous StructureSDR EE4Y20110086Access Panel · crackedNR 2 ENGINE PYLON NR 423DL ACCESS PANEL WITH CRACKS AT SEVERAL PLACES.Feb 4, 2011 · N592EL · Airbus A318111 · Nacelle/Pylon, Plate/SkinSDR EE4Y20110085Skin · dentedRT WING, NR 1 SLAT L/E LOWER SKIN WITH DENT AND CRACK.Feb 4, 2011 · N592EL · Airbus A318111 · Leading Edge DevicesSDR EE4Y20110084Panel · delaminatedENGINE NR 2 AFT SECTION PANEL NR 486 ARE DELAMINATED.Feb 3, 2011 · N592EL · Airbus A318111 · Nacelle/Pylon, Plate/SkinSDR EE4Y20110083Skin · damagedLOWER FUSELAGE FR: 60, STR 30R AND STR 34R DOOR CUTOUT WITH EXISTING BLEND OUTS.Feb 3, 2011 · N592EL · Airbus A318111 · Fuselage Main, Plate/SkinSDR EE4Y20110082Tube · crackedAPU EXHAUST, FELT METAL TUBE WELD WAS REPORTED WITH CRACKS.Feb 3, 2011 · N592EL · Airbus A318111 · APU Exhaust SystemSDR EE4Y20110033Frame · crackedEMPENNAGE TAIL CONE, FRAME 86 LOWER CTR SECTION WITH CRACK. THE FRAME CRACK REQUIRES A MAJOR REPAIR.Jan 18, 2011 · N592EL · Airbus A318111 · Fuselage Main, FrameSDR EE4Y20110031Stop Fitting · wornLOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, STOP FITTING WITH WEAR AT FR 26RH.Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, StructureSDR EE4Y20110030Stop Fitting · wornLOWER FUSELAGE AFT CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, FOUND STOP FITTING WITH WEAR AT FR59 RT.Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, StructureSDR EE4Y20110010Skin · damagedUPPER FUSELAGE FWD PAX/ CREW DOOR RT UPPER CORNERS CUTOUT EXTERNAL SURFACE WITH MARKS.Jan 10, 2011 · N591EL · Airbus A318111 · Fuselage Main, Plate/SkinSDR EE4Y20110009Seal · wornNR 2 ENGINE CORE NOZZLE INNER AND OUTER PYLON SEAL WITH WEAR.Jan 10, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Main FrameSDR EE4Y20110008Support Angle · crackedRT WING T/E CAVITY, HYD LINE WITH SUPPORT ANGLE CRACKED AT STA 3250.Jan 10, 2011 · N591EL · Airbus A318111 · Wing Miscellaneous StructureSDR EE4Y20110007Inlet · crackedAPU MUFFLER-EXHAUST, DUCT INLET AND TUBE ASSY-FELT METAL WITH DENTS, CRACKS AND PUNCTURE. NOTE: INLET AND FELT METAL DENTS, CRACKS AND PUNCTURE REQUIRE MAJOR REPAIR.Jan 9, 2011 · N591EL · Airbus A318111 · APU Exhaust SystemSDR EE4Y20110003Housing · delaminatedAIR CONDITIONING BAY, RT PLENUM'S HSG WITH FIBERGLASS DAMAGE (DELAMINATED & BROKEN). THE HOUSING DAMAGE AREA REQUIRES A MAJOR REPAIR.Jan 7, 2011 · N591EL · Airbus A318111 · Cabin Cooling SystemSDR EE4Y20110002Skin · crackedENGINE NR 1 & NR 2, ENGINE PYLON, PRECOOLER FAIRING SKIN WITH CRACKS (ID ACCESS PANEL NR 413DL & NR 423DL). THE SKIN CRACKS REQUIRE A MAJOR REPAIR.Jan 5, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Plate/SkinSDR EE4Y20110001Panel · delaminatedVERTICAL STABILIZER, RUDDER PN: D5547100300000, SN: TS-3706, LT AND RT SIDE PANEL WITH FLUID INDICATION (WATER INGRESS) IAW THERMOGRAPHY INSP AROUND HOISTING POINTS . LT SIDE PANEL FLUID INDICATION COMMON TO HOISTING POINT NR 1 & 3 AND RT SIDE PANEL FLUID INDIJan 5, 2011 · N591EL · Airbus A318111 · Rudder, Plate/SkinSDR DALAFAR145SDR104Nut · missingUPON DISASSEMBLY OF THE ROTOR STACK, SHOP NOTICED 48 NUTS OUT OF 60 MISSING FROM THE STACK WHICH HOLDS THE LLPS TOGETHER. THE LLPS AND HARDWARE INVOLVED ARE AS FOLLOWS: 1-2 SPOOL PN 1558M31G07, SN GWNOEW92, STAGE 3 HPC DISK PN 2116M23P01, SN XALG9478, 4-9 SPONov 19, 2010 · Airbus A318111 · Turbine Engine Compressor SectionSDR F3LA2010111400550Battery Pack · dischargedBATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.Nov 12, 2010 · N801FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600529Lens · crackedC-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP A 3 AND AMM 33-51-13-020-050 STEP A(1)(A)(B).Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600528Floor Panel · delaminatedC-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, REV G.Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA2010100600527Lens · crackedC-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600526Power Supply · no testC-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. EMERGENCY POWER SUPPLY UNIT 10WL FAILED SYS TEST "BATT FAULT' LIGHT ILLUMINATED. R & R EPSU 10WL IAW Oct 17, 2010 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2010100600525Fitting · gougedC-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED .1250 IN X .2500 IN X .040 INCH. R & R FWD LOWER SEALING SECTION FITTING IAW SRM 51-72-11, PAGE 1.Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010100600524Connector · misinstalledC-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS A318 AMM 33-51-19-400-003 SUBTASK 33-51-19-420-052 STEP A(1)(A)(B). OPS CHECK GOOD IAW AMM 33-51-00Oct 17, 2010 · N803FR · Airbus A318111 · Light System WiringSDR F3LA2010090100490Bypass Valve · leakingAN EMERGENCY DECLARED WAS REPORTED BY THE PILOT. AIR TURN BACK, ECAS WARNING HYD GREEN ENG 1 PUMP LOW PRESSURE. FOUND NOSE GEAR DOOR BYPASS VALVE LEAKING. REPLACE NOSE GEAR DOOR BYPASS VALVE, REF AMM 32-31-15, PAGE BLOCK 401. OPS CHECK AND LEAK NORMAL WITH NAug 28, 2010 · N810FR · Airbus A318111 · Landing Gear Door Retract SectionSDR F3LA2010072500474Encoder · faultyREFERENCE HEAVY MAINTENANCE NON ROUTINE N0526. EMERGENCY LIGHT OPERATIONAL TEST FAILED WITH A CLASS 1 MESSAGE EPSU (11WL) AND (12WL). FOUND HIGH AND LOW CODING SWITCHES ON TERMINATION/CONNECTION BOX 3000RH8-DEU B TO BE CODED ONE NOTCH OFF. SET CODING POTENTJul 21, 2010 · N801FR · Airbus A318111 · Audio/Video MonitoringSDR F3LA2010072500473Light · inoperativeREFERENCE HEAVY MAINTENANCE NON ROUTINE N0499. DURING TEST FORWARD EMERGENCY LIGHT 61WL WOULD NOT ILLUMINATE. TROUBLESHOT SYSTEM IAW A318 TSM 25-62-00-810-813. FOUND TWO BULBS BURNT OUT. REPLACED BULBS IAW A318 AMM 33-51-15 PAGE BLOCK 401. OPERATIONAL TESJul 20, 2010 · N801FR · Airbus A318111 · Emergency LightingSDR F3LA2010072500472Flap · damagedREFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE. DAMAGE MEASURED 1.75 X 0.50 INCH. INSTALLED PERMANENT REPAJul 12, 2010 · N801FR · Airbus A318111 · Trailing Edge FlapsSDR F3LA2010040700379Line · wornREFERENCE LOG PAGE, NR 535350, ITEM 1. ECAM HYD YELLOW LOW LEVEL INDICATION. FOUND DAMAGED HYD LINE IN NR 2 ENG PYLON. REPLACED LINE REF AMM 29-13-49-000-049 AND 29-13-49-400-049.Apr 4, 2010 · N802FR · Airbus A318111 · Hydraulic System, MainSDR F3LA2010031000364Panel · delaminatedREFFERENCE NON ROUTINE NR N0072. DURING C4 S1 C-CHECK INSP NOTED AFT CARGO TRANSITION PANEL 151CH DELAMINATED. MX R & R AFT CARGO TRANSITION PANEL 151CH IAW AMM 53-42-14-400-001.Mar 4, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030800358Plate · corrodedREF NON ROUTINE NR N0250. DURING C4 S1 CHECK INSP NOTED SEVERAL GOUGES ON BOTTOM/ EDGE OF R1 DOOR GIRT BAR FWD BRACKET AND CORROSION AT CORNER. MX R & R PLATE IAW SRM 51-72-11.Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030300355Strip · corrodedDURING C4 SI C-CHECK INSP NOTED CORROSION ON THE R1 DOOR ENTRY WAY STRIP. MX R & R STRIP IAW WC CP053-12.Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030300354Strip · corrodedREF NON ROUTINE NR N0249. DURING C4 S1 C CHECK INSP NOTED CORROSION ON L1 DOOR ENTRYWAY STRIP. MX R & R STRIP IAW WC CP053-12.Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030900360Floor Support · corrodedREFERENCE NON ROUTINE NR N0195. DURING C4 S1 C-CHECK INSP NOTED CABIN MAIN FLOOR EXTRUSION CORRODED ON TOP AND BOTTOM SURFACE LOCATED BETWEEN FR69 AND FR70, 48 INCHES RT OF CTR LINE. MX R & R EXTRUSION IAW SRM 51-72-11.Feb 24, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030800359Threshold · corrodedNON ROUTINE NR N0196. DURING C4 S1 CHECK INSP, NOTED CORROSION ON THE R2 DOOR THRESHOLD AROUND 2 FASTENERS LOCATED INBD OF THE AFT GIRT BAR LATCH. MX REMOVED LEVEL 1 CORROSION, R & R THRESHOLD PLATE IAW SRM 53-41-14 / 51-21-11 / 54-75-12.Feb 24, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030900363Panel · delaminatedDURING C4 S1 C-CHECK INSP NOTED AFT CARGO COMPARTMENT SLOPE PANEL 1151BH DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 9701.Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030900362Panel · delaminatedDURING C4 S1 C-CHECK INSP NOTED FWD CARGO COMPARTMENT AFT WALL PANEL 132PW CRACKED AND DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 2001.Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2010030900361Floor Panel · delaminatedDURING C4 S1 C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151AH DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 9701.Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA2010021200336Line · leakingDURING CLIMB THE FLIGHT CREW NOTED THE GREEN HYD SYS FLUID LEVEL WAS LOW. MX R & R THE RT MLG DOOR ACTUATOR AFT HYD HOSE AND SERVICED THE GREEN HYD SYS AMM IAW 32-31-38 PB 401 AND AMM 29-00-00-870-003.Feb 11, 2010 · N802FR · Airbus A318111 · Hydraulic System, MainSDR F3LA2010011400299Light · inoperativeDURING HEAVY SERVICE CHECK MX NOTED ROW 19 ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MX DEFERRED SEAT MOUNTED EMERGENCY LIGHT AT 19 ABC IAW MEL 33-50-03B, CNTRL NR 1073010. FINAL C/A TO BE ACCOMPLISHED AT A CLASS 1 OR CLASS 2 STATION.Jan 13, 2010 · N802FR · Airbus A318111 · Emergency LightingSDR F3LA2009122900274Cover · out of positionDURING CLIMB OUT, THE FLIGHT CREW RECEIVED SPURIOUS ECAM INDICATIONS RT DOOR EMERGENCY EXIT. MX REINSTALLED RT OVERWING EXIT HANDLE COVER FLAP AND ECAM INDICATION CHECKED NORMAL IAW AMM 25-23-47-420-127.Dec 28, 2009 · N807FR · Airbus A318111 · Emergency ExitsSDR F3LA2009120900252Blanking Plate · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE L2 FWD GIRT BAR FITTING BLANKING PLATES. MX REMOVED AND REPLACED THE GIRT BAR BLANKING PLATES AND INSTALLED IAW WORK CARD C250001-3.Dec 8, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009120900251Profile · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE LT PROFILE AT FRAME 56. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND 51-72-11.Dec 8, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009120800249Floorbeam · corrodedREF NON ROUTINE C075817. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM AT -Y1292 AND FRAME 20. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11.Dec 6, 2009 · N805FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2009120900250Profile · corrodedDURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED AT FRAME 58 AND STRINGER 40R. MX BLENDED THE AREA IAW SRM 51-75-12 AND INSTALLED NEW PROFILE IAW SRM 51-42-11.Dec 4, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009120800244Shear Plate · corrodedREF NON ROUTINE C075822. DURING DEN C4/S1 C-CHECK, INSP NOTED THE SHEAR PLATE LOCATED AT FRAMES 69-70 AND STA -Y1292 HAS CORROSION AROUND THE NUT PLATE HOLES. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11 PARAGRAPHS 6 AND 14 AND STEP 4 OF EO A0-53ENov 30, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009120800243Shear Plate · corrodedREF NON ROUTINE C075819. DURING DEN C4/S1 C-CHECK, INSP NOTED THE SHEAR PLATE LOCATED AT FRAMES 69-70 AND STA Y1292 HAS CORROSION AROUND THE NUT PLATE HOLES. MX REMOVED AND REPLACED THE SHEAR PLATE AND SHEAR SUPPORT IAW SRM 51-42-11 PARAGRAPHS 6, 7, 14 AND STNov 30, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009113000239Floor Support · corrodedDURING C4 S1 C-CHECK, INSP NOTED CORROSION ON FLOOR SUPPORT Y1292 FRAME 66 TO FRAME 68. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 53-41-14, SRM 51-44-11 AND SRM 51-72-11.Nov 30, 2009 · N805FR · Airbus A318111 · Fuselage Miscellaneous Structure
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