Airbus A320-211

Service difficulty reports · 5,271

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320211'
  ORDER BY difficulty_date DESC"

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SDR DALA13029913216Floorbeam · brokenDURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR 33+16" AND -Y254. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4.D, FIG 204 (SHEET 1).Jun 18, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13029883216Floorbeam · brokenDURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4.D FIG 204 (SHEET 1) PAGE 225/226.Jun 18, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13032643218Angle · crackedDURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER. HFEC IAW NTM 51-10-08, PT6 CONFIRMED CRACKS AROUND FASTENER HOLES. REMOVED CRACKED ANGLE IAW SRM 51-42-11. LOCATED AND DRILLED IAW SRM 51-44Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Main, StructureSDR DALA13029903218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152EF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029893218Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF HAS SEVERAL BROKEN EDGES & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029873218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151LF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029863218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029853218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152BF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029843218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151QF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 17, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029833216Threshold · corrodedDURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET LOCATED BETWEEN FR 52A AND FR 56 AND BETWEEN STR 38R AND STR 39R INTERNAL STRUCTURE OF AFT CARGO COMPARTMENT SSI 534107, L=0.400, W=0.260, D=0.002 APPROX. REPLACED TRESHOLD SHEET LOCATED BETWEEN FR 52A ANDJun 17, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA130625010Outflow Valve · failed(CAN) SHORTLY AFTER DEPARTURE, FLIGHT CREW ADVISED OF AVIONICS SMOKE FAULT. DISCUSSED WITH MOC, AND RETURNED TO DEPARTING STATION, LANDING AT 71,000 KG OVERWEIGHT BY 6500KG. NO EMERGENCY DECLARED. SKIN AIR OUTLET VALVE INOPERATIVE, SKIN AIR OUTLET VALVE REPLAJun 16, 2013 · Airbus A320211 · Pressure Regulator/Outflow ValveSDR DALA13029823218Floor Panel · puncturedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151NF HAS SEVERAL PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029813218Floor Panel · puncturedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151HF HAS SEVERAL PUNCTURES & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029803218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151JF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029643218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029633218Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152MF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029623218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029613218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161BF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029603218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029593218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161FF DELAMINATED. FABRICATED FLOOR PANEL IAW BFM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029583218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029573218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029563218Floor Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151FF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029553218Floor Panel · puncturedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 162FF HAS PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029543218Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF HAS SEVERAL BROKEN INSERTS & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029533218Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029523218Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029513218Floor Panel · damagedDURING INSPECTION, FOUND FORWARD CARGO FLOOR PANEL 131JF DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029503218Floor Panel · damagedDURING INSPECTION, FOUND FORWARD CARGO FLOOR PANEL 132KF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jun 16, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR CA130618003Indicator · failed(CAN) ENROUTE THE CREW RECEIVED REPEATED ECAM WARNINGS FOR A, GREEN HYDRAULIC LOW LEVEL. THE CREW CONTACTED FLIGHT DISPATCH AND SET UP A PATCH WITH MAINTENANCE CONTROL. MAINTENANCE CONTROL SUSPECTED A HYDRAULIC LEAK AND PREFERRED A RETURN TO DEPARTING STATIOJun 15, 2013 · Airbus A320211 · Hydraulic Quantity IndicatorSDR DALA13029203216Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 29L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 29L AT LEVEL FR.67 IAW SRM 51-72-11 AND DWG D53480009.Jun 15, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029193216Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 30L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 30L AND AT LEVEL FR 67 IAW SRM 51-72-11 AND DWG D53480009.Jun 15, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029183216Splice · corrodedDURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT FR 67 AT LEVEL STR 30R. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT FR.67 AT LEVEL STR 30R IAW SRM 51-72-11 AND DWG D53480009.Jun 15, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029173216Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, FWD PAX CABIN BETWEEN FR 20 TO FR 24 AND -Y1292 L=3.00", W=0.500",D=0.005" APPROX, REPLACED SEAT TRACK FWD PAX CABIN BETWEEN FR 12 TO FR 24 AND -Y1292 AND FASTENERS IAW SRM 51-72-11 AND DWG D53112812.Jun 15, 2013 · N316US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13029163216Skin · corrodedDURING INSPECTION, FOUND CORROSION ON UPPER SHEET METAL LOCATED BETWEEN FR 24A AND FR 28, S39-41R IN FWD CARGO COMPARTMENT. MEASURES L=1.5" W=0.300", D=0.002 APPROX. MAJOR DIMENSION. REPLACED UPPER SHEET METAL LOCATED BETWEEN FR 24A AND FR 28, STR 39R AND Jun 15, 2013 · N316US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13029133216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 16 AND FR 20 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112198.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13029123216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 RT SIDE L=0.500", W=0.250", D=0.001" APPROX. REPLACED LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 RT SIDE IAW SRM 51-72-11 AND DWG D53480020, D53480505.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029113216Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, FR 66 LEVEL Y-1292. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472230.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13029103216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE, LOCATED AFT PAX CABIN, AT FR 68 LEVEL Y-1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029093216Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, LOCATED AFT PAX CABIN AT FR 67+13", LEVEL Y-1162. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG NR D53472000.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13029073216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 LT SIDE L=1", W=0.500", D=0.002" APROX. REPLACED LOWER SILL AND FASTENERS LOCATED BETWEEN FR 66 AND FR 68 LT SIDE IAW SRM 51-72-11 AND DWGS D53480020 AND D53480505.Jun 14, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029013216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED FR 68 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CORNER FITTING LOCATED FR 68 AT LEVEL STR 23 RT IAW SRM A320 51-72-11 AND DWG D53480505.Jun 13, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029003218Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION. REPLACED FLOOR PANEL IAW SRM 51-72-11.Jun 13, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028993216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT LOCATED AT FR.68 AT LEVEL OF S24R IN AFT PAX CABIN. REPLACED SUPPORT SECTION IAW SRM 51-72-11 AND DWG D53470150.Jun 13, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13028953216Floorboard · corrodedDURING INSPECTION, FOUND CORROSION ON OTBD UPPER FLOORBOARD SPLICE LOCATED AFT PAX CABIN AT FR.64, LEVEL Y-765, SSI 534147. L=1", W=0.5", D=0.003" APPROX. REPLACED OTBD UPPER FLOORBOARD SPLICE IAW SRM 51-72-11.Jun 13, 2013 · N316US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029493216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING AND FASTENERS LOCATED FR 68 AT STR 23. REPLACED CORNER FITTING AND FASTENERS IAW SRM 51-72-11 AND DWG NR D53480019.Jun 12, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13029483216Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FR20 TO FR21 AND AT LEVEL -Y1680 FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53112783.Jun 12, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13029053218Floor Panel · delaminatedDURING INSPECTION, FOUND MID CABIN FLOOR PANEL 252FF DELAMINATED 1" X 24". FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029043218Floorboard · brokenDURING INSPECTION, FOUND FWD UTILITY FLOORBOARD 221DF SEVERAL INSERTS BROKEN & MISSING. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13029033218Floor Panel · puncturedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222CF PUNCTURED 1" X 1". FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor Panel
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