Airbus A320-211

Service difficulty reports · 5,271

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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 = 'A320211'
  ORDER BY difficulty_date DESC"

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SDR DALA2015022401725Web · crackedDURING INSPECTION, FOUND CRACK ON WEB LOCATED BETWEEN FRAME 23 TO FRAME 24 LEVEL STR 34L AFT AVIONIC COMPARTMENT. REPLACED WEB LOCATED BETWEEN FRAME 23 TO FRAME 24 AT STR 34L LEVEL, AVIONIC COMPARTMENT, IAW SRM 51-72-11 AND DWG D53911363.Feb 23, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015022401723None · noneDURING INSPECTION, CONFIRM AT EVALUATION FOR POSSIBLE FCS REPAIR. ON EXTERNAL SKIN LT PAX DOOR LOCATION BETWEEN XP 662 AND XP 297 AND BETWEEN BEAM 7 AND BEAM 6. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN L1 PAX DOOR LOCATED BETWEEN XP 662 AND XP 297 AND BETWFeb 23, 2015 · N327NW · Airbus A320211 · Standard Practices/StructuresSDR DALA2015022301719Skin · damagedDURING INSPECTION, FOUND NICK ON EXTERNAL FUSELAGE SKIN LOCATED FR 24+9" AND BETWEEN STR 42L AND STR 43L. PERFORMED REPAIR ON EXTERNAL FUSELAGE SKIN LOCATED FRAME 24+9" AND BETWEEN STR 42L TO STR 43L IAW SRM 53-00-11, PARA 4W REPAIR 7, FIG 240.Feb 22, 2015 · N327NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015022201638Stringer · corrodedDURING INSPECTION, FOUND CORROSION STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 29 TO FRAME 31, L=1", W=0.5", D=0.003". REWORKED CORROSION ON STRINGER 43L, SECTION FRAME 29 TO FRAME 30+16" FWD CARGO COMPARTMENT IAW 51-74-00.Feb 21, 2015 · N343NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2015022201637Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON TIE CLIP LOCATED ON FR 31 BETWEEN STR 38R AND STR 39R IN FWD CARGO COMPARTMENT REPLACED TIE CLIP LOCATED ON FR 31 BETWEEN STR 38R AND STR 39R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D52231533.Feb 21, 2015 · N327NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015022501640Wire · disconnectedDURING NON ROUTINE CHECK, FOUND SEAT 10ABC RED SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. RECONNECTED WIRES TO FWD RED SEAT EMERGENCY LIGHT AND FUNCTIONAL CHECK WAS NORMAL.Feb 20, 2015 · N377NW · Airbus A320211 · Light System WiringSDR DALA2015022101636Bolt · corrodedDURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING, LOCATED ON SPOILER 3 LT WING. PERFORMED PERMANENT REPAIR ON STOP BOLT OF CENTER FITTING LOCATED ON SPOILER 3 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201.Feb 20, 2015 · N327NW · Airbus A320211 · SpoilersSDR DALA2015022101635Bolt · wornDURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING LOCATED SPOILER NR 4 LT WING. PERFORMED PERMANENT REPAIR ON STOP BOLT CENTER HINGE FITTING LOCATED ON SPOILER NR 4 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201, SHEET 2.Feb 20, 2015 · N327NW · Airbus A320211 · SpoilersSDR DALA2015022101634Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y1292 LOCATED BETWEEN FR 47 TO FR 64. EVALUATED AND FOUND OUT LIMITS ON JC 2500-2032. REPLACED SEAT TRACK, -Y1292 LOCATED BETWEEN FRAME 47 TO FRAME 64 AFT PAX CABIN IAW SRM 51-72-11 AND DWG N D53472000.Feb 20, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015022101632Web · corrodedDURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF RT MOVABLE FAIRING. REPLACED VERTICAL WEB ON RT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.Feb 20, 2015 · N327NW · Airbus A320211 · Nacelle/Pylon Miscellaneous StructureSDR DALA2015022101631Web · corrodedDURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF THE LT MOVABLE FAIRING. REPLACED VERTICAL WEB OF THE LT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.Feb 20, 2015 · N327NW · Airbus A320211 · Nacelle/Pylon Miscellaneous StructureSDR DALA2015022101670Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON TIE CLEAT ON FR 29 AND BETWEEN STR 42L TO STR 43L FWD CARGO COMPARTMENT, SSI 532180. REPLACED TIE CLEAT LOCATED FRAME 29 AND BETWEEN STR 42L TO STR 43L FWD CARGO COMPARTMENT IAW SRM 51-42-11 AND DWG D53231626 AND DWG D532Feb 20, 2015 · N327NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015021901451Structure · corrodedDURING INSPECTION, FOUND CORROSION ON STRUCTURE IN THE RT EMERGENCY EXIT DOOR. REPLACED THE STRUCTURE IAW SRM 51-72-11.Feb 18, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021901450Structure · corrodedDURING INSPECTION, FOUND CORROSION ON CURVE EDGE RT LOWER CORNER IN EMERGENCY EXIT DOOR. REPLACED THE STRUCTURE IAW SRM 51-72-11.Feb 18, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021901449Frame · crackedDURING INSPECTION, FOUND CRACK ON SEGMENT FRAME IN RT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11 AND DWG D52279010.Feb 18, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021901448Angle · crackedDURING INSPECTION, FOUND CRACK ON SEGMENT ANGLE RT, IN EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11.Feb 18, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021901446Angle · crackedDURING INSPECTION, FOUND A CRACK ON SEGMENT ANGLE IN EMERGENCY EXIT DOOR . REPLACED THE ANGLE IAW SRM 51-72-11.Feb 18, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021801380Wire · brokenDURING INSPECTION, FOUND ROW 22 EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AND FUNCTIONAL CHECKED NORMAL.Feb 17, 2015 · N312US · Airbus A320211 · Light System WiringSDR DALA2015021801379Access Panel · damagedDURING INSPECTION, FOUND DAMAGED ACCESS PANEL 640LB. REPLACED THE ACCESS PANEL.Feb 17, 2015 · N343NW · Airbus A320211 · Wing, Plate/SkinSDR DALA2015021801378Access Panel · damagedDURING INSPECTION, FOUND DAMAGED ACCESS PANEL 640KB . REPLACED THE ACCESS PANEL IAW SRM 57-27-11, PARA 4.B, FIG 102.Feb 17, 2015 · N343NW · Airbus A320211 · Wing, Plate/SkinSDR CA150216004Brake Assy · smoke(CAN) WHEN TAXIING OUT FOR DEPARTURE ON R06L, SMOKE BEGAN EMANATING FROM THE LT LG. ERS RESPONDED TO THE ACFT & LOCAL MX WAS DISPATCHED FOR INSPECTION. THE ACFT WAS THEN TOWED BACK TO THE GATE. RESOLUTION LT MLG WHEEL & BRAKES INSPECTED & OPERATIONAL TESTS Feb 16, 2015 · Airbus A320211 · Landing Gear Brake SystemSDR DALA2015021701268Frame · crackedDURING INSPECTION, FOUND CRACK ON FRAME IN THE EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11 AND DWG D52279010.Feb 16, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021701267Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.Feb 16, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021701266Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 35 - 36. FOUND TO BE OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370000.Feb 16, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021701265Floor Support · crackedDURING INSPECTION, FOUND CRACK ON FLOOR SUPPORT Y-254, FRAME 29. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 24 - 35 IAW SRM 51-72-11 AND DWG.Feb 16, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021701264Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL BETWEEN FRAMES 66 - 68. REPLACED THE SILL IAW SRM 51-72-11 AND DWG D534-80019.Feb 16, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021601377Angle · crackedDURING INSPECTION, FOUND CRACKED ANGLE ON RT EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11, DWGS D52279036, AND D52279010.Feb 15, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021601263Frame · crackedDURING INSPECTION, FOUND A CRACK ON THE FRAME IN THE LT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11, DWGS D52279040, AND D52279010.Feb 15, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021601262Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 47 - 64 . FOUND TO BE OUT OF LIMITS IAW JC NR 2500-2032. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND 53-41-15, FIG 202.Feb 15, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021601261Angle · crackedDURING INSPECTION, FOUND A CRACK ON THE ANGLE IN THE LEFT EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11, DWGS D52279036, AND D52279010.Feb 15, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015021601260Frame · crackedDURING INSPECTION, FOUND CRACK ON FRAME IN THE RIGHT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11, DWGS D52279040, AND D52279010.Feb 15, 2015 · N327NW · Airbus A320211 · Emergency ExitsSDR DALA2015022401724Door Sill · corrodedDURING INSPECTION, FOUND LT AFT UTILITY AREA FR68 JUST ABOVE DOOR, DOOR SILL HAS CORROSION, AROUND THE HOLE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12, L=0.95", W=0.75" ORIGINAL MATERIAL 0.098". REMOVED 0.046", REPAIRED FRAME IAW SRM 5Feb 14, 2015 · N335NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021401376Spar · corrodedDURING INSPECTION, FOUND CORROSION ON RT PYLON UPPER SPAR SPIGOT RECEPTACLE. PERFORMED PERMANENT REPAIR IAW SRM 54-51-12, CONFIG 1, PARA 5A FIG 201.Feb 13, 2015 · N327NW · Airbus A320211 · Nacelle/Pylon, Frame/Spar/RibSDR DALA2015021401375Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 35 - 36. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371024.Feb 13, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021401249Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT BETWEEN FRAMES 28 AND 29 STRINGERS 40-41L. REPLACED THE CLEAT IAW SRM 51-72-11 AND DWG D53231626.Feb 13, 2015 · N327NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2015021401248Floor Panel · delaminatedDURING INSPECTION, FOUND CORROSION ON FLOOR PANEL 261FF AT AFT GALLEY AREA. REPLACED FLOOR PANEL 261FF AT AFT GALLEY AREA AND INSTALLATION IS DOCUMENTED IN AMDS 2500-6602.Feb 13, 2015 · N327NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2015021401247Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 30 AND BETWEEN STRINGERS 41-42L. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231626.Feb 13, 2015 · N327NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2015021401250Floor Panel · damagedDURING INSPECTION, FOUND FLOOR PANEL 231 QF HAS FACE SKIN DAMAGE. FABRICATED NEW FLOOR PANEL IAW NW3025-37498.Feb 12, 2015 · N335NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2015021301233Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y765 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021301232Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y765 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021301231Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 41 - 47. FOUND OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021301230Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y1292 BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021301229Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765, BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021301228Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 35 - 36. FOUND OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371034.Feb 12, 2015 · N327NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015021901453Floor Support · crackedDURING INSPECTION, FOUND COCKPIT AREA BETWEEN FRAMES 11 & 12 + Y765 FLOOR SUPPORT CRACKED. REMOVED & REPLACED IAW SRM 51-42-11.Feb 11, 2015 · N335NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021201205Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472216.Feb 11, 2015 · N343NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021201204Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Feb 11, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021201203Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Feb 11, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021201202Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.Feb 11, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2015021201201Structure · corrodedDURING INSPECTION, FOUND CORROSION ON SILL BETWEEN FRAMES 66 - 68. REPLACED THE SILL. IAW SRM 51-72-11 AND DWG D53480019.Feb 11, 2015 · N327NW · Airbus A320211 · Fuselage Miscellaneous Structure
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