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 DALA13003453213Panel · puncturedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152RF PUNCTURED (3" X 1") N/R 100/59. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00, FIG 209.Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13003443213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 161FF IS DAMAGED (3" X 2") PN D5367204800000. N/R 100/69. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00 FIG 209.Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13003433213Panel · erodedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152QF HAS EDGE EROSION (4" X 1") N/R 100/62. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00 FIG 209.Jan 20, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13003423214Floor Panel · damagedDURING INSPECTION, FOUND FORWARD CABIN FLOOR PANEL 222FF DAMAGE AND PUNCTURED. DAMAGED DIM: L=3" W=2" D=.020" NO ESTABLISH LIMIT ON SRM. REPLACED FLOOR PANEL, IAW SRM 5 1-72-11.Jan 20, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR CA130121012Idg · failed(CAN) CREW EXPERIENCED ELECTRICAL POWER INTERRUPTION IN CRUISE WHICH CAUSED MULTIPLE FAILURES INCLUDING THE LOSS OF 6 SCREENS, AUTO PILOT AND AUTO THROTTLE. NO DIVERSION WAS NECESSARY AS SOME SYSTEMS WERE RESTORED, FLIGHT CONTINUED TO DESTINATION AND LANDED WIJan 19, 2013 · Airbus A320211 · AC Generator-AlternatorSDR DALA13003133213Sill · corrodedDURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE LWR DOOR SILL AT AFT FR66 GIRT BAR HOLES UPPER SURFACE HAS REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W= 1.5" D=0.107". ORIG MAT 0.177. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R Jan 19, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13003653213Shackle · damagedDURING INSPECTION, FOUND RT PYLON AFT SHACKLE FWD PIECE, FWD FACE CHAFED AROUND THREE BUSHINGS. REPLACED WITH SERVICEABLE PART. SHACKLE INSTALLED ON W/C 5450-6010-RT DUE TO NO SPECIFIC ALLOWABLE DAMAGE SPECIFIED IAW SRM 54-51-17.Jan 18, 2013 · N313US · Airbus A320211 · Nacelle/Pylon, Attach FittingsSDR CA130117010Line · failed(CAN) APPROXIMATELY 1 HR AFTER TAKEOFF THE CREW REPORTED THEY HAD LOST THEIR BLUE HYDRAULIC SYSTEM. AT THE TIME OF THIS REPORT THERE HAVE BEEN NO FURTHER COMPLICATIONS, ITEM RESOLVE UNDER MDDR: 87626, HYD LINE TO BLUE SYSTEM DAMPENER REPLACED IAW AMM 29-12-00Jan 17, 2013 · Airbus A320211 · Hydraulic System, MainSDR DALA13003573214Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED. REPLACED IAW SRM 51-72-11.Jan 17, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003143219Battery Pack · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST ON SERVICE CHECK FAULT'S INTERIOR AND EXTERIOR. MX REPLACED LT MID EPSU AND BATTERY. FUNCTIONAL CHECK WAS NORMAL.Jan 17, 2013 · N319US · Airbus A320211 · Emergency LightingSDR DALA13003103213Seat Track · corrodedDURING INSPECTION, FOUND FORWARD CABIN SEAT TRACK BETWEEN FR 20 TO FR 21 Y-765 UPPER CROWN HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=3.330"W=.380"D=.037"ORG MAT .125". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. R Jan 17, 2013 · N313US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13002743213Panel · damagedDURING INSPECTION, FOUND FORWARD CARGO COMPARTMENT SLOPE PANEL 131CF IS DAMAGED. 1" X 1". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002733213Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131JF HAS EDGE DAMAGE 3.5" X 4.0". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002723213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 161EF HAS EDGE DAMAGE AROUND TDP CUT OUT (1" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002713213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 162BF IS DAMAGED (3" X 12"). FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002703213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152CF IS DAMAGED (8" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002693213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151EF IS DAMAGED 4" X 1". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002683213Panel · puncturedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151MF HAS PUNCTURE & EDGE EROSION A ROUND TDP CUT OUT (4" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002673213Panel · damagedDURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151NF IS SOFT (3" X 2.5"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002663213Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS EDGE DAMAGED 3.0" X 3.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002653213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF IS DAMAGED. 3.0" X 2.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002643213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF IS DAMAGED. 4.5" X 3.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002633213Floor Panel · damagedDURING INPECTION, FOUND AFT CARGO FLOOR PANEL 151LF IS DAMAGED, 4.0" X 4.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002623213Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF IS DAMAGED, PN D5367205300000. 3" X 2.5". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Jan 17, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002613214Floor Panel · damagedDURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262FF DAMAGED AND CORRODED. DAMAGE DIMENSIONS: L=4" W=2" D=0.015" NO ALLOWABLE LIMIT ESTABLISHED ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.Jan 17, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13003643214Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y765 BETWEEN FR66 AND FR70 HAS SIX AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jan 16, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002503213Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF HAS CORROSION. FLOOR PANEL REPLACED IAW SRM 51-72-00.Jan 16, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002493213Fitting · mismanufacturedDURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER MID FWD SHAPE FITTING EXISTING HOLES MISDRILLED. REMOVED DOORSILL SHAPE FITTING IAW SRM 51-42-11. RECEIVED NEW DOOR SILL SHAPE FITTING, PN: D5348004800104, BATCH 0002379438. LOCATED AND DRILLED SILL SHAJan 16, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002483213Floor Panel · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FLOOR PANEL 222FF HAS CORROSION ON BOTTOM AREA 6" X 1". NO ESTABLISHED LIMITS IAW SRM. REPLACED FLOOR PANEL IAW SRM 51-72-00.Jan 16, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002473213Floor Panel · corrodedDURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FLOOR PANEL 221FF HAS CORROSION ON BOTTOM AREA 3" X 1". NO ESTABLISHED LIMITS IAW SRM. REPLACED FLOOR PANEL.Jan 16, 2013 · N313US · Airbus A320211 · Fuselage Floor PanelSDR DALA13002463214Web · corrodedDURING INSPECTION, FOUND FWD UTILITY AREA FRAME 20, RT WEB CORRODED. REPLACED RT WEB IN FWD UTILITY AREA WITH PN D53112 78520301 IAW SRM 51-42-11. NO ALLOWABLE DAMAGE FOUND IN SRM.Jan 16, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13002203213Hinge Pin · damagedDURING INSPECTION, FOUND LT AILERON, HINGE PIN NR 3 SCORED. NEW LT AILERON NR 3 HINGE INSTALLED. SCORED NR 3 HINGE PIN FOUND OUT OF LIMITS PER AMM 27-14-41, PB 601.Jan 14, 2013 · N313US · Airbus A320211 · Wing, Control Surface Attach FittingsSDR DALA13002193213Structure · corrodedDURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE LOWER MID FWD SHAPE FITTING CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED SHAPE SILL IAW SRM 51-42-11, L=4.0 W=2.0 D=.050.Jan 14, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13001113213Seat Track · gougedDURING INSPECTION, FOUND MID CABIN SEAT TRACK BETWEEN FR35-FR36 Y765 HAS GOUGE. REMOVED DAMAGE & FOUND TO BE OUT OF LIMITS IAW TRM 53-00-15, FIG 1, BOTTOM SURFACE. REPLACED Y765 SEAT TRACK BETWEEN FR35-FR36 IAW SRM 51-42-11.Jan 14, 2013 · N313US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13000843213Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR20 TO FR23, Y-189 UPPER FLANGE CORROSION AND SCRIBE LINE MARKS. BLENDED FLOOR SUPPORT IAW SRM 51-74-00 AFTER REWORK, D=.024", L=1.5", W=.50". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 104.Jan 13, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000833214Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR16 TO FR21, Y1292 UPPER FLANGE HAS CORROSION. BLENDED CORROSION ON Y1292 FLOOR SUPPORT IAW SRM 51-74-00 DIM ON CROWN AT SEAT TRACK IS L=2.0 W=.375 D=.053 FOUND TO BE OUT OF LIMITS IAWJan 12, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000823213Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR64 TO FR66, Y765 UPPER FLANGE AND INSIDE HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, BLENDED AREA MEASURES L=1.83", W=1.80", D=.055", ORIG MAT 0,087 FOUND TO BE OUJan 12, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000803213Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR12 TO FR22, Y254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 51-74-00, AND CHECK LIMITS ORIG THICKNESS .141", L=7.20", W=1.30", D=0.51 FOUND TO BE OUT OFJan 11, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000663213Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 65-67, Y-308 INSIDE HARD POINT HOLES 3EA HAS SURFACE CORROSION. BLENDED AREA IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOOR SUPPORT IAW SRM 51-42-Jan 9, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000583213Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 12-16, Y503.2 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG THICK .149" AFTER BLENDED .089" OUT OF LIMITS IAW SRM 53-11-15, FIG 105 L=1.7 W=1.4" D=.060" REMOVED Jan 8, 2013 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13000413213Floorbeam · corrodedDURING INSPECTION, AFT CABIN UTILITY AREA FLOORBEAM AT FR 66, Y1292 UPPER FLANGE HAS CORROSION AND ELONGATED HOLE. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.9" W=1.3" D=0.020" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOORBJan 7, 2013 · N313US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13000183222Battery Pack · faultedDURING NON ROUTINE CHECK, FOUND EMERGENCY POWER SUPPLY 11WL BATTERY FAULTED. MX REPLACED BATTERY PACK AT 11WL AND FUNCTIONAL CHECK WAS NORMAL.Jan 4, 2013 · N322US · Airbus A320211 · Emergency LightingSDR DALA12016983231Light · missingDURING NON ROUTINE CHECK, FOUND IN SEAT ESCAPE PATH LIGHTING MISSING AT SEAT 5C. MX INSTALLED A NEW IN SEAT ESCAPE PATH LIGHT AND FUNCTIONAL TEST WAS NORMAL.Dec 20, 2012 · N331NW · Airbus A320211 · Emergency LightingSDR DALA12016903210Sill · corrodedDURING INSPECTION, FOUND FWD CARGO PIT DOOR SILL HAS CORROSION IN SEVERAL PLACES AS MARK NR 130/54. REMOVED CORROSION IAW SRM 51-74-00, NO ESTABLISH LIMITS. REMOVED DOOR SILL PLATE IAW SRM 51-42-11, FABRICATED SILL PLATE FROM MATERIAL 2024-T3 .100' IAW SRM Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12016693210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DAMAGED AND DAMAGE DIM L=3" X W=2". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12016683210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152QF DAMAGED WITH DIM OF DAMAGED L=2" X W=1.5". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.Dec 18, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12016423210Beam · corrodedDURING INSPECTION, FOUND FWD LT OVERWING EMERGENCY EXIT DOOR CURVED BEAM HAS CORROSION. REMOVED CORROSION FROM CURVED BEAM IAW SRM 51-74-00 AND CHECK LIMITS ORIG THICK .039" AFTER REWORK .033" MAT. LOSS .006" NO ESTABLISH LIMITS IN SRM. BLENDED AREA L=5.5" Dec 16, 2012 · N310NW · Airbus A320211 · Emergency ExitsSDR DALA12016413210Support Angle · corrodedDURING INSPECTION, FOUND LT FWD OVERWING EMERGENCY EXIT DOOR AFT VERTICAL FRAME ANGLE SUPPORT CORRODED. REMOVED VERTICAL FRAME ANGLE SUPPORT IAW SRM 51-42-11. RECEIVED NEW ANGLE SUPPORT, PN D5227905420400 BATCH NR: 0002049167. INSTALLED NEW VERTICAL FRAME ANDec 16, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12016303226Battery Pack · failedDURING NON ROUTINE CHECK AND WHILE WORKING JIC 2561-4002-RF RECEIVED EPSU BATTERY EMERGENCY RT FAILURE MESSAGE ON CIDS PANEL. REPLACED EPSU BATTERY AT RIGHT AND FUNCTIONAL CHECK WAS NORMAL.Dec 15, 2012 · N326US · Airbus A320211 · Emergency LightingSDR DALA12016243210Frame · corrodedDURING INSPECTION, FOUND RT AFT PASSENGER DOOR SILL AFT FRAME 66, UPPER SURFACE AROUND NUT PLATE HOLES HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-74-00. DIM. L=2", W=1.3", D=.035". FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG1, SH2. ACCOMPLISHED ROTO Dec 13, 2012 · N310NW · Airbus A320211 · Fuselage Main, Frame
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