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 DALA12015343210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF DAMAGED 6.5" X 6.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Nov 28, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015333210Floor Panel · damagedDURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151PF DAMAGED ON EDGE 4.5" X 5.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.Nov 28, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015673210Skin · dentedDURING INSPECTION, FOUND LT SIDE LOWER AFT FUSELAGE FR 58, S23LTO S24L EXTERNAL SKIN SURFACE HAS DENT. PERFORMED DETAILED INSP, FOUND NOT TO BE DENTED BUT INDENTATION FROM PREVIOUSLY REPLACED FASTENER. CUTOUT DAMAGED AREA L=1.8" W=.750" IAW SRM 53-00-11, FIGNov 27, 2012 · N310NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA12015323210Seal Depressor · corrodedDURING INSPECTION, FOUND LT FWD PAX DOOR FRAME, MID SEAL SHAPE HAS CORROSION. REPLACED MID SEAL SHAPE IAW A320 SRM 51-42-11. NO LIMITS IAW SRM 53-11-14 PG BLK 101 DAMAGE DIM. L=1.60" W=1.50" D=0.006".Nov 27, 2012 · N310NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA12015313210Fitting · corrodedDURING INSPECTION, FOUND LT FWD PAX DOOR FRAME, LOWER AFT FITTING CORNER HAS CORROSION. NO ESTABLISHED LIMITS ON LOWER AFT FITTING CORNER OF L1 PAX DOOR FRAME. REPLACED AFT CORNER FITTING IAW SRM 51-42-11.Nov 27, 2012 · N310NW · Airbus A320211 · Fuselage Main, StructureSDR DALA12015663210Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131JF DELAMINATED 6.0" X 6.0". SLOPE PANEL FABRICATED NEW IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015463210Floor Panel · damagedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222EF HAS EDGE DAMAGE 4.0" X 4.0". FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015453210Floor Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DELAMINATED 3.0"X3.0". FLOOR PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015303210Panel · delaminatedDURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151MF DELAMINATED 5.0"X5.0". SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015293210Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131BF DELAMINATED 5.0" X 5.0". SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015283210Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132FF DELAMINATED 3.0" X 4.0". SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015273210Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132KF DAMAGED 4.5" X 4.5". SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015263210Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131KF DAMAGED 3.0" X 3.0". SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015253210Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132JF DAMAGED 4.5"X 3.5. SLOPE PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015243210Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF DAMAGED 2.0"X 2.5". FLOOR PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015233210Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131EF DAMAGED 5.0"X5.0". FLOOR PANEL FABRICATED IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015223210Floor Panel · crackedDURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 232FF CRACKED 4 INCHES LONG. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015213210Floor Panel · puncturedDURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231FF PUNCTURED 1.5" X 1.5". FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015203210Floor Panel · crackedDURING INSPECTION, FOUND CABIN FLOOR PANEL 232WF CRACKED. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 DWG 3D25-37498 DAMAGE DIM. L=2.0"X2.0".Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015193210Panel · delaminatedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132GF DELAMINATED 4.0" X 4.0". SLOPE PANEL FABRICATED NEW IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015183210Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131GF DAMAGED 4.0"X4.0". SLOPE PANEL FABRICATED NEW IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015173210Panel · damagedDURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131FF DAMAGED 6.0"X5.0". FORWARD CARGO SLOPE PANEL FABRICATED NEW IAW DWG 3D25-37705.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015163210Floor Panel · corrodedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222FF CORRODED ON UPPER SURFACE 2.5"X 3.5". FLOOR PANEL REPLACED IAW SRM 51-72-00.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015153210Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF CORRODED 4.0"X4.0". AFT UTILITY FLOOR PANEL 261FF REPLACED IAW SRM 51-72-00.Nov 26, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12015143210Floor Support · crackedDURING INSPECTION, FOUND COCKPIT FLOOR SUPPORT BTW FR 8-11 Y765 WEB CRACKED. REMOVED CRACKED WEB IAW SRM 51-42-11 CRACK MAX, LIMIT REPAIR=.31". LENGTH OF CRACK=.65". OUT OF LIMITS IAW SRM 53-11-14, FIG 205 SHT 1. REPLACED CRACKED WEB IAW SRM 51-42-11 AND Nov 25, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015133210Web · corrodedDURING INSPECTION, FOUND FORWARD CABIN RT SIDE BTW FR 20 TO FR 21 STGR 23 UPPER SURFACE WEB HAS CORROSION. SSI 531184. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=3", W=2",D=.010", ORIGINAL MATERIAL .075". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, Nov 25, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12013953223Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED. INOP LOCATIONS:8AB, ACARS TEXT: FRC3352028ABC, INTERIOR. INSTALLED LENS. OPS CHECK NORMAL.Nov 25, 2012 · N323US · Airbus A320211 · Emergency LightingSDR DALA12015653210Skin · damagedDURING INSPECTION, FOUND LOWER FUSELAGE DOUBLER REPAIR AT FR 23, LT SIDE, LWR AFT CORNER IS BENT AND HAS DENT AFT OF DOUBLER BETWEEN STRINGER 24 AND 25L . CUT-OUT DAMAGE AREA IAW SRM 53-11-11, FIG 214. L=9.250" W=4.250". HFEC IAW NTM 51-10-08, PB 6. NO DEFNov 24, 2012 · N310NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA12015123210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BTW FR 64 -65 Y1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT. .080" DAMAGE DIM. L=1.300" W=.810" D=.035". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED Y1292 FLNov 24, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015113210Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 65 TO FR 66 Y465 UPPER FLANGE HAS CORROSION AND 2 EA MISDRILLED HOLES. BLENDED AREA IAW SRM 51-74-00. ORIG MAT .079" L=1" W=1" D=.074" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Nov 24, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015103210Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR 18 TO FR 21 Y254 UPPER FLANGE HAS CORROSION & SCRIBE LINE AS MARKED. REMOVED CORROSION IAW SRM 51-74-00, DIM L=2.7" W= 1.5" D= .045" ORIG MAT .079" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIGNov 24, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015083210Floor Support · crackedDURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR 24-25 Y254 UPPER FLANGE CRACKED. CUT OUT DAMAGED L=3.5"W=.900" IAW SRM 53-00-14 FIG 204. HFE IAW NTM 51-10-08 NO CRACK INDICATIONS NOTED. FABRICATED REPAIR ANGLE. FABRICATED FILLER IAW SRM 53-0Nov 23, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015073210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68 TO FR 69 Y1292 UPPER FLANGE AND HARD POINT HOLES HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 L=.385"W=0.275"D=0.064" ORIGI NAL MAT 0.157"FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACENov 23, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015063210Fitting · corrodedDURING INSPECTION, FOUND LT AFT PASSENGER DOOR ENTRANCE CENTER SEAL SHAPED FITTING ATTACHED TO DOOR SILL HAS CORROSION. REMOVED L2 DOOR SHAPED SILL IAW SRM 51-42-11. INSTALLED NEW SHAPE SILL IAW SRM 51-42-11. NO SPECIFIC LIMITS IAW SRM 53-00-29.Nov 23, 2012 · N310NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA12013973227Battery Pack · inoperativeEMERGENCY OVERHEAD LIGHTS AFT INOPERATIVE. R & R EPSU AND BATTERY PACK IAW AMM 33-51-38. OPS CHECK NORMAL. TEST GOOD. OK FOR SERVICE.Nov 22, 2012 · N327NW · Airbus A320211 · Emergency LightingSDR DALA12015693210Skin · damagedDURING INSPECTION, FOUND RT SIDE LOWER AFT FUSELAGE FR 63 S28R - S29R EXTERNAL SKIN SURFACE HAS A BLENDED AREA IAW SRM 51-73-00, CHECKED LIMIT L=1.65" W=0.700" D=0.019", FOUND OUT OF LIMITS IAW SRM 53-41-11, DIAGRAM 102. CUTOUT DAMAGED SKIN (L=1.65" W=.700"Nov 21, 2012 · N310NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA12015093210Track · crackedDURING INSPECTION, FOUND COCKPIT CAPTAIN UPPER CENTER SLIDING WINDOW RAIL CRACKED. CUT OUT DAMAGE AREA OF THE RAIL AND DEBURR THE EDGES IAW SRM 53-11-12, FIG 203, SHEET 1 OPTION 1 REPAIR. HFEC IAW NTM 51-10-08 P-6 NO DEFECT NOTED. TREATED & PRIMED REWORK ARNov 21, 2012 · N310NW · Airbus A320211 · Fuselage Main, StructureSDR DALA12015053210Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR 20 TO FR 23 Y-189 UPPER FLANGE HAS CORROSION. BLENDED AREA FOUND TO BE OUT OF LIMITS ORIG MAT .079 DAMAGE DIM L=2.0" W=1.5" D=.013" TR83340. NO ESTABLISHED LIMITS IAW SRM 53-11-15. INSTALLED NNov 21, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12015043210Web · corrodedDURING INSPECTION, FOUND FORWARD CABIN LT SIDE AT FR 20 STRINGER 23 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=3.5 W=2.0 D=.063 ORIG .071 NO ESTABLISHED LIMITS AVAILABLE IAW SRM 53-11-14. INSTALLED NEW WEB IAW SRM 51-42-11.Nov 21, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013633210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 66 TO FR 70 Y765, UPPER FLANGE AND HARD POINT HOLES HAS CORROSION. BLENDED FLOOR SUPPORT ORIG. MAT. .130" DAMAGE DIM. L=2.0" W=1.5" D=.80". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. RNov 20, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013583227Power Supply · inoperativeDURING LANDING, F/A REPORTS LIGHTS OVER REAR EXIT DOORS FAILED TO COME ON WHEN GEAR COMES DOWN. MX REPLACED EPSU AT 13WL, BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Nov 20, 2012 · N327NW · Airbus A320211 · Emergency LightingSDR DALA12013623210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68 TO FR 70 Y254, HARD POINT HOLES HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-42-11,Nov 19, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013613210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 65 TO FR 66 Y765, UPPER FLANGE HAS CORROSION. REMOVED CORROSION ORIG. MAT .130", DAMAGE DIA L=1.7" W=.900" D=.040" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRMNov 19, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013603210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 66 TO FR 70 Y 765. UPPER FLANGE AND HARD POINT HOLES HAS CORROSION. BLENDED FLOOR SUPPORT ORIG MAT .130" DAMAGE DIM. L=2.0" W=1.5" D=.80", FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLNov 19, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013593210Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68 TO FR 70 Y254 HARD POINT HOLES HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Nov 19, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12013573210Fitting · corrodedDURING INSPECTION, FOUND RT AFT PASSENGER DOOR ENTRANCE CTR SEAL SHAPE FITTING ATTACHED TO DOOR SILL CORRODED. REMOVED R2 DOOR CENTER FITTING IAW SRM 51-42-11. RECEIVED CENTER FITTING . INSTALLED R2 NEW DOOR CENTER FITTING IAW SRM 51-42-11. NO SPECIFIED LIMINov 19, 2012 · N310NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA12013563210Sill · corrodedDURING INSPECTION, FOUND RT AFT PASSENGER DOOR ENTRANCE CENTER SEAL SHAPE FITTING ATTACHED TO DOOR SILL CORRODED. REMOVED R2 DOOR CENTER FITTING IAW SRM 51-42-11. INSTALLED R2 NEW DOOR CENTER FITTING IAW SRM 51-42-11. NO SPECIFIED LIMITS IAW SRM 53-00-29.Nov 19, 2012 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12014953210Floor Panel · brokenDURING INSPECTION, FOUND CABIN FLOOR PANEL 251FF BETWEEN FR 51 AND 53 CENTER ISLE IS BROKEN. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Nov 12, 2012 · N310NW · Airbus A320211 · Fuselage Floor PanelSDR DALA12012493229Battery Pack · faultedDURING NON ROUTINE CHECK, FOUND RT EMERGENCY LIGHT BATTERY PACK 12WL FAULTED. MAINTENANCE REPLACED BATTERY PACK AT 12WL AND FUNCTIONAL CHECK WAS NORMAL.Nov 10, 2012 · N329NW · Airbus A320211 · Emergency LightingSDR DALA12012383221Battery Pack · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU BATTERY AT LT FAILED TEST. MX REPLACED BATTERY AND FUNCTIONAL TEST WAS NORMAL.Nov 7, 2012 · N321US · Airbus A320211 · Emergency Lighting
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