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 DALA1231363211Power Supply · inoperativeDURING SERVICE CHECK, FOUND THE LEFT EMERGENCY POWER SUPPLY UNIT AT 10WL FAILED TEST. MAINTENANCE REPLACED POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL. A/C RETURNED TO SERVICE.May 11, 2012 · N311US · Airbus A320211 · Emergency LightingSDR DALA1231373209Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND THE LOWER EMERGENCY EXIT SIGNS AT FWD AND AFT RIGHT OVERWING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. A/C RETURNED TO SERVICE.May 10, 2012 · N309US · Airbus A320211 · Emergency LightingSDR DALA1230823209Skin · damagedDURING INSPECTION, FOUND LT WING INBD FLAP HAS COMPOSITE DAMAGE ON UPPER SKIN APPROX 5FT FROM INBD END. REPAIRED LT WING INBD FLAP IAW SRM 57-52-00 PARAGRAPH 8F FIG 206.May 10, 2012 · N309US · Airbus A320211 · Trailing Edge FlapsSDR DALA1230873209Ring · gougedDURING INSPECTION, FOUND LT ENGINE OTBD THRUST REVERSER 9 O'CLOCK TO 12 O'CLOCK JAY RING GOUGED AND HAS FRETTING DAMAGE. REPLACED LT ENGINE OTBD THRUST REVERSER JAY RING IAW CMM 78-32-35. ADJUSTED LT ENGINE RING IAW AMM 78-36-42-820-001.May 9, 2012 · N309US · Airbus A320211 · Engine Thrust ReverserSDR CA120509006Brake · overheated(CAN) RAMP CREW NOTICED SMOKE EMANATING FROM RT MAIN GEAR ON ARRIVAL AT GATE. CFR REMAINED ON STANDBY UNTIL TEMPERATURES SUBSIDED. RT MLG BRAKE TEMP INDICATING 490C ON NR 3 BRAKE AND 490C ON NR 4 BRAKE. LT 250 C. EMERGENCY DECLARED BY SOMEONE DUE SMOKING May 6, 2012 · Airbus A320211 · Landing Gear Brake SystemSDR DALA1229523209Stringer · corrodedDURING INSPECTION, FOUND FWD CARGO COMPARTMENT BETWEEN FR 30 AND FR 31, STR 41L STRINGER DOUBLER HAS CORROSION. REPLACED STRINGER DOUBLER IAW SRM 51-42-11.May 3, 2012 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA12000693209Shear Tie · corrodedDURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR 32 BETWEEN STR 41R AND STR 42R, FRAME CLIP HAS CORROSION. REMOVED CLIP IAW SRM 51-42-11. FABRICATED NEW CLIP IAW SRM 53-21-12 AND INSTALLED CLIP IAW SRM 51-42-11.May 2, 2012 · N309US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA12000683209Shear Tie · corrodedDURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR32 BETWEEN STR 42R AND STR 43R, FRAME CLIP HAS CORROSION. REMOVED CLIP IAW SRM 51-42-11. FABRICATED NEW CLIP IAW SRM 53-21-12 AND INSTALLED IAW SRM 51-42-11.May 2, 2012 · N309US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA12000663209Angle · corrodedDURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR33 BETWEEN STR 42L AND STR 43L, FRAME ANGLE HAS CORROSION. REMOVED ANGLE IAW SRM 51-42-11. FABRICATED NEW ANGL IAW SRM 53-21-12 AND INSTALLED IAW SRM 51-42-11.May 2, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA12000653209Angle · corrodedDURING INSPECTIONS, FOUND FWD CARGO COMPARTMENT FR30, BETWEEN STR 41R AND STR 42R FRAME ANGLE HAS CORROSION. REMOVED ANGLE IAW SRM 51-42-11. FABRICATED ANGLE AND INSTALLED IAW SRM 51-42-11.May 2, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1228973209Stringer · corrodedDURING INSPECTIONS, FOUND FWD CARGO BAY BETWEEN FRAMES 30 AND 31, STR 42R, STRINGER DOUBLER HAS CORROSION. REMOVED SHEER TIE FOR ACCESS IAW SRM 51-42-11. REMOVED SPLICE FABRICATED NEW SPLICE ON STAM TRAVELER INSTALLED SPLICE AND SHEAR TIE FABRICATED IAW SRMay 2, 2012 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA1228933209Stringer · corrodedDURING INSPECTIONS, FOUND FWD CARGO BAY BETWEEN FRAMES 33 AND 34, STRINGER 42R DOUBLER HAS CORROSION. REMOVED CORROSION, FABRICATED NEW ANGLE AND INSTALLED ANGLE IAW SRM 53-00- 13 FIG 202.May 2, 2012 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA1226883209Floor Panel · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221FF CORRODED 5.0" X 5.0". RECEIVED NEW FLOOR PANEL PN ES367147800600, TO BE INSTALLED ON W/C 2500-6601.Apr 25, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1226863209Floor Panel · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF CORRODED 4.5" X 3.0". RECEIVED NEW FLOOR PANEL PN ES367 147800600, TO BE INSTALLED ON W/C 2500-6601.Apr 25, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1226833209Floor Panel · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221FF CORRODED 5.0" X 5.0". RECEIVED NEW FLOOR PANEL PN ES367147800600, TO BE INSTALLED ON W/C 2500-6601.Apr 25, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA12006953209Structure · corrodedDURING INSPECTIONS, FWD CARGO COMPARTMENT BETWEEN FR 28 AND FR 29 STRINGER 41R HAS CORROSION. REMOVED FASTENERS FROM FR 28 TO FR 29 STGR 41R IAW SRM 51-42- 11. REMOVED CORROSION IAW SRM 51-74-00. INSTALLED REPAIR PARTS IAW SRM 53-21-13 FIG 202.Apr 23, 2012 · N309US · Airbus A320211 · Fuselage Main, StructureSDR DALA1226523209Doubler · corrodedDURING INSPECTIONS, FOUND FWD CARGO COMPT BET FR29 AND FR30, STRG 41R STRINGER DOUBLER HAS CORROSION. REMOVED CORROSION IAW A320 SRM 51-74-00, NO ALLOWABLE LIMITS. FABRICATED REPAIR AND INSTALLED PER SRM 53-21-13 FIG 203 SHEET 2.Apr 23, 2012 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA1231383209Skin · dentedDURING INSPECTIONS, FOUND FWD LWR FUSELAGE SKIN DENTED APPROX 7 O'CLOCK POSITION AT FR 2 REQUIRES RE-EVALUATION. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 DIAGRAM 103 PARAGRAPH 4C. ACCOMPLISHED REPAIR AS PER ER/A NR 501388-14 REV. REV ORIGINAL SECTION 1 PEApr 22, 2012 · N309US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA1226213209Floor Support · crackedDURING INSPECTON, FOUND COCKPIT, FWD OF FR11, LT SIDE AREA, 37 INCHES FROM O/B, FLOOR SUPPORT WEB HAS CRACK AT LOWER AFT CORNER. MEASURED LENGTH OF CRACK IS 0.450 INCH THE ALLOWED IS 0.310 INCH FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-14 FIG 205, REMOVEDApr 22, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1226053209Web · corrodedFORWARD UTILITY AREA LT SIDE AT FR 16 UPPER SURFACE WEB HAS SURFACE CORROSION. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11. NO ESTABLISHED LIMITS. ORIG MAT=0.070" DAMAGE DIM. L=1.70" W=1.40" D=0.008".Apr 22, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA120423016Warning Message · false activation(CAN) ON DEPARTURE THROUGH 800-900 FT, ACFT HAD AN AVIONICS SMOKE MESSAGE ECAM ALERT. THERE WERE NO INDICATIONS OF VISIBLE SMOKE. FLIGHT RETURNED, DECLARE AN EMERGENCY AND LANDED. NO PHYSICAL EVIDENCE OF SMOKE AEVC RESETED. FAULT CLEARED. AEVC SYSTEM TEST OApr 20, 2012 · Airbus A320211 · Smoke DetectionSDR DALA1226043209Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT FROM FR18 TO FR20 RT -Y254 UPPER SURFACE CORRODED. NO ALLOWABLE DAMAGE ON SRM, REMOVED FLOOR SUPPORT AND SPLICES IAW A320 SRM 51-42-11. RECEIVED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW A320 SRM 51-42-11. ORIG MAT 0.12Apr 20, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1226033209Floor Support · damagedMID CABIN AT FR36 Y765 -Y1292 FLOOR SUPPORT UPPER FLANGE HAS SCRIBE MARK. REMOVED AND REPLACED FLOOR SUPPORT AT FR36 Y765 -Y1292 IAW A320 SRM 51-42-11. RETAIN FOR RECORDS.Apr 20, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224663209Floorbeam · corrodedDURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM UPPER LOWER SURFACE HOLES FROM FR66 TO FR68 -Y1292 CORRODED. REMOVED FLOOR SUPPORT BEAM IAW A320 SRM 51-42-11 AND INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.Apr 17, 2012 · N309US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA1224633209Floorbeam · corrodedDURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM FROM FR68-69-Y1292 UPPER AND LOWER SURFACE HOLES CORRODED & SEVERAL BROKEN RIVETS. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.Apr 17, 2012 · N309US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA1224623209Floorbeam · corrodedDURING CHECK, FOUND AFT UTILITY AREA FLOORBEAM UPPER SURFACE FROM FR 64T0 FR 66 RT -Y1292 HARD POINT HOLES CORRODED. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11.Apr 17, 2012 · N309US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA1224503209Floor Support · brokenDURING CHECK, FOUND FWD CABIN BETWEEN FR30 TO FR31 -Y254 FLOOR SUPPORT BROKEN UPPER FLANGE MISSING PIECES BY 2.800" X.900". LOCATED AND DRILLED REPAIR PARTS IAW A320 SRM 53-00-14 FIG 204. TREATED AND PRIMED REPAIR. INSTALLED REPAIR PARTS IAW A320 SRM 53-00-Apr 16, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224563209Sill · corrodedDURING CHECK, FOUND RT AFT PASSENGER DOOR SILL BEAM UPPER SURFACE FROM FR66 TO FR68 & GIRT BAR ATTACH HOLES CORRODED. BLENDED AREA IAW A320 SRM51-74-00 DIM.L=2.0"W=0.400" D=0.072" FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-41-14- FIG 101. REPLACED DOOR SILL IApr 15, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224453209Seat Track · corrodedDURING CHECK, FOUND FWD UTILITY AREA FLOOR SUPPORT FROM FR18TO FR21 UPPER FLANGE & SEAT TRACK CORRODED. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00 CHECKED LIMITS W=.21" L=1.5" D=.035" FOUND TO BE OUT OF LIMITS PER SRM 53-00-15 FIG 101. REPLACED SEATApr 15, 2012 · N309US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1224023209Seat Track · corrodedFORWARD UTILITY AREA FLOOR SUPPORT FROM FR18 TO FR21 UPPER FLANGE AND SEAT TRACK CORRODED -Y765. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00 CHECKED LIMITS W=.21" L=1.5" D=.035". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15 FIG 101. REMOVED AND RApr 15, 2012 · N309US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1223803209Seat Track · corrodedFORWARD UTILITY AREA FLOOR SUPPORT FROM FR18 TOFR21 UPPER FLANGE AND SEAT TRACK CORRODED -Y765. SSI 531189. REMOVED CORROSION BY BLENDING IAW A320 SRM 51-74-00. CHECKED LIMITS W=.21" L=1.5" D=.035". FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15 FIG 101. Apr 15, 2012 · N309US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1224893209Floor Panel · delaminatedDURING INSPECTION, FOUND AFT PIT FLOOR PANEL 151AF IS DELAMINATED, 14" X 12" AREA. FABRICATED FLOOR PANEL 151AF ON STAM TRAVELER #T12/927895 PER DWG 3D25-37705. PANEL TO BE INSTALLED ON W/C 2500-5019.Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224863209Floor Panel · delaminatedDURING INSPECTION, FOUND FWD PIT FLOOR PANEL 131HF DELAMINATED AND IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED FLOOR PANEL 131HF ON STAM TRAVELER T12/927777 PER DWG 3D25-37705. DAMAGE DIA L=6" X W=6". PANEL TO BE INSTALLED ON W/C 2500-5018.Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224853209Floor Panel · delaminatedDURING INSPECTION, FWD PIT FLOOR PANEL 131AF IS DELAMINATED AND MISSING UPPER SKIN AROUND TIE DOWN. FABRICATED FLOOR PANEL 131AF ON STAM TRAVELER #T12/927774 PER DWG 3D25-37705. DAMAGE DIA. L=6" X W=6" PANEL TO BE INSTALLED ON W/C 2500-5018, STAM CRS#MZARO13Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224833209Floor Panel · delaminatedDURING INSPECTION, FWD PIT FLOOR PANEL 131EF IS DELAMINATED,12" X 12" AREA. FABRICATED FLOOR PANEL 131EF ON STAM TRAVELER #T12/927772 PER DWG 3D25-37705. PANEL TO BE INSTALLED ON W/C 2500-5018.Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224753209Floor Panel · delaminatedDURING CHECK, FOUND FWD CABIN FLOOR PANEL 221AB IS DELAMINATED, 8" X 3" AREA. FABRICATED FLOOR PANEL 221AB ON STAM TRAVELER #T12/928077 PER DWG 3D25-37498. DAMAGE DIM L=8" X W=3", PANEL TO BE INSTALLED ON W/C 2500-6617.Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224613209Floor Support · corrodedDURING CHECK, FOUND FWD CABIN FLOOR SUPPORT FROM FR18 TO FR21 RT -Y1292 UPPER SURFACE AND SEAT TRACK CORRODED. INSTALLED NEW FLOOR SUPPORT SUPPORT BEAM P/N D5311278220201 IAW A320 SRM 51-42-11.Apr 14, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224043209Blanking Plate · corrodedR2 DOOR FWD AND AFT BLANKING PLATES CORRODED. RETAIN FOR RECORDS. REPLACED BLANKING PLATES FORWARD AND AFT AT R2 DOOR IAW A320 SRM 51-72-00. INSTALLED ON W/C 2500-6602.Apr 14, 2012 · N309US · Airbus A320211 · Service DoorsSDR DALA1224743209Floor Panel · corrodedDURING CHECK, FOUND AFT CABIN FLOOR PANEL 261FF HAS CORROSION AT LOWER AND UPPER SURFACE. RECEIVED NEW FLOOR PANEL P/N D5367180500200 BATCH#0002216084. PANEL TO BE INSTALLED ON W/C 2500-6602.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224733209Floor Panel · corrodedDURING CHECK, FOUND AFT CABIN FLOOR PANEL 262FF HAS CORROSION AND EDGE DAMAGE. RECEIVED NEW FLOOR PANEL P/N D5367180500300 BATCH#0002216005. PANEL TO BE INSTALLED ON W/C 2500-6602.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224273209Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM AT FR68 TO FR69 LT Y1292 UPPER SURFACE HOLES CORRODED. REMOVED NEW FLOORBEAM. INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11. BLENDED OUT CORROSION IAW A320 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-31-15 FIG 101.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA1224253209Floorbeam · corrodedUTILITY AREA FLOORBEAM AT FR 66 TO FR 68 LT Y1292 UPPER SURFACE SEVERAL HOLES CORRODED. REMOVED FLOORBEAM +Y1292 FR66 TO 68 IAW A320 SRM 51-42-11. RECEIVED NEW FLOORBEAM INSTALLED NEW FLOORBEAM IAW A320 SRM 51-42-11. BLENDED OUT CORROSION IAW A320 SRM 51-74Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA1224233209Floor Panel · damagedAFT CABIN FLOOR PANEL 261DF HAS MULTIPLE PUNCTURES AND DELAMINATED. FABRICATED FLOOR PANEL 261DF IAW DWG 3D25-37498. DAMAGE DIM L=1.5" W=1.5". RETAIN FOR RECORD.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224213209Floor Panel · crackedAFT CABIN FLOOR PANEL 261PF HAS A CRACK AND DELAMINATION AROUND A FASTENER HOLE. FABRICATED FLOOR PANEL 261PF IAW DWG 3D25-37498. DAMAGE DIM L=2.7" W=2.7". RETAIN FOR RECORD.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224193209Floor Panel · damagedFORWARD CABIN FLOOR PANEL 232FF HAS AN ELONGATED HOLE. FABRICATED FLOOR PANEL 231FF IAW DWG 3D25-37498. DAMAGE DIM L=2.4" W=2.4". RETAIN FOR RECORD.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224173209Floor Panel · corrodedFORWARD CABIN FLOOR PANEL 232DF HAS CORROSION AROUND INSERT. FABRICATED FLOOR PANEL 232DF IAW DWG 3D25-37498. DAMAGE DIM L=3.5" W=2.5". RETAIN FOR RECORD.Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Floor PanelSDR DALA1224093209Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT FROM FR12 TO FR16 RT -Y81 HARD POINT HOLES AND UPPER FLANGE CORRODED. REMOVED CORROSION IAW A320 SRM 51-74-00. DAMAGED DIM. L=1.25" W=.042" D=.051". CHECKED LIMITS IAW A320 SRM 53-11-14 FIG 106 FOUND TO BE OUT OF LIMITS. Apr 13, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224713209Panel · damagedDURING CHECK, FOUND AFT PIT SLOPE PANEL 161BF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. FABRICATED SLOPE PANEL ON STAM TRAVELER T12/927902 (161BF) IAW DWG 3D25-37705. DAMAGE DIM. L=8.0" W=8.5".Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224703209Panel · missingDURING CHECK, FOUND AFT PIT SLOPE PANEL 152QF IS MISSING UPPER SKIN AROUND TIE DOWN FITTINGS. AFT PIT SLOPE PANEL 152QF FABRICATED NEW ON STAM TRAVELER T12/927901 IAW DWG 3D25-37705. DAMAGE DIM. L=10" W=10".Apr 12, 2012 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA1224673209Panel · delaminatedDURING CHECK, FOUND AFT CARGO SLOPE WALL PANEL 152 RF DELAMINATED. FABRICATED NEW ON STAM TRAVELLER T12/928061 IAWDWG 3D25-37705.Apr 12, 2012 · N309US · Airbus A320211 · Cargo Compartments
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