Airbus A320-211

Service difficulty reports · 5,271

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA13014353215Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1292. REPLACED FLOORBEAM AND FASTENERS, IAW SRM 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13014213215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 42R TO STR 43R. REPLACED CLEAT IAW SRM 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014203215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 42L TO STR 43L. REPLACED CLEAT IAW SRM A320 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014193215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT. REPLACED CLEAT IAW SRM 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014183215Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM. REPLACED FLOORBEAM AND FASTENERS IAW SRM A320 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13014173215Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1162. REPLACED FLOORBEAM IAW SRM 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13014163215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 28 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. REPLACED CLEAT IAW 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014153215Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM BS 1225. REPLACED FLOORBEAM IAW SRM 51-72-11.Apr 2, 2013 · N315US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13013953215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT FR 28 AND BETWEEN STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. MEASURE APROX L=1.750" W=0.600" D=0.003". REPLACED CLEAT IAW SRM 51-72-11 .Mar 31, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13013943215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT FR 29 AND BETWEEN 42R TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURE APROX. L=3.500" W=0.350" D=0.002". REPLACED CLEAT AND FASTENERS IAW SRM 51-72-11 AND DWG D53231626.Mar 31, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13013933215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 29 AND BETWEEN STR 43R TO STR 44 IN FWD CARGO COMPARTMENT. MEASURE APROX L=2.100" W=0.350" D=0.002". REPLACED CLEAT AND FASTENER AT FR 29 AND BETWEEN STR 43R TO STR 44 FWD CARGO COMPARTMENT IAW SRM 51-72-11.Mar 31, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13013923215Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1732 LOCATED FR.65+19.5" RT SIDE AFT CABIN FLOOR STRUCTURE L=1" W=0.5" D=0.002" APROX. REPLACED FLOORBEAM -Y1732 LOCATED FR 65 TO FR 66 RT SIDE CABIN FLOOR STRUCTURE IAW SRM 51-72-11.Mar 31, 2013 · N315US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13013913215Structure · corrodedDURING INSPECTION, FOUND CORROSION ON BEAM -Y765 LOCATED FR 65+21" AFT CABIN FLOOR STRUCTURE L=0.5" W=0.025" D=0.001" APROX SSI 534147. REPLACED BEAM -Y765 LOCATED FR 65+21" AFT CABIN FLOOR STRUCTURE IAW SRM 51-72-11.Mar 31, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014143215Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FR 66 AND FR 68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.Mar 30, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014133215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.800" W=0.300" D=0.002" REPLACED CLEAT AT FR 32 AND BETWEEN STR 41L TO STR 42L IN FORWARD CARGO COMPARTMENT IAW SRM A320 51-72-11.Mar 30, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014123215Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41L TO STR 42L IN FWD CARGO COMPARTMENT. REPLACED CLEAT AT FR 30 AND BETWEEN STR 41L TO STR 42L IN FORWARD CARGO COMPARTMENT IAW SRM 51-72-11.Mar 30, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014113215Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING FWD PAX CABIN BETWEEN FR 16+5" TO FR 19+5" AND AT LEVEL OF STR 23R. L=0.230", W=0.113", D=0.002". REPLACED CENTER FITTING IAW SRM 51-72-11.Mar 30, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13014103215Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD CABIN LT ENTRY DOOR LOWER SILL, REPLACED CENTER FITTING, FWD CABIN LT ENTRY DOOR LOWER SILL IAW SRM A320 51-72-11, DWG D53112198.Mar 30, 2013 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13013513215Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 LOCATED BETWEEN FR 36 TO FR 41 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53372500.Mar 27, 2013 · N315US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13013503215Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 LOCATED BETWEEN FR 36 TO FR 41 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11, AND DWG D57130146.Mar 27, 2013 · N315US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13013493215Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 LOCATED BETWEEN FR 41 TO FR 47 AND IS BEYOND ALLOWABLE DAMAGE LIMITS IAW ROUTINE CARD 2500-2031. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.Mar 27, 2013 · N315US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR CA130326002Actuator · failed(CAN) THE ACFT ENCOUNTERED A GREEN HYDRAULIC FAILURE MESSAGE AT THE TOP OF DESCENT TO RUNWAY. AS A PRECAUTION, THE FLIGHT CREW DID DECLARE AN EMERGENCY AND CFR WERE ON STANDBY. AFTER LANDING, THE ACFT WAS INSPECTED BY CFR ON THE RUNWAY WITH NIL ADVERSE RESULTSMar 23, 2013 · Airbus A320211 · Autopilot SystemSDR DALA13012753220Wire · brokenDURING CHECK, FOUND EMERGENCY LIGHT AT SEAT 20 ABC INOPERATIVE. MX REPAIRED BROKEN WIRE AND FUNCTIONAL CHECKED NORMAL.Mar 17, 2013 · N320US · Airbus A320211 · Light System WiringSDR CA130318015Feeder Cable · failed(CAN) ON DEPARTURE, CREW IMMEDIATELY LOST POWER FROM THE NR 1 GENERATOR. ECAM RESET WAS CARRIED WITH NO FIX. APU WAS STARTED TO SUPPLEMENT ELECTRICAL POWER. CREW ELECTED TO RETURN WERE A AN OVERWEIGHT LANDING WAS CARRIED OUT. DUTY PILOT WAS ADVISED. FEEDER Mar 16, 2013 · Airbus A320211 · Electrical Power System WiringSDR DALA13010473223Wire · damagedDURING NON-ROUTINE CHECK AND WHILE DEPLOYING LT WING SLIDE, FOUND LIGHTS ON SLIDE TO BE INOPERATIVE. MX REPAIRED WIRE AND REPLACED EPSU W/O BATTERY. FUNCTIONAL CHECK WAS NORMAL.Mar 5, 2013 · N323US · Airbus A320211 · Light System WiringSDR CA130308005Duct · failed(CAN) "AIR LT WING LEAK" ECAM MESSAGE DURING ENGINE START. AIR LEAK FOUND AT DUCT ASSEMBLY AND AUXILIARY POWER UNIT CHECK VALVE. THE FLANGE ON THE DUCT ASSY WAS FOUND WITH A SECTION OF FLANGE MISSING.Mar 4, 2013 · Airbus A320211 · Pneumatic Distribution SystemSDR DALA13010073221Battery Pack · no testDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST FAILED, BATTERY AT AFT LEFT. REPLACED BATTERY PACK AND FUNCTIONAL CHECKED NORMAL.Mar 4, 2013 · N321US · Airbus A320211 · Emergency LightingSDR CA130311015Sensor · failed(CAN) FLIGHT WAS AT FL350 WHEN THE LANDING, EXTENDED WITH OUT COMMAND. THE CAPTAIN HAS DECLARED A PAN PAN AND IS RETURNING. MORE INFO TO FOLLOW WHEN IT BECOMES AVAILABLE. FROM CREW, LEFT MAIN GEAR DOORS OPENED WITHOUT COMMAND AND THEN CLOSED UNCOMMANDED A Mar 2, 2013 · Airbus A320211 · Landing Gear Position and WarningSDR CA130301001Seal · failed(CAN) CREW REPORTED A YELLOW HYD SYS FAILURE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATION. YELLOW SYSTEM HYD LEAK AROUND CHECK VALVE 3059GM. CHECK VALVE REPLACED WITH NEW SEALS, NO FIX. YELLOW SYSTEM MAIN HP MANIFOLD CHECK Feb 28, 2013 · Airbus A320211 · Hydraulic System, MainSDR CA130221008Apu · shutdown(CAN) ACFT DEPARTED WITH ENGINE 1 IDG INOPERATIVE. APU AUTOSHUTDOWN DURING CRUISE. RESTARTED, BUT THEN FAILED AGAIN AND UNABLE TO RESTART. FLIGHT DIVERTED AND LANDED, AUTO SHUTDOWN. IDG NR 1 PREV SNAGGED WERE ABLE TO DESCEND AND RE-START APU. NO FURTHER IFeb 21, 2013 · Airbus A320211 · APU Core EngineSDR CA130218009Engine · shutdown(CAN) AFTER NORMAL APPROACH AND LANDING, NR 1 ENGINE AUTO SHUTDOWN PRIOR TO EXITING THE RUNWAY ENVIRONMENT. UNABLE TO TAXI TO GATE ON SINGLE DUE TO SIGNIFICANT SNOW ON TAXIWAYS AND RAMPS. ACFT TOWED TO GATE. ASR TO FOLLOW.Feb 16, 2013 · Airbus A320211 · Engine (Turbine/Turboprop)SDR DALA13007993274Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK FR 64+5", FR 66 Y765 AFT PAX CABIN. REPLACED SEAT TRACK IAW SRM 51-72-11.Feb 16, 2013 · N374NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13007983214Structure · corrodedDURING INSPECTION, FOUND AFT FUSELAGE, UNDERFLOOR FR66 AT STR26R AREA HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS L=0.90" W=0.450" D=0.20". NO ALLOWABLE DAMAGE LIMITS IN SRM. ACCOMPLISHED REPAIR IAW ER/A 510352-14, REV ORIGINAL SEFeb 14, 2013 · N314US · Airbus A320211 · Fuselage Main, StructureSDR DALA13007813214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT AT FR 31 BET STR 43R AND STR 42R, SHEAR TIE HAS CORRSIOON. RII: BLENDED CORROSION ON SHEAR TIE AT FR 31 BET STR 43R AND 42R IAW SRM 51-74-00,L=.960"W=.670"D=.007" NO ESTABLISHED LIMITS ON SRM. FABRICATED NEW SHEAR Feb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007803214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT AT FR33 BET STR 40R AND STR 41R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE IN FWD CARGO COMPT AT FR33 BETWEEN STR 40R & 41R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=0.90" W=0.30" D=0.00Feb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007793214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT AT FR312 BET STR 41R AND STR 40R, SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE AT FR31 BETWEEN STR 41R-40R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.30" W=0.35" D=0.008" NO ALLOWABLE DAMAFeb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007783214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT AT FR32 BET STR 40R AND STR 41R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE AT FR32 BETWEEN STR 40R-41R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.0" W=0.30" D=0.006" NO ALLOWABLE DAMAGEFeb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007773214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO COMPT AT FR32 BET STR 41R AND STR 42R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE IN FWD CARGO COMPT AT FR32 BETWEEN STR 41R & STR 42R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=0.50" W=0.40" D=0.Feb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007763214Plate · chafedDURING INSPECTION, FOUND RT AFT PASSENGER DOOR UPPER SIDE, FWD EDGE OF CLOSING PLATE HAS CHAFE MARK. DAMAGE DIMENSION L=3.5" W=.50" D=0.006" NO ALLOWABLE LIMIT IN THIS AREA IAW SRM 52-10-00, TABLE 101. REPLACED PLATE COVER IAW DWG 5211475 & AMM 52-13-18. RESFeb 13, 2013 · N314US · Airbus A320211 · Passenger/Crew DoorsSDR DALA13007623214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO BAY AT FR31 BETWEEN STR 43R AND STR 42R, SHEAR TIE HAS CORROSION. BLENDED CORROSION ON SHEAR TIE AT FR31 BTW STR 43R AND 42R, FOUND TO BE OUT OF LIMITS IAW SRM 51-74-00 L=.960" W=.670" D=.007". FABRICATED NEW SHEAR TIE ONFeb 13, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007603214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO BAY AT FR32 BETWEEN CENTER LINE AND STR 43R, SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW SRM 51-42-11 DAMAGE DIM; L=1.5" W=1.020" D=.020". NO ALLOWABLE LIMITS ESTABLISHED IN SRM.Feb 12, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007153214Floor Panel · delaminatedDURING INSPECTION, FOUND MCD FLOOR PANEL 241EF DELAMINATED AT AFT END. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D2537498. (DAMAGE DIM. L=12.0" W=8.0").Feb 12, 2013 · N314US · Airbus A320211 · Fuselage Floor PanelSDR DALA13007143214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO AT FR 31 BETWEEN CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010" NO ALLOWABLE DAMAGE IAW SRM 53-21-12. INSTALLED FABRICATED SHEAR TIE ON STAM TRAVELER T13/982826 MAT 2024-0 .063C BATFeb 11, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007133213Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO AT FR 31 BET CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010". NO ALLOWABLE DAMAGE IAW SRM 53-21-12. REMOVED AND INSTALLED FABRICATED SHEAR TIE ON STAM TRAVELER T13/982826 MAT 2024-0 Feb 11, 2013 · N313US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007123214Attach Fitting · corrodedDURING INSPECTION, FOUND AFT UTILITY RT DOOR SILL AFT GIRT BAR ATTACH HOLES, 3EA HAVE CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101 ORIG MAT .236" MAT LOSS 100 PERCENT OF THICKNESS. REPLACED DOOR SILL PN Feb 11, 2013 · N314US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13007113214Doubler · corrodedDURING INSPECTION, FOUND FWD CARGO BAY BET FR28 AND FR29, STR 43L AND STR 43R, PORTABLE WATER DOUBLER HAS CORROSION. REPLACED STAMPING P/N D532309352000 BATCH 2385934 IAW SRM A320 51-42-11, 51-44-11 AND DWG D53230935.Feb 11, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006693214Floor Support · corrodedDURING INSPECTION, FOUND AFT FUSELAGE UNDERFLOOR BET FR66 AND FR67, STR 26R HAS CORROSION. REPLACED STRINGER, PN D5348004720201, BATCH: 0002384124 IAW SRM 51-42-11 AND DWG D53480024. FABRICATED NEW CLEAT CLIP ON STAM TRAVELER T13/979626, MAT 2024-0 .071C BATFeb 10, 2013 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13006683214Shear Tie · corrodedDURING INSPECTION, FOUND FWD CARGO AT FR32 BET STR 42R AND STR 43R SHEAR TIE HAS CORROSION. REPLACED 1EA SHEAR TIE IAW SRM 51-42-11. DAMAGE DIMENSION L=1 W=.800 D=0.070 NO ESTABLISHED LIMITS ON SRM.Feb 10, 2013 · N314US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA13007613214Profile · crackedDURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE HAS CRACKED. RM 51-44-11, INSTALLED NEW PROFILE IAW SRM 51-42-11, TOUCHED UP PAINT ON FASTENER HEADS COMMON TO EXTERIOR SKIN IAW SRM 51-21-11.Feb 9, 2013 · N314US · Airbus A320211 · Fuselage Main, StructureSDR DALA13007103214Mount Bracket · crackedDURING INSPECTION, FOUND AFT CARGO REAR DOOR ACTUATOR FWD FRAME MOUNT BRACKET HAS CRACK. REPLACED BRACKET IAW SRM 51-42-11. CRACKED LENGTH = 1". P/N D5347212720600.Feb 8, 2013 · N314US · Airbus A320211 · Fuselage Main, Attach Fittings
Back to Airbus A320-211