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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2015051803382Skin · corrodedDURING INSPECTION, FOUND CORROSION WITHIN WIFI AREA FRAME 25 TO 26 STRINGER 44. INSTALLED STR IAW SRM 53-21-13, C/W PRI/ERA 535082-14AD, REV O.SDR CA150515006Vhf Comm · malfunctioned(CAN) TEMPORARY COMMUNICATIONS FAILURE ON APPROACH BELOW 10,000 FEET, RADIO STUCK ON TRANSMIT 3 TIMES FOR APPROX 30 SECONDS EACH TIME BLOCKING THE FREQUENCY. WHILE TRYING TO TROUBLESHOOT THE PROBLEM, THE ACFT DEVIATED SLIGHTLY OFF COURSE ON THE RNAV APPROACH SDR CA150511011Tail Cone · damaged(CAN) LIGHTNING STRIKE ON NOSE CONE ON DEPARTURE. ALL NORMAL, CONTINUING TO STATION. FOUND MULTIPLE MELTED POINTS ON FUSELAGE TAIL CONE. TEMPORARY DISPOSITION ACCOMPLISHED IAW PP. PERMANENT DISPOSITION REQUIRED AT THE NEXT BC-06 CHECK.SDR DALA2015050803130Floor Support · crackedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA L=2", W=1", D=0.003". SSI 531189. REPLACED FLOORBEAM -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110SDR DALA2015050703125Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON RAIL DUMMY Y503.2 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FWD GALLEY AREA L=0.800", " W=0.400, D=0.003". REPLACED RAIL DUMMY Y503.2 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D531128SDR DALA2015050703124Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 70, L=2", W=1", D=0.010". REPLACED FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FR 60 TO FR 70 IAW SRM 51-72-11 AND DWG D5347-2815.SDR DALA2015050703123Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66, L=8", W=4", D=0.009". REPLACED FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FR 64 TO FR 66 IAW SRM 51-72-11 AND DWG D5347-2816.SDR DALA2015050703116Wire · brokenDURING NON-ROUTINE CHECK, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT SEAT ROW 7AB. T/S AND FOUND BROKEN WIRE AT CABIN SEAT ROW 7 A/B. SPLICED WIRE AND FUNCTIONAL CHECK WAS NORMAL.SDR CA150430001Control Unit · failed(CAN) ON TAKE CREW EXPERIENCED A GRINDING NOISE AND A PULL FROM THE NOSE GEAR. THE CREW REJECTED THE TAKEOFF AT 80-100 KNOTS AND RETURNED TO THE GATE. REPLACED IAW AMM 32-42-34 & TESTED SERVICEABLE. LUBRICATED OF THE SHOCK ABSORBER CARRIED OUT IAW TSM 32-20-0SDR DALA2016112209099Stringer · corrodedEVIDENCE OF CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 56 - 57. CUT OUT THE DAMAGED STRINGER SECTION. FABRICATED NEW STRINGER AND COUPLINGS. ALODINED, PRIMED, PAINTED AND INSTALLED NEW PARTS IAW SRM.SDR DALA2016112209098Stringer · corrodedEVIDENCE OF CORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 56 - 57. CUT OUT DAMAGED STRINGER SECTION. FABRICATED NEW STRINGER AND COUPLINGS. TREATED, PRIMED, PAINTED AND INSTALLED NEW PARTS IAW SRM.SDR DALA2015042903008Skin · corrodedCORROSION ON SKIN OTBD OF STRINGER 42L BETWEEN FRAMES 56 & 57. BLENDED OUT DAMAGE IAW SRM 53-00-13 C/P WITH ERA 535534-14AD.SDR DALA2016112209103Stringer · corrodedSTRINGER 43L HAS CORROSION BETWEEN FRAMES 56 & 57. REMOVED AND REPLACED THE STRINGER IAW SRM.SDR DALA2015042002809Power Supply · failedDURING NON ROUTINE CHECK, FOUND EMERGENCY POWER SUPPLY UNIT 11WL FAILS BITE CHECK. REPLACED EPSU AT 11WL.SDR DALA2015041902808Structure · corrodedDURING INSPECTION, FOUND CORROSION FOUND BETWEEN STR 42L AND 43L BETWEEN 56-57 REF PRI 53-5226-14. INSTALLED DOUBLER IAW PRI 535226-12, VER 1, 2 , 874907.SDR DALA2015042002810Connector · damagedDURING NON-ROUTINE CHECK, FOUND 4C SEAT EMERGENCY LIGHT PATH INOPERATIVE. REPLACED LIGHT ASSY PIGTAIL.SDR CA150416003Transceiver · failed(CAN) SOON AFTER DEPARTURE, CREW LOST ALL WEATHER RADAR FUNCTIONS, DUE TO AREA AND ENROUTE CONVECTIVE WEATHER FLIGHT DIVERTED. MAINTENANCE TO INVESTIGATE. RESOLUTION R & R WX RADAR R/T AMM 34-41-33. OPS NORMAL, ACFT OK FOR SERVICE.SDR DALA2015041602792Battery Pack · faultedDURING NON ROUTINE CHECK, FOUND EMERGENCY BATTERY FAULTED. REPLACED RT EMERGENCY BATTERY PACK AND CHECK WAS NORMAL.SDR CA150414003Pump · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A BLUE HYDRAULIC SYSTEM PUMP OVERHEAT, FLIGHT CONTINUED. BLUE ELECTRIC PUMP CHANGED IAW AMM TSK 29-12-51-000-001-A/400-001-A.SDR CA150413007Indicator · malfunctioned(CAN) ENGINE 2 N2 VIBRATIONS INTERMITTENT, EXCEEDING ECAM ADVISORY REACHING 4.4. ALL OTHER INDICATIONS NORMAL, NO VIBRATIONS FELT BY FLIGHT CREW. VIBRATION CHECK TASK 71-00-00-710-009A CARRIED OUT. MAX VIBS UNITS AT MAINTENANCE 96.1 N1, BEARING 1, MAX 2.9 ASDR CA150413003Duct · leaking(CAN) AFTER GETTING AIRBORNE, THE ACFT ENCOUNTERED AN AIR WING LEAK IN CRUISE. IN CONSULTATION WITH MAINTENANCE, THE FLIGHT CREW RETURNED THE ACFT. THE LANDING WAS UNEVENTFUL WITH NO ADVERSE PASSENGER REACTION. THE ACFT WAS TAKEN OFFLINE AND A NEW ACFT WAS USDR CA150410014Probe · leaking(CAN) STRONG CHEMICAL ODOR IN COCKPIT ON DESCENT, LASTED TILL LANDING. ON GND RUN FOUND NR 2 ENGINE N1 PROBE GUIDE TUBE LEAKING. SEALS REPLACED IAW EMM 72-23-00. GND RUN COMPLIED WITHIN LIMITS, AT 12 DROPS A MIN. BLACK LIGHT CHECK COMPLIED WITH ON BOTH ENGSDR CA150406005Seal · leaking(CAN) FLIGHT DIVERT DUE BLEED SNAG. A TECH STOP WOULD BE REQUIRED AS THE CREW ADVISED THEY WOULD BE AT FL300 THE ENTIRE FLIGHT. THE ACFT WOULD BE GROUNDED ONCE IT LANDED. THE DECISION WAS MADE TO DIVERT. FLIGHT LANDED OVERWEIGHT BY 8.6 KGS. FOUND DUCT LEASDR DALA2015050703121Stringer · corrodedDURING INSPECTION, FOUND FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 56-57. PERFORMED DAMAGE CONTAINMENT OF CUTOUT STR AT 43L IAW NDTM 51-10-08, HFEC NO DEFECTS/CRACKS NOTED.SDR CA150406002Duct Seal · failed(CAN) DURING THE FLIGHT THE CREW REPORTED A WING ANTI-ICE FAULT AND ELECTED TO DIVERT DUE TO POSSIBLE ICING CONDITIONS. RESOLUTION LT WING ANTI-ICE DUCT SEAL AT RIB NR 9 REPLACED IAW AMM 30-11-42 & 30-11-51. LEAK CHECK AND FUNCTIONAL TEST C/O, NO FAULT FOUND.SDR CA150318002Computer · failed(CAN) ACFT HAD JUST DEPARTED WHEN CREW HAD FLUCTUATING PRESSURE ON THE NR 2 ENGINE WHICH HAD JUST BEEN REPLACED. IN CONSULT WITH MOC IT WAS DECIDED TO RETURN TO DEPARTURE AIRPORT. R & R NR 1 SDCA IAW AMM 31-55-34, PERFORMED MINIMUM IDLE LEAK CHECK, NO DEFECSDR CA150318001Pressure Switch · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A VENT EXTRACT FAULT, THE FLIGHT RETURNED. R & R EXTRACT FAN BLOWER PRESSURE SWITCH, 30HQ. OPS CHECK GOOD IAW AMM 21-26-11. NO DEFECTS NOTED.SDR CA150306014Servo Valve · failed(CAN) EICAS NOSE WHEEL STEERING FAULT AFTER LANDING. RESET UNSUCCESSFUL. CALLED FOR TOW TO GATE. RESOLUTION REMOVED & REPLACED NLG STEERING SERVO VALVE IAW AMM 32-51-51. OPERATIONS CHECK & FUNCTION CHECK & CAT 3 AUTO LAND CHECKED NORMAL, NO DEFECTS NOTED ISDR DALA2015030402035Frame · corrodedDURING INSPECTION, FOUND LT AFT UTILITY AREA FR 66 JUST ABOVE DOOR SILL HAS CORROSION, AROUND THE HOLE. REMOVED CORROSION IAW A320-53-41-12, FOUND TO BE OUT OF LIMITS, MATERIAL THICKNESS 0.098", MAT LOSS 0.020", REMAINING 0.078". INSTALLED DOUBLER IAW SRM 51-SDR DALA2015030402034Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 42L TO STR 43L, L=0.900", W=0.300", D=0.004". SSI 532180). REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STRINGER 42L TO STRINGER 43L ISDR DALA2015030302033Slat · unknownDURING INSPECTION, FOUND CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON SLAT NR 2 RT WING LOCATED T/E UPPER SURFACE AT 12" FROM INBD EDGE AND 7.5" FROM L/E OF SLAT. REPLACED SLAT 2 RT, PERFORMED ADJUSTMENT OF SLAT 2 RT IS GOOD AND PERFORMED OPS TEST OF SSDR DALA2015030301983Skin · dentedDURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 68 AND BETWEEN STR 43L TO STR 32R AFT FUSELAGE. EVALUATED DENTED AREA ON EXTERNAL SKIN LOCATED AT FRAME 68 AND BETWEEN STR 43L TO STR 32R AFT FUSELAGE IAW ER/A 532995-14, REVISION ORIGINAL AND SDR DALA2015030301982Skin · dentedDURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 69 AND BTW STR 32R TO STR 37R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 69 AND BETWEEN STR 32R TO STR 37R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14, REVSDR DALA2015030301981Skin · dentedDURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 67 AND BETWEEN STR 32L TO STR 32R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 67 AND BETWEEN STR 32L TO STR 32R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14SDR DALA2015030301980Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FRAME 65 AND BETWEEN STR 43L TO STR 44 AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 65 AND BETWEEN STR 43L AND STR 44 IAW ER/A 532995-14 REV ORIGINAL AND PRI 532995-14, REV 0, 1, 2SDR DALA2015030301979Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FRAME 67+6" AND STR 32R AFT FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FRAME 67+6" AND STR 32R AFT FUSELAGE IAW ERA 532995-14, REV ORIGINAL AND PRI 532995-14.SDR DALA2015030301969Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FR66 AND BETWEEN STG 42R TO STG 43R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FR 66 AND BETWEEN STR 42R TO STR 43R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14.SDR DALA2015030501888Connector · damagedDURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 7. FOUND 2 CONNECTORS PULLED APART. INSTALLED 2 NEW CONNECTORS. OPS CHECK WAS GOOD.SDR DALA2015030201972Skin · corrodedDURING INSPECTION, FOUND CORROSION ON EXTERNAL SKIN LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STR31R TO STR32R AFT FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FRAME 69 TO FRAME 70 AND BETWEEN STR 30R TO STR 33 RT REAR FUSELAGE IAW SRMSDR CA150302001Duct · disconnected(CAN) BURNING ODOR, FWD GALLEY ON APPROACH. MOC HAS TAKEN ACFT OFFLINE DUE TO HISTORY. FOUND DUCT TO SKIN EXCHANGER ISOLATION VALVE 24HQ DISCONNECTED. DUCT RE-POSITIONED & SECURED IN PLACE IAW AMM 21-26-42. SYS SERVICEABLE.SDR DALA2017102507772Skin · damagedDENTS AND CREASES WERE FOUND ON FWD FUSELAGE SKIN BETWEEN STRINGERS 14L-15L AND DOOR STOP BEAM , REPAIRED IAW ERA 533192-14, AND PRI 533192-14.SDR DALA2016112209160Bracket · corrodedRIGHT AILERON JACK 1 AND 2 AND HINGE 4 BRACKETS WERE CORRODED. THE BRACKETS WERE REPAIRED PER ER/A.SDR DALA2016112209162Structure · corrodedDURING M CHECK, SEVEN CORROSION SPOTS WERE FOUND ON THE UPPER SURFACE OF THE COVERSHEET LOCATED AT AFT CARGO BAY AREA. DAMAGED AREAS WERE REWORKED IAW IAW SRM AND ER/A.SDR DALA2016112209161Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 - 24. REPAIRED THE FLOOR SUPPORT IAW ER/A.SDR CA150227001Unknown · failed(CAN) AFTER TAKEOFF THE FLIGHT CREW REPORTED THAT THEY HAD A STRONG ELEC BURNING SMELL IN THE FORE & AFT CABIN. THEY BELIEVE IT IS ASSOCIATED WITH THE IFE SYS. AFTER TROUBLESHOOTING THE ISSUE WITH MOC & NO RESOLUTION THE CREW ELECTED AN AIR TURN BACK & ADVISSDR DALA2015022701737Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 9 IS INOPERATIVE. FOUND BROKEN GROUND WIRE AT SPLICE. REPLACED SPLICE AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA2015022601731Bolt · wornDURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING LOCATED SPOILER 2, LT PERFORMED PERMANENT REPAIR ON STOP BOLT OF CENTER FITTING LOCATED ON SPOILER 2 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201.SDR DALA2015022601674Wire · pulledDURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 12 INOPERATIVE. FOUND POWER WIRE PULLED FROM SPLICE. REINSTALLED WIRE TO SPLICE AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA2016112209166Stringer · corrodedCORROSION ON STRINGER 44 IN THE AFT CARGO BAY BETWEEN FRAMES 55 AND 56. REPAIRED THE STRINGER.SDR DALA2016112209165Stringer · corrodedCORROSION ON STRINGER 43R IN AFT CARGO BAY FRAME 56+1. REPAIRED THE STRINGER.
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