Airbus A320-211

Service difficulty reports · 5,271

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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 DALA101793212Skin · damagedDURING "L" CHECK FOUND SKIN DAMAGED ON LT OTBD FLAP. REPAIRED IAW SRM 57-53-00.Jan 26, 2010 · N312US · Airbus A320211 · Trailing Edge FlapsSDR DALA100623232Hinge · damagedDURING GROUND OPERATIONS DOOR 1L ATTACH HINGE AND BEARINGS WERE DAMAGED . REPLACED IAW AMM 20-21-11.Jan 17, 2010 · N332NW · Airbus A320211 · Fuselage, Door HingeSDR DALA100303229Wire · damagedDURING A NON ROUTINE CHECK, FOUND ROW 17 EMERGENCY LIGHT INOPERATIVE. MX REPAIRED A DAMAGED WIRE AND OPS CHECK WAS GOOD.Jan 10, 2010 · N329NW · Airbus A320211 · Emergency LightingSDR CA100113005Hydraulic System · leaking(CAN) THE ACFT ENCOUNTERED A COMPLETE FAILURE OF THE GREEN HYD SYS PRIOR TO LANDING. FLIGHT CREW DECLARED A PAN PAN WITH ATC AS A PRECAUTION AND WERE TO BE MET BY CFR AFTER LANDING. AS RECEIVED IN HGR, GREEN RESERVOIR MECH QTY GAGE READS 5L AND REGISTERS ON ECJan 8, 2010 · Airbus A320211 · Hydraulic System, MainSDR DALA100133215Battery Pack · inoperativeDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK AND PERFORMED FUNCTIONAL CHECK GOOD. ACFT RETURNED TO SERVICE.Jan 4, 2010 · N315US · Airbus A320211 · Emergency LightingSDR DALA100113228Wire · looseDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROW 6 AND 10 INOPERATIVE. REPAIRED AND SECURED WIRING AT BOTH LOCATION AND OPERATIONAL.Jan 1, 2010 · N328NW · Airbus A320211 · Light System WiringSDR CA091210004Slat System · failed(CAN) SLATS FAILED AFTER SELECTION OF THE FLAPS ON APPROACH. GO AROUND AND QRH CARRIED OUT NIL FURTHER. OPERATIONAL TEST CARRIED OUT, OK SYSTEM RESET.Dec 5, 2009 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA091208003Slat System · failed(CAN) DURING APPROACH FLIGHT, ACFT EXPERIENCED A FAILURE OF THE SLATS TO EXTEND AFTER FLAP SELECTION . FLIGHT CREW DISCONTINUED THE APPROACH, COMPLETED THE QRH PROCEDURE AND DISCUSSED THE PROBLEM WITH MOC. PRIOR TO COMPLETING A SECOND UNEVENTFUL APPROACH, FLDec 5, 2009 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA091116006Uplock · damaged(CAN) FLIGHT CREW: ON DEPARTURE LANDING GEAR WOULD NOT LOCK UP, GEAR HANDLE CYCLED NIL FIX. GEAR DOWN INDICATION NORMAL RTG. LANDING GEAR UPLOCK ASSY REPLACED.Nov 3, 2009 · Airbus A320211 · Landing Gear Position and WarningSDR NWAA093793209Power Supply · shortedROW 13-14-15, 18, 19 AND 20 SEAT EVAC LIGHTS INOP. FOUND BAD POWER SUPPLY INTERNALLY SHORTED. REPLACED POWER SUPPLY AND REPAIRED A BARE WIRE AT A CONNECTOR AND TESTED OK. REF LOG 6954560.Nov 1, 2009 · N309US · Airbus A320211 · Emergency LightingSDR NWAA093763209Control Unit · faultyESCAPE PATH LIGHT FOR SEATS 16, 17, 18, 21, 22 & 23 INOP". REMOVED AND REPLACED POWER CONTROL UNIT; OPERATIONAL CHECK OK.Oct 31, 2009 · N309US · Airbus A320211 · Emergency LightingSDR NWAA093663242Battery Pack · failedBATTERY EPSU (12WL) FAILED CAPACITY CHECK. REPLACED BATTERY PACK AND TESTS OK.Oct 20, 2009 · N342NW · Airbus A320211 · Emergency LightingSDR NWAA093463209Wire · brokenEMERGENCY EGRESS AISLE LIGHTING INOP ROWS 5-9. REPAIRED BROKEN WIRE, CHECKS OK.Oct 2, 2009 · N309US · Airbus A320211 · Light System WiringSDR CA090831002Wheel Half · failedBRAKE TEMPS LESS THAN 490 DEG AT TAXI OUT, ACFT PULLS TO LT. RTG FOUND WHEEL LINER RT WAS TILTED AND MELTED ALUMINUM FALLING OFF. UPON INSP FOUND SEVERE DAMAGE TO ASSY.Aug 27, 2009 · Airbus A320211 · Wheel/Ski/FloatSDR CA090827001Warning Light · illuminatedSHORTLY AFTER TAKEOFF, ENG NR 2 FADEC ALTERNATOR FAULT FOLLOWED BY ENG NR 2 FIRE WHICH LASTED APPROX 10 SEC, THEN EXTINGUISHED. CREW PERFORMED ECAM SHUTDOWN AND LANDED.Aug 21, 2009 · Airbus A320211 · Fuel Controlling SystemSDR CA090821004Control Cable · dislodgedFOUND THS CONTROL CABLE HAS CUT INTO FLOORBEAM C14 AT PULLEY ATTACH BRACKET. GOUGE IS APPROX 1/4" DEEP. THIS CABLE FOUND TO BE NOT IN THE GROOVE OF THE ASSOCIATED PULLY. THE RETAINER IS IN PLACE, BUT THE CABLE HAS JUMPED PAST AND HAS STARTED TO "SAW" A GROOAug 19, 2009 · Airbus A320211 · Flight Control SystemSDR NWAA092683214Epsu · failedEMERGENCY EGRESS LIGHT TEST FUNCTION INOP. PLACED PTP (TEST PANEL) ON MEL. NEXT DDG, EMER R, EMERGENCY EXIT RT SUPPLY FAILED. REPLACED RT EPSU, CHECKS GOOD.Aug 1, 2009 · N314US · Airbus A320211 · Emergency LightingSDR CA090717001Turbine Blades · failed(CAN) ON T/O AT 4000 FT, LOUD BANG ON ENG NR 1, VIBRATION UP TO 9.5. ENGINE FAILED. FIRE HANDLE PULLED BUT BOTTLES NOT FIRED BY FLIGHT CREW. THIS IS AN OLD PN HPT BLADE FAILURE - 13,000 CYCLES ON THE OLD PN BLADES. THIS IS THE FOURTH -5A ENGINE SUFFERING THJul 16, 2009 · Airbus A320211 · Turbine SectionSDR NWAA092163210Seal · leakingPASSING 10,000 ON CLIMB-OUT NOTED EXCESSIVE CABIN RATE OF CLIMB OF 1600-1800 FPM. WATCHED CABIN ALTITUDE CLIMB TO 9000 FT PASSING 18,000 FT MSL. ECAM MESSAGE CAB PR EXCESS CAB ALT AT 9500 FT CABIN ALTITUDE. IMMEDIATELY DESCENDED AIRCRAFT TO CONTROL CABIN ALJun 14, 2009 · N310NW · Airbus A320211 · Cargo/Baggage DoorsSDR CA090602008Hub · damaged(CAN) AS REQUESTED, INFO NR 217 (MSN 253) MLG WHEEL NR 4 FAILURE. WHEEL NR4 INBD HUB: - PN 300-796-OPT1 - SN 0146 - TOTAL LANDINGS: 13766 LDGS - PREVIOUS OVERHAULS AT 11176 TOTAL LDGS, 6056 TOTAL LDGS AND 2909 TOTAL LDGS. L4539197 (28-MAY-2009): - SHORTLYMay 29, 2009 · Airbus A320211 · Wheel/Ski/FloatSDR NWAA091863212Light · odorAFT FLIGHT ATTENDANTS REPORT FAINT ELECTRICAL ODOR ON INITIAL CLIMB THAT DISSIPATED IN CRUISE. AFTER GEAR DOWN, THE EMERGENCY EGRESS EXIT LIGHTS ILLUMINATED NORMALLY, FOLLOWED BY FAINT ELECTRICAL ODOR AND EMERGENCY EGRESS LIGHTING TURNING OFF IN REAR OF AIRCRMay 27, 2009 · N312US · Airbus A320211 · Emergency LightingSDR NWAA091813212Light · no testEMERGENCY EGRESS LIGHT TEST FAILS. REPLACED EPSU 13WL, CKS OK.May 21, 2009 · N312US · Airbus A320211 · Emergency LightingSDR CA090604009Duct · cracked(CAN) CREW REPORT: AFTER TAKEOFF EGT OVER LIMIT AND ENG NR2 FIRE WARNING ON ECAM. CREW BOUGHT POWER BACK TO IDLE FIRE WARNING EXTINGUISHED AND RETURN TO DEPARTURE WITH ENGINE AT IDLE. TOWER REPORTED A POSSIBLE BIRD STRIKE TO THE CREW. MX CARRIED OUT TROUBLEApr 30, 2009 · Airbus A320211 · Engine Bleed Air SystemSDR DALA1155463214Skin · gougedRT AFT FUSELAGE AFT OF R2 PASSENGER DOOR, FUSELAGE HAS GOUGES BETWEEN FR69 & FR70 AND STR 20R - STR 21R BLENDED GOUGES AT AREA IAW SRM 51-73-00 OUT OF LIMITS IAW SRM 53-41-11. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 53-00-11 FIG 227. DURING LCK AT BFMApr 2, 2009 · N314US · Airbus A320211 · Fuselage Main, Plate/SkinSDR NWAA09253209Epsu · dischargedEEPL LIGHTING AT SEATS 13L, 14L, 15L, 16L, 18L, 19L, 20L, 24L, 25L, 26L INOPERATIVE. REPLACED (2) EPSU, AND DOOR 2R SLIDE. (K)Jan 27, 2009 · N309US · Airbus A320211 · Emergency LightingSDR NWAA09213224Rib · crackedDURING H-CHECK, FOUND CRACK ON RT WING RIB NR4 AT INBD FACE OF SKIN ATTACHMENT AREA BETWEEN STR 6 AND 7. REPAIRED IAW EA 32-211588. (K)Jan 24, 2009 · N324US · Airbus A320211 · Wing, Rib/BulkheadSDR NWAA09143211Line · leakingECAM MESSAGE: HYD B RSVR LO LVL, FOLLOWED COM PROC 2.29.5. ACFT LANDED UNEVENTFULLY. SECURED FITTINGS ON BLUE HP MANIFOLD. REPLACED RETURN-LINE UNION (I/P 0014316). BRACKETS/CLAMPS (I/P 0014319). FILTERS (I/P 0013907). BLUE ELECTRIC PUMP (I/P 0014418). (KJan 17, 2009 · N311US · Airbus A320211 · Hydraulic System, MainSDR NWAA0913213Epsu · inoperativeEMERGENCY SEAT PATH LIGHTS SEAT ROW 18-21 ARE INOPERATIVE, REPLACED EPSU 13WL AND CHECKS GOOD. (K)Jan 4, 2009 · N313US · Airbus A320211 · Emergency LightingSDR NWAA09133211Pump · malfunctionedOUT OF AIRPORT, AT APPROX 20,000 FT, RECEIVED "HYD GREEN RSVR LO LVL" CAUTION. FOLLOWED COM, LANDING GEAR GRAVITY EXTENDED AND LANDED UNEVENTFULLY. CORRECTION WAS TO REPLACE HYD LINE IN LT WHEEL WELL AND NR 1 ENG DRIVEN PUMP IAW LOG PAGES 4568789 AND 0011489Dec 13, 2008 · N311US · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR NWAA085293277Handle · out of positionUNABLE TO ARM BOTH AFT DOOR SLIDES PROPERLY PRIOR TO FLIGHT. MEM MX REPOSITIONED DOOR HANDLES FROM LT TO THE RT DOOR AND RT TO THE LT DOOR PER MM 52-13-21. DOOR SLIDES WERE ARMED AND OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.Dec 1, 2008 · N377NW · Airbus A320211 · Passenger/Crew DoorsSDR NWAA084603216Pump · failedGREEN RESERVOIR LO LEVEL OCCURRED IN CRUISE. COMPLIED WITH COM, LG GRAVITY EXTENDED PRIOR TO LANDING. ACFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS OK.Oct 12, 2008 · N316US · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR NWAA085013232Epsu · faultyEMERGENCY EGRESS LIGHTING TEST FAILS, FAULTING EPSU EMER R. REPLACED EPSU 12WL, CHECKS OK.Oct 8, 2008 · N332NW · Airbus A320211 · Emergency LightingSDR NWAA084483216Epsu · dischargedEMERGENCY EGRESS PATH LIGHTING INOP BETWEEN ROWS 1 AND 8. REPLACED EPSU 10WL, CHECKS OK.Oct 7, 2008 · N316US · Airbus A320211 · Emergency LightingSDR NWAA084303213Lamp · inoperativeEMERGENCY EGRESS LIGHTING TEST FAILS. RELAMPED EXIT SIGN, RESET POWER SUPPLIES 11WL, 12WL, 13WL. REPLACED EPSU 10WL, CHECKS OK.Sep 20, 2008 · N313US · Airbus A320211 · Emergency LightingSDR NWAA084013217O-Ring · defectiveY HYD RSVR LO LVL DISPLAYED. COMPLIED WITH COM. ACFT LANDED UNEVENTFULLY TOWED TO GATE. REPLACED O-RING AND BACK-UP RING ON NR 2 ENGINE DRIVEN HYDRAULIC PUMP FITTING. CHECKS OK.Aug 22, 2008 · N317US · Airbus A320211 · Hydraulic System, MainSDR NWAA083993215O-Ring · leakingAT CRUISE (FL360) ECAM MESSAGE "YELLOW HYD SYSTEM LO", COMPLIED WITH COM PROCEDURES. ACFT LANDED UNEVENTFULLY. REPLACED O-RING ON YELLOW HP MANIFOLD, NO LEAKS NOTED. (S)Aug 20, 2008 · N315US · Airbus A320211 · Hydraulic System, MainSDR NWAA082923230Power Supply · inoperativeDURING TESTING OF THE EMERGENCY EGRESS LIGHTING, EPSU COMM EMER L ANNUNCIATED. REPLACED POWER SUPPLY 11WL, CHECKS GOOD. (A)Jul 2, 2008 · N330NW · Airbus A320211 · Emergency LightingSDR NWAA082743209Battery Pack · inoperativeWHEN PERFORMING EMERGENCY LIGHT TEST, EPSU 11WL FAILED. REPLACED EPSU BATTERY PACK, CHECKS OK. (A)Jun 13, 2008 · N309US · Airbus A320211 · Emergency LightingSDR NWAA081633212Sill · corrodedDURING "H" CHECK, FOUND SURFACE CORROSION ON AFT LT PASSENGER DOOR SILL AT FR 66. REPAIRED PER EA 32-212484.Apr 7, 2008 · N312US · Airbus A320211 · Fuselage Miscellaneous StructureSDR NWAA081403230Battery · inoperativeCOM EMERGENCY LIGHT FWD FAULT ON CIDS. REPLACED FWD LEFT EPSU BATTERY, EMERGENCY LIGHTS CHECK GOOD. Apr 6, 2008 · N330NW · Airbus A320211 · Emergency LightingSDR NWAA081173210Slide · faultyWHILE PERFORMING EMERGENCY LIGHT SYSTEM CHECK PER LINE CHECK "EXT LOADS AFT L" MESSAGE, REF L/P 4273412. REMOVED AND REPLACED 2L EVACUATION SLIDE. CHECKS GOOD.Mar 23, 2008 · N310NW · Airbus A320211 · Escape SlideSDR NWAA081003226Manifold · leakingSHORTLY AFTER TAKEOFF THE HYD G RSVR LO LVL FAULT ANNUNCIATED. AIRCRAFT RETURNED TO MEM, LANDING GEAR GRAVITY EXTENDED. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. REPLACED GREEN GROUND LEAK MEASUREMENT MANIFOLD AND NR 1 ENGINE DRIVEN GREEN PUMP.Mar 16, 2008 · N326US · Airbus A320211 · Hydraulic System, MainSDR NWAA080803225Uplock Sensor · malfunctionedON CLIMB FROM DTW THROUGH 12,000 ACCELERATING AUDIBLE GEAR DOOR NOISE WITH ASSOCIATED RIGHT MAIN LANDING GEAR RED "UNLK" LIGHT MOMENTARILY. LIGHT EXTINGUISHED AS WELL AS NOISE. REOCCURRED TWICE BUT WITH NO ASSOCIATED ECAM MESSAGE. CONTINUED FLIGHT AT 250 KNFeb 26, 2008 · N325US · Airbus A320211 · Landing Gear Position and WarningSDR NWAA080233224Line · leakingHYDRAULIC "G" LOW QUANTITY, ALSO LOW ON ECAM. FOLLOWED COM, LANDING GEAR GRAVITY EXTENDED AND LANDED UNEVENTFULLY. AIRCRAFT TOWED TO GATE. REPLACED HYDRAULIC LINE ON NR 1 THRUST REVERSER. CHECKS GOOD.Jan 20, 2008 · N324US · Airbus A320211 · Hydraulic System, MainSDR NWAA080253217Skin · puncturedDURING "H" CHECK, FOUND PUNCTURE AT AFT LOWER CORNER OF FORWARD CARGO DOOR INNER SKIN. REPAIRED PER EA 32-211429 SECTION I. SECTION II INSPECTION TO BE DETERMINED BUT NOT LESS THAN 180 DAYS AFTER SECTION I REPAIR.Jan 14, 2008 · N317US · Airbus A320211 · Cargo/Baggage DoorsSDR CA080114002Switch · inoperative(CAN) NR 1 BLEED OVERHEAD SHOWED ON ECAM AIR ENG 1 BLD FAULT COMPLETED ECAM ACTION SHORTLY AFTERWARD AIR ENG 2 BLD FAULT COMPLETED ECAM. BOTH FAN AIR VALVES CHECKED IAW AMM 36-11-54-720-001 NFF. BOTH TCT`S REPLACED ( ENG 1 AND 2) IAW AMM 36-11-43. ENG RUNS CARJan 11, 2008 · Airbus A320211 · Cabin Temperature Control SystemSDR NWAA074053216Buttstrap · corrodedDURING "M" CHECK, FOUND CORROSION ON BUTT STRAP AT FR 64 BETWEEN S43R-S44R. REPAIRED PER EA 32-211424.Dec 16, 2007 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA071205010Thermostat · failed(CAN) WHILE IN CRUISE AT FL 390, THE CREW HAD A BLEED AIR SUPPLY NR 2 FAILURE, AND DURING A DESCENT WHILE REFERING TO THE QRH, ALSO HAD NR 1 BLEED FAIL. CREW LOST BOTH PACKS, AND INITIATED EMERGENCY DESCENT TO 10,000 FT. FLT DIVERTED TO NEARBY AIRPORT. TEMP CNov 26, 2007 · Airbus A320211 · Cabin Temperature Control SystemSDR NWAA073653220Power Supply · malfunctionedAFTER TAKEOFF, FORWARD 2 EXIT LIGHTS AND AISLE EMERGENCY LIGHTS IN FIRST CLASS AND FIRST 3 ROWS OF CABIN WERE FLASHING, THEN ON STEADY. CYCLED COCKPIT EMERGENCY LIGHT SWITCH OFF, THEN TO ARM BUT NO HELP. LIGHTS EXTINGUISHED 20 MINUTES LATER. REPLACED FORWARNov 3, 2007 · N320US · Airbus A320211 · Emergency LightingSDR CA070924006O-Ring · failed(CAN) FOLLOWING A YELLOW HYDRAULIC SYSTEM FAILURE, THE AIRCRAFT SUBSEQUENTLY EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE, AND DIVERTED BACK TO DEPARTURE POINT. THE FLIGHT DECLARED AN EMERGENCY, AND LANDED 4000 KG OVERWEIGHT. AFTER LANDING, A NR 1 AND 3 BRAKE Sep 23, 2007 · Airbus A320211 · Hydraulic System, Main
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