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 DALA2020013100757Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 7.5 INCHES OTBD FROM Y1292, CRACK AT THE 9 O`CLOCK IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTION ON FRAME 36 UPPER SURFACE PRESSURE DECK MEMBRANE IN FWD CARGO COMPARTMENT IAW ER/Jan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020012200507Frame · crackedCRACK FRAME 3 RACK 10VU CENTER LUG IN COCKPIT WORK CARD 2511-01146-01, AD 2019-07-05, REPAIRED IN ACCORDANCE WITH AD 2019-07-05 AND AIRBUS SB A320-92-1087 REV.3 CRACK LENGTH 0.532Jan 21, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA202001220500Battery Pack · no testEMERGENCY TEST FAILS LT BATTERY, REPLACED LT BATTERY FOR EPSUJan 20, 2020 · N332NW · Airbus A320211 · Emergency LightingSDR DALA2020012290496Skin · gougedGOUGE EXTERNAL SKIN LOC. FR 21+19 INCH BTW STR 41R TO STR42R AT LOWER FUSELAGE, PERFORMED REPAIR INSTRUCTION ON GOUGE EXTERNAL SKIN LOC. FR 21 + 19 INCH BTW STR 41R TO STR 42R AT LOWER FUSELAGE AS PER ER/A 584200-14, REV. ORIGINAL AND PRI 584200-14, REV.0Jan 18, 2020 · N319US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2020011100202Intercostal · crackedCRACK INDICATION ON INTERCOSTAL FITTING IN UPPER INBOARD HOLE AT LEVEL DOOR STOP 7 FRAME 16 RH AT FWD GALLEY AREA (1 EA), REPLACED OLD INTERCOSTAL FITTING AND FASTENER ON UPPER LB HOLES AT LEVEL DOOR STOP #7 FR.16 RH FWD GALLEY AREA ASPER A320 SRM 51-42-11 ANDJan 10, 2020 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2024060905895None · noneSHIP 3226 DISC: ER/A 558689-14AD HAS BEEN UPDATED TO REV. 'C' TO INCORPORATE NEW RDAS APPROVAL PER DTE REQUIREMENTS. THE SUBJECT REPAIR IS CLASS IFIED AS CAT. 'B' PERMANENT WITH FOLLOW ON INSPECTION. C/A: ACCOMPLISHED PRI 558689-14AD REV 0, AND 1,2 AND ER/A558Jan 8, 2020 · N326US · Airbus A320211 · Standard Practices/StructuresSDR DALA2020010300047Door Frame · crackedCRACK INDICATION ON FRAME 66 OPEN FASTENER HOLE 4 ON DOOR STOP 2 AFT GALLEY AREA (1 EA) LH SIDE, REPAIRED OPEN HOLE 4 ON FRAME 66 DOOR STOP 2 LH SIDE ASPER A320 SRM 53-41-12-300-010Jan 3, 2020 · N319US · Airbus A320211 · Fuselage Main, StructureSDR DALA2020010300046Strap · corrodedCORROSION LOWER CUTOUT STRAP BELOW THRESHOLD SHEET IN FWD CARGO COMPARTMENT, REPLACED LOWER CUT OUT STRAP BELOW THRESHOLD SHEET IN FWD CARGO COMPARTMENT ASPER SRM A320 51-72-11 AND DWG E53470500Jan 3, 2020 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020010300045Door Sill · corrodedCORROSION LOWER SILL FR 68 AND AT LEVEL STR 23L AT AFT GALLEY AREA, REPLACED LOWER SILL LOC FR66 TO FR 68 AND AT LEVEL STR 23L AT AFT GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG # D53480020Jan 3, 2020 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020010300044Seat Track · damagedSEAT TRACK -Y1292 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 LOC FR41 TO FR47 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53371000Jan 2, 2020 · N319US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020010300043Seat Track · damagedSEAT TRACK -Y1292 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 LOC. BTW FR36 TO FR41 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53371000Jan 2, 2020 · N319US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020010300048Battery · dischargedFOUND EPSU FAULT DURING WORKCARD 3351-2291 TEST, R/R EPSU W/O BATTERYJan 1, 2020 · N326US · Airbus A320211 · Emergency LightingSDR DALA2020011700377Damper · failedDONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DOOR DAMPER AT FWD GALLEY AREA, REPLACED PASSENGER CREW DOOR 841 DOOR DAMPER AT FWD GALLEY AREA.Dec 30, 2019 · N319US · Airbus A320211 · Passenger/Crew DoorsSDR DALA201912317666Fitting · corrodedCORROSION ON THE CENTER FITTING OF THE LOWER SILL AFT ENTRY DOOR AT LEVEL STRINGER 23L IN THE AFT GALLEY AREA , REPLACED THE CENTER FITTING IAW SRM 51-72-11, AND DWG D53480048.Dec 29, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019123197665Floor Support · corrodedCORRODED FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24 IN THE FWD GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.Dec 28, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019122707573Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y1162.5 BETWEEN FRAMES 68 AND 69 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472800.Dec 27, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019122767572Holder · brokenEMERGENCY PATH LIGHT ASSEMBLY BROKEN, REPLACED LAMP HOLDER AT SEAT 25 DEFDec 24, 2019 · N330NW · Airbus A320211 · Emergency LightingSDR DALA2019122757571Floor Support · corrodedCORRODED FLOOR SUPPORT, -Y1162.5 BETWEEN FRAMES 68 AND 69 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472089, AND D53472089.Dec 24, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019122757570Floor Support · corrodedCORRODED FLOOR SUPPORT, -Y1227 BETWEEN FRAMES 66 AND 68 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472800, AND D53472000.Dec 24, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020011700375Damper · failedDONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA, REPLACED PASSENGER CREW DOOR 842 AT AFT GALLEY AREA.Dec 23, 2019 · N319US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2019122737569Support Frame · crackedCRACKED SUPPORT FRAME, FRAME 68 UNDER STRINGER 23L IN THE AFT GALLEY AREA, REPLACED SUPPORT FRAME IAW SRM 51-72-11, AND DWG D53470150.Dec 22, 2019 · N319US · Airbus A320211 · Fuselage Main, StructureSDR DALA2019122727568Support · corrodedCORROSION FRAME SUPPORT LOCATED AT LEVEL STR 23R BETWEEN FRAMES 69 AND 70 IN THE AFT GALLEY AREA, REPLACED THE FRAME SUPPORT IAW SRM 51-72-11, AND DWG D53470100.Dec 22, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019122727567Floor Support · corrodedCORROSION FLOOR BEAM -Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53918123 AND SRM A320 51-72-11Dec 22, 2019 · N319US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019122727566Fitting · crackedCRACK INDICATION ON INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT, FRAME 16 AT FWD GALLEY AREA (2EA), REPLACED INTERCOSTAL FITTING ON UPPER AND LOWER INBOARD HOLES AT LEVEL DOOR STOP 7 LT FRAME 16 AT FWD GALLEY AREA AS PER A320 SDec 21, 2019 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019122727574Dummy Rail · corrodedCORROSION RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 21 AT FWD GALLEY AREA, REPLACED RAIL DUMMY Y503.2 LOC. BTW FR 12 TO FR 21 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND SRM 51-72-11 AND DWG #D53112825 AND DWG #D53110984Dec 21, 2019 · N319US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019121007214Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATION 1C, REPLACED LIGHT FIXTURE AT SEAT 1CDec 10, 2019 · N322US · Airbus A320211 · Emergency LightingSDR DALA2019120637126Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV.ORIGINAL AND PRI 582610-14 REV.0 TO 9Dec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637125Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 12.500 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637124Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 11.325 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637123Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), REPAIR PER ER/A 00-582610Dec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637122Pressure Panel · crackedCRACK INDICATION ON PLATE PRESSURE PANEL OPEN HOLE FR36RH Y-773, CRACK DIRECTION 12 OCLOCK LOOKING AFT. THE CRACK EXCEEDS THE AUTHORIZED REPAIR AREA AT THE PRESSURE PANEL BETWEEN FR35RH AND FR36RH. PERFORMED SECTION 1AS REPAIR AS PER ERA 582610-14AD REV. ORIGIDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, StructureSDR DALA2019120637121Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM -Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR AS PER ERA 582610-14AD REV. ORIGINAL AND PRI 58210-14 REV. 0 TO 9 SECDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637120Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 8.750 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PRE SSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637119Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 3.2 INCH OB FROM +Y1292, CRACK DIRECTION ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV. 0 TO 9Dec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637118Frame · crackedCRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL AREA AND 15.250 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, REPDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637117Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV 0 TO 9 SECDec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637116Frame · crackedCRACK INDICATION ON FRAME 36 ON PRESSURE PANEL AREA AND 17.625 INCHES APPROX. INBOARD POSITION FROM Y +1292.0 ( CRACK DIRECTIONS 7 & 1 OCLOC K, 2 EA IN THE SAME HOLE) IN FWD CARGO COMPARTMENT (1 EA) (A CRACK TH AT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND ADec 2, 2019 · N331NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019120637113Shear Tie · corrodedCORROSION SHEAR TIE LOCATED FR34 AND FROM STR42L TO STR43L IN FWD CARG O COMPARTMENT, REPLACED SHEAR TIE LOCATED FR 34 AND FROM STR-42L TO STR 43L IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11-801 AND DRAWING NO 53231626Nov 29, 2019 · N331NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2019112606941Damper · no test1L DOOR DAMPER WILL NOT PASS FUNCTION CHECK, REPLACED PASSENGER CREW DOOR DAMPERNov 26, 2019 · N325US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2019112606940Shear Tie · corrodedCORROSION SHEAR TIE LOCATED FR34 AND BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT, REPLACED SHEAR TIE LOCATED FR.34 AND BETWEEN STR.41R TO STR.42R IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DWG D53231586Nov 26, 2019 · N331NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2019112606938Floor Support · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66 TO FR 67 +18 INCH +Y1292 AFT IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM +Y1292 LOCATED BTW FR66 TO FR67+18 INCH IN PASSENGER CABIN ASPER A320 SRM 51-72-11 DWG # D53472000Nov 26, 2019 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019112606937Floor Support · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 68 TO FR 69 AND + Y1292 IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEM +Y1292 LOCATED BTW FR 68 TO FR 69 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 DWG #D53472000Nov 26, 2019 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019112646934Cylinder · malfunctionedDONT WORK CORRECTLY PASSENGER CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER IN PASSENGER CABIN 1E/A, REPLACED PASSENGER CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER AS PER 52-13-14-400-001-ANov 23, 2019 · N320US · Airbus A320211 · Emergency EquipmentSDR DALA2019112646933Keelbeam · crackedCRACK KEEL BEAM LOC. ANGLE BTW FR45,FR46 L/H IN MAIN WHEEL WELL (1EA), REPLACED ANGLE LOC ON KEEL BEAM BTW FR 45, FR 46 L/H IN MAIN WHELL WELL (1E/A) AS PER A320 SRM 51-42-11 AND DWG#D53371804Nov 23, 2019 · N320US · Airbus A320211 · Fuselage Main, KeelSDR DALA2019112306858Floor Support · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66 TO FR 70 AND -Y 765 A FT IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM -Y765 LOCATED FLOOR STRUCTURE BTW FR66 TO FR70 IN PASSENGER CABIN ASPER A320 SRM 51-72-11 AND DRAWING D53472B16Nov 22, 2019 · N331NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019112206857Shear Tie · corrodedCORROSION SHEAR TIE LOC. FR32 BTW STR 42 TO STR 43 L/H IN FWD, REPLACED SHEAR TIE LOC FR 32 BTW STR 42 TO STR 43 L/H FWD CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND DRAWING D53231626Nov 21, 2019 · N331NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2019112326856Shear Tie · corrodedCORROSION SHEAR TIE LOCATED FR32 AND BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT, REPLACED SHEAR TIE LOC FR 72 AND BTW STR 41R TO STR 42R IN FWD CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND D53231626Nov 21, 2019 · N331NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2019112326855Anchor Fitting · out of toleranceRT MLG ANCHORAGE FITTING HOLE #67 IS OUT OF TOLERANCE. REF PRI 583035-14 REV 1, REPAIRED HOLE #67 IN RT MLG ANCHORAGE FITTING PER PRI 583025-15 REV 3, REF ER/A 583025-14AD REV ORIGINALNov 21, 2019 · N326US · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR DALA2019112206854Anchor Fitting · noneRT WING ANCHORAGE FITTING REMOVAL REF ER/A 582404-14 REV A PRI REV 3 SEC 2 STEP 4, REMOVED RT MLG ANCHORAGE FITTING, INSPECTED AND REINSTALLED FITTING PER PRI 583025-14 REV O, REV 1, REV 2 AND REV 3, REF ER/A 583025- 14AD REV ORIGINAL ALSO PER PRI 582404-14 RENov 21, 2019 · N326US · Airbus A320211 · Wing, Attach FittingsSDR DALA2019112326853Shear Tie · corrodedCORROSION INTERNAL STRUCTURE SHEAR TIE LOC ON FRAME 33, BTW STRINGER 42L AND STR. 41R IN FWD CARGO COMPARTMENT (3EA), REPLACED CLEAT (3E/A) LOCATED ON INTERNAL STRUCTURE FRAME 33 BTW STRINGER 42L AND STR 41R IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 ANNov 21, 2019 · N320US · Airbus A320211 · Fuselage Internal Mounting Structure
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