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 DALA2020043002319Frame · crackedCRACK INDICATION ON FRAME 36 , CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36, PERFORMED REPAIR AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36 AT HOLE ZONE 1 (INB SIDE) Y1292 IN FWD CARGO COMPARTMENT AS PER PRI 585863-14AD REV 0,1Apr 21, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020043002318Frame · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36. REPAIR PRIOR TO FURTHER FLIGHT. WC 5711-01 036-03B, AD 2018-13-08. HOLE ZONE 2 (OUTBD SIDE) Y 765, DIRECTION IS 1 2 AND 9 OCLOCK, DEPTH IS 0.160 INCH. IN FWD CARGApr 15, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020041502262Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 4 HOLE 2 (INB SIDE) -Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINAApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502261Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 HOLE ZONE 2 FR 36 (INB SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502260Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 FR 36 -Y765 ZONE 1 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502259Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT HOLE ZONE 2 (O/B SIDE) Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV Apr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502258Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502257Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502255Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 3 AT ZONE 2 (O/B SIDE) Y254 AT FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502254Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT ZONE 1 Y254 (INB SIDE) FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502253Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 FR36 AT ZONE 1 Y254 INB ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502252Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 5 AT HOLE ZONE 1 FR 36 (O/B SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020040602190Frame · crackedCRACK INDICATION ON FRAME 36 ON PRESSURE DECK PANEL LOCATED - Y1300 CRACK DIRECTION 3 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), REPLACED WEB LOC. FRAME 36 RH SIDE ON PRESSURE DECK PANEL ASPER A320 SRM 51-42-11 AND DRAWING D53370500, D28270011Apr 4, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602189Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL LOCATED -Y 1301 CRACK DIRECTION 3 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), REPLACED WEB LOC. FRAME 36 RH SIDE ON PRESSURE DECK PANEL ASPER A320 SRM 51-42-11 AND DRAWING D53370500, D28270011Apr 4, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602188Floorbeam · corrodedCORROSION FLOOR BEAM -Y765 BTW FR67 TO FR68 AT AFT GALLEY AREA, REPLACED FLOOR BEAM LOC -Y765 BTW FR 66 TO FR 70 AFT GALLEY AREA FLOOR STRUCTURE AS PER A320 SRM 51-72-11 AND SRM 51-42- 11 AND DWG D53472816Apr 3, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020040602187Frame · corrodedCORROSION WEB FRAME 20 AT LEVEL STR 23R FLOOR STRUCTURE AT FWD GALLEY AREA, REPLACED WEB FRAME 20 AT LEVEL STR 23R FLOOR STRUCTURE AT FWD GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG D53112784Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602186Intercostal · crackedCRACK INDICATION ON FRAME 16 RH SIDE ON DOOR STOP FITTING 7 HOLE 3, CRACK AT 8 O CLOCK ON UPPER FUSELAGE (1 EA), INTERCOSTAL REPLACEMENT IS DOCUMENTED ON NON-ROUTINE CARD 64/200 RII INSPECTION COMPLETEApr 2, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020040602185Floorbeam · corrodedCORROSION FLOOR BEAM -Y765 AT LEVEL FR20 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 AT LEVEL FR.12 TO FR24 AT FWD GALLEY AREA ASPER SRM A320 FAM AMM 51-72-11 AND DWG D53112782Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020040602184Stop Fitting · crackedCRACK INDICATION ON FRAME 16 RH SIDE ON DOOR STOP FITTING 7 HOLE 1, CRACK AT 7 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED NEW LOC. FR.16 RH SIDE ON DOOR STOP #7 7 ASPER A320 SRM 51-42-11 AND 51-72-11 AND DWG D53112300Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2020032001957Structure · corrodedCORROSION INTERNAL STRUCTURE SECTION CONNECTION AT FR67 AND STRG 28L UNDERFLOOR BAY IN AFT CARGO COMPARTMENT (1EA), REPLACED NEW SECTION CONECTION LOC. FR67 AND STR 28L UNDER FLOOR BAY IN AFT CARGO COMPARTMENT (1EA) AS PER A320 SRM 51-72-11 AND DRAWING D534805Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020032001956Door Sill · corrodedCORROSION LOWER SILL AT LEVEL FR68 AND STR23L AT AFT GALLEY AREA, REPAIRED LOWER SILL AT LEVEL FR68 AND STR 23L AT AFT GALLEY AREA AS PER SRM A320 53-41-14-300-001Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020032001955Seat Track · corrodedCORROSION FLOOR BEAM -Y765 AT LEVEL FR66 AT AFT GALLEY AREA, REPLACED SEAT TRACK LOCATED -Y765 BTW FR64 TO FR66 AFT GALLEY AREA FLOOR STRUCTURE AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWG #D53472816Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001954Floorbeam · corrodedCORROSION FLOOR BEAM BTW -Y1292 AND -Y1162.5 BTW FR66 TO FR 68 AT AFT GALLEY AREA, REPLACED FLOOR BEAM -Y1162 LOC BTW -Y1292 AND 1162.5 BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER DWG D53472000Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020032001953Floorbeam · corrodedCORROSION FLOOR BEAM -Y1162.5 BTW FR68 AND FR 69 AFT GALLEY AREA, REPLACED FLOOR BEAM -Y1162.5 NEW LOCATED BTW FR68 AND FR69 AFT GALLEY AS PER A320 SRM 51-72-11 AND DWG #D53472001Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020032001952Stringer · corrodedCORROSION STRINGER 26R AT LEVEL OF FR66 IN AFT CARGO COMPARTMENT (1EA), REPLACED NEW STRINGER 26R AT LEVEL OF FR 66 IN AFT CARGO COMPARTMENT (1EA) AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DRAWING D53480020Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2020032001951Seat Track · corrodedCORROSION SEAT TRACK -Y1292 AT LEVEL OF FR 20 FLOOR AREA AT FWD GALLEY AREA, REPLACED NEW SEAT TRACK -Y1292 AT LEVEL FR20 FLOOR AREA FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53918547Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001950Dummy Rail · corrodedCORROSION RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 16 AT FWD GALLEY AREA, REPLACED BEAM Y503.2 LOCATED BTW FR12 TO FR16 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53112827Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001949Door Sill · corrodedCORROSION LOWER SILL AT LEVEL OF FR 68 AND STR 23RH AT AFT GALLEY AREA, REPLACED LOWER SILL AT LEVEL OF FR 66 TO FR 68 AND STR 23R/H AT AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG #D53480505Mar 18, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020031401838Intercostal · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON DOOR STOP FITTING 7 HOLE 3, CRACK AT 4 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED INTERCOSTAL FITTING IS TO BE ACCOMPLISHED ON NON-RUTINE CARD 66/200Mar 13, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020031401837Intercostal · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON DOOR STOP FITTING 7 HOLE 1, CRACK AT 5 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED INTERCOSTAL FITTING ON FRAME 16 LH SIDE AT LEVEL DOOR STEP 7 ON UPPER FUSELAGE AS PER A320 SRM 51-72-11 AND DRAWING #D53112300Mar 13, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020031401848Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED, LOCATIONS:33D, RESECURED EMERGENCEY FLOOD LIGHT COVERMar 11, 2020 · N329NW · Airbus A320211 · Emergency LightingSDR DALA2020031001778Light · inoperativeDURING SVC FOUND EMERGENCY LIGHT MSG. (EXT. LOADS EMER R"), REPLACED 4 BULBS ON RT SIDE & REPLACED RT MID EPCU 12WL OVER WINGMar 5, 2020 · N317US · Airbus A320211 · Emergency LightingSDR DALA2020030401616Bezel · unsecureEMERGENCY SEAT MOUNTED LIGHTING DAMAGED LOCATIONS:33D , RE-AFFIXED LIGHT BEZELFeb 27, 2020 · N320US · Airbus A320211 · Emergency LightingSDR DALA2020021401165None · noneSHIP 3230 - ATB - DUE TO AFT CARGO SMOKE INDICATION. CARGO FIRE EXTINGUISHER DISCHARGED BY CREW. SUSPECT SMOKE WAS CAUSED BY USE OF GSE EQUIPMENT NEAR THE CARGO DOOR PRIOR TO FLIGHT THAT RESULTED IN ACCUMULATION OF FUMES IN THE COMPARTMENT. CORRECTIVE ACTION: Feb 13, 2020 · N330NW · Airbus A320211 · Standard Practices/StructuresSDR DALA2020021431163Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED, RESECURED EMERGENCY LT MOUNT ON SEAT 13DFeb 12, 2020 · N327NW · Airbus A320211 · Emergency LightingSDR DALA2020020700974Battery Pack · inoperativeDURING S/C FOUND FWD EMER LIGHT BATTERY PAK INOP, R&R RWD BATT PAKFeb 6, 2020 · N378NW · Airbus A320211 · Emergency LightingSDR DALA2020020310858Frame · crackedCRACK INDICATION ON FRAME 2 INTERNAL SIDE UPPER BOLT VERTICAL FLANGE O F THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST LH SIDE. (L=0.500 INCH APPROX.) IN COCKPIT (1 EA), PERFORMED REPAIR INSTRUCTION ON FRAME 2 INTERNAL SIDE UPPER BOLT VERTICAL FLANGEJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100770Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 7.5 INCHES OTBD OF -Y1292, CRACK AT 7 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100769Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 6.5 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100768Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 4.75 INCHES OTBD OF -Y1292. CRACK AT 2 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100767Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 4 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100766Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE. 3 INCHES OTBD OF -Y1292. CRACK AT 6 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV Jan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100765Frame · crackedCRACK INDICATION ON FRAME 36 RT UPPER SURFACE PRESSURE DECK MEMBRANE, 2 INCHES OTBD OF -Y1292. CRACK AT 12 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100764Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 5.75 INCHES OTBD OF Y1292. CRACK AT 12 O`CLOCK IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14AD, REV Jan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100763Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 8.25 INCHES OTBD OF Y1292. CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REVJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100762Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 6.5 INCHED OTBD OF Y1292, CRACK AT 4 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100761Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 4.75 INCHES OTBD OF Y1292, CRACK AT 12 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100760Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE, 4 INCHES OTBD OF Y1292, CRACK AT 4 O`CLOCK IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REV ORIGINJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100759Frame · crackedCRACK INDICATION ON FRAME 36 LT UPPER SURFACE PRESSURE DECK MEMBRANE AT 3 INCHES OTBD FROM Y1292, CRACK AT 4 O`CLOCK IN THE FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS ON THE FRAME IAW ER/A 584069-14AD, REV O, REV 1, REV 2, AND ER/A 584069-14AD, REJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020013100758Frame · crackedCRACK INDICATION ON FRAME 36 LH UPPER SURFACE PRESSURE DECK MEMBRANE AT 2 INCHES OTBD FROM Y1292. CRACK AT THE 12 O`CLOCK, IN THE FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON FRAME 36 IAW ER/A 584069-14AD, REV 0, REV 1, REV 2, AND ER/A 584069-14ADJan 31, 2020 · N319US · Airbus A320211 · Fuselage Main, Frame
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