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 DALA2019092705567Web · corrodedCORROSION WEB LOCATED BETWEEN FR58 TO FR59 AND STR38L IN AFT CARGO COMPARTMENT (1 EA), REPLACED WEB LOC BTW FR58 TO FR59 AND STR 38 LH IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DWG NO.D53470320Sep 26, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019092505510Profile · crackedCRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED TRANSMITTING PROFILE ON EXIT DOOR 833 AS PER SRM 51-72-11 AND DWG D52279010.Sep 25, 2019 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA2019092405509Damper · defectivePASSENGER CREW DOOR 831 DOOR DAMPER DOES NOT PASS OPERATIONAL TEST, REPLACED PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA.Sep 23, 2019 · N333NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA2019092205475Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE AT FRAME 36 AND Y1292 + 5 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 7 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC. AT FSep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205474Pressure Deck · crackedCRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292+5 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOSep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205473Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 +3 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF PRESSURE DECK MEMBRANE LOC AT FR36 Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205472Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 + 2 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 6 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FSTENER HOLE OF THE PRESSURE DECK MEMBRANE LOSep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205471Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205470Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205469Pressure Deck · crackedCRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+3 INCH ON RT SIDE (CRACK INDICATION IS 11 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FRSep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205468Pressure Deck · crackedCRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+2INCH RT SIDE (CRACK DIRECTION IS 10 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DUCT MEMBRANE LOC AT FR 36 ASep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205467Angle · crackedCRACK INDICATION ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED AT FRAME 36 AND Y1292+ 1 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (2 EA) (CRACK LENGTH 0.923 AND 0.498 INCH APPROX), PERFORMED REPAIR INSTRUCTIONS ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019092205466Pressure Deck · crackedCRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +6 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION ARE 6 AND 12 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205465Pressure Deck · crackedCRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +4 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LSep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, BulkheadSDR DALA2019092205464Spar · corrodedCORROSION FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING, PERFORMED REPAIR INSTRUCTIONS ON FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING AS PER PRI 581186-14 REV 0 AND REV 1 AND ER/A 581186-14 REV ORIGINAL.Sep 22, 2019 · N332NW · Airbus A320211 · Wing, Rib/BulkheadSDR DALA2019092205463Stringer · corrodedCORROSION STRINGER 41R LOWER FLANGE, BTW FRAME 25 AND FRAME 28 IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRG 41R LOC BTW FR 24 TO FR 30 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING #D53231586.Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2019092205508Dummy Rail · corrodedCORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 12 TO FR 16 Y+503 .2 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTN FR 12 TO FR 16 Y +503.2 IN PASSENGER CABIN AREA AS PER SRM 51-72-11 AND DWG #D53112825Sep 21, 2019 · N333NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019092205507Profile · crackedCRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 TRANSMITTING PROFILE AFT IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.Sep 21, 2019 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA2019092205506Profile · crackedCRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE AFT IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 TRANSMITTING PROFILE AFT IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.Sep 21, 2019 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA2019092205462Spar · corrodedCORROSION FALSE SPAR BOX SKIN LOCATED RIB5 BOTTOM SURFACE ON RT WING, PERFORMED TIME-LIMITED REPAIR FALSE SPAR BOX SKIN LOCATED RIB 5 BOTTOM SURFACE ON RT WING AS PER PRI 581187-14 REV 0 AND ER/A 581187-14 REV ORIGINAL.Sep 21, 2019 · N332NW · Airbus A320211 · Wing, Rib/BulkheadSDR DALA2019092005505Profile · crackedCRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL FWD IN PASSENGER CABIN, REPLACED EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL FWD IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D52279010.Sep 20, 2019 · N333NW · Airbus A320211 · Emergency ExitsSDR DALA2019092005504Beam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 Y- 1292 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 Y-1292 IN PASSANGER CABIN (1E/A) AS PER SRM 51-72-11 AND DWG D53112814.Sep 19, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019092005503Floorbeam · corrodedCORROSION FLOOR STRUCTURE LOCATED AT FR 67+16INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN, REPLACED FLOORBEAM STRUCTURE LOCATED AT FR 67 +16 INCH TO FR 69 AND Y-1292 IN PASSENGER CABIN AREA AS PER SRM 51-72-11 AND DWG# D5347200.Sep 19, 2019 · N333NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2019092005502Angle · corrodedCORROSION FRAME 71 ANGLE LOCATED BETWEEN STR 27R AND STR 32R AT LOWER FUSELAGE, REPLACED ANGLE LOC AT FR 71 BTW STR 27R AND STR 32R LOWER FUSELAGE AS PER SRM 51-42-11 AND DWG D53571510.Sep 19, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019091805411Dummy Rail · corrodedCORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 14 TO FR 16 Y+940 IN PASSENGER CABIN (1EA), REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR14 TO FR16 Y+940 IN PASSENGER CABIN (1E/A) AS PER SRM 51-72-11 AND DWG D53112822.Sep 17, 2019 · N333NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019091805410Beam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66+6INCH TO FR 70 Y-765 IN PASSENGER CABIN (1E/A), REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR66+6" TO FR70 Y-765 IN PASSENGER CABIN (1E/A) AS PER SRM 51-42-11 AND DWG D53-472816.Sep 17, 2019 · N333NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019091505409Cleat · corrodedCORROSION CLEAT BTW STR 43L TO 42L AT LEVEL OF FR33 IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT BTW STR 43L TO STR 42L LEVEL FR33 FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D5323039820001.Sep 14, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019091505408Cleat · corrodedCORROSION CLEAT AT LEVEL OF FR31 AND BTW STRG 41R AND STRG 42R IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT AT LEVEL OF FR31 AND BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D53230514Sep 14, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019091105299Stringer · corrodedCORROSION STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT, REPLACED STRINGER LOC. STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND 51-42-11. DRAWING D53231626.Sep 10, 2019 · N332NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2019090705246Strap · corrodedCORROSION INTERNAL STRUCTURE (SKIN AREA), LOC FRAME 26+3INCH, STRINGER 40R, IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRAP FITTING ON INTERNAL STRUCTURE FR 26 BTW 40R TO STR 41R AS PER SRM 51-72-11 AND SRM 51-42-11 AND DWG #D53231380.Sep 7, 2019 · N332NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2019090405189Frame · crackedCRACK INDICATION ON FRAME 16 LT IN LOWER INBOARD HOLE OF DOOR STOP FITTING 7 CRACK POSITION 3 O'CLOCK AT FWD GALLEY AREA, REPLACED FITTING LOCATED ON FR 16 ON DOOR STOP FITTING #7 LT SIDE ASPER SRM 51-72-11 AND DWG D53112300.Sep 4, 2019 · N332NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090305159Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE 2"APPROX OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PRI 5802Sep 2, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105158Frame · crackedCRACK INDICATION ON FR36 LT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX (8 E/A) "A CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BTW FR 35 LT AND FR36 LT, PERFORMED REPAIR INSTRUCTION SECTION 1 ON FR36 LT SIDE OFAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105157Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 4.715" APPROX FR OM OTBD -Y1292 PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION 1 ON FR36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX AS PER PAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105156Frame · crackedCRACK INDICATION ON FRAME 36 LT SIDE IN HOLE LOCATED ABOVE + Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 LT SIDE AT THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER Aug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105155Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 2.920" APPROX AND OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION 1 ON FRAME 36 RT SIDE OF THE PRESSURE DECK CENTER WINAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105154Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED ABOVE - Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER Aug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105153Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED 1.800" APPROX INBD FROM -Y1523 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PRESSURE DECK MEMBRANE TO CENTER WING BOX AS PER PRI 580236-14 REV 0, REV 1 , REV 2, REV 3 ANDAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105152Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE IN HOLE LOCATED AT 3.835" APPROX OTBD FROM -Y1292 OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX IN FWD CARGO COMPARTMENT (1 EA), PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DECK MEMBRANE TO CENAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019090105151Frame · crackedCRACK INDICATION ON FRAME 36 RT SIDE OF THE PRESSURE DECK CENTER WING BOX (8EA) A CRACK THAT EXCEEDS THE AUTORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BTW FR 35 RT AND 36RT, PERFORMED REPAIR INSTRUCTION SECTION I ON FR36 RT SIDE OF THE PRESSURE DAug 31, 2019 · N312US · Airbus A320211 · Fuselage Main, FrameSDR DALA2019083005188Seat Track · corrodedCORROSION SEAT TRACK -Y765 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y765 BTW FR 41 TO FR 47 IN PASSENGER CABIN ASPER SRM 53-31-15-02A AND 51-72-11 AND DWG #D53472554.Aug 29, 2019 · N332NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019082905185Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 AT LEVEL OF FR 68 AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1292 LOC. FR68 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND 51-42-11, DWG # D53472000.Aug 28, 2019 · N332NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2019082905184Floorbeam · corrodedCORROSION FLOORBEAM -Y765 AND FR 20 AT FWD GALLEY AREA, REPLACED FLOORBEAM -765 LOC FR 12 TO FR 24 AT FWD GALLEY AREA ASPER SRM 51-72-11 AND 51-42-11 DWG 53112812.Aug 28, 2019 · N332NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2019082905183Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 BTW FR 67 AND FR 68 FLOOR STRUCTURE AT AFT GALLEY AREA, REPLACED FLOORBEAM-Y1292 LOC. FR 68 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND 51-42-11, DWG # D53472000.Aug 28, 2019 · N332NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2019082905182Web · crackedCRACK FLOOR STRUCTURE WEB BTW FR 68 TO FR 69 AT LEVEL STR-23L SIDE AT AFT GALLEY AREA, REPLACED FLOOR STRUCTURE WEB BTW FR 68 TO FR 69 AT LEVEL STR 25L SIDE AT AFT GALLEY AREA (1EA) ASPER SRM 51-72-11 AND DWG # D53480020.Aug 28, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019083005187Seat Track · corrodedCORROSION SEAT TRACK Y1292 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-20 31-DE AND FOUND OUT LIMITS, REPLACED SEAT TRACK Y1292 LOCATED BTW FR41 TO FR47 IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG # D57130146.Aug 27, 2019 · N332NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019083005186Seat Track · corrodedCORROSION SEAT TRACK Y1292 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE AND FOUND OUT LIMITS, REPLACED SEAT TRACK Y1292 LOCATED BETWEEN FR36 TO FR41 IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG # D53371112.Aug 27, 2019 · N332NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019082875034Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1292 AND FR20 AT FWD GALLEY AREA, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 24 IAW SRM A320 51-72-11, DRAWING D53212368, AND DWG D53112812.Aug 27, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019082875030Web · corrodedCORROSION INTERNAL STRUCTURE WEB FR 50 TO FR 51 AND STR 38R IN AFT CARGO COMPARTMENT, REPLACED INTERNAL STRUCTURE WEB FR 50 TO FR 51 AND STR 38R IN AFT CARGO COMPARTMENT (1EA) ASPER SRM A320 51-72-11 AND INSTALLED FASTENERS ASPER SRM A320 51-42-11 AND DRAWING Aug 27, 2019 · N312US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019082855029Floor Support · corrodedCORRODED FLOOR SUPPORT, -Y765, FRAME 68 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66 & 70 IAW DWG D534720000, ISSUE AF, AND SRM 51-72-11.Aug 24, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous Structure
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