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 DALA2021070203674Frame · crackedSHIP 3277 CRACK FRAME 35 LH THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01171-04A. (1649870)Nov 6, 2020 · N377NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2021070203673Frame · crackedSHIP 3277 CRACK FRAME 35 LH THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01171-04A. (1649855)Nov 6, 2020 · N377NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2021070203672Window Frame · crackedSHIP 3277 CRACK INDICATION ON FRAME 4 WINDOW LH SIDE POST LOWER ATTACHMENT INTERNAL SIDE IN COCKPIT. CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01230-01A. (1649492)Nov 6, 2020 · N377NW · Airbus A320211 · Fuselage Main, StructureSDR DALA2020111103677Stiffener · crackedCRACK INDICATION ON FRAME 4 LOWER ATTACHMENT SIDE POST LT SIDE VERTICAL STIFFENER. CRACK LENGTH IS 0.340 INCH. AD 2020-06-10, WORK CARD 5311-01230. CORRECTIVE ACTION: ACCOMPLISHED REPAIR INSTRUCTIONS ON FRAME 4 LOWER ATTACHMENT SIDE POST LT SIDE VERTICAL STNov 3, 2020 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020111103676Stiffener · crackedCRACK INDICATION ON FRAME 4 LOWER ATTACHMENT SIDE POST LT SIDE VERTICAL STIFFENER CRACK LENGTH IS 0.340 INCH. CORRECTIVE ACTION: ACCOMPLISHED REPAIR INSTRUCTIONS ON FRAME 4 LOWER ATTACHMENT SIDE POST LT VERTICAL STIFFENER, AS PER AMDS CARD 5311-01230-01A.Nov 3, 2020 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020110403584Hinge · corrodedCORROSION RUDDER HINGE ATTACHMENT BUSHING LOWER SERVO CONTROL. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON RUDDER HINGE ATTACHMENT BUSHING LOWER SERVO CONTROL ACTUATOR LOWER LUG FIN 1025 GM RUDDER SIDE ON VERTICAL STABILIZER, AS PER DWG D55471202 ISSUE M RNov 2, 2020 · N377NW · Airbus A320211 · Rudder StructureSDR DALA2020110403583Hinge · corrodedCORROSION RUDDER HINGE ON LOWER BUSHING OF RUDDER SERVO CONTROL HINGE ATTACHMENT FIN 2025GM UPPER ACTUATOR ON RUDDER ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON RUDDER HINGE ATTACHMENT BUSHING UPPER SERVO CONTROL ACTUATOR LOWER LUG FNov 2, 2020 · N377NW · Airbus A320211 · Rudder StructureSDR DALA2020110403580Floor Support · corrodedCORROSION FLOOR BEAM -Y1225 LOCATED BETWEEN FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAR -Y1225 LOCATED BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG D53472780 ISSUE K.Nov 2, 2020 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020110403579Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED AT LEVEL FR 68 AND STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162.5 LOCATED AT LEVEL FR 68 TO FR 69 ON STR 23R AT AFT GALLEY AREA, AS PER A320 SRM 51-72-11 AND DWG D53472780 ISSUE: K, RELEASE DANov 2, 2020 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020092903190Strut · corrodedCORROSION INTERCONNECTING STRUT OUTBOARD FLAP ON LT WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OUTBOARD FLAP ON LT WING, AS PER A320 FAM AMM 27-51-44-400-001-A. PERFORMED ADJUSTMENT OF THE INTERCONNECTING STRUT, AS PER A320 FAM AMM 27-51.Sep 22, 2020 · N378NW · Airbus A320211 · Trailing Edge FlapsSDR DALA2020092203146Frame · crackedCRACK INDICATION ON FRAME 16 AT DOUBLE JOGGLE AREA, RT SIDE, HOLE B, AT LEVEL DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: RT SIDE AT LEVEL DOOR STOP 7, AS PER PRI 587478-14AD REV 0 AND REV 1 ER/A NR 587478-14AD REV.Sep 21, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020092103145Flap Track · corrodedCORROSION FLAP TRACK FAIRING 632CB GROUND PLATE ON RT WING. CORRECTIVE ACTION: REPLACED FLAP TRACK FAIRING 632 CB GROUND PLATE ON RT WING, AS PER ER/A 587521-14 PRI REV 0. ER/A 587521-14 REV ORIGINAL.Sep 20, 2020 · N378NW · Airbus A320211 · Trailing Edge FlapsSDR DALA2020092103144Flap Track · corrodedCORROSION FLAP TRACK FAIRING 633CB GROUND PLATE ON RT WING. CORRECTIVE ACTION: REPLACED FLAP TRACK FAIRING 633 CB GORUND PLATE ON RT WING, AS PER ER/A 587521-14 PRI REV 0 ER/A 587521-14 REV ORIGINAL.Sep 20, 2020 · N378NW · Airbus A320211 · Trailing Edge FlapsSDR DALA2020092003136Power Supply · inoperativeINOP EPSU-EMERGENCY POWER SUUPLY UNIT 11WL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT (11WL) IN PASSENGER CABIN (1EA) ON SERVICEABLE CONDITION PN 3214-54-10 SN 2448, AS PER A320 FAM AMM 33-51-38-400-001-A. OPERATIONAL TESep 19, 2020 · N378NW · Airbus A320211 · Emergency LightingSDR DALA2020091903120Frame · crackedCRACK INDICATION ON FRAME 16 LT SIDE, DOOR STOP 7 HOLE ?1 AT FWD GALLEY AREA (1 EA), CRACK AT 5 O CLOCK. CORRECTIVE ACTION: REPLACED INTERCOSTAL ON FRAME 16 LT SIDE DOOR STOP 7 AT FWD GALLEY AREA, AS PER SRM A320 51-72-11 AND DRAWING D53112300 ISSUE "HOO" RELSep 18, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020092103130Frame · crackedCRACK INDICATION ON FRAME 20 AT THE DOUBLE JOGGLE AREA, LT SIDE, HOLE. CORRECTIVE ACTION: REPAIRED FRAME 20 AT THE DOUBLE JUGGLE AREA LT SIDE HOLE A, AT LEVEL DOOR STOP 7 AT FWD GALLEY AREA, AS PER PRI 587474-14AD REV 0 1 AND ER/A 587474-14AD REV ORIGINAL.Sep 18, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020092103129Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE DOOR STOP 7 HOLE 3 AT FWD GALLEY AREA. CORRECTIVE ACTION: C/W ER/A 587495-14AD.Sep 18, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020092103128Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE DOOR STOP 7 HOLE ?1 AT FWD GALLEY AREA (1 EA), CRACK AT 8 O CLOCK, REQUESTING REPAIR DISPOSITION REPAIR. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING ON FRAME 16 RT SIDE DOOR STOP 7 AT FWD GALLEY AREA (1E/A), AS PER PRISep 18, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020091903127Skin · damagedNICK EXTERNAL SKIN BETWEEN STRG 42L AND STRG 43L AND 4.5 INCH AHEAD OF FR 26 AT LOWER FUSELAGE (2 EA). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN STR 42L AND STR 43L AND BETWEEN FR 23 TO FR 23 AT LOWER FUSELAGE, AS PER PRI 587690-1Sep 18, 2020 · N378NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2023090807359Unknown · unknownSHIP 3278 A CRACK WAS FOUND IN FR 16 RHS AT HOLE B. CORRECTIVE ACTION: COMPLIED WITH ERA 587478-14AD. (1615327)Sep 16, 2020 · N378NW · Airbus A320211 · Fuselage Main, FrameSDR DALA2020091403065Hinge Fitting · corrodedCORROSION HINGE FITTING LUG NR 2 ELEVATOR ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) OF HINGE FITTING NR 2 ELEVATOR RT HORIZONTAL STABILIZER, AS PER AIRBUS CMM 55-21-15.Sep 12, 2020 · N378NW · Airbus A320211 · Elevator StructureSDR DALA2020091103044Skin · gougedSHIP 3278, GOUGE EXTERNAL SKIN AT LEVEL OF FR23 AND STRG 23L ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL OF STR.23L FR 23 ON UPPER FUSELAGE, AS PER PRI 587548-14 REV. 0 AND ER/A 587548-14 REV ORIGINASep 11, 2020 · N378NW · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2021072204139Hinge Fitting · corrodedSHIP 3217 STABILIZERS - RH ELEVATOR - LUG BORE OF HINGE ARM FITTINGS CORROSION. CORRECTIVE ACTION: ACCOMPLISHED ER/A 533420-14 REV B SECTION IV INSPECTION. CONTINUE ON MON. (1612034)Sep 10, 2020 · N317US · Airbus A320211 · Elevator StructureSDR DALA2020091603097Skin · corrodedCORROSION INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT. CORRECTIVE ACTION: REPLACED INLET VALVE AIR SKIN IN FWD AVIONIC COMPARTMENT, AS PER A320 FAM AMM 21-26.Sep 10, 2020 · N378NW · Airbus A320211 · Pressure Regulator/Outflow ValveSDR DALA2020091103049Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LT T ANGLE POSITION, IN MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON SECTION I PERMANENT REPAIR ON FR.42 AT AFT LT SIDE "T" ANGLE POSITION IN MAIN WHEEL WELL, AS PESep 10, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090983012Access Panel · crackedSHIP 3278, CRACK ACCESS PANEL 413DL ON LT PYLON. CORRECTIVE ACTION: REPAIRED BY WELDS ACCESS PANEL 413DL ON LT PYLON, AS PER ER/A NO.540187-14MA REV. ORIGINAL SECTION I.Sep 8, 2020 · N378NW · Airbus A320211 · Nacelle/Pylon, Plate/SkinSDR DALA2022111007262Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH REVISION. (1609685)Sep 6, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2022111007261Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH ERA 585867-14. (1609684)Sep 6, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2020090963011Angle · crackedSHIP 3278, CRACK ANGLE AFT TI ANGLE AT FR 42 RT SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: REPLACED TI ANGLE LOC AFT FR 42 RT SIDE IN MAIN WHELL WELL THE REPLACE WAS DOCUMENTED ON AMDS CARD 5353-01006-03.Sep 5, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090953010Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT UPPER RT TI ANGLE POSITION AT MAIN WHEEL WELL. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A N. 587552 14 AD REV ORIGINAL SSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090953009Web · crackedSHIP 3278, CRACK INDICATION ON WEB AT OPEN FASTENER HOLE COMMON TO AFT LOWER RT TI ANGLE POSITION IN MAIN WHEEL WELL. PERFORMED PERMANENT REPAIR ON WEB COMMON TO AFT RT TI ANGLE AT MAIN WHEEL WELL, AS PER ER/A NO. 587552-14AD REV ORIGINAL SECTION I AND PRI NSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090943007Shear Tie · corrodedSHIP 3278, CORROSION SHEAR TIE LOCATED AT FR 33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR33 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUSep 4, 2020 · N378NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2020090943006Shear Tie · corrodedSHIP 3278, CORROSION SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED AT FR30 BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND DRAWING D53232647 ISSUESep 4, 2020 · N378NW · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA2020090943016Guide · out of adjustSHIP 3233, ENTRY DOOR HARD TO OPEN OR CLOSE. CORRECTIVE ACTION: ADJUSTED L1 DOOR GUIDE FITTING, PAR A320 AMM 52-11. OPS CHECK GOOD.Sep 3, 2020 · N333NW · Airbus A320211 · Passenger/Crew DoorsSDR DALA2020090232925Light · malfunctionedCABIN EMERGENCY LIGHTS ARE "ON" AND WILL NOT RESET W/ COCKPIT OR CABIN SWITCH . CORRECTIVE ACTION: RESET A/X D/C PWR OPS CK OKAug 28, 2020 · N312US · Airbus A320211 · Emergency LightingSDR DALA2020090232924Support · corrodedCORROSION WEB SUPPORT LOCATED AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED WEB SUPPORT AT LEVEL -Y1732 BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11-001 AND DWG # D53112783, ISSUE F00 RELEASE DATE:28-MAY-98.Aug 28, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090202926Floor Support · corrodedCORROSION SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT FLOOR LOCATED AT LEVEL -Y1584 AND FR20 AT FWD GALLEY AREA. AS PER A320 SRM 51-72-11 AND DWG D53112786, ISSUE B00.Aug 28, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090302944Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR68 TO FR69 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162.5 LOC BTW FR68 TO FR69 AT AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG #D53472458 ISSUE E RELEASE DATE 09MAY11 DWG # D53472089 ISSUE L Aug 25, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090262922Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED (FLOOR BEAM) SEAT TRACK -Y1292 LOCATED BETWEEN FR12 TO FR24 AT FWD GALLEY AREA ASPER SRM A320 51-72-11 AND DRAWINGS # D53112812 ISSUE E00 RELEASE DATE 08JAug 25, 2020 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020090262921Floor Support · corrodedCORROSION FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1225 FROM FR66 TO FR68 AFT GALLEY AREA ASPER SRM A320 51-72-11 AND DWG # 53472845 ISSUE A RELEASE DATE 02APR98Aug 25, 2020 · N378NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020090262920Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53112814 RELEASE DATE:14-MAR-03, ISSUE:B00 AND DWG D53110920, RELEAAug 25, 2020 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA202008112759Linkage · lack of lubeFWD CARGO DOOR SHOWED OPEN DURING CRUISE. FAULTING THE HANDLE PROX SENSOR 28WV. LUBRICATED THE HANDLE FLAP LINKAGE. CHECKED GOOD IAW AMM 52-31.Aug 5, 2020 · N321US · Airbus A320211 · Cargo/Baggage DoorsSDR DALA2022111507362Door Frame · damagedSHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT DOOR STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD. (1587429)Jul 31, 2020 · N332NW · Airbus A320211 · Fuselage Main, StructureSDR DALA2022111507359Web · crackedSHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD REV A. (1587431)Jul 31, 2020 · N332NW · Airbus A320211 · Fuselage Main, StructureSDR DALA2020051302394Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE DOUBLE JOGGLE AREA OPEN FASTENER HOLE A, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA), PERFORMED REPAIR INSTRUCTIONS ON FR.16 L/H SIDE AS PER ER/A 585862-14AD REV. ORIGINAL AND PRI 585862-14AD REV.0, REV.1, REV.2May 13, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020051302395Damper · failedOPERATIONAL TEST PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA DID NOT PASS, REPLACED DOOR DAMPER PASS/CREW DOOR 831 AS PER A320 FAM AMM 52-11-14-400-001-A AND CHECKED CORRECT DAMPER OPERATIONMay 12, 2020 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2020051302393Hinge Fitting · crackedCRACK DOOR ON HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1 EA), PERFORMED PERMANENT REPAIR ON DOOR HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1EA) ASPER A320 SRM 55-36-42-300-003May 12, 2020 · N321US · Airbus A320211 · Vertical StabilizerSDR DALA2020050802377Structure · corrodedCORROSION INTERNAL STRUCTURE SECTION CONNECTION AT FRAME67 AND STRINGER 30 RIGHT UNDERFLOOR BAY IN AFT CARGO COMPARTMENT (1 EA), REPLACED INTERNAL STRUCTURE SECTION CONNECTION (1EA) LOC FR67 AND STR 30R UNDERFLOOR BAY IN AFT CARGO COMPARTMENT ASPER SRM 51-42-1May 3, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020050802376Damper · unserviceable841 DOOR DAMPER AT FWD GALLEY AREA DONT PASS OPERATIONAL TEST, REPLACED CYLINDER DOOR DAMPER IN UNSERVICEABLE CONDITION P/N FE174-004 S/N 129 AT CREW DOOR 841 AS PER FAM AMM 52-11-14- 000-001-AMay 1, 2020 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2020043002323Frame · corrodedCORROSION ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE, PERFORMED PERMANENT REPAIR ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE AS PER PRI 522853-14 REV O, REV 1,REV 2,REV 3 AND ER/A 522853-14 REV "C"Apr 28, 2020 · N321US · Airbus A320211 · Fuselage Main, Frame
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