N478UA

Service difficulty reports · 95

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N478UA' AND registry_match = 'registration'
  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 CALA2026042815744Thrust Reverser · damagedENG 1 REVERSER FAULT CLEARING THE RUNWAY, NR 1 ENG OTBD REVERSER WILL NOT FULLY STOW DUE TO BROKEN PLATE AND AFT BRACKET BROKE ON OTBD ACTUATOR ROD. LOCKED OUT HYDRAULIC CONTROL UNIT FOR NR 1 ENG THRUST REVERSER IAW AMM 78-30-00-040-013-A. LOWER TR ACTUATORApr 22, 2026 · N478UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2025123012528Light · damagedROW 31 EMERGENCY LIGHT LENS MISSING AND HOUSING CRACKED. REPLACED THE HOUSING IAW AMM 33-51-18. OPS CHKD NORMAL.Dec 28, 2025 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2025120511797Fuel Cap · missingFUEL CAP MISSING. DEFERED ON LOG PAGE 7156404 FUEL CAP MISSING DEFERED ON LOG PAGE 7156404Dec 3, 2025 · N478UA · Airbus A320232 · Fuel StorageSDR CALA2025101610182Fuel Cap · missingCREW REPORTED FUEL CAP IS MISSING. UNABLE TO LOCATE FUEL COUPLING CAP. REPLACED CAP REF APPLICABLE STEPS WITHIN AMM TASK 28-25-41.Oct 15, 2025 · N478UA · Airbus A320232 · Fuel StorageSDR CALA2025090508514Lens · missingFOUND MISSING ESCAPE PATH LIGHT LENS ON SEAT 25ABC. INSTALLED LENS COVER AS REQUIRED IAW AIPC 33-51-19.Sep 4, 2025 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2025082508081Power Supply · no testEMERGENCY LIGHTING TESTS SHOWS THE FOLLOWING FAULTS: EPSU COMM FWD L, EPSU COMM AFT L, EPSU ARMED/ON EMER R, EPSU ARMED/ON L. T/S & FOUND FAULTY FWD ESPU 10WL IAW TSM 33-51-00-810-806A. REMOVED & REPLACED ESPU 10WL IAW AMM 3-51-38-000-001A & 33-51-3 4-400-00Aug 22, 2025 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2025061805652Ecs · odorBIRD STRIKE FWD OF RIGHT PACK INLET NO EVIDENCE VISIBLE IN PACK INLET DUCT, NEED TO RUN RIGHT PACK OFF APU BLEED TO ENSURE NO ODOR PRESENT REF LOG PAGE 5219952 FOR ECS SYSTEM LEVEL A DECONTAMINATION PER BIRD STRIKE INSPECTION PROCEDURESJun 16, 2025 · N478UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2025041003674Battery · no testEPSU BATTERY FWD L MESSAGE ON EMERGENCY LIGHTS TEST REMOVED AND REPLACED ESPU BATTERY REF AMM 33-51-38. OKAY FOR SERVICE.PARTS USED: 18-3351-3-0001,QTY :1Apr 9, 2025 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2024112002907Support Angle · damagedAFT CARGO, AT FR 62 S37L SUPPORT ANGLE HAS VISIABLE DAMAGE ()Nov 18, 2024 · N478UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024112002906Support Angle · damagedAFT CARGO, AT FR 59 S37L SUPPORT ANGLE HAS VISIABLE DAMAGE.Nov 18, 2024 · N478UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024070500145Thermostat · intermittentAIR ENG2 BLEED ABNORM PR PFR AND BMC 2 BITE SHOWING: PRESS REG-V 4001HA2 OR SOL 10HA2 OR SENSE LINE. T/S REF TSM 36-11-00-810-810-A. PERFORMED LEAK CHECK ON THE #2 ENG PRV BRAIDED SENSE LINE AND RIGID LINES. NO LEAKS NOTED. PERFORMED HEALTH CHECK ON PRV 4001HAJul 3, 2024 · N478UA · Airbus A320232 · Engine Bleed Air SystemSDR CALA2024052401577Fuel Cap · missingRAMP REPORTED FUEL CAP MISSING. NOTED TO TOMC. REF LP 8038451 - FUEL CAP LOCATED AND RE-INSTALLED.May 22, 2024 · N478UA · Airbus A320232 · Fuel StorageSDR CALA2024011900155Fuel Cap · missingAIRCRAFT CAME IN WITH NO FUEL CAP. PLANE CAME IN WITH NO FUEL CAP. PLACE ON CDL 28A. AIRCRAFT CAME IN WITH NO FUEL CAP. PLACE ON CDL 28A. DISPATCH DESK: 8 NAME: BK DATE: 14-JAN-24- OK TO DEFER PER CDL 28A CAP, COUPLING R OFF 31-2825-9-0001 1481 ON 31-2825-9-00Jan 14, 2024 · N478UA · Airbus A320232 · Fuel StorageSDR CALA2023021600468Safety Valve · unknownGEAR WOULD NOT EXTENDNORMALLY. GRAVITY EXTPER ECAM. REPLACED PRIORITY VALVE, GREEN SYSTEM REF AMM 29-11-33. LEAK CHECKED NO HELP. GEARS AND GEAR DOORS WOULD NOT RETRACT. REPLACED HYD SYTEM SAFETY VALVE. NEED OPERATIONAL TEST. ACCOMPLISHED RII INSPECTION. REPLAFeb 16, 2023 · N478UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR CALA2022061701525Servo Control · failedDIVERTED TO IAD DUE TO DCA HAVING AVAILABLE RUNWAY BELOW MINIMUM REQUIREMENT FOR MEL 2764R. SR MGR MC NEELEY NOTIFIED. SPOILER 3 INOP PLACED ON MEL. HAS HISTORY. DDP COMPLIED WITH. ADD EMP:U244875 PLACE NUMBER THREE SPOILER ON MAL. DDP COMPLIED WITH THIS ISJun 17, 2022 · N478UA · Airbus A320232 · Drag Control SystemSDR CALA2022051801282None · cracked(AD2020-20-05) DURING ROTO PROBE OF RH FR16 FOUND HOLES #A #B #C #8 & #9 WITH CRACK INDICATION ON THE FRAME LAYER REPAIR BEFORE NEXT FLIGHT. () REPAIRED RH FR16 HOLES A,B,C, 8 & 9 BY OVERSIZING & BUSHING INST ALLATION IAW EC/RA 5311-02807. ACCOMPLISHED BY EMP#May 18, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022051601254None · cracked(AD2020-20-05) DURING ROTO PROBE OF RH FR16 FOUND HOLES #A #B #C #8 & #9 WITH CRACK INDICATION ON THE FRAME LAYER REPAIR BEFORE NEXT FLIGHT. ()May 15, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022051601248Skin · corrodedDURING HMV-3 CHECK AT VTMAE BFM CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LH S18 UPPER FUSELAGE SKIN BETWEEN FR69 & 70 STGR 1L & 2L. ECRA 5331-02902. WORK ACCOMPLISHED BY VTMAE EMP V934143. UPON AN INSPECTION OF THE UPPER SURFACE OF THE LH S18 UPPER FUSEMay 15, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022051601247None · cracked(AD2016-14-03) DURING ROTO PROBE OF FR35 STRINGER 28-31 FOUND LH S HOLE #2 CRACKED AND HOLE #4 WITH REJECTABLE DAMAGE. CONTACT EN GNEERING FOR REPAIR INSTRUCTIONS BEFORE FURTHER FLIGHT (REPAIR I AW R DWG & ECRA)May 15, 2022 · N478UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022051301223None · noneAD2022-02-11 DURING ROTO PROBE LH FR16 DOOR STOP #7 FOUND HOLES #1 & #3 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYER. R EPAIR BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUIRE D) REPAIRED L/H FR16 DOOR STOP #7 HOLES #1 & #3 BY INTERCOSTAL REPMay 12, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022050901167None · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR53/FR59 STRG 42LH HAS CORROSION. DOT 52-43. () REMOVED CORROSION AT AFT CARGO PIT BETWEEN FR53-FR59 IAW SRM 51- 002. REMOVE AND REPLACED STRG 42LH BETWEEN FR53-FR60 IAW SRM 51- 74-00 AREA 1 BETWEEN FR53-5May 6, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022050601154None · crackedDURING HMV-3 CHECK AT VT MAE, PRODUCTION REPORTED CRACK INDICATION AT PRESSURE PANEL LAYER (LHS) ON HOLES #24 AND #26, ADDITIONALLY HOLES #5 THRU #12 WERE FOUND CRACKED. ON OR BEFORE AIRCRAFT 4278 ACCUMULATES 80,400 TOTAL FLIGHT CENTER FUSELAGE PRESSURE DECK MMay 5, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022042701090Structure · cracked(A3NB-52-4-6031) MIDDLE FUSELAGE, EMERGENCY EXIT AFT RH, INTERNA L STRUCTURE HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT 132-93 () REMOVED AND REPLACED DAMAGED SEGMENT ANGLE P/N D5227902620551 BA TCH #0003925895 IAW SRM 57-42-11, & DWG 52279010. ACCOMPLISHEDApr 27, 2022 · N478UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022042701081Angle · cracked(A3NB-52-4-6031) MIDDLE FUSELAGE, EMERGENCY EXIT AFT RH, INTERNA L STRUCTURE HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT 132-93 () REMOVED AND REPLACED DAMAGED SEGMENT ANGLE P/N D5227902620551 BA TCH #0003925895 IAW SRM 57-42-11, & DWG 52279010. ACCOMPLISHEDApr 26, 2022 · N478UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022042101042Stringer · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKEDApr 20, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022042101041Frame · cracked(AD2022-02-11) DURING ROTO PROBE RH FR20 DOOR STOP #7 FOUND HOLE #1 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYERS. REPAI R BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUIRED) REPAIRED RH FR20 DOOR STOP #7 HOLE #1 BY INTERCOSTAL REPLACEMENT & Apr 20, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022042101039Frame · cracked(AD2022-02-11) DURING ROTO PROBE RH FR16 DOOR STOP #7 FOUND HOLE S #1 & #3 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYERS REPAIR BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUI RED) REPAIRED RH FR16 DOOR STOP #7 HOLE''S 1 & 3 BY INTERCOSTAL REApr 20, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022042101038Beam · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN BEAM STRUCTURE HAS CORR OSION BETWEEN FR 17 & 18 Y254 DOT 132-96 () REMOVED FLOOR BEAM AND REPLACED P/N D5311281820401, BATCH 003938 281 IAW SRM 51-42-11, AND RESTORE SURFACE PROTECTION IAW 51-21-1 1. ACCOMPLISHED BY EMApr 20, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022041801014Frame · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKEDApr 18, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022041801010Bonding Plate · broken(A3NB-55-3-6005) LH HORIZONTAL STABILIZER, ELEVATOR HINGE FITTIN G N.5 HAS PLATE BONDING BROKEN. DOT 132-134() REMOVED BONDING PLATE IAW SRM 51-42-11. FABRICATED NEW BONDING P .07 MILLIOHMS IAW AMM 20-28-00 T91450. ACCOMPLISHED BY EMP#V9347 LATE IAW DRAWING #DApr 17, 2022 · N478UA · Airbus A320232 · Elevator Control SystemSDR CALA2022041100952Frame · cracked(EA 5340-01724 REV C) FRAME 68 LH DOOR STOP FITTING #1 LOWER I/B HOLE CRACK INDICATION AT 6 O''CLOCK IN THE FRAME. () WASHER, THIS TASK IS CATEGORY B. I AW SRM 53-41-12-300-010. REI W SRI 53-41-12-205-009 INSP THRESHOLD FROM TIME OF ADL/REPAIR EM TERVALS 1070Apr 10, 2022 · N478UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022040600906Seat Track · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN SEAT TRACK HAS CORROSIO N AT FR 20 -Y765 DOT 132-99() EVALUATED BLENDING OUT IAW SRM 51-42-15 FOUND TO BE OUT OF LIMIT S AND REMOVED AND INSTALL NEW SEAT TRACK -Y765 FR20 ON FLOOR CAB IN IAW SRM 51-42-11/001. ACCOMPLISHApr 6, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022040600905None · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN STRUCTURE HAS CORROSION AT FR20 DOT 132-98() BLEND OUT AREA AT MAIN CABIN STR FR20 -Y1588 ORG. THICKNESS 0.07 6 AND INSTALLED FLOOR CABIN WEB IAW SRM 51-42-1144-008. ACCOMPLI 1", MAT REMOVED 0.020, MAT REMAINING 0.051" Apr 6, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022040400871Floor Support · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN STRUCTURE HAS CORROSION AT FR20 DOT 132-98() BLEND OUT AREA AT MAIN CABIN STR FR20 -Y1588 ORG. THICKNESS 0.07 6 AND INSTALLED FLOOR CABIN WEB IAW SRM 51-42-1144-008. ACCOMPLI 1", MAT REMOVED 0.020, MAT REMAINING 0.051" Apr 3, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022040400870Beam · corroded(A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN SEAT TRACK HAS CORROSIO N AT FR 20 -Y765 DOT 132-99() EVALUATED BLENDING OUT IAW SRM 51-42-15 FOUND TO BE OUT OF LIMIT S AND REMOVED AND INSTALL NEW SEAT TRACK -Y765 FR20 ON FLOOR CAB IN IAW SRM 51-42-11/001. ACCOMPLISHApr 3, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022033100825None · none(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR56/FR57 STRG 40RH HAS CORROSION. REPLACED AFT CARGO PIT BETWEEN FR56 TO FR58 STR 40RH IAW A320 SR M 51-42-11 AND SRM 51-72-11-911-001. P/N:D5347552623400 BTCH:000 3865486 AT BFM ST AEROSPACE MOBILE. NR#00Mar 29, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022032800810Stringer · corroded(A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR56/FR57 STRG 40RH HAS CORROSION. REPLACED AFT CARGO PIT BETWEEN FR56 TO FR58 STR 40RH IAW A320 SR M 51-42-11 AND SRM 51-72-11-911-001. P/N:D5347552623400 BTCH:000 3865486 AT BFM ST AEROSPACE MOBILE. NR#00Mar 28, 2022 · N478UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022032800802Bonding Plate · damaged(A3NB-55-3-6005) LH HORIZONTAL STABILIZER, ELEVATOR HINGE FITTIN G N.5 HAS PLATE BONDING BROKEN. DOT 132-134() REMOVED BONDING PLATE IAW SRM 51-42-11. FABRICATED NEW BONDING P .07 MILLIOHMS IAW AMM 20-28-00 T91450. ACCOMPLISHED BY EMP#V9347 LATE IAW DRAWING #DMar 28, 2022 · N478UA · Airbus A320232 · Elevator Control SystemSDR CALA2019120302133Battery · failedDURING TEST FND ESPU BATT 13WL LOW VOLTAGE. REPLACED 13WL ESPU BATTERY PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000-002 REV.103, AMM 33-51-38-400-002 REV103 AMM 33-51-00-710-001 REV.103.Nov 28, 2019 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2019120302132Battery · failedDURING TEST FND ESPU BATT 12WL LOW VOLTAGE REF ROUTINE NO. 9491373 - ORIGINATED BY EMP V924351, SPEC NO.A3NB-33-3-6012 PERFORMED BY EMP V924351, PERFORMED REPLACEMENT OF 12WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33Nov 28, 2019 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2019120302131Battery · failedCAB ESPU 10WL BATTERY FOUND LOW VOLTAGE REF ROUTINE NO.9490827 - ORIGINATED BY EMP V905504, SPEC NO.A3NB-24-3-6062. PERFORMED BY EMP V924351, REPLACED 10WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33 -51-38-000-002 REVNov 28, 2019 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2019120302130Battery · failedDURING TEST FND ESPU BATT 11WL LOW VOLTAGE REF ROUTINE NO. 9491372 - ORIGINATED BY EMP V924351 , SPEC NO.A3NB-33-3-6012. PERFORMED BY EMP V924351,REPLACED 11WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33 -51-38-000-002Nov 28, 2019 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2019053100864Release Cable · frayedREF. N/R: 9459059 LEFT OVERWING EMERGENCY EXIT MANUAL RELEASE CABLE FWD AND AFT HAVE FRAYED WIRES. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT N/R 9459059 WORK ACCOMPLISHED BY MECHANIC INSPECTED BY QC REMOVED AND INSTALLED NEW MANUAL RELEASE SLIDE CABLE ASSY LEFTMay 30, 2019 · N478UA · Airbus A320232 · Emergency ExitsSDR CALA2018011200174Warning Light · false activationDOOR AFT EMERGENCY EXIT ECAM ILLUMINATED TWICE WHILE AT CRUISE, 370 AND DISAPPEARED. CABIN PRESSURE FINE, COULD NOT DUPLICATE PROBLEM. PERFORMED A GV INSPECTION OF EXTERIOR AND INTERIOR EMERGENCY HATCH, NO FAULTS FOUND. REMOVED HANDLE COVER AND INSPECTEDJan 12, 2018 · N478UA · Airbus A320232 · Door Warning SystemSDR CALA2017063002062Cover · looseLEFT DOOR FWD EMERGENCY EXIT FOUND LOOSE. SECURED THE EMERGENCY EXIT COVER.Jun 30, 2017 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2015070994071Unknown · malfunctionedFORWARD EMER LIGHTS FAILED TO COME ON WHEN ACFT LOST POWER AT THE GATE. ACCOMPLISHED BITE OF FWD EPSU IAW AMM 33-51-38. ACCOMPLISHED EMER LIGHT TEST OF ENTIRE CABIN OF ATTENDANT PTP PANEL. EMER LIGHTS TESTS PASSED.Jul 8, 2015 · N478UA · Airbus A320232 · Emergency LightingSDR CALA2014122692866Engine · malfunctionedNUMBER 2 ENG OIL QTY LOW & DECREASING EVENTUALLY TO ZERO. PRESS & TEMP GOOD. ENG SHUTDOWN INFLIGHT. SUSPECTED ENG OIL PUMP HOUSING FAILURE. NR 2 ENG R & R. ACCOMPLISHED AMM TASK 72-00-00-200-021-BM INFLIGHT SHUTDOWN PROCEDURE.Dec 21, 2014 · N478UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2014021390372Sill · corrodedL1 DOOR SILL BENEATH AFT GIRT BAR ATTACH FITTING HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH TWO EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.Feb 12, 2014 · N478UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014021390371Sill · corrodedR1 DOOR SILL BENEATH FWD & AFT GIRT BAR ATTACH FITTINGS HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH FOUR EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.Feb 12, 2014 · N478UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2014021090336Stringer · corrodedSTRINGER 42 RT HAS CORROSION BETWEEN FRAME 63 &64. REPLACED STRINGER IAW A320 SRM 51-42-11 PG 24 NR 21308.Feb 7, 2014 · N478UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
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