Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  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 YENA2018120730814Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED BTWN RIB 8-9 UPPER SURFACE ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 8-9 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AEROMDec 3, 2018 · N509JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2018120730813Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y1162 LOCATED BTW FR 68 TO FR 70 AT AFT GALLEY AREA; REF BP NR # 2018-395184 REPLACED FLOOR BEAM -Y1162 LOCATED BTW FR 68 TO FR 70 AFT GALLEY AREA IAW SRM A320 51-42-11 & 51-72-11 AND DRAWING D5Dec 3, 2018 · N509JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018120632989Flashlight Assy · no testFWD OUTBOARD FA SEAT FLASHLIGHT WILL NOT TEST. ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R/R FLASHLIGHT ASSY IAW AMM 25-60-00. NEXT INSPECTION DUE 12-5-2019. THIS CLEARS DMI 2394357-1. PLACARD REMOVED. MOC NOTIFIED.Dec 3, 2018 · N645NK · Airbus A320232 · Emergency EquipmentSDR YENA201812020812A/C Pack · odorFT 861, BOS-SJU. FUME/ODOR (SOCK ODOR) REPORTED BY CABIN CREW DURING DESCENT OUT OF 15000' ENG BLEED USED (APU OFF). C/W INFORMATION NOTICE 2017 SECTION A. A/C OK FOR SERVICE. RVR PACK 1 & 2 NO ODOR DETECTED PERFORMED EXTERIOR INSPECTION NO DEFECTS FOUND AS PDec 2, 2018 · N649JB · Airbus A320232 · Cabin Cooling SystemSDR GTIA2018120322986Unknown · odorFUME EVENT AFT CABIN TURNED OFF PACK 2 SMELL DISSIPATED-PERFORMED IDENT OF COS REF TSM 05-50-00-810-831-A NO ODARS PRESENT AT THIS TIME APU CHECKED REF AMM 29-00-00 ENG RUN W/ FLT CREW & OPS CHECKED REF AMM 71-00-00Dec 2, 2018 · N609NK · Airbus A320232 · Air Distribution SystemSDR CALA2018120702497Stop Fitting · not reportedR1 DOOR FR16 NO.7 STOP FITTING BOTH INBD BOLT HOLES PRODUCE REJE CTABLE INDICATIONS DURING RFHEC INSPECTION A3NB-53-4-6304 GENERA TED BY V061690 ON HAECO LCQ NR 9294675 REMOVED AND REPLACED #7 INTERCOASTAL @ R1 DOOR FR16 IAW A320 SRM 51-72-11 BY MECH V913402 IDec 1, 2018 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018120702496Plate · corroded(SPEC A3NB-53-3-6185 A-41 L-46 DOT 042) REINFORCEMENT PLATE U NDER STRGR 39R FROM FR 65-FR66 CORRODED IN MULTIPLE AREAS AAR N ONROUTINE 9019926 REMOVED AND REPLACED REINFORCEMENT PLAT UNDER STR 39R IAW A320 S RM 51-72-11-911-001. INSTALLED FASTENERS COMMONDec 1, 2018 · N420UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018120702495Doubler · not reportedA3NB-53-3-6179(A33-124) AFT CARGO BAY FUSELAGE INTERNAL REINFOR EMENT DOUBLER IAW A320 SRM 51-72-11-911-001, INSTALLED FASTENERS COMMON TO LAV SERVICE CAP IAW ECRA 5341-01140 AAR NONROUTINE 9019887 REMOVED AND REPLACED INTERNAL REINFORCMENT DOUBLER IAW A320Dec 1, 2018 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018120702494Stringer · corroded(A3NB-533-6185)(L-69-003) CORROSION FOUND ON STR 39R AFT OF FR66 AAR NONROUTINE 9020117 REPAIRED STR 39 AFT OF FR66 IAW A320 SRM 53-00-13-300-001 AAR N ONROUTINE 9020117 ADD EMP:V918822Dec 1, 2018 · N420UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018120702492Frame · crackedLH FRAME 35 FORWARD AT LEVEL OF STRINGER 30 HOLE 2 IS CRACKED IN THE SIDE SHELL AT 7:00 INBOARD LOOKING OUTBOARD AN IN THE FRAME LAYER AT 6:00 AND 2:00 PER HAECO LCQ NON ROUTINE 9296424 GENERA TED BY V061633 REPAIRED LH FR35 FORWARD AT LEVEL OF STR30 HOLE#2 INDec 1, 2018 · N424UA · Airbus A320232 · Fuselage Main, FrameSDR YENA2018120610810Power Supply · no testFT # 225, JFK-TPA. EMERG LIGHT TEST FAILED; REMOVED & REPLACED ESPU AT 11WL PER AMM 33-51-38.Dec 1, 2018 · N779JB · Airbus A320232 · Emergency LightingSDR YENA2018120610809Battery Pack · no testFT # 225, JFK-TPA. FAILED EMERG LIGHT TEST; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT 11WL, 12WL & 13WL PER AMM 33-51-38. P/N OFF/ON 3214-31 S/N OFF094878 ON 831693. P/N OFF/ON 3214-31 S/N OFF 094867 ON 805202. P/N OFF/ON 3214-31 S/N OFF 094868 ON 9Dec 1, 2018 · N779JB · Airbus A320232 · Emergency LightingSDR YENA2018120610808Battery Pack · no testFT # 225, JFK-TPA. FAILED EMERG LIGHT TEST; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT 11WL, 12WL & 13WL PER AMM 33-51-38. P/N OFF/ON 3214-31 S/N OFF094878 ON 831693. P/N OFF/ON 3214-31 S/N OFF 094867 ON 805202. P/N OFF/ON 3214-31 S/N OFF 094868 ON 9Dec 1, 2018 · N779JB · Airbus A320232 · Emergency LightingSDR YENA2018120610807Battery Pack · no testFT # 225, JFK-TPA. FAILED EMERG LIGHT TEST; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT 11WL, 12WL & 13WL PER AMM 33-51-38. P/N OFF/ON 3214-31 S/N OFF094878 ON 831693. P/N OFF/ON 3214-31 S/N OFF 094867 ON 805202. P/N OFF/ON 3214-31 S/N OFF 094868 ON 9Dec 1, 2018 · N779JB · Airbus A320232 · Emergency LightingSDR AALA201812049036Cover · brokenEMERGENCY LIGHT COVER WAS BROKEN AT THE L1 DOOR. MAINTENANCE REPLACED THE LIGHT COVER AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.Dec 1, 2018 · N673AW · Airbus A320232 · Emergency LightingSDR AALA201812039011Pressure Panel · crackedCRACKED PRESSURE PANEL, AT FRAME 36, STRINGER 28, LBL Y2192. REPLACED THE PRESSURE PANEL IAW EO 5316Y209-001, AND EA 287487.Dec 1, 2018 · N601AW · Airbus A320232 · Fuselage Main, BulkheadSDR GTIA2018120312984A/C Pack · odorON DECENT THROUGH APPROXIMATELY FL 250, FLIGHT ATTENDANTS AND PILOTS NOTICED FUME EVENT PACK 2 WAS SHUT OFF AND FUMES SEEMED TO DISSIPATE-PER TSM 05-50-00-810-831A PACK 2 WAS FOUND TO BE SOURCE OF ODOR TRANSFERRED TO DMI 247045002 IAW MEL 21-52-01-14 CAT C DATDec 1, 2018 · N645NK · Airbus A320232 · Cabin Cooling SystemSDR CALA2018120702491Stop Fitting · crackedL1 DOOR FR16 NO.7 STOP FITTING BOTH UPPER BOLT HOLES AND THE LOW ER INBD BOLT HOLE PRODUCES REJECTABLE INDICATIONS DURING RFHEC I NSPECTION AD 2017-22-03 A3NB-53-4-6304 GENERATED BY V061690 ON H AECO LCQ NR 9294683 REMOVED AND REPLACED LH FR 16 NO.7 INTERCOASTNov 30, 2018 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR AALA201812039015Floorboard · damagedFLOORBOARD 231AF WAS SPONGY. MAINTENANCE REPLACED THE FLOORBOARD IAW AMM 53-00-00-400-801-A, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Nov 30, 2018 · N654AW · Airbus A320232 · Fuselage Floor PanelSDR CALA2018120202488Skin · crackedREFERENCE AAR LOG ITEM 9019374, ROTO PROBE INSEPCTION SHOWS CRAC K INDICATION IN MULTIPLE LAYERS @ FR35, STR 30L LOWER AFT HOLE AAR ACCOMPLISHED INTERIM REPAIR, PART 1 STEPS 1-23 OF ECRA 5331- 02304. NEED TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 ON OR BE FONov 30, 2018 · N420UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018120202475Cleat · corrodedFWD CARGO COMPARTMENT FR31 STRINGER 39R-40R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT ON FWD CARGO FR31 STRINGER 39R-40R. REMOVED CORROSION ORIGINAL MAT. .055", MATERIAL LOSS .031", MATERIAL REMAINING .029", MAX ALLOWED THICKNESS .004", FOUND OUT LIMITS Nov 30, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018120202474Cleat · damagedAFT CARGO CLEAT FR62 STR 41R-40R HAS ELONGATED HOLES. REMOVED AND REPLACED AFT CARGO CLEAT AT FR 62 STR 41R-40R IAW SRM 51-72-11-911-001.Nov 30, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018120202473Cleat · damagedAFT CARGO FRAME CLEAT HAS 2EA OUT OF ROUND HOLES FR63 ST41-42R. REMOVED AND REPLACED AFT CARGO CLEAT AT FR63 STR 41R-42R IAW SRM 51-72-11-911-001.Nov 30, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018120202472Cleat · corrodedFWD CARGO COMPARTMENT FR30 STRINGER 43R-43L CLEAT HAS CORROSION. REMOVED AND REPLACED 01 CLEAT (FABRICATED) ON FWD CARGO COMPARTMENT FR30 STRINGER 43R-43L IAW SRM 51-42-11-001, TREATED, PRIMED AND TOP COAT AREA IAW SRM 51-75-12-001.Nov 30, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018120202471Cleat · corrodedFWD CARGO COMPARTMENT FR32 STRINGER 42L-43L CLEAT HAS CORROSION FCD 5300-01440. REMOVED CORR AND REPLACED CLEAT ON FWD CARGO COMPARTMENT FR 32 STRINGER 42L-43L. ORIGINAL MAT .055",MATERIAL LOSS .011" MAT REMAINING .044" FOUND OUT LIMITS IAW SRM 51-74-00, SRM 5Nov 30, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490803Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y450 .8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490802Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816.Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490801Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM - Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AN DRAWING # D53472816Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490800Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA; REF BP NR # 2018-374614 REPLACED FLOOR BEAM + Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490799Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374616 REPLACED FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490798Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y 1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374620 REPLACED FLOOR BEAM - Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490797Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB AT STR 23R AT AFT GALLEY AREA; REF BP NR # 2018-374680 REPLACED SUPPORT WEB AT STR 23R BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER SRM A320-51-72-11 AND DRAWING # D53474180.Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490796Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y1162.5 BETWEEN FR 66-FR 68 AT AFT GALLEY AREA; REPLACED FLOOR BEAM-Y1162.5 BETWEEN FR 66-FR 68 AY AFT GALLEY AREA IAW SRM A320-51-72-11 AND DRWG D53472780. REF AEROMAN NR 2018-374619.Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490795Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 43L LOCATED BTW FR 62 TO FR 63 IN AFT CARGO COMPARTMENT; REF BP NR # 2018-374610 REPLACED STRINGER 43L BTW FR 60 60 FR 64 IN AFT CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND DRAWING # E 53470342.Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2018120490794Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA; REF BP NR # 2018-374621 REPLACED RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING # 53112825Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2018120490793Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1292 LOC. BTW FR 12 TO FR 24 IN PASSENGER CABIN; REF BP NR # 2018-374613 REPLACED FLOOR BEAM LOC +Y1292 BTW FR 12 TO FR 24 IN PASSENGER CABIN AS PER SRM A32051-72-11 AND DRAWING # D53112812.Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018120490792Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y 1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA; REPLACED FLOOR BEAM LOCATION -Y1292 BTW FR 12 TO 24 AT FWD GALLEY AREA AS PER SRM A320-51-72-11 AND DWG D53112812. ALL WORK ACCOMPLISHED ON AERONov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201812049791Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y254 LOC. BTW FR 12 TO FR 24 AT FWD GALLEY AREA; REF BP NR # 2018-374617 REPLACED FLOOR BEAM LOC +Y254 LOC. BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER SRM A320-51-72-11 AND DRAWING # D53110 9Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201812049790Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED FLOORBEAM -Y 254LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA; REPLACED FLOOR BEAM LOC -Y 254 BTW FR12 TO 24 AT FWD GALLEY AREA AS PER SRM A320-51-72-11 AND DRWG # D53110920,D53112816. ALL WORK ACCOMPLISHED ON AERNov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201812049789Warning Message · illuminatedFT # 714, DFW-BOS. EMERGENCY DECLARED. AT CRUISE ALT, F/CTL ALTN LAW, F/CTL ELEV SERVO FAULT. ELAC 1 PITCH FAULT. F/CTL STABALIZER JAM; SUPPLEMENTAL INFORMATION TO FOLLOW.Nov 29, 2018 · N568JB · Airbus A320232 · Stabilizer Control SystemSDR GTIA201812032983Unknown · odorDIRTY SOCK SMELL FROM TOP OF DESCENT DOWN TO ABOUT 10,000FT. -PERF. ENG. RUN IAW AMM 71-00-00 TO MATCH A/C CONFIG. UPON EVENT & COULD NOT DUPLICATE. PERF. VISUAL INSP. OF APU & NO DEFECT. NO DIRTY SMELL NOTED IN CABIN OR CKPT W/ ENG. OR APU BLEED.Nov 29, 2018 · N650NK · Airbus A320232 · Air Distribution SystemSDR CALA2018120202462Idg · faultedGEN 1 FAULT REF TSM TASK 24-20-00-810-803-A, STEP 4 A . INSPECTED POWER FEEDER CONNECTOR AT FIREWALL. NO BURNING/ARCING DAMAGE OR CORROSION. RECONNECTED POWER FEEDER CONNECTOR. VERIFIED NO BURNING/ARCING OR SIGNS OF CORROSION ON POWER FEEDER CONNECTOR AT PYLONNov 29, 2018 · N405UA · Airbus A320232 · AC Generator-AlternatorSDR CALA2018120202461Door Frame · crackedL1 DOOR FRAME 16 STOP FITTING NR 1 LOWER INBOARD HOLE IS CRACKED IN FRAME LAYER AT 7:00 ON REF 9296599 SPEC A3NB-53- 4-6304 AD 2017-22-03. REPAIR ACCOMPLISHED IAW ECRA 5311-02046 PER ECRA 5311-02046PATR 1 STEP 2.Nov 29, 2018 · N424UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018120202455Stringer · corrodedSTR 40R TO STR 41R BETWEEN FR 67-FR 68 HAS MULTIPLE CORRODED FASTENERS. REMOVED AND REPLACED FASTENERS AT STR 40R BETWEEN FR 67-FR 68. BLENDED CORROSION AT STR 41R BETWEEN FR 67-FR 68. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR 41R AT FR 64-FR 69. RENov 29, 2018 · N420UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA201812037788Filter · failedFT # 878, LAS-BOS. FA#2 REPORTS DIRTY SOCK ODOR ROW 11-14. PERFORMED ODOR RECOGNITION ISOLATION PRPROCEDURE. ODOR GONE WITH PACK 1 OFF. ( PACKS - SINGLE (SPEEDBRAKES OK) (N503-N665) ); REMOVED AND REPLACED OZONE FILTER PACK IAW AMM 21-51-41. RUN PACK 1 NO SMWENov 27, 2018 · N658JB · Airbus A320232 · Air Distribution SystemSDR GTIA2018112972981Panel · looseDURING CLIMB VERY STRONG VIBERATION WERE FELT. CLIMB SPEED WAS 332/.79. REDUCED SPEED TO 300/.78 VIBERATION DISAPPEARED, F/A REPORTED ALO THE SAME-T/S VIBERATION IAW TSM 05-5000-810-801-A FOUND PANEL 192BT LOOSE. TIGHTENED IAW 53-35-00Nov 27, 2018 · N622NK · Airbus A320232 · Standard Practices/StructuresSDR AALA201811299016Unknown · odorTHE AIRCRAFT WAS GROUNDED. CABIN ODOR OCCURRED DURING DECENT. A SUPPLEMENTAL REPORT TO BE SUBMITTED TO INCLUDE AIRCRAFT TOTAL TIME, CORRECTIVE ACTION AND PART INFORMATION. (OPEN)Nov 26, 2018 · N647AW · Airbus A320232 · Air Distribution SystemSDR CALA2018120102442Stringer · corrodedAFT CARGO BAY STR 39R AT FR58-64 IS CORRODED. AFTER EVALUATION OF STR 39R AT FR58-64 FOUND CORROSION NEXT TO PRODUCTION SPLICE, PROXIMITY OF MINIMUM REPAIR DISTANCE NOT MEET, FOUND TO BE OUT OF LIMITS. PREFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13Nov 26, 2018 · N420UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018120102441Stringer · corrodedAFT CARGO BAY STR 40R AT FR58-64IS CORRODED. AFTER EVALUATION OF STR40R AT FR58-FR64 FOUND CORROSION UNDER FR 59. FOUND TO BE OUT OF LIMITS DUE TO LOCATION OF CORROSION. PERFORMED REPAIR IAW SRM 53-00-13-300-001 AND SRI 53-00-13-205-001.Nov 26, 2018 · N420UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018120202447Check Valve · brokenY RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. HYD FOUND CHECK VALVE ON YELLOW SYSTEM MANIFOLD TO BE BROKEN. REPLACING CHECK VALVE AND THEN WILL LEAK CHECK.Nov 26, 2018 · N410UA · Airbus A320232 · Hydraulic System, Main
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