Airbus A320-232

Service difficulty reports · 32,653

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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"

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SDR CALA2018110972314Stop Fitting · crackedROTO INSP SHOWED CRACK INDICATION AT L1 DOOR, FR16 STOP #7, INBD UPPER HOLE. HAECO NR 22652. REPAIRED LH FR 16 #7 INTERCOSTAL PER ECRA 5311-02033. PER PART 1 ITEM 2 OF ECRA DTA LOG PAGE REQUIRED TO ACP INITIAL INSPS PER PA RT 2 OF ECRA 5311-02033 ON OR BEFORE Nov 5, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018110972313Stop Fitting · crackedR-1 DOOR STOP FITTING #1 FRAME 20 INBOARD LOWER HOLE IS CRACKED IN FRAME WEB AT 6:00. REPAIRED R-1 FR20 IB LWR HOLE PER ECRA 5311-02033. HAECO NR 2266 6. ECRA REQUIRES DTA LOG PAGE TO ACP INIT INSPECTIONS PER PART2 OF ECRA 5311-02033 ON OR BEFORE ACFT REACHES Nov 5, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR AALA2018110879010Apu · odorFLIGHT ATTENDANT REPORTED STRONG ELECTRICAL ODOR IN THE GALLEY AFTER TAKEOFF. THE AIRCRAFT WAS GROUNDED. DUE TO CHRONIC NATURE SOF EVENTS. REPLACED APU IAW JC 26L31049005. PERFORMED JC 26L00021002, AND 26L00021004. NO ODORS PRESENT.Nov 5, 2018 · N647AW · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2018110502306Power Supply · inoperativeFOUND EPSU 11WL BAD. REPLACED EPSU IAW AMM 33-51-38-400-001A. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103608 SN OFF 2897 POWER SUPPLY, C OFF 31-3350-9-9001 2897 ON 31-3350-9-9001 5406 PART UPDATE ONLY ROTABLE PARTS CHANGE WAS INDICATED - TT # 1810908 SN Nov 5, 2018 · N467UA · Airbus A320232 · Emergency LightingSDR CALA2018110502305Skin · dentedFUSELAGE EXTERNAL SURFACE FR-23 STRG 23 DENT REQS FURTHER EVAL L OG #3534741 AT HAECO LCQ PER REF NO.9297300 BY MECH N078570 REMOVED DAMAGE & REPAIRED EXTERNAL SURFACE FR23 STRG23 PER SRM 5 3-00-11-300-029. NOMINAL SKIN THICKNESS 0.047". DOUBLER THICKNE SS 0.0Nov 5, 2018 · N422UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018110502304Stop Fitting · crackedROTO INSP SHOWED CRACK INDICATION AT L1 DOOR, FR16 STOP #7, INBD UPPER HOLE. HAECO NR 22652. REPAIRED LH FR 16 #7 INTERCOSTAL PER ECRA 5311-02033. PER PART 1 ITEM 2 OF ECRA DTA LOG PAGE REQUIRED TO ACP INITIAL INSPS PER PA RT 2 OF ECRA 5311-02033 ON OR BEFORE Nov 5, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018110502302Engine · making metal#2 ENG MAIN MCD FOUND 1 ROUND METALIC MAGNETIC JAGGED BALL APROX DIA .045". INSPECTED MASTER MCD PER AMM 79-00-00-200-011-A. UPLOAD DEBRIS P ICTURES TO RVI SITE. CONTACTED TOMC ENGINE DESK: BRIAN. DEBRIS/ CHIP SAMBLE TAKEN AND TO BE SENT TO SFO LAB FOR ANALYSINov 5, 2018 · N477UA · Airbus A320232 · Engine Oil System (Airframe Furnished)SDR CALA2018110502299Contactor · warning messageDC ESS BUS SHED DISPLAYED ON UPPER ECAM SCREEN. - EL EC REF TSM 24-60-00-710-801. BERG TOMC. REPLACED DC SHED ESSENTIAL BUS CONTACTOR, CKS OK, REF AMM24-62-5 5.Nov 5, 2018 · N488UA · Airbus A320232 · Electrical Power System WiringSDR YENA2018110840768Bulb · inoperativeFT # 405, BOS-LGB. DURING SCHEDULED MX FOUND AFT BULB OF RH AFT OVERWING EMERGENCY LIGHT INOP (62WL); RELAMPED AFT BULB OF RH AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHK NORMAL.Nov 4, 2018 · N807JB · Airbus A320232 · Emergency LightingSDR YENA2018110840767Light · brokenFT #319, FLL-SLC. SEAT 1C EMERGENCY EXIT LIGHT BROKEN ( FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP) ); REPLACED EMERGENCY LIGHT HOUSING AT SEAT 2C, PER AMM 33-51-19. OPS CHECK OK. MX4 UPDATED, PLACARD RENov 4, 2018 · N656JB · Airbus A320232 · Emergency LightingSDR AALA201811069020Light · damagedAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT DAMAGED AT 4L. MAINTENANCE REPLACED FIXTURE AT 4L PER 33-51-18 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Nov 4, 2018 · N654AW · Airbus A320232 · Emergency LightingSDR CALA2018110502297Fitting · corrodedAAR N/R SEQ NO. 9019739. UPON REMOVAL OF L2 LOWER GIRTBAR FITTIN GS, FOUND SILL TO BE CORRODED IN MULTIPLE AREAS THAT ARE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR SILL. REF A320 SRM 51-72-11-911-001Nov 4, 2018 · N420UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2018110502296Skin · corrodedL-2 DOOR SKIN INNER SURFACE LOWER FWD & AFT SECTIONS CORROSION A ROUND FASTENER HOLES (12 EA) ON HAECO LCQ REF 9297399 SPEC A3NB- 06-3-6001 GENERATED BY N078570Nov 4, 2018 · N422UA · Airbus A320232 · Passenger/Crew DoorsSDR GTIA2018110542943Bottle · low pressureR2 DOOR ASSIST ACCUMULATOR HAD LOW PRESSURE. SERVICED THE DOOR ASSIST ACCUMULATOR IAW AMM 52-10-00.Nov 4, 2018 · N638NK · Airbus A320232 · Emergency EquipmentSDR YENA201811030953Structure · corrodedAT CURRENT (10/2018) C6 CHECK (SAL), CORROSION WAS FOUND ON CENTER WING BOX TOP SKIN UPPER SURFACE BETWEEN FR41-42 & +Y1292. SEE THE REF /1/ EA FOR MORE DETAILS. THE SRM DOES NOT PROVIDE ALLOWABLE DAMAGE LIMITS NOR REPAIR GUIDELINES FOR THE DAMAGE LOCATION. RENov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811030952Stringer · corrodedDURING C6 CHECK AT (SAL), CORROSION WAS FOUND ON STRINGER 38L BTWN FR 53-64 AND STRINGER 37L BTWN FR 60-64 AT THE AFT FUSELAGE. SEE THE REF /1/ EA FOR MORE DETAILS. EVALUATED THE DAMAGE AGAINST SRM 53-41-13 AND THERE IS NO ALLOWABLE NOR APPLICABLE REPAIR FOR TNov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA201811030949Door Frame · crackedDURING HEAVY CHECK AT SAL, UNDERGOING REF /2/ INSPECTION WHEN CRACK DAMAGE WAS REPORTED AT FR16 LT JUST ABOVE DOOR STOP 7 ON HOLES A AND C. CONTACTED AND PROVIDED REF. /4/. HOLES A & C WERE REAMED, COLD WORKED, AND BUSHING AND DOUBLERS WERE INSTALLED. ADJACNov 3, 2018 · N504JB · Airbus A320232 · Fuselage Main, StructureSDR YENA201811030948Door Frame · crackedDURING HEAVY CHECK AT SAL, UNDERGOING REF /2/ INSPECTION WHEN CRACK DAMAGE WAS REPORTED AT FR16RH JUST ABOVE DOOR STOP 7 ON HOLES A AND C. CONTACTED AND PROVIDED REF. /4/. HOLES A & C WERE REAMED, COLD WORKED, AND BUSHING AND DOUBLERS WERE INSTALLED. ADJACENov 3, 2018 · N504JB · Airbus A320232 · Fuselage Main, StructureSDR YENA201811030947Panel · crackedDURING C11 HEAVY CHECK, UNDERGOING REF /4/ SB EMBODIMENT WHEN SIX FASTENER HOLES WERE FOUND CRACKED ON THE LT PRESSURE DECK PANEL FR35/36 WERE REPORTED. CONTACTED AND PROVIDED REF /2/ TD FOR CUTOUT AND FILLER & DOUBLER REPAIR; APPROVED THIS REPAIR PER REF /3/Nov 3, 2018 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110830765Angle · crackedDURING HEAVY MAINTENANCE, HOLE ELONGATED ON CLIP AND ANGLE AT FRAME 63 RIGHT 31 INCHES ABOVE STR 22R (PRIMARY STRUCTURE) (MAJOR REPAIR); REMOVED FABRICADED AND INSTALLED FR63 R/H ST22-26R ATTACH ANGLE AND ATTACH CLIP IAW A320 SRM REF 51-72-11, 51-26-11 REF HAENov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073764Shear Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RH MAIN CAVIN SHEAR WEB FRAME SUPPORT FR 69-70 STR 23R LOWER SURFACE; REMOVED AND REPLACED RH AFT CABIN SHEAR WEB SUPPORT FR 69-70 STG 23R IAW SRM 51-72-11, 53-41-14 FIG 002. WORK ACCOMPLISHED ON HAECO NR 4Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073763Threshold · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO COMPT THRESHOLD SILL UPPER SURFACE FRAME 26-28 STR 38R; REMOVED AND REPLACED FWD CARGO THRESHOL SILL IAW SRM 53-21-29-283-001 AND 53-21-29 FIG 004. WORK ACCOMPLISHED ON HAECO NR 440519-36227.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073762Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL AT FR 66+4; STR 23L Y1732; REMOVED AND REPLACED DOOR SILL. AS PER SRM REF 53-41-14 REF HAECO NR 440519-36663 AND 36664.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073761Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM CORRODED AT FR 68 -Y765; REPLACED FLOOR BEAM AS PER SRM REF 51-72-11 REF HAECO NR 440519-36668.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073760Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM AT FR 66+4; -Y765; REPLACED FLOOR BEAM AS PER SRM REF 51-72-11 REF HAECO NR 36671Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073759Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM AT FR66 + 1, Y1292; REPLACED FLOOR BEAM AS PER SRM REF 51-72-11 REF HAECO NR 440519-36662Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073758Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO COMPT WEB SILL UPPER SURFACE. CORRODED AT FR26-27 RT; REMOVED AND REPLACED FWD CARGO WEB SILL AS PER SRM REF 53-21-13-283-002 AND 53-21-13 FIG 004Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073757Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL AT FR 66 STR 23L Y1732; REMOVED AND REPLACED DOOR SILL SRM REF 53-41-14 FIG 021 REF HAECO NR 440519-36663Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073756Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO PIT AT ENTRANCE DOOR SILL FROM FRAME 52 TO 56; REMOVED AND REPLACED CORRODED DOOR SILL AS PER SRM REF 51-42-11 PAR. 2.E STEPS 2 & 4 AND 51-73-11Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073755Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FWD WET AREA FLOOR BEAM Y1292 FR 16 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y1292 FR 16 STR 23L IAW A320 SRM 51-72-11-911-001 PAR 1C&D & 53-11-14 FIG 007. REF HAECO NR 36643 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073754Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN WET AREA FLOOR BEAM Y-1292 FR 20 STR 23R; REMOVED AND REPLACED FLOOR BEAM Y-1292 FR 20 STR 23R IAW A320SRM 53-00-15-283-001& 51-42-11. REF. HAECO NR 36639 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20181103753Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM Y-1292 FR 66+5 TO 66+8 STR 23R; REMOVED AND REPLACED FLOOR BEAM Y-1292 FR 66+5 STR 23R IAW A320 SRM 53-00-1`4-283-002 & 53-41-14 FIG. 001. REF. HAECO NR 36667 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073752Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM Y1292 FR 67 +17 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y1292 FR 67+17 STR 23L IAW A320 SRM 53-00-14-283-002 & 53-41-14 FIG.001.REF. HAECO NR 36659 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073751Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM Y-1292 FR 68 STR 23R; REMOVED AND REPLACED FLOOR BEAM Y-1292 FR 68 STR 23R IAW A320 SRM 53-00-14-283-002 AND 53-41-14 FIG. 001. REF. HAECO NR 36666 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073750Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM Y1292 FR 67 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y1292 FR 67 STR 23L IAW A320 SRM 53-00-14-283-002 & 53-41-14 FIG.001.REF HAECO NR 36660 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073749Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FWD WET AREA FLOOR BEAM SUPPORT Y-1732 FR 20 STR 23R; REMOVED AND REPLACED FLOOR BEAM SUPPORT Y-1732 FR 20 STR 23R IAW A320 SRM 53-73-11 DRW D53112571 & 51-72-11-901-001 PAR 1C&D. 53-11-14 FIG.007. RENov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073748Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FWD WET AREA FLOOR BEAM Y765 FR 16 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y765 FR 16 STR 23L IAW A320 SRM 53-00-14-283-001 & 51-72-11-911-001 PAR. 1C&D. REF. HAECO NR 36644 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073747Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN WET AREA FLOOR BEAM Y254 FR 16-20 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y254 FR16-20 STR 23L IAW A320 SRM 53-11-14-283-004 & 51-72-11. REF. HAECO NR 36642 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073746Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FWD WET AREA FLOOR BEAM Y254 FR 16-20 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y254 FR16-20 STR 23L IAW A320 SRM 53-11-14-283-004 & 51-72-11. REF. HAECO NR 36642.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811073745Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM Y1292 FR 67 +7 STR 23L; REMOVED AND REPLACED FLOOR BEAM Y1292 FR 67+7 STR 23L IAW A320 SRM 53-00-14-283-002 & 53-41-14 FIG.001. REF HAECO NR 36661 FOR DETAILS.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201811073744Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN SEAT TRACK Y765 FR 60-61 STG 23L; REPAIRED MAIN CABIN SEAT TRACK Y765 FR 60-61 IAW A320 SRM 53-41-15-300-002. WORK ACCOMPLISHED ON HAECO NR 440519-36782Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201811073743Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN SEAT TRACK Y765 FR 62-63 STG 23L; REPAIRED MAIN CABIN SEAT TRACK Y765 FR 62-63 IAW A320 SRM 53-41-15-300-002. REF HAECO NR 440519-36783Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201811073742Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK AT FR 35 -34, STR 23R; -Y765; REPLACED SEAT TRACK AS PER SRM REF 53-31-15 REF HAECO NR 440519-36771Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201811073741Seat Track · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN SEAT TRACK AT FR 35-36 STR23L Y1292; REPLACED SEAT TRACK AS PER SRM REF 53-31-15 REF HAECO NR 440519-36778.Nov 3, 2018 · N579JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201811069016Power Supply · inoperativeAIRCRAFT WAS GROUNDED: L1 DOOR EMERGENCY LIGHT INOPERABLE. MAINTENANCE FOUND EMERGENCY POWER SUPPLY UNIT FAULT AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.Nov 3, 2018 · N660AW · Airbus A320232 · Emergency LightingSDR AALA2018110659048Wire Harness · damagedFORWARD EMERGENCY POWER SUPPLY FAILED FOR THE INTERIOR AND EXTERIOR LIGHTS. REPLACED A DAMAGED WIRE HARNESS AT THE L4 DOOR, PERFORMED A TEST IAW AMM 33-51-00-710-001-A, CHECKED OK.Nov 3, 2018 · N660AW · Airbus A320232 · Light System WiringSDR CALA2018110502289Skin · gougedLOWER AFT FUSELAGE AT FR51-FR52, BETWEEN STR37R AND STR38R HAS A 0.40" GOUGE (A3NB-53-4-6229) PER HAECO LCQ NR 9296167. GENERATE D BY V923923. CUTOUT DAMAGED AREA AT FR50 STR38R TO STR 39R PER SRM53-00-11-30 0-013 PARA 2(A)(1)(C)&(D). FABRICATED & INSTALLED DONov 3, 2018 · N422UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018110502288Stop Fitting · crackedL-1 DOOR CUTOUT FRAME 16 STOP FITTING #1 OB HOLE IS CRACKED IN F RAME WEB AT 6:00. STEP REAMED FR16 #1 DOOR STOP FITTING UPPER OB HOLE TO CRACK FRE E CONDITION PER SRM51-44-11-001. PERFORMED REPAIR PER AIRBUS SB A320-53-1339/ALI53-11-03. R&R''D DOOR STOP FITTINov 3, 2018 · N422UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018110502287Support · corrodedRH SHEAR PLATE SUPPORT FR69-70 IS CORROED (A3NB-53-3-6222) PER H AECO LCQ REF. NO. 9297144. GENERATED BY V061742.Nov 3, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110502283Skin · dentedFUSELAGE EXTERNAL SURFACE FR-62 STRG 41L,42L HAS DENT (A3NB-05-3 -6003) PER HAECO LCQ NR 9296352. GENERATED BY N078570. PERFORMED DAMAGE CUT-OUT, FABRICATED & INSTALLED DOUBLER & FILLE R PER SRM53-00-300-043 PARA 2(A)(1)(G-L)(N-O) & FIG 20144 SHEET 1. TREATED,Nov 3, 2018 · N422UA · Airbus A320232 · Fuselage Main, Plate/Skin
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