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 AALA202206163562Hook · wornAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 842 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-11-21.May 19, 2022 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA202206165648Hook · wornAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 INNER CONTROL HANDLE HOOK WORN. REPLACED HOOK PER AMM 52-11-21.May 19, 2022 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA2022052300523Frame · crackedDURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AFT OVERWING EXIT DOOR FWD RH EEH DOOR (843) L= 0.130"; REF AEROMAN NR 2022-233223 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052300522Frame · crackedDURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AFT OVERWING EXIT DOOR (FWD LH EEH DOOR 833) L= 0.128"; REF AEROMAN NR 2022-233224 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052300521Frame · crackedDURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AT OVERWING EXIT DOOR (AFT LH EEH DOOR 834) L=0.135"; REF AEROMAN NR 2022-233225 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052300520Frame · crackedDURING HEAVY MAINTENANCE, CRACK: FR SEGMENT 1 AT OVERWING EXIT DOOR (AFT RH EEH DOOR 844) L=0.133"; REF AEROMAN NR 2022-233226 W/O: 2022 8/1: ACCOMPLISHED EC A320-52-1144.May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052300519Slide Raft · failedDURING HEAVY MAINTENANCE, R1 DOOR SLIDE FAILS EMERGENCY LIGHT TEST; REMOVED AND REPLACED R1 DOOR SLIDE REF AEROMAN NR 2022-233166 W/O 2022 8/1: IAW AMM 25-62-44-000-804-A, AMM 25-62-44-400-803-A AND AMM 33-51-00-710-001. OPS CHECKS OK.'May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052300518Slide Raft · failedDURING HEAVY MAINTENANCE, L1 DOOR SLIDE FAILS EMERGENCY LIGHT TEST; REF AEROMAN NR 2022-233167 W/O 2022 8/1: REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-62-44-000-012-A, AMM 25-62-44-400-007-A, AND AMM 33-51-00-710-001. OPS CHECKS GOOD.'May 19, 2022 · N634JB · Airbus A320232 · Emergency EquipmentSDR YENA2022052000510Cabin Air Sys · odorFLT#2303, JFK-SJU. 'INFLIGHT CREW REPORTS ODOR IN AFT CABIN. MX-270 FORM FILLED OUT; COMPLIED WITH INFO NOTICE 2017-T015I SECTION A(A), ISOLATED FAULT TO TYPE 10(A),1,C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. AIRCRAFT OK FOR SERVICE.'May 19, 2022 · N618JB · Airbus A320232 · Air Distribution SystemSDR YENA2022052000508Check Valve · failedFLT#163, JFK-SRQ. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK). ' YELLOW HYDRAULIC SYSTEM OVERHEAT AFTER TAKEOFF; R/S REF TSM 29-13-00. REMOVED AND REPLACED CHECK VALVE Y REF AMM 29-24-21. ON OPS CHECK OF ENG #2 EDP. ENGINE-DRIVEN PUMMay 19, 2022 · N709JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR YENA2022052700532Idg · failedFLT#1597, JFK-DEN. 'DESCENDING ON ARRIVAL OUT 13,00 FEET GEN #1 FAILED ALSO A/P2 AND AUTO THRUST DISCONNECTED AS WELL AS FLIGHT DIRECTORS. THE TOP MCDU SCREEN FAILED MOMENTARILY ALSO. ( IDG 1 DISCONNECTED (N503-N655) ); REPLACED #1 ENG IDG IAW AMM 24-21-51. OPMay 18, 2022 · N559JB · Airbus A320232 · AC Generator-AlternatorSDR YENA2022052000509Apu · odorFLT#1079, LAS-LAX. ' DIRTY SOCK SMELL ( APU BLEED AIR SUPPLY SYSTEM ) DIRTY SOCK SMELL REPORTED BY INFLIGHT IN REAR OF CABIN DURING INITIAL DESCENT AND FINAL APPROACH.' (SUPPLEMENTAL TO FOLLOW).May 18, 2022 · N595JB · Airbus A320232 · APU Start/Ignition SystemSDR YENA2022052000507Cabin Air Sys · odorFLT#163, JFK-SRQ. 'LEVEL 2 ODOR EVENT DURING APPROACH PHASE ODOR DISSIPATED. NO ODOR ON LANDING HEAVY ODOR OVER JUMPSEAT C. F/A MOVED HER SEAT POSITION NO MEDICAL ATTENTION ASKED FOR; COMPLIED WITH TSM 05-50-00-810-831-A LEVEL A DECONTAMINATION WITH ENG 1&2 RUMay 18, 2022 · N624JB · Airbus A320232 · Air Distribution SystemSDR YENA2022052000505Transceiver · failedFLT#2851, FLL-UIO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL). 'WX-RT FAULT; REMOVED AND REPLACED WX RADAR-TRANSCEIVER IAW AMM 34-41-00. PERFORMED OPS CHECK AND OPS CHECK GOOD.'May 18, 2022 · N809JB · Airbus A320232 · Inertial Guidance SystemSDR CALA2022052001289None · noneFR68 LHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155215-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 18, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052001288None · noneFR68 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.2 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155217-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 18, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052001287None · noneFR66 LHS AFT DOOR STOP FITTINGS #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260 SEQ:1602. LTPR NR 005001155209-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 18, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052001286None · noneFR66 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.2 FIGURE 01 SHEET 02. ZONE:260 SEQ:1602. LTPR NR# 5001155213-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SRMay 18, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052001284Beam · corrodedDURING REMOVAL OF NTF ON AFT WET AREA, CORROSION FOUND ON PREVIOUS REPAIR OF L2 DOOR SILL BEAM, EVALUATION IS RECORDED UNDER LP# 8445827. PERFORMED INSTALLATION OF REPAIR PARTS OH LH DOOR 2 SILL BEAM FR.68 IAW A320-200 SRM 53-41-14-300-001 REV 140, AS NOTED ONMay 18, 2022 · N445UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051801283None · missingPDA 3 OPS REPORTS FUEL CAP LANYARD MISSING WAGSTAFF, MARK (V081328)APPLIED CDL 28A. LANYARD MISSING PER CDL DISPATCH DESK: 21 NAME: AL DATE: 16-MAY-22- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VEMay 18, 2022 · N463UA · Airbus A320232 · Aircraft Fuel 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 YENA2022052000502Bleed Valve · fault messageFLT#1018, FLL-JAX. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL). ' ENG 1 COMPRESSOR VANE, AVOID THRUST CHANGES ECAM; SEE L/P 3327939 ITEM 2 (ACCOMPLISHED VISUAL CHECK OF ELEC CONNECTORS ON 2.5 BLEED ACTUATOR. NO DAMAGE OR MISALIGNMENT WAS FOUND. PERFORMED LUBRMay 17, 2022 · N639JB · Airbus A320232 · Compressor Bleed ControlSDR YENA2022051800498Cabin Air Sys · odorFLT#2107, BOS-BNA. ' A LEVEL 2 MUSTY 2 FROM THE ENVIRONMENTAL SYSTEM WAS DETECTED IN THE COCKPIT, FWD GALLEY, AND MID CABIN. BY SEVERAL CREW MEMBERS AND CUSTOMERS DURING BOARDING THE SMELL LINGERED AFTER THE APU BLEED WAS ON AND BOTH PACKS WERE PRESSURIZED. THMay 17, 2022 · N637JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022051900499Computer · failedFLT#2798, JAX-LAX. (AIRCRAFT DIVERTED TO MSY). ' ANTI ICE F/O L/R STATIC ECAM AT FL 340 IMMEDIATE BURNING SMELL FILLED COCKPIT (PROBE HEAT COMPUTERS - FO); REMOVED AND REPLACED PHC # 2 PER AMM 30-31-34. OPS TEST OF PROBE ICE PROTECTION SYSTEM GOOD. THIS CLEARSMay 16, 2022 · N558JB · Airbus A320232 · Pitot/Static Anti-Ice SystemSDR CALA2022051601261Fitting · noneFR68 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.2 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155217-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 16, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051601260Frame · noneFR66 RHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.2 FIGURE 01 SHEET 02. ZONE:260 SEQ:1602. LTPR NR# 5001155213-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW SRMay 16, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051601259Frame · noneFR68 LHS AFT DOOR STOP FITTING #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C, OPERATION 002 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260, SEQ 1605, LTPR NR# 5001155215-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 16, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051601258Fitting · noneFR66 LHS AFT DOOR STOP FITTINGS #1 TO #7 HOLES FOUND BEYOND THE REQUIRED STARTING HOLE DIAMETER OF 8-1-N AS PER EA 5340-01724 REV.C OPERATION 001 STEP 6.1 FIGURE 01 SHEET 02. ZONE 260 SEQ:1602. LTPR NR 005001155209-0010. RPR IS CONSIDERED CAT B. REINSPECT IAW May 16, 2022 · N443UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR YENA2022051800497Filter · failedFLT#494, DEN-BOS. 'OIL / DIRTY SOCK SMELL FROM TAKEOFF UNTIL TOP OF CLIMB. SMELL RETURNED DURING DESCENT THROUGHOUT 12,000 AND CONTINUED UNTIL TOUCHDOWN; PER L/P 3291728 ITEM 1 (REMOVED AND REPLACED APU COOLING FAN ASSY IAW AMM 49-52-51) AND ITEM 2 (PERFORMEDMay 15, 2022 · N637JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022051800496Cooling Fan · failedFLT#494, DEN-BOS. 'OIL / DIRTY SOCK SMELL FROM TAKEOFF UNTIL TOP OF CLIMB. SMELL RETURNED DURING DESCENT THROUGHOUT 12,000 AND CONTINUED UNTIL TOUCHDOWN; PER L/P 3291728 ITEM 1 (REMOVED AND REPLACED APU COOLING FAN ASSY IAW AMM 49-52-51) AND ITEM 2 (PERFORMEDMay 15, 2022 · N637JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022051800495Cooling Fan · failedFLT#494, DEN-BOS. 'OIL / DIRTY SOCK SMELL FROM TAKEOFF UNTIL TOP OF CLIMB. SMELL RETURNED DURING DESCENT THROUGHOUT 12,000 AND CONTINUED UNTIL TOUCHDOWN; PER L/P 3291728 ITEM 1 (REMOVED AND REPLACED APU COOLING FAN ASSY IAW AMM 49-52-51) AND ITEM 2 (PERFORMEDMay 15, 2022 · N637JB · Airbus A320232 · Air Distribution SystemSDR AALA202205176845Door · unsecureAIRCRAFT WAS NOT GROUNDED: FIRST OFFICERS ESCAPE STRAP DOOR FELL 3 TIMES IN FLIGHT. SECURED ESCAPE ROPE PANEL / DOOR PER AMM 25-10-00.May 15, 2022 · N649AW · Airbus A320232 · Emergency EquipmentSDR YENA2022051600470None · noneFLT#1229, EWR-CUN. 'FA COMPLAINED OF OIL ODOR FROM PACKS PASSING 10,000 ON CLIMB & DESCENT ( APU SYSTEM ); IAW WO 1178771 MDDR 473536 (TSI). REPLACED HEPA FILTERS IAW AMM 21-21-41. PERFORMED LEAK CHECK OF APU IAW AMM 49-00-00-200-812-A. ALL OPS CHECKS ARE GOODMay 15, 2022 · N821JB · Airbus A320232 · Fuselage Structure (General)SDR 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 CALA2022051601253Angle · cracked(A3NB-52-4-6031) RH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO. 17-46() REMOVED AND INSTALLED NEW SEGMENT ANGLE (P/N: D5227902620451) IA W SRM 51-42-11. REMOVED AND REINSTALLED BRACKET SUPPORT (FOR ACC ESS) IAW SRM 51-42-11. EMP# May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601252Skin · dentedA3NB-53-3-6358, RH FWD LOWER FUSELAGE 1EA DENT TO OUT SIDE BETWE EN FR31-FR32 AND STR28R AND STR29R. DOT #54-46() M ON NR# 0029972. REPETITIVE INSPECTIONS REQUIRED PER SRI 53-21 TH SUBSEQUENT INSPECTIONS EVERY 1700 FC OR 3400 FH WHICH EVER O -11-205-071 AT 4May 15, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022051601250Angle · cracked(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO.17-51() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D227902620451, IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934344 WORMay 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601249Angle · cracked(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-52() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D5227902620551 IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934377 WORMay 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR 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 CALA2022051601246Angle · cracked(A3NB-52-4-6031) RH FWD EMERGENCY EXIT DOOR HAS A CRACK AT LH LO AD TRANSMITTING PROFIL. DOT NO.17-48.()May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601245Angle · cracked(A3NB-52-4-6031) RH FWD EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-49() REMOVED & REPLACED SEGMENT ANGLE ON R/H FWD EMERGENCY EXIT DOOR R/H IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V934342 AT ST BFM AERO SPACE MOBILE. NR#0029818May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR YENA2022051700484Slide Raft · failedDURING HEAVY MAINTENANCE, CUT ON SLIDE RAFT PASSENGER CREW DOOR 841 SURVIVAL KIT LANYARD (WHITE) IN PASSENGER CABIN; REF AEROMAN N/R 2022-234729. REMOVED AND REPLACED ESCAPE SLIDE RAFT DOOR 841 IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A. (P/N OFF D3May 14, 2022 · N746JB · Airbus A320232 · Emergency EquipmentSDR YENA2022051700485Slide Raft · failedDURING HEAVY MAINTENANCE, PERFORM SLIDE RAFT CONTROL DEPLOYMENT PASSENGER CREW DOOR 832 DUE TO PIN CAN NOT BE SECURED AT AFT GALLEY; REF AEROMAN N/R 2022-234621, REMOVED AND REPLACED ESCAPE SLIDE RAFT DOOR 832 IAW AMM 25-62-44-000-011 AND 25-62-44-400-007-A( May 14, 2022 · N746JB · Airbus A320232 · Emergency EquipmentSDR YENA2022051700483None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 RH SIDE, UPPER OPEN FASTENER HOLE SIDE BOX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-234656, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME 43May 14, 2022 · N746JB · Airbus A320232 · Fuselage, Stabilizer Attach FittingsSDR YENA2022051700482None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 RH SIDE, MIDDLE OPEN FASTENER HOLE SIDE B OX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-234655, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME May 14, 2022 · N746JB · Airbus A320232 · Fuselage, Stabilizer Attach FittingsSDR YENA2022051700481None · noneDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 43 LH SIDE, MIDDLE OPEN FASTENER HOLE SIDE BOX BEAM FLANGE IN PASSENGER CABIN; REF AEROMAN N/R 2022-237654, PERFORMED SERVICE BULLETIN A320-53-1258, LOCATED FUSELAGE / TORSION BOX / LOWER SIDE SHELL / FRAME 4May 14, 2022 · N746JB · Airbus A320232 · Fuselage, Stabilizer Attach FittingsSDR CALA2022051601239None · corroded(A3NB-53-4-6179) AFT CARGO PIT BETWEEN FR56/FR59 STRG 42LH HAS CORROSION. DOT 52-72.() REPLACED STRINGER 42L BETWEEN FR53 TO FR60, IAW A320 SRM 51-42-1 1 P/N:DAN50B09 BATCH: 0003906803. ACCOMPLISHED BY EMP#V934585 AT ST BFM AEROSPACE MOBILE. NR#0029746May 13, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051301230None · none(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-52() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D5227902620551 IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934377 WORMay 13, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051301229None · none(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO.17-51() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D227902620451, IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934344 WORMay 13, 2022 · N442UA · Airbus A320232 · Emergency Exits
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