N446UA

Service difficulty reports · 150

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 = 'N446UA' 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 CALA2026091419392Wire · detachedDURING EMERGENCY LIGHT TEST FOUND AISLE PATH LIGHTING AT SEAT 11ABC INOP. INSPECTED CONNECTOR UNDER SEAT FOUND WIRE DETACHED VERIFIED DISCREPANCY, FOUND SEAT HARNESS FOR EMERGENCY LIGHT DAMAGED. R & R EMERGENCY LIGHT HARNESS AND EMERGENCY LIGHT IAW AMM 33-51-Sep 11, 2026 · N446UA · Airbus A320232 · Light System WiringSDR CALA2026030414324Smoke Detector · false activationLAVATORY SMOKE DETECTOR FAULTED AFTER PAX WENT IN, NO ODOR DETECTED. PERFORMED AN OPS CHECK OF LAV SMOKE DETECTION. CLEARED MESSAGE IAW 26-17-00-710-001A.Mar 3, 2026 · N446UA · Airbus A320232 · Smoke DetectionSDR CALA2025102410482Bottle · low pressureDOOR 1L PRESSURE LOW SERVICED L1 DOOR DAMPER REF AMM 52-10-00-614-001-AOct 22, 2025 · N446UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025082508087Rivet · missingSERVICE CHECK EXTERIOR WALK-AROUND PROCEDURE - 2, MISSING RIVETS ON CNA T/E, 12 CLOCK POSITION OF FWD ROW ON INNER SKIN SIDE. .NO OTHER RIVETS FELT OR LOOK LOOSE. REPLACED THE CNA AS PER EC/RA: 7811-01400 STEP: G.1. OKAY FOR 78-DIP FOR ENG 1 CNA TRAILING EAug 23, 2025 · N446UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR CALA2025082208031Filter · odorCAPTAIN REPORTS RUBBER SMELL IN THE FLT DECK CAPTAIN REPORTS RUBBER SMELL IN THE FLT DECK DURING TAXI PER TOMC. REMOVED AND REPLACED RECIRCULATION FILTERS IAW 21-21-41-000-001-A. RAN APU AND PACKS NO SMELLS NOTED.Aug 18, 2025 · N446UA · Airbus A320232 · Air Distribution SystemSDR CALA2025061605570Elec Connector · inoperativeDURING 2SC FOUND EMERGENCY LIGHT SEAT 32 ABC INOP. UPON INSPECTION, FOUND EMERGENCY LIGHT INOP DUE TO CUT BLACK ELECTRICAL WIRE RESECURED CONNECTOR IN REF WITH ESPM 20-53-55-02. OPS CHECK NORMAL IN REF WITH AMM 33-51-19.Jun 15, 2025 · N446UA · Airbus A320232 · Light System WiringSDR CALA2024112001200Light · inoperative34C EMERGENCY LIGHT INOP REQUEST MEL 3350C FOR 34C MEL 3350C APPROVED FOR SEAT 34C DDP FOLLOWED *DM* UPDATED M/L WITH HARNESS AND LIGHT ASSY FOR EMERGENCY PATH LIGHTING IN CASE NEEDED AFTER T/S. REMOVED AND REPLACED 34C SEAT/WALL-MOUNTED EMERGENCY LIGHT HARNESNov 18, 2024 · N446UA · Airbus A320232 · Emergency LightingSDR CALA2024090600593Pump · faultyHYD Y RSVR LOW LEVEL ECAM - TOMC ITEM LOCKED TO CONFIRM FINDINGS. FOUND Y RSVR EMPTY, SERVICED Y HYD SYSTEM TASK 12-12-29-611-001-A, TURNED YELLOW ELECTRIC PUMP ON, PRESSURE IS LOW AND GREEN PRESURE DROPS AND FLUCTUATES. REF TSM 29-13-00-810-801-A ENG PUMP POSSep 4, 2024 · N446UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR CALA2023102303134Fuel Cap · missingFUEL CAP MISSING APPLY CDL28A FOR FUEL CAP. COMPLIED WITH CDL NO LEAKAGE NOTED PLACARD APPLIED DISPATCH DESK: 36 NAME: DS DATE: 27-SEP-23- APPROVED FOR CDL 28A CAP, COUPLING R OFF 31-2825-9-0001 0941 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 0941 ON 31-2825-9Sep 27, 2023 · N446UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2023060901796Circuit Board · inoperativeON MLG EXTENSION, 3 GREEN WERE INDICATED ON WHEELS PAGE ONLY. NO NDICATION ON PANEL LTS RETRACTED NORMAL. 15 MIN LATER, MLG NORMAL EXTENDED. RECEIVED 3 DOWNLOCKED INDS ON WHEELS ECAM PAGE, BUT NO MLG LIGHTS ON CENTER INSTR PANEL. ON MLG EXTENSION, RECEIVED 3 Jun 8, 2023 · N446UA · Airbus A320232 · Landing Gear SystemSDR CALA2023020600350Epsu · not reportedMAIN CABIN FWD, EMERGENCY LIGHT DOES NOT WORKS (TROUBLESHOOT) REMOVED AND REPLACED EPSU 10WL OK IAW AMM 33-51-39-000-006-C1 AN D 33-51-39-400-006-C1. OPS CHECK PERFORMED IAW AMM 33-51-00-710- 002-C2 GOOD FOR SERVICE.Feb 6, 2023 · N446UA · Airbus A320232 · Emergency LightingSDR CALA2023011600114Profile · crackedRH FWD EMERGENCY EXIT DOOR BOTH LOAD TRANSMITTING PROFIL HAVE CRACKS. REMOVED 2EA PROFILE DAMAGE IAW SRM 51-42-11 LOCATED AND DRILLED 2EA NEW PROFILE IAW SRM 51-44-11 INSTALLED 2EA NEW PROFILE IAW SRM 51-42-11 PAINTED SURFACE IAW SRM 51-75-12.Jan 13, 2023 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2023011300113Stringer · corrodedAFT CARGO COMPARTMENT RH SIDE AT BETWEEN FR64 AND FR65 STR 31 HAD CORROSION. AFTER EVALUATION OF CORROSION NO ALLOWABLE DAMAGE ON BLEND IAW S INGER IAW SRM 51-42-11, AND INSTALLED OUTFLOW VALVE IAW AMM 21-3 RM 53-41-13-283-002, REMOVED OUT FLOW VALVE IAW AMMJan 12, 2023 · N446UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2023010600045Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE. L/H SEAT TRACK Y1292. INSIDE OF CROW N, CROWN, OUTBOARD AND INBD FLANGE CORRODED FROM FRAME 47 TO 64. (BETWEEN EVERY FRAME.) () REMOVED CORROSION ON SEAT TRACK Y1292 OUT OF LIMITS, IAW SRM 53- ATED APPLIED IAW SRM 51-75-12 SEE ATTACJan 5, 2023 · N446UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023010200001Floor Support · corrodedMAIN CABIN FLOOR STRUCTURE. R/H FR 66 OTBD BEAM CORRODED 3 PLACE S. () REPLACED FLOOR BEAM AT MAIN CABIN FLOOR STRUCTURE RH BTW FR65 AND FR66 IAW SRM 51-42-11 AND SRM 51-72-11 EMP#: WORK ACCOMPLISHED AT ST ENGINEERING O F MOBILE AT BFM ON NR#: 48056Dec 30, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022123003518Beam · corrodedMAIN CABIN FLOOR STRUCTURE. R/H FR 66 OTBD BEAM CORRODED 3 PLACE S. () REPLACED FLOOR BEAM P/N: D5347207500100 B/N: 0004033258 AT MAIN CABIN FLOOR STRUCTURE RH BTW FR65 AND FR66 IAW SRM 51-42-11 AND SRM 51-72-11 EMP#: V936035 WORK ACCOMPLISHED AT ST ENGINEERINDec 29, 2022 · N446UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2022122603489Floorbeam · corrodedMAIN CABIN FLOORBEAM FRM 66 R/H OTBD CORRODED. REMOVED & REPLACED FLOORBEAM IAW SRM 51-72-1 1-911-001 AND SRM 51-42-11 AND APPLY TOP COAT I.A.W SRM 51-75-12.Dec 24, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022122303474Door Sill · corrodedMAIN CABIN FLOOR STRUCTURE. R2 DOOR SILL FR 66 CORROSION AT FAST ENER HOLE IN PLATE UNDER GIRT BAR FITTING. INBD AND AFT OF GIRT BAR FITTING. VISUAL INSPECTION, CORROSION NOTED OUT OF LIMITS IAW SRM 51-75-12. REMOVED DOOR SILL IAW SRM 51-42-11/001. LOCATEDDec 23, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022122303473Stringer · corrodedAFT CARGO PIT BILGE STRINGER 42L FR57-FR58 HAS CORRSION. REMOVED FASTENERS ON AREA IAW SRM 53-41-13-300-010, INSTALLED REPAIR ANGLE AND APPLIED TOP COAT IAW SRM 53-41- PERFORMED 13-300-010.Dec 23, 2022 · N446UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022122303472Profile · crackedLEFT FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED THE PROFILE IAW SRM 51-42-11.Dec 23, 2022 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2022122303468Profile · crackedLH AFT EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REMOVED AND REMPLACED PROFIL AT LT EMERGENCY EXIT DOOR FAN NEW PROFILE IAW SRM 51-72-11-91 1-001.Dec 21, 2022 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2022122303467Stringer · corrodedAFT CARGO PIT BILGE STRINGER 42L FR57-FR58 HAS CORRSION. DOT NO. 17-154 () REMOVED FASTENERS ON AREA I.A.W SRM 53-41-13-300-010, REMOVED CO EA, INSTALLED REPAIR ANGLE AND APPLIED TOP COAT I.A.W SRM 53-41- RROSION IN AREA D= 0.0185 L= 2.2265 I.A.W 51-42-11 SRM,Dec 21, 2022 · N446UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022122303466Profile · crackedLH FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED FWD LOAD TRANMITTING PROFILE IAW SRM 51-42-11.Dec 21, 2022 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2022122303465Door Sill · corrodedMAIN CABIN FLOOR STRUCTURE. R2 DOOR SILL FR 66 CORROSION AT FAST ENER HOLE IN PLATE UNDER GIRT BAR FITTING. INBD AND AFT OF GIRT BAR FITTING. () VISUAL INSPECTION AROUND DOT. CORROSION NOTED OUT OF LIMITS IAW W SRM 51-75-12. ACCOMPLISHED IAW SRM 53-41-14-283-0Dec 21, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022122103459Profile · crackedLH AFT EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. DOT NO. 17-30 () REMOVED AND REMPLACED PROFIL AT LH EMERGENCY EXIT DOOR FAN NEW P ROFILE P/N D5227907620551 BATCH# 0004041671 I.A.W SRM 51-72-11-91 1-001 EMP#: V940362 WORK ACCOMPLISHED AT ST ENDec 21, 2022 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2022121603404Beam · corrodedMAIN CABIN FLOOR STRUCTURE. FR 66 BEAM AT Y1292 CORRODED. () REMOVED CORROSION I.A.W 51-74-00 L= 0.657", W= 0.740", D= 0.035" BEAM FROM MAIN CABIN FLOOR STRUCTURE I.A.W SRM 51-42-11 EMP#: V9 FOUND OUT OF LIMITS I.AW 53-00-14-283-002, REMOVED LH OTBD BEAM 36321Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022121603403Beam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM FWD OF FR 68 AT -Y969 AT FASTEN ER HOLE CORRODED. () REMOVED AND REPLACED FLOOBEAM FWD OF FR68 IAW SRM 51-42-11 SEE F ORM 44-008 ATTACHED EMP#: V936761 WORK ACCOMPLISHED AT ST ENGINE ERING OF MOBILE AT BFM ON NR#: 48036Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022121603402Beam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM AFT OF FR 66 AT -Y969 CORRODED. () REMOVED AND REPLACED FLOORBEAM AFT OF FR66 IAW SRM 51-42-11 SEE FORM 44-008 ATTACHED EMP#: V936761 WORK ACCOMPLISHED AT ST ENGIN EERING OF MOBILE AT BFM ON NR#: 48037Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022121603401Beam · corrodedMAIN CABIN FLOOR STRUCTURE. L/H OTBD BEAM AT FR 68 TO 69 CORRODE D. () REMOVED CORROSION I.A.W SRM 51-74-00 L= 0.776" W= 2.034", D= 0.0 1, INSTALLED FLOOR BEAM LH OTBD I.A.W SRM 51-42-11 EMP#: V936321 25 FOUND OUT OF LIMITS I.A.W SRM 53-00-14-283-002, REMOVED Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022121403375Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM AFT OF FR 66 AT -Y969 CORRODED. () REMOVED AND REPLACED FLOORBEAM AFT OF FR66 IAW SRM 51-42-11 SEE FORM 44-008 ATTACHED EMP#: V936761 WORK ACCOMPLISHED AT ST ENGIN EERING OF MOBILE AT BFM ON NR#: 48037Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022121403374Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM AT Y765 CORRODED AT FR68 AND FWD OF FR70. () REMOVED AND REPLACED NEW BEAM PART# D534721922000 BATCH# 0003916 319 AT Y765 IAW SRM 51-42-11-001 EMP#: V914954 WORK ACC0MPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 48024Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022121403373Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE BETWEEN FR 68 AND FR 69 BEAM AT Y 160.5 LAV/GALLEY HARWARE AND STRUCTURE CORRODED. () REMOVED CORROSION AT MAIN CABIN FLOOR STR BTW FR68 AND FR69 BEAM M 51-42-11. EMP#: V936035 WORK ACCOMPLISHED AT ST ENGINEERING OF Y160.5 BLEND OUT Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022121403372Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM FWD OF FR 68 AT -Y969 AT FASTEN ER HOLE CORRODED. () REMOVED AND REPLACED FLOOBEAM FWD OF FR68 IAW SRM 51-42-11 SEE FORM 44-008 ATTACHED EMP#: V936761 WORK ACCOMPLISHED AT ST ENGINE ERING OF MOBILE AT BFM ON NR#: 48036Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022121403371Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE. L/H OTBD BEAM AT FR 68 TO 69 CORRODED. () REMOVED CORROSION I.A.W SRM 51-74-00 L= 0.776" W= 2.034", D= 0.0 1, INSTALLED FLOOR BEAM LH OTBD I.A.W SRM 51-42-11 EMP#: V936321 25 FOUND OUT OF LIMITS I.A.W SRM 53-00-14-283-002, REMOVED LDec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022121403390Beam · corrodedMAIN CABIN FLOOR STRUCTURE. BEAM AT Y765 CORRODED AT FR68 AND FW D OF FR70. () REMOVED AND REPLACED NEW BEAM PART# D534721922000 BATCH# 0003916 319 AT Y765 IAW SRM 51-42-11-001 EMP#: V914954 WORK ACC0MPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 48024Dec 12, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2022121403389Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE BETWEEN FR 68 AND FR 69 BEAM AT Y 160.5 LAV/GALLEY HARWARE AND STRUCTURE CORRODED. () REMOVED CORROSION AT MAIN CABIN FLOOR STR BTW FR68 AND FR69 BEAM M 51-42-11. EMP#: V936035 WORK ACCOMPLISHED AT ST ENGINEERING OF Y160.5 BLEND OUT Dec 12, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022051101213None · missingPDA 3 #1 ENG AFT STRUT AT LOWER DRAIN TUBE HAS RIVETS BROKEN OFF/ MISSING AND LOOSE -- SEE PHOTO,S PHOTO,S ADDED MISSING SHIMS & TEFLON STRIP -- SEE PHOTO -- PARTS IPC PHOTO ADDED ORDERED AVAILABLE TEFLON STRIPS AND ARE PLACED IN FLIGHT DECK REMOVED #1 ENG LOWMay 11, 2022 · N446UA · Airbus A320232 · Nacelle/Pylon StructureSDR CALA2022051101212None · missingPDA 3 #2 ENG AFT STRUT FAIRING MISSING ONE FASTENER AND OTHERS LOOSE -- SEE PHOTO PHOTO ADDED REMOVED AND INSTALLED NEW FASTENERS REF SRM 54-54-11-283-004.May 11, 2022 · N446UA · Airbus A320232 · Nacelle/Pylon StructureSDR CALA2021022500226Intercostal · damagedEA 5311-02164 REV ORIGINAL LT FWD DOOR FR 20 NR 1 STOP FITTING LWR I/B HOLE HAS DISCREPANT INDICATION. REF TO PEMCO NR 10380.0377 REPAIRED FR20 NR 1 DOORSTOP FITTING HOLE NR 3 AND REPLACED THE ADJACENT INTERCOSTAL PER ECRA 5311-02495 STEPS 6 - 11, PART 1 WITHOFeb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021022500225Fitting · damagedEA- 5311-02164 REV ORIGINAL LT FWD DOOR FR 16 NR 1 STOP FITTING LWR I/B HOLE HAS DISCREPANT INDICATION. REF TO PEMCO NR 10380. 0376 REPAIRED LT FR 16 NR 1 DOORSTOP FITTING HOLES 3 AND 4, FABBED AND INSTALLED FREZZE PLUGS, REPLACED THE ADJACENT INTERCOSTAL PERFeb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021022500224Intercostal · damagedEA 5311-02164 REV ORIGINAL RT FWD DOOR FR 16 NR 7 STOP FITTING I/B UPPER AND LOWER HOLES HAVE DISCREPANT INDICATIONS. REF TO PEMCO NR 10380.0375 REPAIRED LT FR 16 NR 7 DOOR STOP FITTING HOLES NR 1 AND NR 3, REPLACED THE ADJACENT INTERCOSTAL PER ECRA 5311-0249Feb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021021000165Frame · cracked(A3NB-52-4-6031) LT FWD OVERWING EXIT DOOR CRACKED IN AREA OF LH LOAD TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0505 REMOVED AND REPLACED L/H FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001. WORK PERFOMED BY V915767, INSPECTED BY Q930, ENTERED BY V9278Feb 10, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021021000164Frame · cracked(A3NB-52-4-6031) RT AFT OVERWING EXIT DOOR CRACKED IN AREA OF LH LOAD TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0499 REMOVED AND REPLACED L/H FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001. WORK PERFOMED BY V915737, INSPECTED BY Q930, ENTERED BY V9278Feb 10, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021021000163Frame · cracked(A3NB-52-4-6031) RT AFT OVERWING EXIT DOOR CRACKED IN AREA OF RT LOAD TRANSMITTING PROFILE (MARKED). FER TO PEMCO NR 10380.0500 REMOVED AND REPLACED R/H FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001. WORK PERFOMED BY V915737, INSPECTED BY Q930, ENTERED BY V9278Feb 10, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021021000162Frame · cracked(A3NB-52-4-6031) LT AFT OVERWING EXIT DOOR CRACKED IN AREA OF LH TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0507 REMOVED AND REPLACED L/H FRAME SEGMENT IAW A320 SRM 51-72-11-911 -001. WORK PERFOMED BY V915737, INSPECTED BY Q930, ENTERED BY V927860 REFeb 10, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021020800135Profile · cracked(A3NB-52-4-6031) RT AFT OVERWING EXIT DOOR CRACKED IN AREA OF RT LOAD TRANSMITTING PROFILE (MARKED). FER TO PEMCO NR 10380.0500. MORE DETAILS AWAITED.Feb 5, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021020800134Profile · cracked(A3NB-52-4-6031) RT AFT OVERWING EXIT DOOR CRACKED IN AREA OF LH LOAD TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0499 . MORE DETAILS AWAITED.Feb 5, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021020800142Profile · cracked(A3NB-52-4-6031) LT AFT OVERWING EXIT DOOR CRACKED IN AREA OF LH TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0507. MORE DETAILS AWAITEDFeb 5, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2021020800141Profile · cracked(A3NB-52-4-6031) LT FWD OVERWING EXIT DOOR CRACKED IN AREA OF LH LOAD TRANSMITTING PROFILE (MARKED). REF TO PEMCO NR 10380.0505. MORE DETAILS AWAITEDFeb 5, 2021 · N446UA · Airbus A320232 · Emergency ExitsSDR CALA2019042900660Computer · failedF/CTL SLATS LOCKED AIR RETURN, LOCKING LOG REPLACED SFCC2 UNLOCKED SLATS AND RESET WTB (WING TIP BRAKE) MSG REF AMM 27-80-00-869-004-A. PFMD OPS CK OF SLAT SYS. OPS GOOD REF 27-84-00-710-001-A...UPON TS OF SLAT/FLAP SYS FOUND SFCC #2 HOT TO THE TOUCH WHEN RMVDApr 27, 2019 · N446UA · Airbus A320232 · Leading Edge Slat Control System
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