# Service difficulty reports: N446UA

A list on [N446UA](https://openairdocs.org/aircraft/N446UA.md).

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

Page 1 of 3 · 150 reports

- [SDR CALA2026091419392](https://openairdocs.org/sdr/CALA2026091419392.md): Wire · detached · Sep 11, 2026 · N446UA · Airbus A320232 · Light System Wiring
  > DURING 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-
- [SDR CALA2026030414324](https://openairdocs.org/sdr/CALA2026030414324.md): Smoke Detector · false activation · Mar 3, 2026 · N446UA · Airbus A320232 · Smoke Detection
  > LAVATORY 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.
- [SDR CALA2025102410482](https://openairdocs.org/sdr/CALA2025102410482.md): Bottle · low pressure · Oct 22, 2025 · N446UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR 1L PRESSURE LOW SERVICED L1 DOOR DAMPER REF AMM 52-10-00-614-001-A
- [SDR CALA2025082508087](https://openairdocs.org/sdr/CALA2025082508087.md): Rivet · missing · Aug 23, 2025 · N446UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > SERVICE 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 E
- [SDR CALA2025082208031](https://openairdocs.org/sdr/CALA2025082208031.md): Filter · odor · Aug 18, 2025 · N446UA · Airbus A320232 · Air Distribution System
  > CAPTAIN 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.
- [SDR CALA2025061605570](https://openairdocs.org/sdr/CALA2025061605570.md): Elec Connector · inoperative · Jun 15, 2025 · N446UA · Airbus A320232 · Light System Wiring
  > DURING 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.
- [SDR CALA2024112001200](https://openairdocs.org/sdr/CALA2024112001200.md): Light · inoperative · Nov 18, 2024 · N446UA · Airbus A320232 · Emergency Lighting
  > 34C 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 HARNES
- [SDR CALA2024090600593](https://openairdocs.org/sdr/CALA2024090600593.md): Pump · faulty · Sep 4, 2024 · N446UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > HYD 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 POS
- [SDR CALA2023102303134](https://openairdocs.org/sdr/CALA2023102303134.md): Fuel Cap · missing · Sep 27, 2023 · N446UA · Airbus A320232 · Aircraft Fuel System
  > FUEL 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 31-2825-9
- [SDR CALA2023060901796](https://openairdocs.org/sdr/CALA2023060901796.md): Circuit Board · inoperative · Jun 8, 2023 · N446UA · Airbus A320232 · Landing Gear System
  > ON 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
- [SDR CALA2023020600350](https://openairdocs.org/sdr/CALA2023020600350.md): Epsu · not reported · Feb 6, 2023 · N446UA · Airbus A320232 · Emergency Lighting
  > MAIN 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.
- [SDR CALA2023011600114](https://openairdocs.org/sdr/CALA2023011600114.md): Profile · cracked · Jan 13, 2023 · N446UA · Airbus A320232 · Emergency Exits
  > RH 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.
- [SDR CALA2023011300113](https://openairdocs.org/sdr/CALA2023011300113.md): Stringer · corroded · Jan 12, 2023 · N446UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT 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 AMM
- [SDR CALA2023010600045](https://openairdocs.org/sdr/CALA2023010600045.md): Seat Track · corroded · Jan 5, 2023 · N446UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 ATTAC
- [SDR CALA2023010200001](https://openairdocs.org/sdr/CALA2023010200001.md): Floor Support · corroded · Dec 30, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN 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#: 48056
- [SDR CALA2022123003518](https://openairdocs.org/sdr/CALA2022123003518.md): Beam · corroded · Dec 29, 2022 · N446UA · Airbus A320232 · Passenger/Crew Doors
  > MAIN 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 ENGINEERIN
- [SDR CALA2022122603489](https://openairdocs.org/sdr/CALA2022122603489.md): Floorbeam · corroded · Dec 24, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR CALA2022122303474](https://openairdocs.org/sdr/CALA2022122303474.md): Door Sill · corroded · Dec 23, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN 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. LOCATED
- [SDR CALA2022122303473](https://openairdocs.org/sdr/CALA2022122303473.md): Stringer · corroded · Dec 23, 2022 · N446UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT 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.
- [SDR CALA2022122303472](https://openairdocs.org/sdr/CALA2022122303472.md): Profile · cracked · Dec 23, 2022 · N446UA · Airbus A320232 · Emergency Exits
  > LEFT FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED THE PROFILE IAW SRM 51-42-11.
- [SDR CALA2022122303468](https://openairdocs.org/sdr/CALA2022122303468.md): Profile · cracked · Dec 21, 2022 · N446UA · Airbus A320232 · Emergency Exits
  > LH 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.
- [SDR CALA2022122303467](https://openairdocs.org/sdr/CALA2022122303467.md): Stringer · corroded · Dec 21, 2022 · N446UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT 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,
- [SDR CALA2022122303466](https://openairdocs.org/sdr/CALA2022122303466.md): Profile · cracked · Dec 21, 2022 · N446UA · Airbus A320232 · Emergency Exits
  > LH FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED FWD LOAD TRANMITTING PROFILE IAW SRM 51-42-11.
- [SDR CALA2022122303465](https://openairdocs.org/sdr/CALA2022122303465.md): Door Sill · corroded · Dec 21, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN 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 53-41-14-283-0
- [SDR CALA2022122103459](https://openairdocs.org/sdr/CALA2022122103459.md): Profile · cracked · Dec 21, 2022 · N446UA · Airbus A320232 · Emergency Exits
  > LH 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 EN
- [SDR CALA2022121603404](https://openairdocs.org/sdr/CALA2022121603404.md): Beam · corroded · Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, Structure
  > MAIN 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 36321
- [SDR CALA2022121603403](https://openairdocs.org/sdr/CALA2022121603403.md): Beam · corroded · Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, Structure
  > MAIN 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#: 48036
- [SDR CALA2022121603402](https://openairdocs.org/sdr/CALA2022121603402.md): Beam · corroded · Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Main, Structure
  > MAIN 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#: 48037
- [SDR CALA2022121603401](https://openairdocs.org/sdr/CALA2022121603401.md): Beam · corroded · Dec 15, 2022 · N446UA · Airbus A320232 · Fuselage Floor Panel
  > MAIN 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
- [SDR CALA2022121403375](https://openairdocs.org/sdr/CALA2022121403375.md): Floorbeam · corroded · Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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#: 48037
- [SDR CALA2022121403374](https://openairdocs.org/sdr/CALA2022121403374.md): Floorbeam · corroded · Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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#: 48024
- [SDR CALA2022121403373](https://openairdocs.org/sdr/CALA2022121403373.md): Floorbeam · corroded · Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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
- [SDR CALA2022121403372](https://openairdocs.org/sdr/CALA2022121403372.md): Floorbeam · corroded · Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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#: 48036
- [SDR CALA2022121403371](https://openairdocs.org/sdr/CALA2022121403371.md): Floorbeam · corroded · Dec 14, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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 L
- [SDR CALA2022121403390](https://openairdocs.org/sdr/CALA2022121403390.md): Beam · corroded · Dec 12, 2022 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN 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#: 48024
- [SDR CALA2022121403389](https://openairdocs.org/sdr/CALA2022121403389.md): Floorbeam · corroded · Dec 12, 2022 · N446UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN 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
- [SDR CALA2022051101213](https://openairdocs.org/sdr/CALA2022051101213.md): None · missing · May 11, 2022 · N446UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 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 LOW
- [SDR CALA2022051101212](https://openairdocs.org/sdr/CALA2022051101212.md): None · missing · May 11, 2022 · N446UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 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.
- [SDR CALA2021022500226](https://openairdocs.org/sdr/CALA2021022500226.md): Intercostal · damaged · Feb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EA 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 WITHO
- [SDR CALA2021022500225](https://openairdocs.org/sdr/CALA2021022500225.md): Fitting · damaged · Feb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EA- 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 PER
- [SDR CALA2021022500224](https://openairdocs.org/sdr/CALA2021022500224.md): Intercostal · damaged · Feb 24, 2021 · N446UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EA 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 5311-0249
- [SDR CALA2021021000165](https://openairdocs.org/sdr/CALA2021021000165.md): Frame · cracked · Feb 10, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 V9278
- [SDR CALA2021021000164](https://openairdocs.org/sdr/CALA2021021000164.md): Frame · cracked · Feb 10, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 V9278
- [SDR CALA2021021000163](https://openairdocs.org/sdr/CALA2021021000163.md): Frame · cracked · Feb 10, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 V9278
- [SDR CALA2021021000162](https://openairdocs.org/sdr/CALA2021021000162.md): Frame · cracked · Feb 10, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 RE
- [SDR CALA2021020800135](https://openairdocs.org/sdr/CALA2021020800135.md): Profile · cracked · Feb 5, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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.
- [SDR CALA2021020800134](https://openairdocs.org/sdr/CALA2021020800134.md): Profile · cracked · Feb 5, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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.
- [SDR CALA2021020800142](https://openairdocs.org/sdr/CALA2021020800142.md): Profile · cracked · Feb 5, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 AWAITED
- [SDR CALA2021020800141](https://openairdocs.org/sdr/CALA2021020800141.md): Profile · cracked · Feb 5, 2021 · N446UA · Airbus A320232 · Emergency Exits
  > (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 AWAITED
- [SDR CALA2019042900660](https://openairdocs.org/sdr/CALA2019042900660.md): Computer · failed · Apr 27, 2019 · N446UA · Airbus A320232 · Leading Edge Slat Control System
  > F/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 RMVD

Next page: https://openairdocs.org/aircraft/N446UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N446UA/reports

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