# Service difficulty reports: N469UA

A list on [N469UA](https://openairdocs.org/aircraft/N469UA.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 2 · 70 reports

- [SDR CALA2025081107583](https://openairdocs.org/sdr/CALA2025081107583.md): Indicator · faulted · Aug 9, 2025 · N469UA · Airbus A320232 · Attitude and Direction Data System
  > STDBY ATTITUDE INDICATOR HAS FAILED REPLACED STANDBY ATTITUDE INDICATOR, OPS CHECK GOOD MM 34-22-24.APARTS USED: 31-4170-9-0001,QTY:1 ROTABLE PARTS CHG:TT # 1449521 SN OFF 2440 PN OFF 31-4170-9-0001 INDICATOR, STAN OFF 31-4170-9-0001 2440 ON 31-4170-9-0001
- [SDR CALA2025012402023](https://openairdocs.org/sdr/CALA2025012402023.md): Girt Bar · lack of lube · Jan 21, 2025 · N469UA · Airbus A320232 · Emergency Equipment
  > DOOR 2L SLIDE ARM LEVER DIFFICULT TO ARM. SHOWED ARMED ON THE GROUND B4 T/O. RED CAB PRS LIGHT LUBED LOWER GIRT BAR FLOOR LATCHES AND LOWER GIRT BAR BALL ENDS. DOOR ARM/DISARM OPS CHECK GOOD AT 18 FT LBS. REF: AMM TASK 12-22-52-640-014-A AND AMM TASK 52-10-
- [SDR CALA2025010601784](https://openairdocs.org/sdr/CALA2025010601784.md): Light · missing · Jan 3, 2025 · N469UA · Airbus A320232 · Exterior Lighting
  > LEFT LANDING LIGHT MISSING ON ARRIVAL. REF LOG# 3413284 SEE LOG #3413284 FOR CORRECTIVE ACTION. LT LDG LIGHT MISSING WIRES EXPOSED, REPLACED LH LANDING LIGHT HOUSING REF AMM 33-42-11-400-003-A. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2024031100688](https://openairdocs.org/sdr/CALA2024031100688.md): Reservoir · overserviced · Mar 7, 2024 · N469UA · Airbus A320232 · Hydraulic System, Main
  > CREW REPORTS YELLOW RESERVOIR OVERHEAT IN FLIGHT. YELLOW RESERVOIR APPEARS OVER SERVICED. ITEM LOCKED TO CONFIRM FIX. SERVICED AND COMPLIED WITH TSM REF TSM 29-13-00-810-802-A. - TOMC KROWN PERFORM INITIAL EVALUATION HYD OVERHEAT MSG. FOUND YELLOW SYSTEM WAY O
- [SDR CALA2023092502869](https://openairdocs.org/sdr/CALA2023092502869.md): Frame · cracked · Sep 21, 2023 · N469UA · Airbus A320232 · Fuselage Main, Frame
  > LH FR35 STG 30 AT FASTENER HOLE #14. CRACK INDICATION NOTED AT 3 O''CLOCK AND 9 O''CLOCK ON FWD SURFACE OF THE FRAME LAYER. PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A 5331-03052 ON OR BEFORE 20-MAR-2024. SOLUTION WITH INSPECTION REQUIREMENTS
- [SDR CALA2023050301348](https://openairdocs.org/sdr/CALA2023050301348.md): Seal · missing · May 3, 2023 · N469UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 3 #1 ENGINE INBOARD TR FLEX SEAL SEGMENT DEPARTED AIRCRAFT. REPLACED DAMAGED PANEL.
- [SDR CALA2022052501351](https://openairdocs.org/sdr/CALA2022052501351.md): Seal · departed · May 25, 2022 · N469UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 1 P/N D5461038200100 PEELED BACK AND BROKE OFF DEPARTING A/C APPROXIMATELY 15" X 4" THIN METAL PART. REMOVED REMAING PIECE OF SEAL AND REPLACED WITH NEW SEAL.
- [SDR CALA2022052501337](https://openairdocs.org/sdr/CALA2022052501337.md): Seal · damaged · May 25, 2022 · N469UA · Airbus A320232 · Nacelle/Pylon Structure
  > LEFT NUMBER 1 ENGINE COWL SEAL BROKE OFFBY HINGE ACCESS PANEL REPLACED FWD INBD PYLON SEAL. P/N D5461038200000. NO.1 ENG.AMM 54-57-22-400-003-A
- [SDR CALA2022032300769](https://openairdocs.org/sdr/CALA2022032300769.md): None · missing · Mar 23, 2022 · N469UA · Airbus A320232 · Steering Unit
  > PDA 3 NLG ELECTRIC BOX LEVER MISSING BOTH SPRING CLIPS...SEE PHOTO PHOTO ADDED PARTS ADDED PER IPC 32-51-12-01E INSTALLED BOTH SPRING CLIPS...REF IPC 32-51-12-01E..
- [SDR CALA2020051700969](https://openairdocs.org/sdr/CALA2020051700969.md): Fuel Cap · missing · May 15, 2020 · N469UA · Airbus A320232 · Fuel Storage
  > PDA 2 WING FUEL CAP FOUND MISSING ON ARRIVAL.
- [SDR CALA2020010600018](https://openairdocs.org/sdr/CALA2020010600018.md): Control Cable · damaged · Dec 22, 2019 · N469UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > (AAR N/R 9031569) (SUPPORT TASK) FOUND BROKEN STRANDS ON L/H MLG FREE FALL CABLE BETWEEN FR42 AND FR46. REMOVED & REPLACED L/H MLG FREE FALL CABLE BETWEEN FR42 & FR46 P ER AMM A320 32-33-16-000-002-A STEPS 3.E.(2) & 4.C.(9) & AMM 32- 33-16-400-002-A. PERFORMED
- [SDR CALA2019120902168](https://openairdocs.org/sdr/CALA2019120902168.md): Connector · broken · Dec 8, 2019 · N469UA · Airbus A320232 · Electrical Power System Wiring
  > AAR NR 9031839 (SUPPORT TASK) L-81 NO DOT CONNECTOR 201WL-A HAS BROKEN STRAIN RELIEF ON BACKSHELL REMOVED AND REPLACED BACKSHELL FOR CONNECTOR 201WL-A IAW A320 ES PM 20-33-45. OPS CHECK TO BE COMPLETED ON CUSTOMER WORK CARD #18 -2373-1-7907 SEQ #108 IDT ADD
- [SDR CALA2019120702153](https://openairdocs.org/sdr/CALA2019120702153.md): Wire Harness · damaged · Dec 6, 2019 · N469UA · Airbus A320232 · Light System Wiring
  > AAR NR 9031773 SUPPORT TASK L-76 DOT 008. EMERGENCY LIGHT HARNES S DAMAGED SEAT ROW 23 ABC REMOVED AND REPLACED DAMAGED EMERGENCY LIGHT HARNESS SEAT ROW 23 ABC IAW A320 ESPM 20-33-22PB 0201 CONFIG 01 AND NAT WIRE AND RA CEWAY DRAWING 40N00648, OPERATIONAL CHEC
- [SDR CALA2019112862083](https://openairdocs.org/sdr/CALA2019112862083.md): Pressure Panel · cracked · Nov 25, 2019 · N469UA · Airbus A320232 · Fuselage Main, Structure
  > REF AAR DLH N/R 9031510, LH SIDE PRESSURE PANEL BETWEEN FR35-36 HOLES 4 AND 13 HAVE CRACK INDICATIONS. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5331-02510. DIP L OGPAGE TO READ AS FOLLOWS, A
- [SDR CALA2019112862082](https://openairdocs.org/sdr/CALA2019112862082.md): Window Frame · cracked · Nov 25, 2019 · N469UA · Airbus A320232 · Fuselage Main, Structure
  > REF AAR DLH N/R 9031350, ROTO PROBE INSPECTION SHOWS CRACK INDIC ATION AT WINDSHIELD SIDE POST UPPER ATTACHMENT, LH SIDE. HOLE ID ENTIFIED AS #3 LHS. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5331-02523. DIP L OGPAGE TO BE CREATED TO READ AS FOLLOWS, ACCO
- [SDR CALA2019112542053](https://openairdocs.org/sdr/CALA2019112542053.md): Frame · cracked · Nov 21, 2019 · N469UA · Airbus A320232 · Fuselage Main, Frame
  > REFERENCE AAR DLH N/R 9031163 & 9031164, ROTO PROBE INSPECTION S HOWS CRACK INDICATION AT DOUBLE JOGGLE, RH SIDE, FRAME 16 AT DOO R STOP #7, HOLES 4 AND B ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5311-02316 ON HOL ES 4 AND B AT RH FRAME 16 DOOR STOP #7 D
- [SDR CALA2019112532032](https://openairdocs.org/sdr/CALA2019112532032.md): Threshold · corroded · Nov 18, 2019 · N469UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6299) R2 DOOR SURROUND LOWER STR 22-23 FR 66-68. UNDE RSIDE OF DOOR THRESHOLD HAS CORROSION. MARKED ON TOP. REFER TO A AR N/R: 9031514. REPLACED R2 THRESHOLD AT FR 66-68 IAW A320 SRM 51-423-11-801. RT ESTORED SURFACE PROTECTION IAW A320 SRM 51-75-12
- [SDR CALA2019112532031](https://openairdocs.org/sdr/CALA2019112532031.md): Threshold · corroded · Nov 18, 2019 · N469UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6299) L2 DOOR SURROUND LOWER STR 22-23 FR 66-68. UNDE RSIDE OF DOOR TYHRESHOLD HAS CORROSION. MARKED ON TOP. REPLACED L2 DOOR THRESHOLD FR66-68 IAW A320 SRM 51-42-11-801.3 R ESTORTED SURFACE PROTECTIONB IAW A320 SRM 51-75-12-801.
- [SDR CALA2019061700974](https://openairdocs.org/sdr/CALA2019061700974.md): Bolt · missing · Jun 17, 2019 · N469UA · Airbus A320232 · Nose/Tail Landing Gear
  > PDA 2 FOUND NLG TORQE LINK CENTER CONNECT PIN/ BOLT MISSING. (COVERED ON ORIGINAL LOG PAGE 3496551) MAINTENANCE HAS LOCATED THE MISSING BOLT. ITEM WILL BE CORRECTED ON ORIGINAL LOG PAGE 3496551 CENTER PIN REPLACED ON ORIGINAL LOG PAGE
- [SDR CALA2018102902222](https://openairdocs.org/sdr/CALA2018102902222.md): Pressure Switch · faulty · Oct 29, 2018 · N469UA · Airbus A320232 · Hydraulic Pressure Sensor
  > G ENG 1 PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. - HYD HYD PUMP 31-2914-9-9003, AMM 29-11-51. FURTHER TSM REF 29-11-00- 810-804. BERG TOMC FAILING. NEEDS NEW SWITCH REF TSM TASK 29-11-00-810-804. FOUND PRESSURE SWITCH1074GK REMOVED AND REPLACED NR 1 ENG PU
- [SDR CALA2018011900247](https://openairdocs.org/sdr/CALA2018011900247.md): Panel · delaminated · Jan 19, 2018 · N469UA · Airbus A320232 · Escape Slide
  > LEFT OVERWING EMERGENCY SLIDE PANEL 193AT HAS DELAMINATION ON AFT LOWER CORNER. REMOVED AND REPLACED THE SLIDE PANEL IAW AMM 25-62-42-000-001, AND 25-62-42-400-001-A.
- [SDR CALA2017091103153](https://openairdocs.org/sdr/CALA2017091103153.md): Battery · no test · Sep 11, 2017 · N469UA · Airbus A320232 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT BATTERY DID NOT PASS A BITE CHECK. REPLACED THE BATTERY AND PERFORMED BITE CHECK IAW AMM 33-51-00-710.
- [SDR CALA2017041400984](https://openairdocs.org/sdr/CALA2017041400984.md): Unknown · smoke · Apr 14, 2017 · N469UA · Airbus A320232 · Air Distribution System
  > BEHIND FIRST CLASS SEATS 3AB. A PUFF OF SMOKE NOTED IN CABIN VISUALLY WITH ELECT SMELL PERFORMED FORM 46-6020 AND INSPECTION AND CHECK IAW 05-51-10-200 -801C1. INSPECTED AREA AND FOUND NO ELECTRICAL ISSUES WITH ANY OF THE SEAT ELEC UNITS. CHECK ALL CONNECTION
- [SDR CALA2016120901062](https://openairdocs.org/sdr/CALA2016120901062.md): Battery Pack · no test · Dec 9, 2016 · N469UA · Airbus A320232 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST BATTERY FAULT LEFT MESSAGE. REPLACED BATTERY PACK IN LEFT POWER SUPPLY. OPS CHECKED GOOD.
- [SDR CALA2013103092515](https://openairdocs.org/sdr/CALA2013103092515.md): Cone · cracked · Oct 28, 2013 · N469UA · Airbus A320232 · Engine Collector/Tailpipe/Nozzle
  > NR 2 ENG EXHAUST CONE HAS 4.5" CRACK IN ZONE 1 AT 4 O'CLOCK POSITION. STOP DRILLED CRACK IAW AMM 78-11-12-200-011-C.
- [SDR CALA2013090490983](https://openairdocs.org/sdr/CALA2013090490983.md): Check Valve · faulty · Sep 1, 2013 · N469UA · Airbus A320232 · Hydraulic System, Main
  > GREEN HYDRAULIC RESERVOIR PRESSURE SYSTEM TROUBLESHOOTING - CHECK OF PRESSURE LINES FOR INTEGRITY-LEAKS. REMOVE SEAT ROWS 22-24 ABC, REMOVED FLOOR PANEL 241LF, FOUND CHECK VALVE 1388GM & REMOVE CHECK VALVE FROM MANIFOLD. APPLY EXT AIR PRESSURE AT 50 PSI THR
- [SDR CALA2013082990841](https://openairdocs.org/sdr/CALA2013082990841.md): B-Nut · loose · Aug 26, 2013 · N469UA · Airbus A320232 · Hydraulic System, Main
  > G RESERVOIR LOW AIR PRESSURE DISPLAYED ON UPPER ECAM SCREEN. FOUND 'B'-NUT LOOSE AT RESERVOIR PRESSURE GAUGE SERVICED SYSTEM LIGHT OUT AT UPPER ECAM SCREEN. OPERATION CHECKED GOOD IAW MM.
- [SDR UALA2013051303313](https://openairdocs.org/sdr/UALA2013051303313.md): Proximity Switch · inoperative · May 12, 2013 · N469UA · Airbus A320232 · Escape Slide
  > LEFT AFT SLIDE INDICATION INOPERATIVE ON DOOR OXYGEN SYS ECAM PAGE. SLIDE INDICATION SHOWED ARM AT THE GATE. IAW CREW DOOR 2L SLIDE ARMED INDICATION OUT IN CRUISE AND REARMED ITSELF ON DESCENT THRU 15,000 MSL. CABIN PRESS DELTA 4.8 PSI CABIN ALT 3100' -ADJU
- [SDR UALA2013040802350](https://openairdocs.org/sdr/UALA2013040802350.md): Unknown · unknown · Apr 6, 2013 · N469UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS, NO SMOKING SIGN, CABIN LIGHTS ON BRIGHT AND SEAT BELT LIGHT ALL STUCK ON. PERFORMED CIDS RESET AND OP CHECK THRU CFDS PER AMM 23-73-00-740-005-A. OP CHECKED NS FSB LIGHTS PER AMM 23-73-63-400-002-A, ALSO OP CHECKED EMERGENCY LIGHTS PER
- [SDR UALA2013040302171](https://openairdocs.org/sdr/UALA2013040302171.md): Placard · wrong part · Apr 4, 2013 · N469UA · Airbus A320232 · Placards and Markings
  > LEFT FWD OVERWING EMERGENCY EXIT DOOR HAS THE WRONG PLACARD ON DOOR. REMOVED AND REPLACED PLACARD.
- [SDR UALA2013031801643](https://openairdocs.org/sdr/UALA2013031801643.md): Power Supply · faulty · Mar 17, 2013 · N469UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY SYS TEST FAULTED, EPSU INT LOAD EMERGENCY L. REPLACED EPSU AT 11WL. OP CHECKED GOOD.
- [SDR UALA2013030601330](https://openairdocs.org/sdr/UALA2013030601330.md): Plate · worn · Mar 5, 2013 · N469UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON CNA ANTI CHAFING PLATE WORN AT RIB 5. INSTALLED ANTI-CHAFING PLATE PER SRM 54-51-12 FIG 202.
- [SDR UALA2013012800500](https://openairdocs.org/sdr/UALA2013012800500.md): Strap · missing · Jan 26, 2013 · N469UA · Airbus A320232 · Emergency Equipment
  > COCKPIT CRASH AXE LOWER RETAINING LEATHER STRAP MISSING. REPLACED LOWER STRAP.
- [SDR UALA2012122407370](https://openairdocs.org/sdr/UALA2012122407370.md): Hydraulic Line · leaking · Dec 24, 2012 · N469UA · Airbus A320232 · Hydraulic System, Main
  > CREW REPORTS GREEN HYD QTY RESERVOIR LOW LEVEL. REMOVED AND REPLACED HYD LINE REF IPC 29-11-06-02L ITEM 260 PAGE 14 NO LEAKS NOTED. SERVICED GREEN HYD TO FULL.
- [SDR UALA2012121707275](https://openairdocs.org/sdr/UALA2012121707275.md): Spring · deformed · Dec 15, 2012 · N469UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > RIGHT NOSE GEAR DOWN LOCK SAFETY SPRING SHOWS SIGNS OF UNUSUAL DEFORMATION. UPPER COILS DO NOT MEET MINIMUM ENGAGEMENT ON RETAINER OF TWO WRAPS. ISSUE IS ON RT SPRING UPPER COILS. REPLACED RIGHTT NLG LOCK SPRING.
- [SDR UALA2012121007157](https://openairdocs.org/sdr/UALA2012121007157.md): Nose Cowl · cracked · Dec 10, 2012 · N469UA · Airbus A320232 · Engine Cowling System
  > INLET COWL INNER SURFACE 6:00 7 INCH CRACK THROUGH 9 RIVET HOLES. REPLACED NR 2 NOSE COWL FOR CRACKS.
- [SDR UALA2012112606755](https://openairdocs.org/sdr/UALA2012112606755.md): Battery · failed · Nov 24, 2012 · N469UA · Airbus A320232 · Emergency Lighting
  > FWD LEFT EPSU BATTERY FAILS EMERGENCY LIGHT TEST. REPLACED BATTERY IAW MM, TESTS GOOD.
- [SDR UALA2012111906633](https://openairdocs.org/sdr/UALA2012111906633.md): Starter · faulty · Nov 15, 2012 · N469UA · Airbus A320232 · Engine Starter
  > SPARKS FROM FRONT OF ENGINE 2 DURING START. COCKPIT INDICATIONS NORMAL. MAINT ATTEMPTED AUTO START AND START VALVE MANUAL START WITH NO ROTATION. WILL NEED TO REPLACE START VALVE AND STARTER PER MM. REPLACED THE STARTER AND START VALVE PER MM. ACP FUNCTIO
- [SDR UALA2012100805707](https://openairdocs.org/sdr/UALA2012100805707.md): Unknown · odor · Oct 5, 2012 · N469UA · Airbus A320232 · Air Distribution System
  > FOUL ODOR IN CABIN ELECTRICAL PERHAPS. INSPECTED E AND E COMPARTMENTS AND PITS CABIN SEEMED TO HAVE URINE TYPE SMELL. DISCONNECTED PC AIR RAN PACKS CABIN SMELLS NORMAL.
- [SDR UALA2012071703848](https://openairdocs.org/sdr/UALA2012071703848.md): Oxygen Mask · failed · Jul 15, 2012 · N469UA · Airbus A320232 · Crew Oxygen System
  > FIRST OFFICERS OXYGEN MASK DOES NOT REPRESSURIZE AFTER SELF TEST. REPLACED FIRST OFFICERS OXYGEN MASK STOWAGE BOX, LEAK CHECKED GOOD. OPS CHECKED NORMAL
- [SDR UALA2012071603815](https://openairdocs.org/sdr/UALA2012071603815.md): Battery · no test · Jul 15, 2012 · N469UA · Airbus A320232 · Emergency Lighting
  > PERFORMED EMERGENCY LIGHT TEST PER 3SVC, FOUND EPSU BATTERY FWD LT DISPLAYED. REPLACED BATTERY, TESTED NORMAL.
- [SDR UALA2012060303063](https://openairdocs.org/sdr/UALA2012060303063.md): Nut · loose · Jun 2, 2012 · N469UA · Airbus A320232 · Passenger Compartment Equipment
  > SEAT BACK LOOSE, ROCKING AT 24C. FOUND JAM NUT LOOSE ON HYDRO LOCK, OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR UALA2012051002688](https://openairdocs.org/sdr/UALA2012051002688.md): Fadec · malfunctioned · May 7, 2012 · N469UA · Airbus A320232 · Fuel Controlling System
  > FADEC A FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET FADEC AND EIU. SYSTEM OPS NORMAL.
- [SDR UALA2012032901973](https://openairdocs.org/sdr/UALA2012032901973.md): Connector · not seated · Mar 28, 2012 · N469UA · Airbus A320232 · Water/Waste System Wiring
  > UNABLE TO UPLOAD WATER.:WHEN OPENING AFT PANEL FILL VALVE THE FWD DUMP VALVE THE FWD SVC PANEL DRIVES TO OPEN AND DUMPS THE WATER RENDERED POTABLE WATER SYS INOP PER MEL 38050. RESET CB'S AND RESEAT CONNECTOR OF 16MA MOTOR GRD CHK NORM. RETURNED SYS BACK T
- [SDR UALA2011090904889](https://openairdocs.org/sdr/UALA2011090904889.md): Packing · damaged · Sep 7, 2011 · N469UA · Airbus A320232 · Turbine Engine Oil System
  > CREW REPORT: ON WALK-AROUND OBSERVED OIL DRIPPING PUDDLING UNDER ENG 1. SAMC TEXT: FBO TO EVALUATE SOURCE AND TYPE OF FLUID AND REPORT FINDINGS TO SAMC-EMC. FBO FOUND PACKING DAMAGED ON PRESSURE LINE TO NR 5 BEARING CAVITY MATING SURFACE. PIX POSTED ESN V
- [SDR UALA2011082904631](https://openairdocs.org/sdr/UALA2011082904631.md): Switch · broken · Aug 26, 2011 · N469UA · Airbus A320232 · Crew Oxygen System
  > CAPTAIN'S OXYGEN MASK PRESS TO TEST SWITCH BROKE OFF. REPLACED CAPT OXYGEN MASK BOX PER MM, OPS CHECKS GOOD.
- [SDR UALA2011082204469](https://openairdocs.org/sdr/UALA2011082204469.md): Smoke Detector · false activation · Aug 19, 2011 · N469UA · Airbus A320232 · Smoke Detection
  > SMOKE LAV DET FAULT. REPLACED LAV 'A' SMOKE DETECTOR, TESTED OKAY.
- [SDR UALA2011081204258](https://openairdocs.org/sdr/UALA2011081204258.md): Computer · faulty · Aug 11, 2011 · N469UA · Airbus A320232 · Flight Control System
  > ELAC 2 FAULT. REPLACED ELAC 2 PER AMM. TESTS OKAY. ACCOMPLISHED CAT3 TEST. TESTS SATISFACTORILY.
- [SDR UALA2011071203474](https://openairdocs.org/sdr/UALA2011071203474.md): Bracket · bent · Jul 11, 2011 · N469UA · Airbus A320232 · Fire Bottle, Portable
  > FIRE EXT BRACKET BADLY BENT BEHIND LAST ROW SEATS RIGHT SIDE. REPLACED BRACKET.
- [SDR UALA2011070103263](https://openairdocs.org/sdr/UALA2011070103263.md): Trim Panel · loose · Jun 30, 2011 · N469UA · Airbus A320232 · Passenger Compartment Equipment
  > SEAT 27D HAS EXPOSED METAL ON FLOOR. SECURED METAL TRIM ON LOWER DADO PANEL AT SEAT 27F, (NOT 27D).

Next page: https://openairdocs.org/aircraft/N469UA/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 = 'N469UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N469UA/reports

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