# Service difficulty reports: N467UA

A list on [N467UA](https://openairdocs.org/aircraft/N467UA.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 · 127 reports

- [SDR CALA2026081118471](https://openairdocs.org/sdr/CALA2026081118471.md): Unknown · odor · Aug 10, 2026 · N467UA · Airbus A320232 · Air Distribution System
  > HOT ELECTRICAL ODOR IN COCKPIT, CHECKED ACFT FOR ELECTRICAL ODOR, DISCONNECT GROUND AIR, OPENED ALL E & E COMPARTMENTS FOR ABNORMALITIES. NONE FOUND. RAN APU PACKS NO ODOR OF ELECTRICAL IN COCKPIT AND CABIN NOTED AT THIS TIME. ACFT OK TO CONTINUE.
- [SDR CALA2026072618014](https://openairdocs.org/sdr/CALA2026072618014.md): Fuel Cap · missing · Jul 25, 2026 · N467UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING DURING FUEL TRANSFER FOR CENTER TANK PUMP. INSTALLED A NEW FUEL COUPLING AND FUEL LANYARD IAW AMM 28-25-41. NO DEFECTS NOTED.
- [SDR CALA2026063017479](https://openairdocs.org/sdr/CALA2026063017479.md): Power Supply · faulted · Jun 28, 2026 · N467UA · Airbus A320232 · Emergency Lighting
  > LEFT AFT EPSU IS FAULTING DURING EMERGENCY LIGHT TEST. R & R EPSU BOX PER AMM33-51-38, OPS CHECKED GOOD.
- [SDR CALA2026012313179](https://openairdocs.org/sdr/CALA2026012313179.md): Engine · odor · Jan 20, 2026 · N467UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > EXCESSIVE SMOKE COMING FROM NR 1 ENG. APON SHUTDOWN WITH A STRONG SMELL OF OIL. MOTORED NR1 ENG. SMOKE AND OIL SMELL STILL PRESENT AFTER MOTORING SHUTDOWN. RAN ENGINE NR 1 PER AMM 71-00-00-710-043-A FOR 15 MINS. ENGINE OPERATED WITHIN NORMAL PARAMETERS. NO EXC
- [SDR CALA2025102410477](https://openairdocs.org/sdr/CALA2025102410477.md): Battery · discharged · Oct 22, 2025 · N467UA · Airbus A320232 · Emergency Lighting
  > WHILE WORKING JOB CARD 18-3351-1-0003 FOUND EPSU EMERGENCY BATTERY LEFT FAULT. REMOVED AND REPLACE EPSU BATTTERY LEFT WITH SERVICEABLE FROM STOCK. REF AIPC 33-51-38-01B. OPS CHECK GOOD.
- [SDR CALA2025102310449](https://openairdocs.org/sdr/CALA2025102310449.md): Web · cracked · Oct 8, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SURVEY OF THE LT INSP AREA SHOWS EVIDENCE OF A PREVIOUS REPAIR. PERFORMED REPAIR PER PART 1 INTERIM REPAIR IAW EC/RA 5330-07609 AND REO-L25569 REV IR WITH NO DEVIATIONS.
- [SDR CALA2025101009901](https://openairdocs.org/sdr/CALA2025101009901.md): Skin · damaged · Oct 8, 2025 · N467UA · Airbus A320232 · Wing, Plate/Skin
  > RIGHT WING FUEL PANEL LANDING 604JB HAS 2EA HOLES OUT OF ROUND. REPAIRED 2 EA HOLES AT RT WING FUEL PANEL LANDING 640JB IAW A32 0 SRM 51-21-11-300-002 AND REO L2559B EC/RA 5721-01516 CAT A.
- [SDR CALA2025102310448](https://openairdocs.org/sdr/CALA2025102310448.md): Window Frame · cracked · Oct 2, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT WINDSHIELD FWD NODE, MOST INBD HOLE FROM CENTER LINE HAS A CRACK INDICATION AT THE 6:O CLOCK POSITION 100% SH. PERFORMED REPAIR IAW PART 1 INTERIM REPAIR IAW EC/RA 5311-03390 AND REO-L25578 REV IR WITH NO DEVIATIONS
- [SDR CALA2025092309171](https://openairdocs.org/sdr/CALA2025092309171.md): Support Beam · corroded · Sep 22, 2025 · N467UA · Airbus A320232 · Emergency Exits
  > RH AFT EMERGENCY HATCH INTERNAL STRUCTURE, ABOVE WINDOW, HAS 2 G OUGES WITH EVIDENCE OF CORROSION. REMOVED & REPLACED BEAM SUPPORT AT R/H AFT EMERGENCY HATCH INTER NAL/STRUCTURE IAW A320 SRM 51-72-11 & 51-42-11.
- [SDR CALA2025092209101](https://openairdocs.org/sdr/CALA2025092209101.md): Door Sill · corroded · Sep 19, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > L1 DOOR SILL IS CORRRODED AT UPPER ATTACH HOLES FOR SCUFF PLATE CENTER SHAPE SILL. R & R CORRODED L1 DOOR SILL AS REQUIRED IAW SRM 51- 72-11-911-001.
- [SDR CALA2025092209100](https://openairdocs.org/sdr/CALA2025092209100.md): Fitting · cracked · Sep 19, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT WINDSHIELD LOWER NODE AREA, CONTINUITY FITTING CRACKED AT AFT FACE OF HORIZONTAL FLANGE, AFT OF INBD FASTENER. LEFT WINDSHIELD LOWER NODE AREA, CONTINUITY FITTING CRACKED AT AFT FACE OF HORIZONTAL FLANGE, AFT OF INBD FASTENER. R & R CONTINUITY FITTING
- [SDR CALA2025092209096](https://openairdocs.org/sdr/CALA2025092209096.md): Beam · gouged · Sep 18, 2025 · N467UA · Airbus A320232 · Emergency Exits
  > LEFT AFT EMERGENCY HATCH INTERNAL STRUCTURE ABOVE WINDOW HAS 2 GOUGES WITH EVIDENCE OF CORROSION. REMOVED AND REPLACED L/H AFT EMERGENCY HATCH BEAM SUPPORT IAW A320 SRM 51-42-11.
- [SDR CALA2025092209095](https://openairdocs.org/sdr/CALA2025092209095.md): Beam · gouged · Sep 18, 2025 · N467UA · Airbus A320232 · Emergency Exits
  > LH FWD EMERGENCY EXIT HATCH UPPER HORIZONTAL BEAM HAS 2 NOTCHES AND GOUGES FROM CHAFING ON LINER FASTENERS. REMOVED AND REPLACED L/H FWD EMERGENCY HATCH SUPPORT BEAM IAW A320 SRM 51-42-11.
- [SDR CALA2025092209092](https://openairdocs.org/sdr/CALA2025092209092.md): Beam · gouged · Sep 18, 2025 · N467UA · Airbus A320232 · Emergency Exits
  > AFT LH EMERGENCY HATCH INTERNAL STRUCTURE HAS CORROSION AT THE SECOND FROM THE BOTTOM SUPPORT STRUCTURE. R & R SUPPORT BEAM AT AFT L/H EMERGENCY HATCH IAW A320 SRM 51-42-11.
- [SDR CALA2025092209091](https://openairdocs.org/sdr/CALA2025092209091.md): Beam · gouged · Sep 18, 2025 · N467UA · Airbus A320232 · Emergency Exits
  > RIGHT FWD EMERGENCY HATCH INTERNAL STRUCTURE ABOVE WINDOW HAS 2 GOUGES WITH EVIDENCE OF CORROSION. R AND R BEAM SUPPORT AT RH FWD EMERGENCY HATCH INTERNAL STRUCTURE IAW A320 SRM 51-72-11.
- [SDR CALA2025100609633](https://openairdocs.org/sdr/CALA2025100609633.md): Window Frame · cracked · Sep 16, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS. LEFT WINDSHIELD FWD NODE, MOST INBD HOLE FROM CENTER LINE HAS A CRACK INDICATION AT THE 6:O CLOCK POSITION 100% SH. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 5,600 FLIGHT CYCLES CURRENT HOURS 74772:19 FL
- [SDR CALA2025091708995](https://openairdocs.org/sdr/CALA2025091708995.md): Shear Tie · corroded · Sep 10, 2025 · N467UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > AFT CARGO FRAME SHEAR TIE AT FR 62 BETWEEN STRINGER 42L AND 43L HAS CORROSION. REMOVED AFT CARGO FRAME SHEAR TIE FR 62 STR 42L & 43L. FABRICATED AND INSTALLED NEW SHEAR TIE AS REQUIRED IAW SRM 51-72-11-911-00 1.
- [SDR CALA2025091108777](https://openairdocs.org/sdr/CALA2025091108777.md): Seat Track · corroded · Sep 9, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK Y765 FR 25-35 HAS CORROSION. PERFORMED REPAIR ON SEAT TRACK Y765, FR 25-35 IAW SRM 53-21- 15-300-004.
- [SDR CALA2025090908639](https://openairdocs.org/sdr/CALA2025090908639.md): Seat Track · corroded · Sep 6, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > Y1292 HAS CORROSION FR12-24. SEAT TRACK AT Y1292 FR12-24 FOUND TO BE OUT OF LIMITS WITH A DEP TH OF.041" AND A MAX ALLOWED DEPTH OF.031" IAW A320 SRM 53-11- 14-283-007 REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-11 -911-001 AND SRM 51-42-11.
- [SDR CALA2025090908638](https://openairdocs.org/sdr/CALA2025090908638.md): Seat Track · corroded · Sep 6, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > -Y1292 HAS CORROSION JUST FWD OF FR 20. EVALUATED FOUND OUT OF LIMITS IAW SRM 53-11-15-283-011 REMOVED A ND REPLACED -Y1292 FR12-FR24 IAW SRM 51-42-11/001.
- [SDR CALA2025090908637](https://openairdocs.org/sdr/CALA2025090908637.md): Structure · corroded · Sep 6, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > Y503.2 HAS CORROSION FR12-16. EVALUATED BEAM Y503.2 FOUND TO BE OUT OF LIMITS IAW SRM 53- 11-14-283-001, REMOVED AND REPLACED Y503.2 AS REQUIRED IAW A 320 SRM 51-42-11/001.
- [SDR CALA2025091708994](https://openairdocs.org/sdr/CALA2025091708994.md): Plate · corroded · Sep 5, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT PIT CORROSION AT 38R PROFILE FR 52. REMOVED AND REPLACED CORRODED PROFILE PANEL AT FR43-FR52A IAW SRM 51-72-11.
- [SDR CALA2025090808586](https://openairdocs.org/sdr/CALA2025090808586.md): Floor Support · corroded · Sep 5, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT Y765 HAS CORROSION FR12-24. REMOVED AND REPLACED FLOOR SUPPORT Y765 AT FR 12-24 IAW A320 SRM 51 -72-11.
- [SDR CALA2025090808580](https://openairdocs.org/sdr/CALA2025090808580.md): Seat Track · corroded · Sep 4, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FR47-FR52 Y1292 MULTIPLE SPOTS OF CORROSION. REMOVED CORRODED SEAT TRACK Y1292 AT FR 47-FR52, INSTALLED SPLICE REPAIR AS REQUIRED IAW A320 SRM 53-41-15-300-003.
- [SDR CALA2025091708993](https://openairdocs.org/sdr/CALA2025091708993.md): Skin · contaminated · Sep 3, 2025 · N467UA · Airbus A320232 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 131 IN CHES FROM IB EDGE AND 15 INCHES FROM AFT EDGE, I INCH DIA. REPAIRED L/H ELEVATOR UPPER SURFACE 131IN FROM I/B 15IN FROM T/E 1.38IN DIA ZONE A IAW A320 SRM 55-21-11-300-004 CATEGORY A REPAIR.
- [SDR CALA2025091708992](https://openairdocs.org/sdr/CALA2025091708992.md): Frame · cracked · Aug 31, 2025 · N467UA · Airbus A320232 · Fuselage Main, Frame
  > AFT PIT AT FRAME 59RT UNDER STRINGER 41RT WEDGE IS CRACKED. REMOVED AND REPLACED WEDGE IN AFT CARGO PIT FR59RT AT STRINGER 4 1 IAW A320 SRM 51-72-11.
- [SDR CALA2025090808565](https://openairdocs.org/sdr/CALA2025090808565.md): Stringer · corroded · Aug 31, 2025 · N467UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BILGE AREA BETWEEN FR 63 & 64 STRINGER 41R HAS CORROSI ON. REMOVED AND REPLACED STRINGER 41R FR59-61 IAW SRM 51-72-11.
- [SDR CALA2025091708991](https://openairdocs.org/sdr/CALA2025091708991.md): Hinge · broken · Aug 28, 2025 · N467UA · Airbus A320232 · Elevator Structure
  > LEFT ELEVATOR NR 4 HINGE HAS A BROKEN TAB. REPAIRED LT ELEVATOR NR 4 HINGE LUG FITTING IAW SRM 55-26-41- 300-002.
- [SDR CALA2025090408469](https://openairdocs.org/sdr/CALA2025090408469.md): Fitting · damaged · Aug 28, 2025 · N467UA · Airbus A320232 · Elevator Structure
  > R/H ELEVATOR INBD ACTUATOR FITTING LOCKING LUG GOUGED. REPAIRED RH ELEVATOR I/B ACTUATOR FITTING LOCKING LUG IAW A320 S RM 55-26-47-300-001 THIS REPAIR IS CATEGORY A NO FURTHER ACTION REQUIRED.
- [SDR CALA2025082708196](https://openairdocs.org/sdr/CALA2025082708196.md): Seat Track · corroded · Aug 26, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE L/H SEAT TRACK Y254 CORRODED AT FRS 21, 22, 23. REMOVED AND REPLACED SEAT TRACK Y254 FR 12-24 LH IAW A320 SRM 51 -72-11-911-001 AND SRM 51-42-11 ACMP BY MECH V937285 INSP BY V89 2429
- [SDR CALA2025082708195](https://openairdocs.org/sdr/CALA2025082708195.md): Seat Track · corroded · Aug 26, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FR58 Y765 UPPER FLANGE CROWN GOUGED. REMOVED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15-300-003 REV 154 REPLACED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15 -300-003 REV 154.
- [SDR CALA2025082708192](https://openairdocs.org/sdr/CALA2025082708192.md): Floor Support · corroded · Aug 25, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT, FRAME 28 STR33 LH TO 33 RH FLOOR PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR28 STR33 LH TO 33 RH IAW A320 SRM 51-42-11.
- [SDR CALA2025082708191](https://openairdocs.org/sdr/CALA2025082708191.md): Floor Support · corroded · Aug 25, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR BEAM Y765 FR 66-70 L/H HAS CORROSION. REMOVED CORRODED FLOOR BEAM AND REPLACED WITH NEW FLOOR BEAM AT Y765 FR 66-70 LH IAW A320 SRM 51-42-11/001.
- [SDR CALA2025082708188](https://openairdocs.org/sdr/CALA2025082708188.md): Seat Track · corroded · Aug 21, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > R/H WET AREA SEAT TRACK -1292 AT FR64-66 IS CORRODED. REMOVED SEAT TRACK, -1292 FR 64-66 IAW A320 SRM 51-42-11/0 01 REV 154 REPLACED BEAM-SEAT TRACK -1292 FR64-66 IAW A320 SRM 5 1-42-11/001 REV 154
- [SDR CALA2025082508078](https://openairdocs.org/sdr/CALA2025082508078.md): Support Angle · cracked · Aug 21, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > EXTERNAL RT FUSELAGE FAIRING OUTER VERTICAL SUPPORT AT FR 34 IS CRACKED. REMOVED AND REPLACED FR 34 VERTICAL ANGLE IAW SRM 51-42-11 P 18-25.
- [SDR CALA2025082108013](https://openairdocs.org/sdr/CALA2025082108013.md): Floor Support · corroded · Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT -Y765 RT FR 66-70 SHOWS EVIDENCE OF CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.
- [SDR CALA2025082108012](https://openairdocs.org/sdr/CALA2025082108012.md): Floor Support · corroded · Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT WET AREA FLOOR SUPPORT AT FR 68-69 LT Y1292 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM TASK 51-72-11-911-001.
- [SDR CALA2025082108011](https://openairdocs.org/sdr/CALA2025082108011.md): Floor Support · corroded · Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR AFT WET AREA AT FR68-70 L/H FLOOR SUPPORT Y254 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.
- [SDR CALA2025082108010](https://openairdocs.org/sdr/CALA2025082108010.md): Shear Plate · corroded · Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SHEAR PLATE AT L/H FR69-70 WET AREA HAS SHEARED FASTENERS & POSS IBLE CORROSION. REMOVED AND REPLACED SHEAR PLATE AT LH FR 69-70 WET AREA IAW A32 0 SRM TASK 51-72-11-911-001.
- [SDR CALA2025081307693](https://openairdocs.org/sdr/CALA2025081307693.md): Floorbeam · corroded · Aug 12, 2025 · N467UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA FLOOR BEAM -Y1292 R/H BETWEEN FR68-69 HAS EVI DENCE OF CORROSION. REMOVED AND REPLACED FLOOR BEAM RT - Y1292 RH FR68-69 IAW A320 S RM 51-72-11-911-001.
- [SDR CALA2025081407730](https://openairdocs.org/sdr/CALA2025081407730.md): Door Sill · corroded · Aug 11, 2025 · N467UA · Airbus A320232 · Fuselage Main, Structure
  > AFT MAIN CABIN R2 DOOR SILL HAS CORROSION. REPAIRED AFT MAIN CABIN R2 DOOR SILL IAW A320 SRM 53-41-14-300-0 01. CAT A.
- [SDR CALA2025063006033](https://openairdocs.org/sdr/CALA2025063006033.md): Faucet · leaking · Jun 27, 2025 · N467UA · Airbus A320232 · Potable Water System
  > WATER CONTINUOUSLY LEAKING FROM FORWARD GALLEY WITH VERY STRONG ODOR. FORWARD GALLEY WATER FAUCET ADJUSTED AND WATER LEAK STOP AND DRAIN WATER FROM SYSTEM DRAIN TWICE AND REFILLED FOT ODOR MM 12-15-38-613-001-A
- [SDR CALA2024123001693](https://openairdocs.org/sdr/CALA2024123001693.md): Smoke Detector · faulted · Dec 27, 2024 · N467UA · Airbus A320232 · Smoke Detection
  > LAV SMOKE DETECT ACTIVE ON ALL 3 LAVS NO SMOKE OR FIRE INDICATIN S UPON OPS CHECK OF THE LAV SMOKE DETECTORS. FOUND AURUAL AND LIGHT INDICATORS NOT INDICATING WITH TEST. REMOVED AND REPLACED SDCU REF 26-17-34. OPS CHECK GOOD. PARTS USED: 31-2610-9-0001,QTY:1
- [SDR CALA2024100700765](https://openairdocs.org/sdr/CALA2024100700765.md): Fuel Cap · missing · Oct 5, 2024 · N467UA · Airbus A320232 · Fuel Storage
  > PDA 2 REF LP 9465269 - FUEL CAP FOUND MISSING AT DFW ENTERED INTO HISTORY FOR SDR ON WALK AROUND FOUND FUEL CAP MISSING. REQUEST CDL REFERENCE # 28 A. NO PARTS AVALIBLE..DFW. COMPLIED WITH CDL 28A. OKAY TO DEFER MISSING FUEL CAP PER CDL 28A CAP, COUPLING R O
- [SDR CALA2024041101040](https://openairdocs.org/sdr/CALA2024041101040.md): Control Servo · failed · Apr 7, 2024 · N467UA · Airbus A320232 · Landing Gear Steering System
  > REJECTED TAKEOFF APPX 95 KTS AIRCRAFT PULLED HARD LEFT. DEBRIEFED CREW. CREW STATES BRAKES WERE NOT DRAGGING. WIND AT TIME OF TAKEOFF WAS 9 KTS. ALL INDICATIONS WERE NORMAL AND NO FAULT MESSAGES DISPLAYED. CREW STATED IT FELT LIKE ENGINE FAILURE. UPON MX ARRIV
- [SDR CALA2024050701341](https://openairdocs.org/sdr/CALA2024050701341.md): Cover · cracked · Mar 19, 2024 · N467UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > INSPECT (GENERAL VISUAL) ENTRY DOOR LININGS, SLIDE BUSTLES, AND SURROUNDING CLOSEOUT TRIM AND SEAL FOR: {A3NB-25-3-6025} - CRACKED L2 DOOR HINGE COVER DECORATIVE ITEM, NO HAZARD FOR PASSENGERS, PLACED UNDER INTERIOR PROGRAM PER GMM 05-30-06
- [SDR CALA2023070502164](https://openairdocs.org/sdr/CALA2023070502164.md): Cap · missing · Jul 4, 2023 · N467UA · Airbus A320232 · Aircraft Fuel System
  > ACFT ARRIVED WITH NO FUEL CAP NOTIFIED TOMC. INSPECT (GENERAL VISUAL) FUEL TANKS FOR: {A3NB-28-3-6004} - AIRCRAFT ARIVED MISSING FUEL CAP. CAP REQUIRED 31-2825-9-0001 NOT AVALIBLE IN SAN. REQUEST TO APPLY MEL 28A VERIFIED TO LEAKAGE FROM CONNECTOR WITH CAP MIS
- [SDR CALA2022102702966](https://openairdocs.org/sdr/CALA2022102702966.md): Skin · missing · Oct 26, 2022 · N467UA · Airbus A320232 · Passenger/Crew Doors
  > DAMAGE FOUND ON OUTSIDEOF DOOR 1R AT THE LOWER AREA. SHEETMETAL R IPPED OFF OF DOOR. LOCKING FOR FERRY FLT. LOG PAGE UNLOCKED UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN POSSIBLE REPAIR SRM 52-10-00-300-003. PLEASE
- [SDR CALA2022061501509](https://openairdocs.org/sdr/CALA2022061501509.md): None · failed · Jun 15, 2022 · N467UA · Airbus A320232 · Flight Control System
  > FLT/CONTRL SPOILERFAULT ON DEPARTURERIGHT INBOARD 1 REMAINEDEXTE NDED..RTB COMPLIED WITH MEL, SPOILER 1 RIGHT SIDE LOCKED OUT, PER MEL. PK PER TOMC ADD EMP:U116706,U167027 DISPATCH DESK: 23 NAME: VS DATE: 13-JUN-22- 2764A APPROVED. TROUBLE
- [SDR CALA2022011000090](https://openairdocs.org/sdr/CALA2022011000090.md): Lanyard · missing · Jan 9, 2022 · N467UA · Airbus A300* · Aircraft Fuel System
  > PDA 3 REF LP7766813 FUEL CAP LANYARD MISSING. PDA 3 NOTED REF LP 7766813 FOR CDL APPLIED.

Next page: https://openairdocs.org/aircraft/N467UA/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 = 'N467UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N467UA/reports

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