Skip to content

Public Record · As of May 5, 2026

N816UA

Airbus Industrie A319-131 · 1998 View Type →

Status

Registration Valid

Type

Fixed Wing Multi Engine

Engine

IAE V2500SERIES

Last Cert Issue

—

Aircraft Resources

Engine · International Aero Engines → Search FAA TCDS for AIRBUS INDUSTRIE A319-131 →

01 /  Registration

Filed with the Federal Aviation Administration

Every cell below is a literal field from the FAA Aircraft Registry. Click any value to open the FAA registry record for N816UA.

Tail Number

N816UA

Serial Number

0871

Make

AIRBUS INDUSTRIE

Model

A319-131

Year of Manufacture

1998

Mfr / Model Code

3930317

Type Aircraft

Fixed Wing Multi Engine

Type Engine

Turbo-jet

Engines

2

Seats

179

Engine Manufacturer

IAE

Engine Model

V2500SERIES

Horsepower

—

Weight Class

CLASS 3

Certification

Standard (+1 flag) · code 1T

Registrant

UNITED AIRLINES INC · Corporation

Address

ATTN: TREASURER WILLIS TOWER · 233 S WACKER DR · CHICAGO, IL 60606-7147

FAA Region

Central · County 031

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

AB2169

Mode S (Octal)

52620551

Live position via ICAO24 AB2169

ADS-B Exchange → FlightAware → FlightRadar24 →

External services. Live tracks are unaffiliated with TallyAero or the FAA.

02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to AIRBUS INDUSTRIE A319-131

Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.

  • Sep 11, 2003

    Airworthiness Directives; Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 Series Airplanes

    This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 series airplanes, that requires installing new anti-swivel plates and weights on the engine fan cowl door latches and a new hold-open device. This action is necessary to prevent separation of the eng…

    Atlas AD 03-22705 → Federal Register ↗

  • Nov 21, 2002

    Airworthiness Directives; Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 Series Airplanes

    This document revises an earlier proposed airworthiness directive (AD), applicable to certain Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 series airplanes, that would have required installing new anti-swivel plates and weights on the engine fan cowl door latches. This new action revises the proposed rule by adding airplan…

    Atlas AD 02-29679 → Federal Register ↗

  • Sep 4, 2001

    Airworthiness Directives; Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 Series Airplanes

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A319-131 and -132; A320-231, -232, and -233; and A321-131 and -231 series airplanes. This proposal would require installing new anti-swivel plates and weights on the engine fan cowl door latches. This action is necessary to prevent separation…

    Atlas AD 01-22091 → Federal Register ↗

  • Dec 8, 1999

    Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes

    This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319, A320, and A321 series airplanes, that requires a one-time inspection of the forward engine mount assembly of the left and right engines to verify that the part number on each assembly is correct; re-identification of the forward engine mount assembly; and foll…

    Atlas AD 99-31471 → Federal Register ↗

  • Oct 13, 1999

    Airworthiness Directives; Airbus Model A319-131, A320-232 and - 233, and A321-131 and -231 Series Airplanes

    This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319-131, A320-232 and -233, and A321-131 and -231 series airplanes, that requires replacement of all titanium thrust links with steel thrust links. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthi…

    Atlas AD 99-26274 → Federal Register ↗

  • Aug 4, 1999

    Airworthiness Directives; Airbus Model A319-131, A320-232 and - 233, and A321-131 and -231 Series Airplanes

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A319-131, A320-232 and -233, and A321-131 and -231 series airplanes. This proposal would require replacement of all titanium thrust links with steel thrust links. This proposal is prompted by issuance of mandatory continuing airworthiness inf…

    Atlas AD 99-20065 → Federal Register ↗

  • Nov 23, 1998

    Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A319, A320, and A321 series airplanes. This proposal would require a one-time inspection of the forward engine mount assembly of the left and right engines to verify that the part number on each assembly is correct; re- identification of the…

    Atlas AD 98-31177 → Federal Register ↗

04 /  Service Difficulty Reports

FAA SDR filings

The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →

05 /  Related

More on Airbus Industrie A319-131 in the Atlas

Airbus Industrie A319-131 type page → — 50 registered · 7 ADs · 6 NTSB records

Other Airbus Industrie A319-131 aircraft

N801UA N802UA N803UA N804UA N805UA N806UA N807UA N808UA

Recent NTSB events · this type

Search the full US registry → · All airworthiness directives → · Accident & safety surface →

06 /  Sources & Methodology

Every fact on this page links to its primary US-government source

We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.