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Public Record · As of May 5, 2026

N561UP

Swearingen SA227-AT · 1983 View Type →

Status

Registration Valid

Type

Fixed Wing Multi Engine

Engine

AIRESEARCH TPE331 SERIES

Last Cert Issue

—

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 N561UP.

Tail Number

N561UP

Serial Number

AT-561

Make

SWEARINGEN

Model

SA227-AT

Year of Manufacture

1983

Mfr / Model Code

8780610

Type Aircraft

Fixed Wing Multi Engine

Type Engine

Turbo-prop

Engines

2

Seats

12

Engine Manufacturer

AIRESEARCH

Engine Model

TPE331 SERIES

Horsepower

904 hp

Weight Class

CLASS 2

Certification

Standard (+1 flag) · code 1N

Registrant

UAS TRANSERVICES INC · Corporation

Address

2000 NW CORPORATE BLVD · BOCA RATON, FL 33431-7304

FAA Region

7 · County 099

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

A72C71

Mode S (Octal)

51626161

Live position via ICAO24 A72C71

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02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to SWEARINGEN SA227-AT

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

  • Mar 4, 2016

    Airworthiness Directives; M7 Aerospace LLC Airplanes

    We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA26-AT, SA226-T(B), SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C- 26B), and SA227-TT airplanes. This AD was prompted by information that the airplane flight manual (AFM) does not provide adequate guidance in the handling of…

    Federal Register →

  • Aug 25, 2015

    Airworthiness Directives; M7 Aerospace LLC Airplanes

    We propose to adopt a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA26-AT, SA226-T, SA226-AT, SA226-T(B), SA226- TC, SA227-AT, SA227-TT, SA227-AC (C-26A), SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) airplanes. This proposed AD was prompted by information that the airplane flight manual (AFM) does not provide adequate guidance in th…

    Federal Register →

  • May 28, 2009

    Airworthiness Directives; M7 Aerospace LP Models SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) Airplanes

    We are adopting a new airworthiness directive (AD) to supersede AD 2008-12-16, which applies to certain M7 Aerospace LP SA226 and SA227 series airplanes. AD 2008-12-16 currently requires you to inspect wires and tube assemblies for chafing, arcing, or insufficient clearance between components. If chafing, arcing, or insufficient clearance between components…

    Federal Register →

  • Feb 12, 2009

    Airworthiness Directives; M7 Aerospace LP Models SA226-AT, SA226-T, SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B) Airplanes

    We propose to supersede Airworthiness Directive (AD) 2008-12- 16, which applies to certain M7 Aerospace LP SA226 and SA227 series airplanes. AD 2008-12-16 currently requires you to inspect wires and tube assemblies for chafing, arcing, or insufficient clearance between components. If chafing, arcing, or insufficient clearance between components is found, AD…

    Federal Register →

  • Jun 18, 2008

    Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

    We are adopting a new airworthiness directive (AD) for certain M7 Aerospace LP SA226 and SA227 series airplanes. This AD requires you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at all feed-through…

    Federal Register →

  • Mar 14, 2008

    Airworthiness Directives; M7 Aerospace LP SA226 and SA227 Series Airplanes

    We propose to adopt a new airworthiness directive (AD) for certain M7 Aerospace LP SA226 and SA227 series airplanes. This proposed AD would require you to inspect electrical wires/components, hydraulic and bleed air tube assemblies at left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas, LH/RH wing stations 51.167 to 81.174, and at…

    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 /  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.