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Public Record · As of May 5, 2026

N69MA

Taylorcraft BC12-D View Type →

Status

Registration Valid

Type

Fixed Wing Single Engine

Engine

—

Last Cert Issue

—

Aircraft Resources

Search FAA TCDS for TAYLORCRAFT BC12-D → Type Club · Taylorcraft Aviation Association →

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 N69MA.

Tail Number

N69MA

Serial Number

6902

Make

TAYLORCRAFT

Model

BC12-D

Year of Manufacture

—

Mfr / Model Code

8850316

Type Aircraft

Fixed Wing Single Engine

Type Engine

Reciprocating

Engines

1

Seats

2

Engine Manufacturer

—

Engine Model

—

Horsepower

—

Weight Class

CLASS 1

Registrant

HALLAM CARSON S · Individual

Address

PO BOX 314 · WILLOW, AK 99688-0314

FAA Region

5 · County 170

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

A92971

Mode S (Octal)

52224561

Live position via ICAO24 A92971

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 TAYLORCRAFT BC12-D

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

  • May 2, 2008

    Airworthiness Directives; Taylorcraft, Inc. Models A, B, and F Series Airplanes

    The FAA adopts a new airworthiness directive (AD) for certain Taylorcraft, Inc. Models A, B, and F series airplanes. This AD requires you to inspect the wing strut attach fittings for corrosion or cracks and requires repair or replacement if corrosion or cracks are found. This AD results from data collected from an accident involving a Taylorcraft Model BF1…

    Federal Register →

  • Feb 22, 2008

    Airworthiness Directives; Taylorcraft A, B, and F Series Airplanes

    We are adopting a new airworthiness directive (AD) to supersede AD 2007-16-14, which applies to all Taylorcraft (Taylorcraft) A, B, and F series airplanes. AD 2007-16-14 currently requires you to do an initial visual inspection of the left and right wing front and aft lift struts for cracks and corrosion and replace any cracked strut or strut with corrosion…

    Federal Register →

  • Feb 20, 2008

    Airworthiness Directives; Taylorcraft Models A, B, and F Series Airplanes

    We propose to adopt a new airworthiness directive (AD) for certain Taylorcraft Models A, B, and F series airplanes. This proposed AD would require inspection of the wing strut attach fittings for corrosion or cracks and would require repair or replacement if corrosion or cracks are found. This proposed AD results from data collected from an accident involvi…

    Federal Register →

  • Dec 10, 2007

    Airworthiness Directives; Taylorcraft Aviation, LLC A, B, and F Series Airplanes

    We propose to supersede Airworthiness Directive (AD) AD 2007- 16-14, which applies to all Taylorcraft Aviation, LLC (Taylorcraft) A, B, and F series airplanes. AD 2007-16-14 currently requires you to do an initial visual inspection of the left and right wing front and aft lift struts for cracks and corrosion and replace any cracked strut or strut with corro…

    Federal Register →

  • Aug 13, 2007

    Airworthiness Directives; Taylorcraft A, B, and F Series Airplanes

    The FAA is adopting a new airworthiness directive (AD) for all Taylorcraft A, B, and F series airplanes. This AD requires you to initially inspect the left and right wing front and aft lift struts for corrosion and cracks, replace any cracked strut or strut with corrosion that exceeds certain limits with either sealed or non-sealed struts, and repetitively…

    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.