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Aircraft record

N969WC2001 Estumkeda Ltd DBA Micco Acft MAC-145B

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply3 service difficulty reports

Registration
Valid
expires May 31, 2028
Based in
San Marcos, TX
owner city / state
Engine
IO-540 SER · 300 hp
Lycoming
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Texas State Aviation
Owner type
Corporation
City, state
San Marcos, TX
Certificate issued
May 6, 2015
Expires
May 31, 2028
Airworthiness
Standard · Utility, Acrobatic
Airworthiness date
Mar 8, 2002

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Estumkeda Ltd DBA Micco Acft
Model
MAC-145B
Year
2001
Serial number
260010
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AD7F8C

Engine

Make and model
Lycoming Io-540 Ser
Type
Reciprocating
Power
300 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2015 – nowTexas State AviationSan Marcos, TX · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (2)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2005-19-11Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360…Oct 21, 2005Engine (IO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999.
2004-05-24Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and…Mar 30, 2004Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Wings · strap · crackedMar 17, 2004

    DURING AN ANNUAL INSPECTION THE BUTT WELDS IN THE LOWER MAIN SPAR REINFORCEMENT STRAP, APPROX 3.25 INCHES IB FROM EACH END OF THE REINFORCEMENT STRAP, DO NOT HAVE PROPER PENETRATION AND ARE CRACKED THRU THE WELD. MFG WAS CONTACTED AND REPAIR INSTRUCTIONS WERE PROVIDED. THE WELDS WERE PROPERLY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · strap · crackedMar 17, 2004

    DURING AN ANNUAL INSPECTION THE BUTT WELDS IN THE LOWER MAIN SPAR REINFORCEMENT STRAP. APPROX 6.50 INCHES IB FROM EACH END OF THE REINFORCEMENT STRAP. DO NOT HAVE PROPER PENETRATION AND ARE CRACKED THRU THE WELD. MFG WAS CONTACTED AND REPAIR INSTRUCTIONS WERE PROVIDED. THE WELDS WERE PROPERLY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · attach bracket · crackedMar 17, 2004

    DURING AN ANNUAL INSPECTION THE WELD JOINT THAT ATTACHES THE UPPER WING SKIN ATTACH BRACKET TO THE UPPER MAIN WING SPAR CENTER SECTION JUST ABOVE THE UPPER LT WING ATTACHMENT FITTING WAS CRACKED. MANUFACTURER WAS CONTACTED AND REPAIR INSTRUCTIONS WERE PROVIDED. THE LT WING WAS REMOVED FOR ACCESS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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