Skip to content
KnownTail
Aircraft record

N744HWaco CTO

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:1 NTSB accident (substantial damage, Mar 2016)No ADs since 1998 matched1 service difficulty report

Registration
Valid
expires Feb 28, 2031
Based in
Breckenridge, TX
owner city / state
Engine
760E-2 · 350 hp
Wright
Owners
1
since 2024
NTSB events
1
substantial, 2016
ADs may apply
0
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Individual owner
City, state
Breckenridge, TX
Certificate issued
Feb 15, 2024
Expires
Feb 28, 2031
Airworthiness
Standard · Normal
Airworthiness date
Jun 19, 1986

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
Waco
Model
CTO
Serial number
A-95
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AA0215

Engine

Make and model
Wright 760e-2
Type
Reciprocating
Power
350 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. 2024 – nowIndividual ownerBreckenridge, 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 (1)

Accident · substantial damage

Mar 29, 2016 · Ridgeland, SC

The pilot's failure to maintain directional control during the landing roll, which resulted in a ground loop.

Damage
Substantial
Injuries
None
Report
GAA16CA170

From NTSB records; matched by serial number.Read NTSB report (search CAROL for GAA16CA170)

Accident history for this model

ADs published since 1998 that may apply (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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

Service Difficulty Reports (1)

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.

  • Landing gear · bolt · shearedMar 29, 2016

    UPON LANDING, THE LT MAIN GEAR ATTACHING POINT BOLT SHEARED CAUSING THE LT MLG TO FOLD UNDER THE AIRCRAFT. A VISUAL INSPECTION REVEALED THAT THE LT TRAILING GEAR ATTACHING POINT HOLE THAT CONNECTS TO THE FUSELAGE WAS ELONGATED CAUSING ADDITIONAL STRESS ON THE BOLT AND ITS SUDSEQUENT FAILURE. DUE…

    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

Request owner name removalReport an error in this record