Skip to content
KnownTail
Aircraft record

N911571969 Cessna 207

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jun 2023)3 ADs may apply1 service difficulty report

Registration
Valid
expires Jan 31, 2028
Based in
Harlingen, TX
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
since 2007
NTSB events
2
substantial, 2023
ADs may apply
3
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
Garza Aircraft INC
Owner type
Corporation
City, state
Harlingen, TX
Certificate issued
Aug 14, 2007
Expires
Jan 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
May 27, 1969

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
Cessna
Model
207
Year
1969
Serial number
20700096
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AC9D89

Engine

Make and model
Cont Motor Io 520 Series
Type
Reciprocating
Power
285 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. 2007 – nowGarza Aircraft INCHarlingen, TX · current
  2. 1952 – 1954Individual ownerSheboygan, WI · different airframe: North American Navion S/N Nav453

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (2)

Accident · substantial damage

Jun 6, 2023 · Harlingen, TX

The improper installation of the throttle control arm to the throttle control cable attachment end, which resulted in a failure of the control arm and a loss of engine power in flight.

Damage
Substantial
Injuries
None
Report
CEN23LA231

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN23LA231)

Accident · substantial damage

Sep 18, 1985 · Chuathbaluk, AK

THE ACFT MADE AN EMERGENCY LANDING IN A RIVER AFTER AN ENG FAILURE DUE TO FUEL EXHAUSTION. THE PLT STATED THAT HE COULD NOT DETERMINE EXACT FUEL QUANTITY PRIOR TO TAKEOFF DUE TO A BROKEN CAP ON RIGHT FUEL TANK. THE OPERATOR TOLD THE PLT TO FLY THE ACFT DESPITE HIS KNOWLEDGE OF THE BROKEN FUEL CAP AND THE UNCERTAIN FUEL QUANTITY.

Damage
Substantial
Injuries
None
Report
ANC85LA179

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC85LA179)

Accident history for this model

ADs published since 1998 that may apply (3)

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
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (207)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.
2008-10-02Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…May 12, 2008Airframe (207)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007.

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.

  • Engine controls · throttle arm · failedJun 6, 2023

    FAA ONSITE EXAMINATION OF THE ENGINE INSTALLATION FOUND THAT THE ENGINES (BRONZE) LEVER-THROTTLE CONTROL DISCONNECTED FROM THE AIRCRAFT CONTROL THROTTLE ROD END. THIS RESULTED IN LOSS OF THROTTLE CONTROL FROM THE COCKPIT. INCORRECT INSTALLATION: THE AIRCRAFT HAS A BRONZE THROTTLE ARM LEVER…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

Request owner name removalReport an error in this record