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
208B
Serial number
208B0140
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
12
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A59C3B
Engine
Type
Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2006 – 2020Martinaire Aviation LLCAddison, TX
until 1955Cessna Aircraft CompanyWichita, KS · different airframe: Cessna 180 S/N 31500
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · destroyed
Dec 10, 2019 · Victoria, TX
The pilot’s loss of control due to spatial disorientation. Contributing to the accident were the inoperative attitude indicator and horizontal situation indicator on the pilot’s side of the cockpit, and the pilot’s failure to reference the flight instruments that were operative.
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.
Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…
May 12, 2008
Airframe (208B)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.
Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes
Jan 21, 1998
Airframe (208B)
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
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.
Fuselage · support · crackedDec 28, 2011
THE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · housing · damagedMay 12, 2008
BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONEIDION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Flight controls · bearing · corrodedMay 5, 2008
THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
Flight controls · bellcrank · corrodedMay 5, 2008
THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.