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
Gulfstream Am Corp Comm Div
Model
690C
Year
1982
Serial number
11727
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
11
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
AB81B4
Engine
Make and model
Airesearch Tpe331 Series
Type
Turbo-prop
Power
904 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2000 – 2018Mid Kansas Agri CoPawnee Rock, KS
1937 – 1938Individual ownerBelzoni, MS · different airframe: Waco Aso S/N 3211
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
Feb 3, 2014 · Bellevue, TN
The pilot's failure to maintain airspeed with one engine inoperative, which resulted in a loss of control while on approach. Contributing to the accident were airframe ice accumulation due to conditions conducive to icing and the loss of engine power on one engine for reasons that could not be determined due to the extent of damage to the airplane.
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 (2)
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.
Propellers · lock · brokenNov 27, 2000
START-LOCK BROKE AND PIN FELL OUT BECAUSE RETAINING COTTER PIN WAS TOO WEAK. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Landing gear · clevis · failedJun 17, 1999
THE LEFT MAIN LANDING GEAR INBOARD RETRACT CYLINDER CLEVIS BROKE CAUSING THE LEFT MAIN GEAR TO COLLAPSE ON LANDING. THE LEFT GEAR INBOARD EXTENSION/RETRACTION ACTUATOR IS CONNECTED TO THIS RETRACT CYLINDER CLEVIS. THIS IS THE PHYSICAL CONNECTION BETWEEN THE ACTUATOR AND THE STRUT TO EXTEND AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.