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
Hughes
Model
269B
Year
1966
Serial number
106-0267
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
4H12
Mode S code
AD29AA
Engine
Make and model
Lycoming I0360 Ser
Type
Reciprocating
Power
180 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2007 – 2015Hrad Group LLCSalina, KS
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 (2)
Accident · substantial damage
May 3, 2006 · Sullivan, OH
Fatigue failure of the fuselage-to-tail boom cluster fitting, and the secondary failure of the tail rotor drive shaft. An additional cause was the incomplete compliance with an applicable Airworthiness Directive. A factor was the ditch.
THE PLT LANDED THE HELICOPTER IN A GRASSY AREA TO TALK TO A FRIEND. DURING DEPARTURE, HE FLEW OVER A CORN FIELD, & AT THAT TIME, AN EMPTY PAPER/PLASTIC CORN SEED SACK WAS DRAWN UP INTO THE MAIN ROTOR & A SEVERE VIBRATION BEGAN. HE THEN LANDED IN THE FIELD & SLID ABOUT 30 FT, THE SKIDS DUG INTO THE GROUND & THE HELICOPTER ROLLED OVER.
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.
Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters
May 8, 2002
Airframe (269B)Only with: With tailboom support strut assemblies P/N 269A2015 or 269A2015-5, tailboom center attach fitting P/N 269A2324, or center frame aft cluster fitting P/N 269A2234 or 269A2235 installed.