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
Enstrom
Model
F-28C
Year
1978
Serial number
437
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H1CE
Mode S code
A7071C
Engine
Make and model
Lycoming Hio-360 Ser
Type
Reciprocating
Power
205 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
until 2012Individual ownerLongmont, CO
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
Nov 23, 2002 · Morrison, CO
the pilot not maintaining clearance from the telephone lines during landing. Factors contributing to the accident were the pilot not being able to see the telephone lines, the low altitude, and the dark night.
THE PILOT STATED THAT, 'I LANDED IN AN OPEN UNPOPULATED AREA FOR THE MECHANIC ... TO MAKE ADJUSTMENTS ON THE MAIN BLADE (WE WERE TRACKING AND BALANCING THE BLADES). I NEVER SHUT THE ENGINE DOWN. I DISENGAGED THE CLUTCH. AFTER THE ADJUSTMENT WAS MADE, I ENGAGED THE CLUTCH AND BROUGHT IT UP TO FULL POWER WITH ALL THE CHECKS BEFORE LIFTING OFF. EVERYTHING CHECKED OUT OK. I HAD LANDED INTO THE WIND…
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.
Airframe (F-28C)Only with: Helicopters with trim relay P/N KUP14D55-24, KUP14D55-472, M83536/10-015M, or M83536/10-024M installed; does not apply to helicopters with reversible trim motor P/N 28-16621 or P/N AD1R-10.
Airframe (F-28C)Only with: Helicopters with a trim relay P/N KUP14D55-472, M83536/10-015M, or M83536/10-024M installed; does not apply to helicopters with reversible trim motor P/N 28-16621 or AD1R-10.