19960711044029A

Accident · Substantial damage

FAA accident report · Hiller UH-12E · Cottondale, FL · July 11, 1996

Date
July 11, 1996 · 17:30 local
Place
Cottondale, FL
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N102HT
NTSB investigation
NTSBATL96LA104
Reported as
Hiller UH12E
Reported engine
Lycoming VO540C2A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
5,567 total77 in this make and model166 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Loud bang vibration on climbout. Lost tail rotor control. Impacted inverted main drive clutch and gimble failed.

As the FAA filed it

LOUD BANG VIBRATION ON CLIMBOUT. LOST TAIL ROTOR CONTROL. IMPACTED INVERTED MAIN DRIVE CLUTCH AND GIMBLE FAILED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N102HT · 1

Matched to the same aircraft by N-number and date.