20110317009549A

Accident · Substantial damage

FAA accident report · Hiller UH-12D · Iowa, LA · March 17, 2011

Date
March 17, 2011 · 11:30 local
Place
Iowa, LA
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N11CU
NTSB investigation
NTSBCEN11CA231
Reported as
Hiller UH-12D
Reported engine
Lycoming VO-435 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
406 total81 in this make and model7 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.

It was determined the aircraft entered a dynamic roll over after hard contact with the landing surface occurred. It is believed, the aircraft was subjected to an unanticipated gust of tail wind causing loss of tail rotor effectiveness (lte). It was further determined that neither a flight control continuity nor airworthiness check was conducted leaving an open question of possible mitigating airworthiness issues. Due to the findings of this secondary investigation it was decided to change the FAA recommendation to airman counseling vs a 44709. This now completed airman counseling included methods for wind direction determination via pilot observation techniques during all phases of flight. Which when covered, the airman stated these techniques were new to him and he was most appreciative of the counseling session.

As the FAA filed it

IT WAS DETERMINED THE AIRCRAFT ENTERED A DYNAMIC ROLL OVER AFTER HARD CONTACT WITH THE LANDING SURFACE OCCURRED. IT IS BELIEVED, THE AIRCRAFT WAS SUBJECTED TO AN UNANTICIPATED GUST OF TAIL WIND CAUSING LOSS OF TAIL ROTOR EFFECTIVENESS (LTE). IT WAS FURTHER DETERMINED THAT NEITHER A FLIGHT CONTROL CONTINUITY NOR AIRWORTHINESS CHECK WAS CONDUCTED LEAVING AN OPEN QUESTION OF POSSIBLE MITIGATING AIRWORTHINESS ISSUES. DUE TO THE FINDINGS OF THIS SECONDARY INVESTIGATION IT WAS DECIDED TO CHANGE THE FAA RECOMMENDATION TO AIRMAN COUNSELING VS A 44709. THIS NOW COMPLETED AIRMAN COUNSELING INCLUDED METHODS FOR WIND DIRECTION DETERMINATION VIA PILOT OBSERVATION TECHNIQUES DURING ALL PHASES OF FLIGHT. WHICH WHEN COVERED, THE AIRMAN STATED THESE TECHNIQUES WERE NEW TO HIM AND HE WAS MOST APPRECIATIVE OF THE COUNSELING SESSION.

NTSB investigation

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