20051029025739A

Accident · Substantial damage

FAA accident report · Hughes 269C-1 · Titusville, FL · October 29, 2005

Date
October 29, 2005
Place
Titusville, FL
Airport
Space Center Executive Airport
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1567C
NTSB investigation
NTSBMIA06CA013
Reported as
Hughes 269C1
People aboard
2
Fatal injuries
0
Pilot’s flight hours
250 total175 in this make and model25 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.

(-23) privacy data omitted was acting as PIC of N1567C a H269C helicopter on 29 oct 2005. The pilot privacy data omitted was the applicant during an initial CFI helicopter practical test. The winds at the time of the accident were 020 at 12 KTS. The pilot privacy data omitted was executing a 180 degree touchdown autorotation. Mechanical fitting resulting in windshear was the causal factor in this accident. The investigation revealed a hard landing causing the main rotor blade to contact the boom and sever the boom forward of the tail rotor. privacy data omitted

As the FAA filed it

(-23) ^PRIVACY D^ WAS ACTING AS PIC OF N1567C A H269C HELICOPTER ON 29 OCT 2005. THE PILOT ^PRIVACY D^ WAS THE APPLICANT DURING AN INITIAL CFI HELICOPTER PRACTICAL TEST. THE WINDS AT THE TIME OF THE ACCIDENT WERE 020 AT 12 KTS. THE PILOT ^PRIVACY D^ WAS EXECUTING A 180 DEGREE TOUCHDOWN AUTOROTATION. MECHANICAL FITTING RESULTING IN WINDSHEAR WAS THE CAUSAL FACTOR IN THIS ACCIDENT. THE INVESTIGATION REVEALED A HARD LANDING CAUSING THE MAIN ROTOR BLADE TO CONTACT THE BOOM AND SEVER THE BOOM FORWARD OF THE TAIL ROTOR. ^PRIVACY DATA OMITTED^

NTSB investigation

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