20000228004549A

Accident · Substantial damage

FAA accident report · Hughes TH-55 · Odessa, FL · February 28, 2000

Date
February 28, 2000 · 10:30 local
Place
Odessa, FL
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9518K
NTSB investigation
NTSBMIA00LA097
Reported as
Hughes TH55
Reported engine
Lycoming HIO360B1A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,592 total153 in this make and model19 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.

On February 29, 2000, at 1030 hrs. (EST), a Hughes 269 (TR55) helicopter owned by pasco county mosquito control and operated byprivacy data omittedcrashed helicopter into the ground during a practice autorotation on aerial observation flight. VFR flight conditions prevailed, and no flight plan was filed. The aircraft received substantial damage and the pilot received no injuries. The PIC holds a commercial certificate (asel/ with instrument and helicopter ratings. The flight originated at the pasco county mosquito control, Odessa, Florida at 0945 hrs. The accident was pilot induced by the pilot mismanaging the controls. (.4)on February 28, 2000, at about 1030 eastern standard time, a Hughes TH-55, N9518K, registered to pasco county mosquito control, operating as a 14 CFR part 91 training flight crashed during a training autorotation. Visual meteorological conditions prevailed and no flight plan was filed. The helicopter sustained substantial damage. The commercial pilot reported no injuries. The pilot departed from a private state heliport about 30 minutes before the accident. The pilot stated he was conducting an autorotation with tur n. he started his deceleration between 75 to 100 feet. The helicopter was not slowing down, he applied aft cyclic and the helicopter entered into a vertical rate of descent. Collective pitch was increased, the helicopter collided with the ground in a tail low attitude separating the tail boom, and rolled over on its right side.

As the FAA filed it

ON FEBRUARY 29, 2000, AT 1030 HRS. (EST), A HUGHES 269 (TR55) HELICOPTER OWNED BY PASCO COUNTY MOSQUITO CONTROL AND OPERATED BY^PRIVACY DATA O^CRASHED HELICOPTER INTO THE GROUND DURING A PRACTICE AUTOROTATION ON AERIAL OBSERVATION FLIGHT. VFR FLIGHT CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE AND THE PILOT RECEIVED NO INJURIES. THE PIC HOLDS A COMMERCIAL CERTIFICATE (ASEL/ WITH INSTRUMENT AND HELICOPTER RATINGS. THE FLIGHT ORIGINATED AT THE PASCO COUNTY MOSQUITO CONTROL, ODESSA, FLORIDA AT 0945 HRS. THE ACCIDENT WAS PILOT INDUCED BY THE PILOT MISMANAGING THE CONTROLS. (.4)ON FEBRUARY 28, 2000, AT ABOUT 1030 EASTERN STANDARD TIME, A HUGHES TH-55, N9518K, REGISTERED TO PASCO COUNTY MOSQUITO CONTROL, OPERATING AS A 14 CFR PART 91 TRAINING FLIGHT CRASHED DURING A TRAINING AUTOROTATION. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE. THE COMMERCIAL PILOT REPORTED NO INJURIES. THE PILOT DEPARTED FROM A PRIVATE STATE HELIPORT ABOUT 30 MINUTES BEFORE THE ACCIDENT. THE PILOT STATED HE WAS CONDUCTING AN AUTOROTATION WITH TUR N. HE STARTED HIS DECELERATION BETWEEN 75 TO 100 FEET. THE HELICOPTER WAS NOT SLOWING DOWN, HE APPLIED AFT CYCLIC AND THE HELICOPTER ENTERED INTO A VERTICAL RATE OF DESCENT. COLLECTIVE PITCH WAS INCREASED, THE HELICOPTER COLLIDED WITH THE GROUND IN A TAIL LOW ATTITUDE SEPARATING THE TAIL BOOM, AND ROLLED OVER ON ITS RIGHT SIDE.

NTSB investigation

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