20030515015319A

Accident · Destroyed

FAA accident report · Amtr RANS S9 · Green Cove Spr, FL · May 15, 2003

Date
May 15, 2003 · 19:40 local
Place
Green Cove Spr, FL
Airport
Haller Airpark Airport
Phase of flight
Takeoff
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N93WD
NTSB investigation
NTSBMIA03LA109
Reported as
Amtr RANSS9
Reported engine
HIRTH
Fatal injuries
0
Pilot’s flight hours
2,651 total80 in this make and model10 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) Witness, vince webster stated that around 1900-1930 Mr. Tower was seen taking off to the south from runway 18/36. At approximately 200 feet the aircraft lost power, continued to climb then turned left and crashed into an area of trees and thick underbrush approximately 400 feet to the left side of the runway. The aircraft appeared to descend straight down and land vertically, there was no indication of a glide path to the crash scene. The entire wreckage was contained within approximately a 20-foot diameter. Flight control continuity was normal and the engine rotated freely. Flight control continuity was checked by privacy data omitted and found to be satisfactory. privacy data omitted Also checked the engine for free rotation. The engine rotated freely and was not seized. June 30, 2003, the pilot stated that he lost power, possibly caused by a failure of the electronic ignition, or a failure of the fuel injector system.

As the FAA filed it

(-23) WITNESS, VINCE WEBSTER STATED THAT AROUND 1900-1930 MR. TOWER WAS SEEN TAKING OFF TO THE SOUTH FROM RUNWAY 18/36. AT APPROXIMATELY 200 FEET THE AIRCRAFT LOST POWER, CONTINUED TO CLIMB THEN TURNED LEFT AND CRASHED INTO AN AREA OF TREES AND THICK UNDERBRUSH APPROXIMATELY 400 FEET TO THE LEFT SIDE OF THE RUNWAY. THE AIRCRAFT APPEARED TO DESCEND STRAIGHT DOWN AND LAND VERTICALLY, THERE WAS NO INDICATION OF A GLIDE PATH TO THE CRASH SCENE. THE ENTIRE WRECKAGE WAS CONTAINED WITHIN APPROXIMATELY A 20-FOOT DIAMETER. FLIGHT CONTROL CONTINUITY WAS NORMAL AND THE ENGINE ROTATED FREELY. FLIGHT CONTROL CONTINUITY WAS CHECKED BY ^PRIVACY DATA OMITTED^ AND FOUND TO BE SATISFACTORY. ^PRIVACY DATA OMITTED^ ALSO CHECKED THE ENGINE FOR FREE ROTATION. THE ENGINE ROTATED FREELY AND WAS NOT SEIZED. JUNE 30, 2003, THE PILOT STATED THAT HE LOST POWER, POSSIBLY CAUSED BY A FAILURE OF THE ELECTRONIC IGNITION, OR A FAILURE OF THE FUEL INJECTOR SYSTEM.

NTSB investigation

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