19990516005179A

Accident · Substantial damage

FAA accident report · Amtr Titantornado · Monroe, CT · May 16, 1999

Date
May 16, 1999 · 07:40 local
Place
Monroe, CT
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N194PA
NTSB investigation
NTSBNYC99LA112
Reported as
Amtr Titantornado
Reported engine
ROTAX ROTAX583
Fatal injuries
0
Pilot’s flight hours
1,596 total450 in this make and model49 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.

Acft crashed into a residential area under unknown circumstances. (From .19) on may 16, 1999, about 0740 eastern daylight time, a homebuilt titan tornado, N194PA, was substantially damaged during a forced landing and collision with terrain in Monroe, Connecticut. The certificated private pilot was seriously injured. Visual meteorological conditions prevailed and no flight plan had been filed for the flight that departed the twin pine airport, pennington, new jersey, about 0610, destined for orange, Massachusetts. The personal flight was conducted under 14 CFR part 91. In an interview with a federal aviation administration (FAA) inspector, the pilot stated he was flying at 1,500 feet above the ground, when the airplane's engine sputtered for a second or two. The engine then lost total power. During the forced landing, the airplane's left wing contacted the ground and the airplane nosed over. The wreckage was examined by an FAA inspector. The fuel line which exited the fuel tank was severed, and approx. 1 pint of fuel remained in the fuel tank. The engine was primed, started, and run at the accident site. It ran for about 8 to 12 seconds before it stopped. Additionally, metallic particles were observed inside the engine crankcase. The engine will be examined further at a later date. (.4) on may 16, 1999, about 0740 eastern daylight time, a homebuilt titan tornado, N194PA, was substantially damaged during a forced landing and collision with terrain in Monroe, Connecticut. The certificated private pilot was seriously injured. Visual meteorological conditions prevailed and no flight plan had been filed for the flight that departed the twin pine airport, pennington, new jersey, about 0630, destined for the waterbury-oxford airport, oxford, Connecticut. The personal flight was conducted under 14 CFR part 91. The airplane was owned and built by the pilot. In a written statement, the pilot said he was flying at 1,500 feet above the ground, when the airplane's engine "missed" once and then lost total power. The pilot stated the airplane was too low to attempt a restart, and he established a glide for landing. During the forced landing, the airplane's left wing contacted the ground and the airplane nosed over. Examination of the wreckage by a federal aviation administration (FAA) inspector, revealed metallic particles inside the engine's crankcase. The engine was retained for further examination. The engine was reexamined on may 26, 1999, by an NTSB investigator, the FAA inspector, and a representative of the engine manufacturer. The examination revealed that the mag cylinder connecting rod bearing had failed. Additionally, the 2 cycle Rotax 583 engine had been manufactured as a snowmobile engine. (-23) forced landing in residential area due to sudden stoppage of engine.

As the FAA filed it

ACFT CRASHED INTO A RESIDENTIAL AREA UNDER UNKNOWN CIRCUMSTANCES. (FROM .19) ON MAY 16, 1999, ABOUT 0740 EASTERN DAYLIGHT TIME, A HOMEBUILT TITAN TORNADO, N194PA, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING AND COLLISION WITH TERRAIN IN MONROE, CONNECTICUT. THE CERTIFICATED PRIVATE PILOT WAS SERIOUSLY INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN HAD BEEN FILED FOR THE FLIGHT THAT DEPARTED THE TWIN PINE AIRPORT, PENNINGTON, NEW JERSEY, ABOUT 0610, DESTINED FOR ORANGE, MASSACHUSETTS. THE PERSONAL FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91. IN AN INTERVIEW WITH A FEDERAL AVIATION ADMINISTRATION (FAA) INSPECTOR, THE PILOT STATED HE WAS FLYING AT 1,500 FEET ABOVE THE GROUND, WHEN THE AIRPLANE'S ENGINE SPUTTERED FOR A SECOND OR TWO. THE ENGINE THEN LOST TOTAL POWER. DURING THE FORCED LANDING, THE AIRPLANE'S LEFT WING CONTACTED THE GROUND AND THE AIRPLANE NOSED OVER. THE WRECKAGE WAS EXAMINED BY AN FAA INSPECTOR. THE FUEL LINE WHICH EXITED THE FUEL TANK WAS SEVERED, AND APPROX. 1 PINT OF FUEL REMAINED IN THE FUEL TANK. THE ENGINE WAS PRIMED, STARTED, AND RUN AT THE ACCIDENT SITE. IT RAN FOR ABOUT 8 TO 12 SECONDS BEFORE IT STOPPED. ADDITIONALLY, METALLIC PARTICLES WERE OBSERVED INSIDE THE ENGINE CRANKCASE. THE ENGINE WILL BE EXAMINED FURTHER AT A LATER DATE. (.4) ON MAY 16, 1999, ABOUT 0740 EASTERN DAYLIGHT TIME, A HOMEBUILT TITAN TORNADO, N194PA, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING AND COLLISION WITH TERRAIN IN MONROE, CONNECTICUT. THE CERTIFICATED PRIVATE PILOT WAS SERIOUSLY INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN HAD BEEN FILED FOR THE FLIGHT THAT DEPARTED THE TWIN PINE AIRPORT, PENNINGTON, NEW JERSEY, ABOUT 0630, DESTINED FOR THE WATERBURY-OXFORD AIRPORT, OXFORD, CONNECTICUT. THE PERSONAL FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91. THE AIRPLANE WAS OWNED AND BUILT BY THE PILOT. IN A WRITTEN STATEMENT, THE PILOT SAID HE WAS FLYING AT 1,500 FEET ABOVE THE GROUND, WHEN THE AIRPLANE'S ENGINE "MISSED" ONCE AND THEN LOST TOTAL POWER. THE PILOT STATED THE AIRPLANE WAS TOO LOW TO ATTEMPT A RESTART, AND HE ESTABLISHED A GLIDE FOR LANDING. DURING THE FORCED LANDING, THE AIRPLANE'S LEFT WING CONTACTED THE GROUND AND THE AIRPLANE NOSED OVER. EXAMINATION OF THE WRECKAGE BY A FEDERAL AVIATION ADMINISTRATION (FAA) INSPECTOR, REVEALED METALLIC PARTICLES INSIDE THE ENGINE'S CRANKCASE. THE ENGINE WAS RETAINED FOR FURTHER EXAMINATION. THE ENGINE WAS REEXAMINED ON MAY 26, 1999, BY AN NTSB INVESTIGATOR, THE FAA INSPECTOR, AND A REPRESENTATIVE OF THE ENGINE MANUFACTURER. THE EXAMINATION REVEALED THAT THE MAG CYLINDER CONNECTING ROD BEARING HAD FAILED. ADDITIONALLY, THE 2 CYCLE ROTAX 583 ENGINE HAD BEEN MANUFACTURED AS A SNOWMOBILE ENGINE. (-23) FORCED LANDING IN RESIDENTIAL AREA DUE TO SUDDEN STOPPAGE OF ENGINE.

NTSB investigation

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