19970827024189A

Accident · Destroyed

FAA accident report · Amtr GENESIS · Columbia Statio, OH · August 27, 1997

Date
August 27, 1997 · 19:50 local
Place
Columbia Statio, OH
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9091B
NTSB investigation
NTSBNYC97LA171
Reported as
Amtr Genesis
People aboard
1
Fatal injuries
1

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.

Lost power and crashed. Investigation underway. Observed low level engine sputtering. (-23) the aircraft had impacted the soybean field at about a 30 degree angle nose down wings were level. The airspeed indicator was stuck at 80 mph. Hobbs meter reading was 54.8 hrs. Voltmeter reading stuck at 10V. The propeller (wooden) was broken off at both blades, one at mid span and one at outer midspan. The cockpit area was severely damaged by the engine assy. Most instruments unreadable at this time. The tail section of the aircraft was broken off at the frame and laying directly behind the engine compartment. The rudder and elevator were not damaged severely and the flight control hinge points were intact and secure. The main wings were damaged to include the struts. Ailerons were intact and hinges secure. There were three fuel tanks, one in each wing and a aux tank just below the engine compartment. The wing tanks had 1/4 fuel l/h and 1/8 fuel r/h. aux tank could not be determined at this time. There was fuel in the line below the inline fuel filter and very little in the filter bowl itself. This line was positio ned below the aux tank. All witness statements reveal that the aircraft was at tree top level or above and one witness statement indicated just above tree top level at about 200 feet. One witness indicated that he heard the engine sputter and then a "boom" he assumed to be the impact. He was in his garage and did not see the aircraft but distinctively heard the noises.

As the FAA filed it

LOST POWER AND CRASHED. INVESTIGATION UNDERWAY. OBSERVED LOW LEVEL ENGINE SPUTTERING. (-23) THE AIRCRAFT HAD IMPACTED THE SOYBEAN FIELD AT ABOUT A 30 DEGREE ANGLE NOSE DOWN WINGS WERE LEVEL. THE AIRSPEED INDICATOR WAS STUCK AT 80 MPH. HOBBS METER READING WAS 54.8 HRS. VOLTMETER READING STUCK AT 10V. THE PROPELLER (WOODEN) WAS BROKEN OFF AT BOTH BLADES, ONE AT MID SPAN AND ONE AT OUTER MIDSPAN. THE COCKPIT AREA WAS SEVERELY DAMAGED BY THE ENGINE ASSY. MOST INSTRUMENTS UNREADABLE AT THIS TIME. THE TAIL SECTION OF THE AIRCRAFT WAS BROKEN OFF AT THE FRAME AND LAYING DIRECTLY BEHIND THE ENGINE COMPARTMENT. THE RUDDER AND ELEVATOR WERE NOT DAMAGED SEVERELY AND THE FLIGHT CONTROL HINGE POINTS WERE INTACT AND SECURE. THE MAIN WINGS WERE DAMAGED TO INCLUDE THE STRUTS. AILERONS WERE INTACT AND HINGES SECURE. THERE WERE THREE FUEL TANKS, ONE IN EACH WING AND A AUX TANK JUST BELOW THE ENGINE COMPARTMENT. THE WING TANKS HAD 1/4 FUEL L/H AND 1/8 FUEL R/H. AUX TANK COULD NOT BE DETERMINED AT THIS TIME. THERE WAS FUEL IN THE LINE BELOW THE INLINE FUEL FILTER AND VERY LITTLE IN THE FILTER BOWL ITSELF. THIS LINE WAS POSITIO NED BELOW THE AUX TANK. ALL WITNESS STATEMENTS REVEAL THAT THE AIRCRAFT WAS AT TREE TOP LEVEL OR ABOVE AND ONE WITNESS STATEMENT INDICATED JUST ABOVE TREE TOP LEVEL AT ABOUT 200 FEET. ONE WITNESS INDICATED THAT HE HEARD THE ENGINE SPUTTER AND THEN A "BOOM" HE ASSUMED TO BE THE IMPACT. HE WAS IN HIS GARAGE AND DID NOT SEE THE AIRCRAFT BUT DISTINCTIVELY HEARD THE NOISES.

NTSB investigation

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