19970419006239A

Accident · Substantial damage

FAA accident report · Univar 1081 · Smithfield, NC · April 19, 1997

Date
April 19, 1997 · 13:20 local
Place
Smithfield, NC
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9063K
NTSB investigation
NTSBMIA97LA144
Reported as
Univar 1081
Reported engine
Franklin 6A4150B3
People aboard
1
Fatal injuries
0
Pilot’s flight hours
516 total92 in this make and model8 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.

Lost powr en route. Nosed over landing soft dirt field. Broken crankshaft. (-23) the aircraft departed a private strip (talton) at approximately 1300 EDT, 19 April 1997. This was a federal aviation regulation part 91 pleasure flight conducted in the local area. There were no passengers onboard. At approximately 1320 a reported engine failure caused the pilot to make an emergency landing in a recently plowed field. The aircraft rolled approximately 280 feet prior to the landing gear settling into the soft ground and flipping the aircraft onto its' back. Field inspection of the aircraft revealed that there was a crack in the engine block and the left engine mount broken away from the engine. At this time it is unclear if the engine block cracked in flight or if ground impact initiated the crack. There was no evidence of oil coming from the crack. The engine was hand propped approximately 8-12 inches after removing the right magneto cover and the #5 valve over. There was no motion detected in either the magneto or the valve train. This engine has a gear box located in the rear of the engine. This gear box drives the camshaft, both magnetos, tachometer, generator, and starter. A failure in this area could cause the engine to fail. The oil screen and fuel bowl were removed. There was no evidence of contamination in either. The pilot reported approximately 30 gallons of fuel on board. This engine has the automotive gas STC incorporated. The NTSB requested that a tear down be conducted. The owner can perform the tear down provided that an FAA inspector is present and that the NTSB or the FAA does not incur any charges for the tear down report. Other damage to the aircraft consisted of the vertical stabilizer being crushed, the left wing support struts bent, wheel pants damaged, engine cowling damaged, prop bent from ground impact, and other minor "cosmetic" damage.

As the FAA filed it

LOST POWR EN ROUTE. NOSED OVER LANDING SOFT DIRT FIELD. BROKEN CRANKSHAFT. (-23) THE AIRCRAFT DEPARTED A PRIVATE STRIP (TALTON) AT APPROXIMATELY 1300 EDT, 19 APRIL 1997. THIS WAS A FEDERAL AVIATION REGULATION PART 91 PLEASURE FLIGHT CONDUCTED IN THE LOCAL AREA. THERE WERE NO PASSENGERS ONBOARD. AT APPROXIMATELY 1320 A REPORTED ENGINE FAILURE CAUSED THE PILOT TO MAKE AN EMERGENCY LANDING IN A RECENTLY PLOWED FIELD. THE AIRCRAFT ROLLED APPROXIMATELY 280 FEET PRIOR TO THE LANDING GEAR SETTLING INTO THE SOFT GROUND AND FLIPPING THE AIRCRAFT ONTO ITS' BACK. FIELD INSPECTION OF THE AIRCRAFT REVEALED THAT THERE WAS A CRACK IN THE ENGINE BLOCK AND THE LEFT ENGINE MOUNT BROKEN AWAY FROM THE ENGINE. AT THIS TIME IT IS UNCLEAR IF THE ENGINE BLOCK CRACKED IN FLIGHT OR IF GROUND IMPACT INITIATED THE CRACK. THERE WAS NO EVIDENCE OF OIL COMING FROM THE CRACK. THE ENGINE WAS HAND PROPPED APPROXIMATELY 8-12 INCHES AFTER REMOVING THE RIGHT MAGNETO COVER AND THE #5 VALVE OVER. THERE WAS NO MOTION DETECTED IN EITHER THE MAGNETO OR THE VALVE TRAIN. THIS ENGINE HAS A GEAR BOX LOCATED IN THE REAR OF THE ENGINE. THIS GEAR BOX DRIVES THE CAMSHAFT, BOTH MAGNETOS, TACHOMETER, GENERATOR, AND STARTER. A FAILURE IN THIS AREA COULD CAUSE THE ENGINE TO FAIL. THE OIL SCREEN AND FUEL BOWL WERE REMOVED. THERE WAS NO EVIDENCE OF CONTAMINATION IN EITHER. THE PILOT REPORTED APPROXIMATELY 30 GALLONS OF FUEL ON BOARD. THIS ENGINE HAS THE AUTOMOTIVE GAS STC INCORPORATED. THE NTSB REQUESTED THAT A TEAR DOWN BE CONDUCTED. THE OWNER CAN PERFORM THE TEAR DOWN PROVIDED THAT AN FAA INSPECTOR IS PRESENT AND THAT THE NTSB OR THE FAA DOES NOT INCUR ANY CHARGES FOR THE TEAR DOWN REPORT. OTHER DAMAGE TO THE AIRCRAFT CONSISTED OF THE VERTICAL STABILIZER BEING CRUSHED, THE LEFT WING SUPPORT STRUTS BENT, WHEEL PANTS DAMAGED, ENGINE COWLING DAMAGED, PROP BENT FROM GROUND IMPACT, AND OTHER MINOR "COSMETIC" DAMAGE.

NTSB investigation

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

Other reports on N9063K · 1

Matched to the same aircraft by N-number and date.