19970815022579A

Accident · Substantial damage

FAA accident report · Airtrc AT-301 · Waynesboro, GA · August 15, 1997

Date
August 15, 1997 · 21:30 local
Place
Waynesboro, GA
Airport
Burke County Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N4411S
NTSB investigation
NTSBMIA97LA233
Reported as
Airtrc AT301
Reported engine
Pratt & Whitney R1340AN1
People aboard
1
Fatal injuries
0
Pilot’s flight hours
12,888 total2,000 in this make and model750 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.

Aircraft engine failed during aerial application and aircraft crashed and flipped over. (.4)after completion of spray application while returning to the departure airport, the engine experienced a partial loss of power and engine oil began covering the windscreen. The pilot initiated a forced landing on a road but during the landing roll, the airplane drifted off the road into a ditch and nosed over. Examination of the engine revealed that the head of the no. 1 cylinder was cracked from one spark plug hole to the other. (-23) engine loss power after takeoff. Aircraft made forced landing into field. Aircraft sustained substantial damage. Investigation revealed that the #1 cylinder (p/n 399359, cylinder head split from spark plug hole to spark plug hole. M & d report submitted & safety recommendation initiated.

As the FAA filed it

AIRCRAFT ENGINE FAILED DURING AERIAL APPLICATION AND AIRCRAFT CRASHED AND FLIPPED OVER. (.4)AFTER COMPLETION OF SPRAY APPLICATION WHILE RETURNING TO THE DEPARTURE AIRPORT, THE ENGINE EXPERIENCED A PARTIAL LOSS OF POWER AND ENGINE OIL BEGAN COVERING THE WINDSCREEN. THE PILOT INITIATED A FORCED LANDING ON A ROAD BUT DURING THE LANDING ROLL, THE AIRPLANE DRIFTED OFF THE ROAD INTO A DITCH AND NOSED OVER. EXAMINATION OF THE ENGINE REVEALED THAT THE HEAD OF THE NO. 1 CYLINDER WAS CRACKED FROM ONE SPARK PLUG HOLE TO THE OTHER. (-23) ENGINE LOSS POWER AFTER TAKEOFF. AIRCRAFT MADE FORCED LANDING INTO FIELD. AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. INVESTIGATION REVEALED THAT THE #1 CYLINDER (P/N 399359, CYLINDER HEAD SPLIT FROM SPARK PLUG HOLE TO SPARK PLUG HOLE. M & D REPORT SUBMITTED & SAFETY RECOMMENDATION INITIATED.

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 N4411S · 3

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