19981028039839A

Accident · Destroyed

FAA accident report · Cessna 152 · Douglasville, GA · October 28, 1998

Date
October 28, 1998
Place
Douglasville, GA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N25037
NTSB investigation
NTSBMIA99LA019
Reported as
Cessna 152
Fatal injuries
0

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)Takeoff initiated a approximately 0830 hours from south fulton airport, pilot experienced a decrease in power, 2300 RPM to 1500 RPM then complete power loss. Approximately 60 feet from crash site, the horizontal stabilizer impacted a telephone pole approximately 3-4 inches from the top. Horizontal stab completed torn from aircraft and found at the base of the telephone pole. Aircraft turned left and crashed into a pile of railroad crossties in the middle of a pasture. The pilot and student exited the aircraft and the engine immediately caught on fire. The fuselage and engine incurred major fire damage. Left and right wings and the tail section did not incur fire damage but sustained major structural damage. The right wing impacted a small cow causing a fatal injury to the cow. Engine teardown completed on 10-29-98-N25037 incurred catastrophic failure of the #1 cylinder intake valve.

As the FAA filed it

(-23)TAKEOFF INITIATED A APPROXIMATELY 0830 HOURS FROM SOUTH FULTON AIRPORT, PILOT EXPERIENCED A DECREASE IN POWER, 2300 RPM TO 1500 RPM THEN COMPLETE POWER LOSS. APPROXIMATELY 60 FEET FROM CRASH SITE, THE HORIZONTAL STABILIZER IMPACTED A TELEPHONE POLE APPROXIMATELY 3-4 INCHES FROM THE TOP. HORIZONTAL STAB COMPLETED TORN FROM AIRCRAFT AND FOUND AT THE BASE OF THE TELEPHONE POLE. AIRCRAFT TURNED LEFT AND CRASHED INTO A PILE OF RAILROAD CROSSTIES IN THE MIDDLE OF A PASTURE. THE PILOT AND STUDENT EXITED THE AIRCRAFT AND THE ENGINE IMMEDIATELY CAUGHT ON FIRE. THE FUSELAGE AND ENGINE INCURRED MAJOR FIRE DAMAGE. LEFT AND RIGHT WINGS AND THE TAIL SECTION DID NOT INCUR FIRE DAMAGE BUT SUSTAINED MAJOR STRUCTURAL DAMAGE. THE RIGHT WING IMPACTED A SMALL COW CAUSING A FATAL INJURY TO THE COW. ENGINE TEARDOWN COMPLETED ON 10-29-98-N25037 INCURRED CATASTROPHIC FAILURE OF THE #1 CYLINDER INTAKE VALVE.

NTSB investigation

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