20030609028529A

Accident · Destroyed

FAA accident report · Ayres S2R-G10 · Maricopa, AZ · June 9, 2003

Date
June 9, 2003 · 15:15 local
Place
Maricopa, AZ
Phase of flight
Normal Cruise
Operating rules
Agricultural (Part 137)
Operator
C80G
Damage
Destroyed
Aircraft
N6117X
NTSB investigation
NTSBLAX03LA188
Reported as
Ayres S2RG10
Reported engine
Garrett TPE33110
Fatal injuries
0
Pilot’s flight hours
8,200 total

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) While enroute to dispense fertilizer at a low altitude the aircraft struck the ground in a plowed field in the vicinity of Maricopa AZ. The pilot fred wordon indicated that he was dealing with a torque meter failure when the engine failed causing the aircraft to crash in the field. Inspection of the engine and all systems failed to find a cause of an engine failure, however the cause of the torque meter failure was determined to be a failed gasket on the combustion case directing hot gases against the torque meter cannon plug melting the solder and shorting the wires. The engine was torn down by Honeywell and determined to have been running at the time the engine struck the ground based on evaluation of deposits on the hot section components I.e. vanes and turbine blades. The failure of the torque meter and the pilots attention being drawn to resetting the circuit breaker twice in flight may have drawn his attention away from flying the aircraft. The aircraft was inspected at the air transport yard in phoenix on three different occasions and three evaluations by Honeywell were attended by FAA iic over a five month period.

As the FAA filed it

(-23) WHILE ENROUTE TO DISPENSE FERTILIZER AT A LOW ALTITUDE THE AIRCRAFT STRUCK THE GROUND IN A PLOWED FIELD IN THE VICINITY OF MARICOPA AZ. THE PILOT FRED WORDON INDICATED THAT HE WAS DEALING WITH A TORQUE METER FAILURE WHEN THE ENGINE FAILED CAUSING THE AIRCRAFT TO CRASH IN THE FIELD. INSPECTION OF THE ENGINE AND ALL SYSTEMS FAILED TO FIND A CAUSE OF AN ENGINE FAILURE, HOWEVER THE CAUSE OF THE TORQUE METER FAILURE WAS DETERMINED TO BE A FAILED GASKET ON THE COMBUSTION CASE DIRECTING HOT GASES AGAINST THE TORQUE METER CANNON PLUG MELTING THE SOLDER AND SHORTING THE WIRES. THE ENGINE WAS TORN DOWN BY HONEYWELL AND DETERMINED TO HAVE BEEN RUNNING AT THE TIME THE ENGINE STRUCK THE GROUND BASED ON EVALUATION OF DEPOSITS ON THE HOT SECTION COMPONENTS I.E. VANES AND TURBINE BLADES. THE FAILURE OF THE TORQUE METER AND THE PILOTS ATTENTION BEING DRAWN TO RESETTING THE CIRCUIT BREAKER TWICE IN FLIGHT MAY HAVE DRAWN HIS ATTENTION AWAY FROM FLYING THE AIRCRAFT. THE AIRCRAFT WAS INSPECTED AT THE AIR TRANSPORT YARD IN PHOENIX ON THREE DIFFERENT OCCASIONS AND THREE EVALUATIONS BY HONEYWELL WERE ATTENDED BY FAA IIC OVER A FIVE MONTH PERIOD.

NTSB investigation

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