20080710839869A

Accident · Destroyed

FAA accident report · Scwzer G-164B · Patterson, CA · July 10, 2008

Date
July 10, 2008 · 05:25 local
Place
Patterson, CA
Phase of flight
Low Level Operations
Operating rules
Agricultural (Part 137)
Operator
RQEG
Damage
Destroyed
Aircraft
N6792Q
NTSB investigation
NTSBLAX08CA223
Reported as
Scwzer G164B
Fatal injuries
0
Pilot’s flight hours
11,150 total10,000 in this make and model144 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.

(-23) At the beginning of the first spray pass on a field (melons) the pilot noticed a electrical power line going from a high voltage feed line to a irrigation well pump that bordered the approach end of the field. The pilot attempted to pull up over the line but contacted a wood power pole with the aircraft (engine). Damage to the engne and propeller precluded the possiblity of the aircraft being able to maintain flight. The aircraft struck the ground with the left wing tip in the field, turned approximately 180 degrees in direction and came to rest right side up. The fuselage of the aircraft burned to a point just behind the cockpit. Section 21A is blank due no technical factors for this accident.

As the FAA filed it

(-23) AT THE BEGINNING OF THE FIRST SPRAY PASS ON A FIELD (MELONS) THE PILOT NOTICED A ELECTRICAL POWER LINE GOING FROM A HIGH VOLTAGE FEED LINE TO A IRRIGATION WELL PUMP THAT BORDERED THE APPROACH END OF THE FIELD. THE PILOT ATTEMPTED TO PULL UP OVER THE LINE BUT CONTACTED A WOOD POWER POLE WITH THE AIRCRAFT (ENGINE). DAMAGE TO THE ENGNE AND PROPELLER PRECLUDED THE POSSIBLITY OF THE AIRCRAFT BEING ABLE TO MAINTAIN FLIGHT. THE AIRCRAFT STRUCK THE GROUND WITH THE LEFT WING TIP IN THE FIELD, TURNED APPROXIMATELY 180 DEGREES IN DIRECTION AND CAME TO REST RIGHT SIDE UP. THE FUSELAGE OF THE AIRCRAFT BURNED TO A POINT JUST BEHIND THE COCKPIT. SECTION 21A IS BLANK DUE NO TECHNICAL FACTORS FOR THIS ACCIDENT.

NTSB investigation

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