20000927013989A

Accident · No damage

FAA accident report · Airtrc AT-602 · Rock Island, WA · September 27, 2000

Date
September 27, 2000 · 14:30 local
Place
Rock Island, WA
Operating rules
Agricultural (Part 137)
Operator
PXSG
Damage
No damage
Aircraft
N5111A
NTSB investigation
NTSBSEA00LA192
Reported as
Airtrc AT602

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) A/c struck static wire of high voltage transmission lines during aerial application operations. Pilot was conducting pullup manuever after swath run when line was encountered. Pilot indicated that he did overfly and review the area prior to application operations for this field but did not see this wire. Wire strick damage was primarily to the propellor, which immediately affected the pitch change mechanism for at least one blade. This resulted in a severe vibration aand loss of oil through the propellor hub. As pilot was no longer able to generate safe thrust through the propellor an emergency landing was affected, resulting in the eventual encounter with mature orchard trees, resulting in substantial damage to a/c

As the FAA filed it

(-23) A/C STRUCK STATIC WIRE OF HIGH VOLTAGE TRANSMISSION LINES DURING AERIAL APPLICATION OPERATIONS. PILOT WAS CONDUCTING PULLUP MANUEVER AFTER SWATH RUN WHEN LINE WAS ENCOUNTERED. PILOT INDICATED THAT HE DID OVERFLY AND REVIEW THE AREA PRIOR TO APPLICATION OPERATIONS FOR THIS FIELD BUT DID NOT SEE THIS WIRE. WIRE STRICK DAMAGE WAS PRIMARILY TO THE PROPELLOR, WHICH IMMEDIATELY AFFECTED THE PITCH CHANGE MECHANISM FOR AT LEAST ONE BLADE. THIS RESULTED IN A SEVERE VIBRATION AAND LOSS OF OIL THROUGH THE PROPELLOR HUB. AS PILOT WAS NO LONGER ABLE TO GENERATE SAFE THRUST THROUGH THE PROPELLOR AN EMERGENCY LANDING WAS AFFECTED, RESULTING IN THE EVENTUAL ENCOUNTER WITH MATURE ORCHARD TREES, RESULTING IN SUBSTANTIAL DAMAGE TO A/C

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 N5111A · 1

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