Casualties unknown

1999-05-08: Beech 36 (N6222V) — Portland, OR

Portland, OR, US

On May 8, 1999, a Beech 36 (registration N6222V) was involved in an aviation accident near Portland, OR. Investigators recorded the probable cause as: Improper installation of the strobe light system. Factors include a leak in the fuel bladder and electrical arcing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

During takeoff, a loud explosion and left yaw led to a runway excursion. Post-incident examination revealed fuel bladder damage, preexisting holes, and improperly installed strobe light wiring with chafing and arcing.

Event Description

During the takeoff roll, the pilot heard a loud explosion and the aircraft violently yawed to the left. The aircraft veered off the runway and came to rest in a grassy area between the runway and the taxiway.

Fuel System Examination

Examination of the aircraft's fuel system revealed evidence of a preexisting fuel leak. Blue streaking and staining, consistent in color with 100 low lead aviation fuel, was noted on the ventral surfaces of the aircraft. Examination of the aircraft's fuel bladder revealed that the plastic interconnect nipple for the vent line, and the plastic interconnect nipple for the fuel return line, located at the distal end of the aircraft's fuel bladder, were fractured. Further examination of the fuel bladder revealed approximately 20 preexisting holes in the bladder's fabric.

Strobe Light System Examination

The aircraft's maintenance logbook indicated that the aircraft was equipped with a strobe light kit. Examination of the strobe light system revealed that the installation of the strobe kit was not in accordance with the manufacturer's installation instructions. Instead, the wiring harness for the strobe light was routed parallel to a stringer, between the wing ribs and the skin of the aircraft. Examination of the wiring revealed that the wire's insulation was chafed, cut, and discolored. The discoloration of the wiring was indicative of arcing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18883. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.