20200419004179I

Incident · Minor damage

FAA incident report · Aeronca 7AC · Mulino, OR · April 19, 2020

Date
April 19, 2020 · 15:20 local
Place
Mulino, OR
Airport
Mulino State
Phase of flight
Ground/Ramp/Ma
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N82278
Reported as
Aeronca 7AC
Reported engine
Continental A&C65 series
People aboard
0
Fatal injuries
0
Other 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.

While outside the aircraft, the aircraft owner rotated the propeller by hand in the opposite direction of normal rotation in an attempt to clear a perceived flooded-engine condition. Upon the fourth or fifth rotation, the owner stated the engine started and went to the full RPM. With no occupants onboard, the aircraft moved across the airport ramp, momentarily going airborne before the engine shut down. The aircraft set down on the taxiway, struck a taxi light with the main landing gear and struck the ground with the wing tip. The aircraft came to rest after rotating 180 degrees in the grass on the adjacent taxiway. Aircraft records reviewed during the post-incident investigation indicated the mixture control was previously wired in the ?full rich? Position and the control marked inop. A post-incident interview with the owner indicated the aircraft engine is shut down after each flight utilizing the magneto switch.

As the FAA filed it

WHILE OUTSIDE THE AIRCRAFT, THE AIRCRAFT OWNER ROTATED THE PROPELLER BY HAND IN THE OPPOSITE DIRECTION OF NORMAL ROTATION IN AN ATTEMPT TO CLEAR A PERCEIVED FLOODED-ENGINE CONDITION. UPON THE FOURTH OR FIFTH ROTATION, THE OWNER STATED THE ENGINE STARTED AND WENT TO THE FULL RPM. WITH NO OCCUPANTS ONBOARD, THE AIRCRAFT MOVED ACROSS THE AIRPORT RAMP, MOMENTARILY GOING AIRBORNE BEFORE THE ENGINE SHUT DOWN. THE AIRCRAFT SET DOWN ON THE TAXIWAY, STRUCK A TAXI LIGHT WITH THE MAIN LANDING GEAR AND STRUCK THE GROUND WITH THE WING TIP. THE AIRCRAFT CAME TO REST AFTER ROTATING 180 DEGREES IN THE GRASS ON THE ADJACENT TAXIWAY. AIRCRAFT RECORDS REVIEWED DURING THE POST-INCIDENT INVESTIGATION INDICATED THE MIXTURE CONTROL WAS PREVIOUSLY WIRED IN THE ?FULL RICH? POSITION AND THE CONTROL MARKED INOP. A POST-INCIDENT INTERVIEW WITH THE OWNER INDICATED THE AIRCRAFT ENGINE IS SHUT DOWN AFTER EACH FLIGHT UTILIZING THE MAGNETO SWITCH.

Other reports on N82278 · 1

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