20010623033189I

Incident · Minor damage

FAA incident report · Piper PA-38-112 · Tablerock, MO · June 23, 2001

Date
June 23, 2001 · 09:30 local
Place
Tablerock, MO
Airport
Private
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2484G
Reported as
Piper PA38112
Reported engine
Lycoming O235*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
7,345 total750 in this make and model28 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) On June 23, 2001 at approximately 0930 hours local time, the pilot in command of a Piper tomahawk, PA-38-112, exited a Private airstrip at the departure end of the landing runway and proceeded to a designated parking area abeam a "fly-in" reception area. During the taxi phase, the front wheel descended into a small gopher hole whereupon, the propeller contacted the earth. The engine was secured immediately; an inspection of the propeller was performed. It was discovered that both tips of the propeller blades had sustained rock damage. No further damage was sustained.

As the FAA filed it

(-23) ON JUNE 23, 2001 AT APPROXIMATELY 0930 HOURS LOCAL TIME, THE PILOT IN COMMAND OF A PIPER TOMAHAWK, PA-38-112, EXITED A PRIVATE AIRSTRIP AT THE DEPARTURE END OF THE LANDING RUNWAY AND PROCEEDED TO A DESIGNATED PARKING AREA ABEAM A "FLY-IN" RECEPTION AREA. DURING THE TAXI PHASE, THE FRONT WHEEL DESCENDED INTO A SMALL GOPHER HOLE WHEREUPON, THE PROPELLER CONTACTED THE EARTH. THE ENGINE WAS SECURED IMMEDIATELY; AN INSPECTION OF THE PROPELLER WAS PERFORMED. IT WAS DISCOVERED THAT BOTH TIPS OF THE PROPELLER BLADES HAD SUSTAINED ROCK DAMAGE. NO FURTHER DAMAGE WAS SUSTAINED.

Other reports on N2484G · 1

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