20071016021459I

Incident · Minor damage

FAA incident report · Piper PA-28R-201T · Tooele, UT · October 16, 2007

Date
October 16, 2007 · 11:45 local
Place
Tooele, UT
Airport
Bolinder Field-Tooele Valley
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N3588M
Reported as
Piper PA28R201T
People aboard
2
Fatal injuries
0
Pilot’s flight hours
156 total3 in this make and model3 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 the third touch-and-go with flaps set at one notch and at landing flare, the pilot heard the prop ticking the runway, recognized that the landing gear had not been extended and immediately initiated a go-around by pitching up and applying power. The pilot flew a normal pattern, returned to the airport and landed without further incident. The pilot had no recollection of hearing the landing gear warning horn, but indicated that it functioned properly on the previous two approaches. The pilot stated that the extent of visible damage to the aircraft was limited to the last two inches of each propeller blade.

As the FAA filed it

(-23) ON THE THIRD TOUCH-AND-GO WITH FLAPS SET AT ONE NOTCH AND AT LANDING FLARE, THE PILOT HEARD THE PROP TICKING THE RUNWAY, RECOGNIZED THAT THE LANDING GEAR HAD NOT BEEN EXTENDED AND IMMEDIATELY INITIATED A GO-AROUND BY PITCHING UP AND APPLYING POWER. THE PILOT FLEW A NORMAL PATTERN, RETURNED TO THE AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. THE PILOT HAD NO RECOLLECTION OF HEARING THE LANDING GEAR WARNING HORN, BUT INDICATED THAT IT FUNCTIONED PROPERLY ON THE PREVIOUS TWO APPROACHES. THE PILOT STATED THAT THE EXTENT OF VISIBLE DAMAGE TO THE AIRCRAFT WAS LIMITED TO THE LAST TWO INCHES OF EACH PROPELLER BLADE.

Other reports on N3588M · 1

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