20050831023989A

Accident · Substantial damage

FAA accident report · Piper PA-22-150 · Davenport, WA · August 31, 2005

Date
August 31, 2005 · 18:40 local
Place
Davenport, WA
Airport
Davenport Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1829P
NTSB investigation
NTSBSEA05LA185
Reported as
Piper PA22150
People aboard
2
Fatal injuries
0
Pilot’s flight hours
215 total214 in this make and model60 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) Pilot reported that during landing roll-out, tail wheel shimmy became severe. Pilot could not maintain directional control. A/c departed runway during ensuing ground loop. A/c suffered damage to left wing spar, tail surfaces and aft fuselage twisted.

As the FAA filed it

(-23) PILOT REPORTED THAT DURING LANDING ROLL-OUT, TAIL WHEEL SHIMMY BECAME SEVERE. PILOT COULD NOT MAINTAIN DIRECTIONAL CONTROL. A/C DEPARTED RUNWAY DURING ENSUING GROUND LOOP. A/C SUFFERED DAMAGE TO LEFT WING SPAR, TAIL SURFACES AND AFT FUSELAGE TWISTED.

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 N1829P · 1

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