20160823018029A

Accident · Substantial damage

FAA accident report · Simmons Noel SDL · Naches, WA · August 23, 2016

Date
August 23, 2016 · 14:30 local
Place
Naches, WA
Airport
Tieton State Airport
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N945PL
NTSB investigation
NTSBGAA16CA452
Reported as
Simmons Noel SDL
Reported engine
Lycoming I0360 EXP
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
364 total360 in this make and model47 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.

Airplane landed at Tieton State Airport (4S6). Pilot didn?t notice any adverse winds during approach and landing but anticipated that there was a possibility of afternoon mountain wind gusts. The pilot touched down softly and straight without a need for crosswind correction. During the landing roll the pilot applied normal brake pressure for directional control. The airplane ground looped to the right and as it skidded sideways the left gear collapsed, folding under the airplane allowing the left wing to impact the ground. Wing damage included rear spar and a number of ribs.

A determination was not made

As the FAA filed it

AIRPLANE LANDED AT TIETON STATE AIRPORT (4S6). PILOT DIDN?T NOTICE ANY ADVERSE WINDS DURING APPROACH AND LANDING BUT ANTICIPATED THAT THERE WAS A POSSIBILITY OF AFTERNOON MOUNTAIN WIND GUSTS. THE PILOT TOUCHED DOWN SOFTLY AND STRAIGHT WITHOUT A NEED FOR CROSSWIND CORRECTION. DURING THE LANDING ROLL THE PILOT APPLIED NORMAL BRAKE PRESSURE FOR DIRECTIONAL CONTROL. THE AIRPLANE GROUND LOOPED TO THE RIGHT AND AS IT SKIDDED SIDEWAYS THE LEFT GEAR COLLAPSED, FOLDING UNDER THE AIRPLANE ALLOWING THE LEFT WING TO IMPACT THE GROUND. WING DAMAGE INCLUDED REAR SPAR AND A NUMBER OF RIBS.

A DETERMINATION WAS NOT MADE

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.