20040814018929A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Irby, WA · August 14, 2004

Date
August 14, 2004 · 09:00 local
Place
Irby, WA
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4195J
NTSB investigation
NTSBSEA04LA161
Reported as
Piper PA28140
Reported engine
Lycoming O320E2A
Fatal injuries
0
Pilot’s flight hours
435 total300 in this make and model10 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) The pilot stated that on the second attempt to land at his private east-west airstrip near Irby, WA he made a decision to go around and the engine did not respond when the throttle was advanced. The aircraft ended up on a path of approximately 230 degrees descending into a gully on the south side of the airstrip. Due to ground contact, the aircraft lost the r/h main landing gear, nose gear, and miscellaneous fairings. The aircraft slid approx. 34 yards, rotating to a northerly heading and contacting a tree at the intersection of the l/h wing and aft fuselage. No mechanical damage was noted with the engine and the propeller was bent, the propeller damage did not show signs of power at the time of impact. The engine was fitted with a suitable propeller and was ground run at the salvage yard with no defects noted.

As the FAA filed it

(-23) THE PILOT STATED THAT ON THE SECOND ATTEMPT TO LAND AT HIS PRIVATE EAST-WEST AIRSTRIP NEAR IRBY, WA HE MADE A DECISION TO GO AROUND AND THE ENGINE DID NOT RESPOND WHEN THE THROTTLE WAS ADVANCED. THE AIRCRAFT ENDED UP ON A PATH OF APPROXIMATELY 230 DEGREES DESCENDING INTO A GULLY ON THE SOUTH SIDE OF THE AIRSTRIP. DUE TO GROUND CONTACT, THE AIRCRAFT LOST THE R/H MAIN LANDING GEAR, NOSE GEAR, AND MISCELLANEOUS FAIRINGS. THE AIRCRAFT SLID APPROX. 34 YARDS, ROTATING TO A NORTHERLY HEADING AND CONTACTING A TREE AT THE INTERSECTION OF THE L/H WING AND AFT FUSELAGE. NO MECHANICAL DAMAGE WAS NOTED WITH THE ENGINE AND THE PROPELLER WAS BENT, THE PROPELLER DAMAGE DID NOT SHOW SIGNS OF POWER AT THE TIME OF IMPACT. THE ENGINE WAS FITTED WITH A SUITABLE PROPELLER AND WAS GROUND RUN AT THE SALVAGE YARD WITH NO DEFECTS NOTED.

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 N4195J · 1

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