N5781F

Substantial
None

Piper PA-28-140S/N: 28-25088

Accident Details

Date
Wednesday, August 28, 2002
NTSB Number
SEA02LA167
Location
Big Creek, ID
Event ID
20020904X01527
Coordinates
45.116664, -115.321662
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain directional control during the aborted takeoff. Factors include high density altitude, variable winds, and a ditch near the point where the aircraft departed the side of the runway.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-25088
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-140P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Country
United States

Analysis

On August 28, 2002, approximately 1650 mountain daylight time, a Piper PA-28-140, N5781F, impacted the terrain during an aborted takeoff from Big Creek Airport, Big Creek Lodge, Idaho. The private pilot and his passenger were not injured, but the aircraft, which is owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which was departing for McCall, Idaho, was being operated in visual meteorological conditions. No flight plan had been filed.

According to the pilot, during the takeoff roll, just as the main gear were lifting off, the aircraft seemed to lose lift and "dropped" back onto the runway surface. At that point, the pilot looked at the windsock at the far end of the runway and determined that it was indicating a tailwind. He therefore made the decision to abort, but as he tried to bring the aircraft to a stop, he was unable to maintain directional control and the aircraft departed the left side of the runway. After departing the runway, the aircraft's nose gear and right main gear entered a nearby drainage ditch, thus allowing the right wing to impact the terrain and sustain substantial damage.

Based on the ambient conditions of 70 degrees Fahrenheit and an altimeter setting of 30.20 inches of mercury, it was determined that the density altitude at the time of the attempted takeoff was approximately 7,550 feet.

According to the pilot, the engine seemed to be producing "peak power," and there were no indications that there had been any problem with the engine or the aircraft's systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA02LA167