N70P

Destroyed
Fatal

Paulick Wittman W-10S/N: 588

Accident Details

Date
Sunday, August 1, 2004
NTSB Number
SEA04LA152
Location
Langley, WA
Event ID
20040806X01162
Coordinates
48.018054, -122.438331
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's inadequate preflight preparation to assure adequate takeoff performance to clear obstacles, and his failure to maintain obstacle clearance.

Aircraft Information

Registration
N70P
Make
PAULICK
Serial Number
588
Engine Type
Reciprocating
Year Built
1991
Model / ICAO
Wittman W-10SA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HAGLER LOUIS A
Address
5636 SO LENZ
Status
Deregistered
City
LANGLEY
State / Zip Code
WA 98260
Country
United States

Analysis

On August 1, 2004, about 1030 Pacific daylight time, an experimental Paulick Wittman W-10, N70P, registered to and flown by the pilot as a 14 CFR Part 91 personal flight, collided with trees shortly after takeoff from Whidbey Air Park, Langley, Washington. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The aircraft was destroyed by impact damage and post-crash fire. The private pilot, the sole occupant, was fatally injured.

A witness reported that shortly after the aircraft took off from runway 16, the aircraft did not attain an altitude sufficient to clear trees. After the impact, a post-crash fire consumed the wreckage.

The pilot's flight logbook was not located for review. The Federal Aviation Administration Aero Medical Division reported that the pilot's last medical certificate, a Class III, was issued on February 3, 1999. At this time, the pilot reported a total flight time of 4,000 hours.

The wreckage was removed from the accident site and transported to the pilot's hangar at the airpark. Inspectors from the Seattle, Washington, Federal Aviation Administration Flight Standards District Office, reported that the engine displayed severe heat distress and impact damage. The crankcase was distorted, however, all connecting rods appeared to be connected to the crankshaft. The crankshaft would not turn. The oil pan was melted away. Both magnetos were heat distressed and their function could not be determined. The carburetor was destroyed. The fuel strainer and oil filter adapter assembly were intact, however, the lines to both were destroyed.

Control continuity to the elevator control system was established, however, damaged and heat distressed. The fuselage structure was heat distressed and the fabric covering was burned away.

Maintenance logbooks were not located for review.

The Island County Coroner's Office, Coupeville, Washington, conducted an autopsy. Dr. Andrea R. Capiola, Island County Deputy Coroner, reported that pilot's cause of death as: "Thermal burns" The coroner's report indicated an interview with the pilot's wife. During the interview, the Coroner learned that the pilot had experienced "a minor heart attack" about a year ago, but that since, the pilot was "in excellent health and was very lively." The pilot's wife reported that on the morning of the accident, he indicated to her that he was not planning on flying that day. The wife also indicated that the pilot was planning on selling the aircraft that was involved in the accident.

Toxicological samples were sent to the Federal Aviation Administration Civil Aeromedical Institute, Oklahoma City, Oklahoma, for analysis. The results of the analysis were positive for Metoprolol detected in blood and present in urine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA04LA152