2 fatalities

31 Mar 2012: PIPER PA-18 (N7276D) — RICHARD I. WILMARTH — Sleetmute, AK

Sleetmute, AK, United States

On 31 Mar 2012, a PIPER PA-18 (registration N7276D) operated by RICHARD I. WILMARTH was involved in an aviation accident near Sleetmute, AK. 2 people were killed. Investigators recorded the probable cause as: Operation of the airplane by a non-certificated pilot and his failure to maintain adequate airspeed and airplane control, which resulted in an aerodynamic stall. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On March 30, 2012, a ski-equipped Piper PA-18 (N7276D) collided with trees and terrain during landing near Sleetmute, Alaska. The uncertificated pilot and passenger sustained fatal injuries. A witness observed a loss of control during approach.

History of Flight

On March 30, 2012, about 1708 Alaska daylight time, a ski-equipped Piper PA-18 airplane, N7276D, sustained substantial damage when it collided with trees and snow-covered terrain following a loss of control while landing. The accident occurred about 26 miles south of Sleetmute, Alaska. The airplane was being operated as a visual flight rules (VFR) cross-country personal flight under Title 14, CFR Part 91. The uncertificated pilot and the one passenger both sustained fatal injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The accident flight originated at the Sleetmute Airport at an unknown time.

During a telephone interview with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on November 6, a witness and personal friend of the uncertificated pilot and passenger reported that the airplane was being used to shuttle fuel and camping supplies to a remote cabin on the banks of the Holitna River. He said that before the airplane arrived, he and another friend used snow machines to pack down a makeshift landing site on the frozen, snow-covered river. After the uncertificated pilot finished transporting all of the fuel and supplies, he and the passenger departed the site to check the condition of the river ice upstream. About 30 minutes later, the witness saw the airplane flying towards the makeshift site, flying low and slow over the treetops as it approached. He said that as the airplane flew towards the landing site threshold, it began a slight right turn, then nosed down abruptly, and he heard the engine speed increase to a very high rpm setting. The airplane descended, nose down, in a near vertical attitude, and began a 3/4 spiral turn downward, before descending from view into the trees at the approach end of the site. The airplane collided with snow and tree-covered terrain in a near-vertical attitude.

Personnel Information

The uncertificated pilot, age 42, did not have, nor had he ever had, a valid pilot certificate. His last student pilot/third class medical certificate was issued June 22, 1995, when he was 25 years old. A student pilot certificate for an individual under 40 years old is valid for 60 months. No records of the uncertificated pilot's flight history or experience were located.

Aircraft Information

The accident airplane was equipped with a Lycoming O-320 engine, rated at 150 horsepower. No aircraft maintenance logs were located for the accident airplane.

Meteorological Information

The closest weather reporting facility was the Sleetmute Airport, 26 miles north of the accident site. At 1716, a weather observation from the Sleetmute Airport reported wind 020 degrees true at 4 knots, visibility 10 statute miles, clouds and sky condition 9,000 feet, temperature 39 degrees F, dew point 16 degrees F, and altimeter 29.30 inches Hg.

Wreckage and Impact Information

On March 31, the NTSB IIC, two Alaska State Troopers, and an FAA operations inspector from the Anchorage Flight Standards District Office examined the airplane wreckage at the accident site. All major components were found at the main wreckage area. The airplane collided with snow and tree-covered terrain in a near-vertical, nose-down attitude and remained in that position throughout the on-scene investigation. The upper surface of the fuselage was oriented on about a 205-degree heading and canted to the right about 20 degrees.

The right wing exhibited extensive spanwise leading edge aft crushing and extensive aft chordwise wrinkling and folding. The aileron and flap remained attached to the wing, and the flap was retracted. The entire right wing was broken at the inboard wing attach points and had spanwise downward displacement of the aft edge. The left wing had spanwise leading edge aft crushing from the inboard end to about midspan, and aft folding and crushing on about a 45-degree angle from midspan to the wingtip. The left aileron remained attached and had an upward bend at the outboard end. The left flap was extended about 30 degrees. Both lift struts remained attached to their respective wing and fuselage attach points. The empennage was undamaged. The elevator trim position appeared mid-range. Flight control surfaces remained connected, and flight control system cable continuity was established to the cabin/cockpit area. The engine was entirely buried in soft snow-covered terrain on about a 45-degree nose-down attitude, almost to the firewall. One propeller blade was visible in the snow and appeared to have a slight aft bend. There were no preaccident mechanical anomalies with the airplane.

Medical and Pathological Information

A postmortem examination was conducted under the authority of the Alaska State Medical Examiner on April 2, 2012. The cause of death for the uncertificated pilot was attributed to blunt force traumatic injuries, including an aortic laceration. The FAA Civil Aero Medical Institute conducted a toxicological examination on August 30, 2012, which revealed ethanol in the brain (19 mg/dL), blood (18 mg/dL), and vitreous (17 mg/dL). The NTSB's chief medical officer reviewed the reports and remarked that the pilot was not likely to have been impaired at these low levels of ethanol.

Tests and Research

The uncertificated pilot was using a Garmin GPSMAP 276 portable GPS receiver capable of storing route-of-flight data. The unit was sent to the NTSB's Vehicle Recorders Division for examination. An NTSB electrical engineer extracted GPS data for the accident flight, including time, latitude, longitude, and GPS altitude. Groundspeed and course information were derived. The data logs for March 30, 2012, revealed that at 1646 the airplane departed from a remote cabin on the banks of the Holitna River. After departure, the airplane turned south and followed the river at low altitude, then turned north again, following the river. As the airplane approached the cabin, it began a series of turns near the cabin. As it approached the makeshift landing site, it began a gradual descent and the GPS-derived groundspeed decreased. The last groundspeed and direction were 52 mph on a 253-degree true course at 1708.

Contributing factors

PilotAirspeed — Not attained/maintainedPerformance/control parameters — Not attained/maintained