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February 6, 1999 · Piper PA-18-150 · N8075D

Belle Fourche, SD

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 6, 1999
Injury Outcomes
2 injuries (2 fatalities)
Location
Belle Fourche, SD
Aircraft
Piper PA-18-150
Tail Number
N8075D
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
CHI99FA089

The aircraft was resting on a magnetic heading of 320 degrees in a grass field located approximately 1/4 mi west southwest of the private airstrip. There was no ground scarring present in the area around the resting position of the aircraft. There was no evidence of fire. The aircraft's wing leading edges and nose section exhibited a crush angle of approximately 45 degrees. Aileron, elevator and rudder flight control continuity was established. Elevator trim was in the neutral position. Examination of the carburetor bowl and accelerator pump did not reveal fuel. One drop of liquid was noted when the fuel line leading to the carburetor disconnected. There was no liquid in each fuel tank. The engine tachometer showed 1,900 rpm. The last inspection of the airframe was a 100-hour inspection completed on June 26, 1996.

NTSB Probable Cause

inadequate preflight planning/preparation, refueling not performed, and aircraft control not maintained by the pilot. The inadvertent stall by the pilot was an additional cause. Fuel exhaustion was a contributing factor.

Full Narrative

HISTORY OF FLIGHT On February 6, 1999, at 1415 mountain standard time, a Piper PA-18-150, N8075D, piloted by private pilot/mechanic, was destroyed on impact with terrain following a total loss of engine power during initial climb from a private airstrip near Belle Fourche, South Dakota. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 flight was not operating on a flight plan. The pilot and passenger were fatally injured. The local flight originated from the private airstrip at 1415. A witness located at the private airstrip stated that the pilot moved the aircraft out of a hanger, completed a preflight inspection and idled the engine on the ground for 8-10 minutes. The aircraft departed without the use of flaps, rolled about 1/2 down the runway and then climbed "OK" to an altitude of 500-600 feet agl when the engine stopped. He added that there were no unusual sounds. The aircraft then descended vertically. A respondent to the accident reported that there was not an overwhelming smell of fuel. Another respondent reported a little smell of fuel but did not feel any sloshing of fuel when the aircraft's wings were turned over. He added that there was no puddling of fuel beneath the wings. PERSONNEL INFORMATION The pilot, age 23, held a private pilot certificate with an airplane single engine land rating. He also held a certified aircraft mechanic with airframe and powerplant ratings. The pilot reported a total flight time of 175 hours at the issuance of his a third class medical certificate on June 4, 1998. The passenger, age 53, had occupied the rear seat of the aircraft and had obtained a third class medical certificate, without restrictions, on August 3, 1992. AIRCRAFT INFORMATION A review of aircraft logbooks revealed an entry for an 100-hour inspection was completed by the pilot on June 26, 1996 at a tachometer time of 291.1 hours and a total airframe time of 2,325.1 hours. A second entry, below the first, was signed by an airframe and powerplant mechanic with inspection authorization indicating that an annual inspection had been performed. A later entry without a date, airframe time or description of work was signed by the same airframe and powerplant mechanic indicating that an aircraft annual inspection had been performed. An annual inspection of the engine was performed on June 28, 1997 at a tachometer time of 297.2 hours and a time since major overhaul of 6.1 hours. WRECKAGE AND IMPACT INFORMATION The aircraft was resting on a magnetic heading of 320 degrees in a grass field located approximately 1/4 mi west southwest of the private airstrip. The accident site revealed no ground scarring to be present in the area around the resting position of the aircraft. There was no evidence of fire. The aircraft's wing leading edges and nose section exhibited a crush angle of approximately 45 degrees. Aileron, elevator and rudder flight control continuity was established. Elevator trim was in the neutral position. Examination of the carburetor bowl and accelerator pump did not reveal fuel. One drop of liquid was noted when the fuel line leading to the carburetor was disconnected. There was no liquid in each fuel tank. The engine tachometer showed 1,900 rpm and a time of 309.65 hours. MEDICAL AND PATHOLOGICAL INFORMATION Autopsies were conducted by the Butte County Coroner on February 9, 1999. Federal Aviation Administration Toxicological examinations were negative for all substances tested for the private rated pilot. FAA Toxicological results for the student rated pilot tested positive for Pseudoephedrine and Phenylpropanolamine. 102 (ug/ml, ug/g) of Acetaminophen was also detected. TESTS AND RESEARCH The aircraft had last obtained 15.3 gallons of fuel at the Bell Fourche Airport on November 30, 1998. The aircraft had been fueled with 12.1 gallons of fuel on October 18, 1998 and 19.8 gallons on June 13, 1998. ADDITIONAL INFORMATION The Federal Aviation Administration and Textron Lycoming were parties to the investigation. The wreckage was released to Tri State Aviation on February 7, 1999.

Flight

Event TypeAccident
Event Time14:15 MST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18-150
Tail NumberN8075D
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-B3B · Reciprocating · 150
Seats2

People & Injuries

Injury Summary2 injuries (2 fatalities)
Fatal2
Serious0
Minor0
Uninjured0
Total2
Crew 1Age 23 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point54 / 46
Altimeter0
Observation Time21:55
Weather SourceWFAC

Appendix: Source Data