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NTSB Identification: CHI01FA001.
The docket is stored in the Docket Management System (DMS). Please contact
Public Inquiries
14 CFR Part 91: General Aviation
Accident occurred Monday, October 02, 2000 in Rapid City, SD
Probable Cause Approval Date: 6/3/2002
Aircraft: Piper PA-44-180, registration: N294ND
Injuries: 1 Fatal.
The airplane was destroyed during an in-flight collision with the terrain following an intentional pitch-up maneuver, approximately at mid-field to an altitude of 1,000 feet above ground level, and subsequent intentional nose-down maneuver which resulted in the collision with the runway. According to an Investigation Report prepared by the Pennington County Sheriff's Office, the pilot's cause of death was, "...blunt force trauma due to an airplane crash with the manner of death as suicide."
The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
Suicide
CHI01FA001
HISTORY OF FLIGHT
On October 2, 2000, at 1933 mountain daylight time (mdt), a Piper PA-44-180,
N294ND, owned and operated by the University of North Dakota and piloted by a
commercial pilot, was destroyed during an in-flight collision with runway 32
(8,701 feet by 150 feet, dry/concrete) at the Rapid City Regional Airport, Rapid
City, South Dakota. There was a post-impact explosion and fire. The airplane had
been conducting touch and go operations on runway 32 prior to the accident.
Visual metrological conditions prevailed at the time of the accident. The
personal flight was operating under the provisions of 14 CFR Part 91 without a
flight plan. The commercial pilot, the sole occupant on the airplane, sustained
fatal injuries. The flight departed Custer State Park Airport (3V0), Fairburn,
South Dakota, at an undetermined time.
A witness observed the accident airplane land at 3V0 about 1800. The accident
pilot told the witness that he had flown from Nebraska and was thinking about
flying to Denver that evening. After a few minutes of conversation, the accident
pilot stated to the witness that he was thinking about flying by Mount Rushmore
and wanted to know if there were any flight restrictions over the monument. The
witness told the accident pilot that there were altitude restrictions over the
monument and discussed specific details on how to depart from the 3V0. The
witness stated that the accident airplane and pilot were still at 3V0 when he
departed after 1830.
According to a transcript of Air Traffic Control (ATC) communications between
the accident airplane (N294ND) and the Rapid City Regional Airport (RAP) local
controller (LC), the accident airplane approached RAP from the southwest.
The communications between N294ND and the RAP LC were transcribed as follows:
1852:14
N294ND rapid city tower seminole two niner four november delta out of six
thousand five
hundred for stop and go's seven to---the---west
1852:28
LC (unintelligible) two niner four november delta rapid city tower runway three
two
cleared to land win---correction cleared for the option wind zero three zero at
eight
1852:34
N294ND cleared for the option four november delta thank you
1856:47
LC four november delta can make left closed traffic
1856:50
N294ND roger four november delta
1858:24
LC four november delta runway three two cleared for the option traffic bonanza
on the
go be right turn
1859:29
N294ND kay traffic in sight cleared for the option four november delta
1901:02
LC four november delta make right traffic this pass traffic cessna four miles
northwest
be entering left downwind
1901:08
N249ND roger right traffic four november delta
1901:42
N249ND four november delta we can we'll make it a tight one this time
1901:47
LC four november delta roger cleared for the option
1901:49
N249ND cleared for the option four november delta
1904:35
N294ND and four november delta did you want me on left traffic again
1904:38
LC four november delta your choice this pass left or right traffic is approved
1904:42
N294ND kay i guess we'll go left traffic four november delta
1904:45
LC roger and squawk and maintain v f r
1904:47
N294ND okay v f r four november delta
1905:58
LC four november delta is cleared for the option wind zero two zero at eight
1906:01
N294ND cleared for the option four november delta
1910:40
LC four november delta is cleared for the option
1910:42
N294ND cleared for the option four november delta
1910:53
N294ND how late is ah tower open till tonight
1910:55
LC open till ten
1914:49
N294ND and four november delta are we clear
1914:51
LC four november delta is cleared for the option
1914:54
N294ND cleared for the option four november delta
1918:37
LC four november delta's cleared for the option wind zero two zero at eight
1918:40
N294ND four november delta cleared for the option thank you
1921:32
N294ND and for four november delta do you have ah a second to take down a phone
number
really quick
1921:39
LC go ahead
1921:41
N294ND it is one eight hundred three four four zero three one four and that's ah
u n d flight
operations
1921:53
LC roger we got one eight hundred three four four zero three one four
1921:57
N294ND roger four november delta and ah you don't need to use it
1922:03
N294ND yet
1922:04
LC roger
1925:13
N294ND so it looks like about one more option then ah full stop for four
november delta
1925:18
LC four november delta roger
1926:32
LC four november delta is cleared for the option wind zero two zero at eight
1926:36
N294ND cleared for the option for four november delta
1930:35
N294ND for four november delta you still have that phone number
1930:37
LC affirm
1930:39
N294ND kay four november delta after all this ah that's the people that you can
contact at
u n d um and we'll be full stop this time and ah
1931:01
N294ND and four november delta still cleared to land right
1931:03
LC four november delta is cleared to land and what did you want me to tell em
when
i call em
1931:09
N294ND stand by four november delta
1932:06
N294ND okay for four november delta uh
1932:14
N294ND yea standby
1932:18
N294ND for four november delta we've got ah thirty gallons a fuel on board one
soul on
board and my name is bob thompsen and if you can give them a call at that one
eight hundred number and let them know it's ah where i'm at and also if you
could
tell my family and friends that i love them very much
1932:44
N294ND my name again is bob thompsen
1932:47
LC you just ah were you going to depart out of here or stay the night
1932:49
N294ND um i'll stay the night
1932:51
LC roger we'll let em know
1932:55
N294ND and ah it be a good idea to get ah airport rescue and fire fighting out
here too please
1933:02
LC four november delta are you declaring an emergency
1933:13
LC four november delta tower
1933:20
LC two niner four november delta rapid city tower
1933:26
N294ND (unintelligible)
According to a written statement provided by the ATC controller who was working
at the time of the accident, the airplane had been conducting touch and go
maneuvers prior to the accident. The controller stated that the pilot requested
a full stop landing and on approach, "[the pilot] proceeded to level off at
about 100 [feet above ground level] on short final and increase his speed, on
the go. Shortly past A4 intersection, the pilot pulled nearly straight up,
appearing to stall out around 1,000 ft agl[,] coming down at a steep angle and
crashing just past A3 intersection."
PERSONNEL INFORMATION
According to Federal Aviation Administration (FAA) records, the pilot was the
holder of a commercial pilot certificate with ratings for airplane single-engine
land, airplane multi-engine land, and instrument airplane operations. The pilot
was also the holder of a certified flight instructor (CFI) certificate with
ratings for airplane single-engine, airplane multi-engine, and instrument
airplane operations. FAA records show the pilot's last medical examination date
was December 17, 1999, and the pilot was issued a first-class medical
certificate with the limitation, "Must wear corrective lenses".
According to the pilot's flight logbook and University of North Dakota flight
records, the pilot had accumulated a total time of 1,203.3 flight hours as of
his last flight record, dated September 30, 2000. As of the last fight record,
the pilot had logged 969.6 hours of flight time in single-engine airplanes and
233.7 hours in multiengine airplanes. The pilot satisfied the requirements of a
biennial flight review on December 13, 1999, when he satisfactorily completed a
FAA checkride for an additional CFI rating.
AIRCRAFT INFORMATION
The aircraft was a Piper PA-44-180, N294ND, serial number 4496029. The Piper
PA-44-180 is a production built, two engine, low wing monoplane of all metal
construction, equipped with a retractable landing gear and controllable pitch
propellers. According to FAA records, the airplane was issued a Standard
Airworthiness Certificate on December 18, 1999. According to the airplane's
service records, the last aircraft phase inspection was completed on September
21, 2000, at 598.3 total hours. According to the service records, the airplane
had accumulated a total-time of 652.7 hours on October 2, 2000.
The left engine was a Textron Lycoming O-360-A1H6, serial number L3718336A, and
had accumulated a total-time of 652.7 hours on October 2, 2000.
The right engine was a Textron Lycoming LO-360-A1H6, serial number L61271A, and
had accumulated a total-time of 652.7 hours on October 2, 2000.
METEOROLOGICAL INFORMATION
An automated surface observing system (ASOS) located at the Rapid City Regional
Airport reported the weather three minutes prior to the accident as:
Observation Time: 1930 mdt
Wind: 020-degrees at 5 knots
Visibility: 10 statute miles
Sky Condition: Sky clear
Temperature: 11-degrees Celsius
Dew Point: 04-degrees Celsius
Pressure: 29.93 inches of mercury
WRECKAGE AND IMPACT INFORMATION
The National Transportation Safety Board's (NTSB) on-scene investigation began
on October 3, 2000.
The aircraft was recovered from the accident site prior to the arrival of the
NTSB investigator and was positioned behind a hangar located at the Rapid City
Regional Airport. Flight control continuity was verified for the aileron,
elevator, and rudder control systems. Both left and right crankshaft flanges
were broken loose from their respective crankshafts. The breaks had signatures
consistent with torsional overload failure. Both left and right propeller hubs,
including all propeller blades, were separated from their respective engines.
All propeller blades had chordwise scratching, S-shape bending, and leading edge
gouges.
MEDICAL AND PATHOLOGICAL INFORMATION
An autopsy was performed on the pilot at the Clinical Laboratory of the Black
Hills, Rapid City, South Dakota, on October 3, 2000.
A Forensic Toxicology Fatal Accident Report was prepared by the FAA Civil
Aeromedical Institute, Oklahoma City, Oklahoma.
The toxicology results for the pilot were:
* No Carbon Monoxide detected in Blood
* No Cyanide detected in Blood
* No Ethanol detected in Vitreous
* No Drugs detected in Blood
ADDITIONAL DATA/INFORMATION
According to an Investigation Report prepared by the Pennington County Sheriff's
Office, the pilot's cause of death was, "...blunt force trauma due to an
airplane crash with the manner of death as suicide."
Parties to the investigation included the Federal Aviation Administration,
University of North Dakota, The New Piper Aircraft Company, and Textron
Lycoming.
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