MIA96LA042

NTSB accident investigation · Otis King COBRA-B · Newberry, FL · December 16, 1995

Accident · FatalLimited investigationFinal report
Date
December 16, 1995, 12:45 local (17:45 UTC)
Place
Newberry, FL
Injuries
2 fatal
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N102DJOtis King COBRA-B
Weather
Visual (VMC) · Day
Status
Completed · report September 9, 1996
Report
Approved by Office Director
FAA report
19951216040669A
Case key
37960

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

an in-flight loss of control for undetermined reasons.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightManeuvering
Reason for occurrence undeterminedCause
Flt control syst,rudder control attach points - cut/severed
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Witnesses observed the airplane start a turn towards the north and then to the west over a state road. The airplane then turned towards the east, banked to the right, the nose pitch down, and the airplane crashed. The engine appeared to be running until the airplane collided with the ground. Visual examination of the airframe, engine assembly and accessories revealed no evidence of a precrash failure or malfunction. Continuity of the flight control system was confirmed for pitch and roll. The right rudder cable was attached to the rudder. The left rudder cable was not attached. The attach point and retainer pin were in place; however, the clevis pin safety ring was missing and later found by a recovery crew. Safety Board metallurgical examination of the safety ring revealed features indicative that it was cut.

Factual narrative

On December 16, 1995, about 1245 eastern standard time, N102DJ, an Otis King Cobra-B crashed in Gainesville, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The private pilot and pilot rated passenger received fatal injuries and the airplane was substantially damaged. The flight had originated from a small private airstrip about 10 minutes earlier.

Witnesses stated they observed the airplane flying towards the north and to the west in the vicinity of state road 45. The airplane turned towards the east, banked to the right, and the nose pitched down. The engine appeared to be running until the airplane collided with the ground.

The wreckage of N102DJ was located in a pasture behind a residence located at 25010 N. W. 71st Place, Newberry, Florida.

Examination of the crash scene by the FAA revealed the airplane collided with the ground in a nose down attitude. Visual examination of the airframe, engine assembly and accessories revealed no evidence of a precrash failure or malfunction. The engine was not disassembled based on witness statements that the engine was operating until the airplane collided with the ground. Continuity of the flight control system was confirmed for pitch and roll. The left rudder cable was not attached to the rudder. The attach point and retainer pin were in place; however the clevis pin safety ring was missing. The right rudder cable was attached to the rudder.

According to Mr. Phillip A. Power, Air Safety Investigator for Carson Brooks Inc., Atlanta, Georgia, the separated clevis pin safety ring was located by a recovery crew, and forwarded to Beverly Morton, FAA Orlando Flight Standards District Office.

Examination of the separated clevis pin safety ring was conducted by the NTSB materials laboratory. Optical microscope and subsequent scanning electron microscope examinations revealed an indentation at the inside diameter surface of the ring adjacent to one of the separated ends. A small portion of the ring in the area located between the indentation and separation was squeezed out forming a shear lip. These features are indicative that the ring was cut. For additional information see NTSB Metallurgist's Factual Report No. 96-100.

Post-mortem examination of the private pilot who was removed from the left seat was conducted by Dr. William F. Hamilton Medical Examiner's Office, District 8, Gainesville, Florida, on December 17, 1995. The cause of death was multiple blunt traumatic injuries. Post-mortem toxicology studies of specimens obtained from the pilot was performed by the Forensic Toxicology Research Section, Federal Aviation Administration, Oklahoma City, Oklahoma. These studies were negative for basic, acidic, and neutral drugs. Azacyclonol was detected in the urine, lung and liver fluid.

Examination of the pilot-rated passenger who was removed from the right seat was conducted on December 17, 1995. The cause of death was multiple blunt traumatic injuries. Post-mortem toxicology studies of specimens obtained from the pilot rated passenger was performed by the Forensic Toxicology Research Section, Federal Aviation Administration, Oklahoma City, Oklahoma. These studies were negative for acidic, basic, and neutral drugs. Tetrahydrocannabinol carboxylic acid (marihuana), 0.183 ug/ml was detected in the urine. 0.014 ug/ml was detected in the blood. 0.003 ug/ml tetrahydrocannabinol was detected in the blood.

Review of the pilot-rated passenger logbook revealed he had recorded as logged 11,289 total flight hours. The pilot's last recorded flight was August 18, 1994. No flights were recorded as logged in N102DJ.

The components retained by the NTSB for further testing was released to Detective Legran Hewitt, Alachua County Sheriff's Office, Gainesville, Florida, on June 3, 1996. The private pilot's logbook and aircraft logbook were released to R. Dennis Comfort, P.A. Gainesville, Florida, on June 7, 1996. The pilot-rated passenger log book was released to Mr. Terry N. Silverman, P.A. Gainesville, Florida, on June 11, 1996.

Aircraft

Registration
N102DJ
Reported as
Otis King COBRA-B (KING COBRA)
Category
Airplane, amateur-built
Serial number
1
Engine
Rotax 532, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
David L. Jenkins
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 30, 1995 · 69 hours before
Departed
OJ8 · High Springs, FL

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
62
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
331 total · 194 in this make and model · 221 as pilot in command · 35 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 5 knots
Visibility
7 statute miles
Lowest ceiling
6,000 ft broken
Temperature
77 °F, dew point 61 °F
Altimeter
30.00 inHg
Observed at
GNV, 16 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.