ATL96FA027

NTSB accident investigation · Piper J-3-C65 · Belzoni, MS · December 26, 1995

Accident · FatalField investigationFinal report
Date
December 26, 1995, 15:30 local (21:30 UTC)
Place
Belzoni, MS
Injuries
2 fatal
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N3615KPiper J-3-C65
Weather
Visual (VMC) · Day
Status
Completed · report October 4, 1996
Report
Approved by Office Director
FAA report
19951226042509A
Case key
3640

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

failure of the student pilot to maintain adequate airspeed, while maneuvering, which resulted in a stall/spin and subsequent collision with the ground.

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
Maneuver - performedPilot in command
Airspeed - inadequatePilot in commandCause
Stall/spin - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

A witness saw the airplane as it was maneuvering in the vicinity of the accident site. The airplane was then observed to enter a spin and disappear behind trees, where it impacted in a plowed field. Examination of the airplane failed to disclose a mechanical problem. There was evidence that the airplane impacted the ground in a stalled attitude. Both wing assemblies sustained aft crushing damage to the leading edges. The student pilot's medical certificate was dated 8/11/93. No pilot flight logs were recovered for examination.

Factual narrative

History of flight

On December 26, 1995, at approximately 1530 central standard time, a Piper J-3-C65, N3615K, collided with the ground while maneuvering near Belzoni, Mississippi. The personal flight operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The aircraft sustained substantial damage; the two student pilots were fatally injured. The flight departed a private airstrip in Belzoni, at approximately 1400 hours.

Reportedly, an eyewitness observed the airplane as it maneuvered above the trees, and as it subsequently entered a spin. After the airplane completed two turns, it disappeared below the tree tops. Several minutes later, the property owner located the aircraft wreckage in a freshly plowed field.

Personnel information

Information on the pilot is included in this report on page 3 of the factual report under the data field labeled "First Pilot Information". A review of the student pilot's medical records disclosed that, on August 11, 1993, he had been issued a student pilot's certificate with the restriction, "valid for student pilot purposes only". According to the Federal Aviation Administration (FAA), the student pilot will not be allowed to solo until he has completed a medical flight test with a Flight Standard District Office. There was no record of the student pilot accomplishing a medical flight test for the lack of depth perception described in the medical restriction. The medical record also disclosed that the student pilot's last medical certificate was issued on August 11, 1993 (see attached student pilot's medical information).

Aircraft information

Information on the airplane is included in this report on page 2 of the factual report under the data field labeled "Aircraft Information". The aircraft maintenance records were not recovered for examination. According to the previous owner, N3615K was sold to Mr.T.A.Tharp in 1987. FAA records still reflect the previous owner.

Meteorological information

Visual weather conditions prevailed at the time of the accident. Weather information is contained in this report on page 3 of the factual report under the data field labeled "Weather Information".

Wreckage and impact information

Examination of the accident site revealed that the airplane rested with the engine and propeller assembles buried several inches into the ground. All wreckage debris was located in the immediate vicinity of the ground impact. Both wings sustained ground impact damage along the leading edges. All flight controls were attached to the airframe, and all control cables were attached to the respective control surfaces.

The propeller assembly was attached to the engine at the accident site. The propeller bade tips sustained chordwise damage alone the leading edges. Ignition sparks were generated when the engine magnetos were rotated during the engine examination. Powertrain continuity was also established during the engine examination.

Examination of the airframe disclosed that the cockpit and passenger areas were buckled and displaced aft from their normally installed positions. Both seat assemblies were also displaced aft and were dislodged from their respective attach points. The airframe and engine examinations failed to disclose a mechanical malfunction or a component failure.

Medical and pathological information

On December 26, 1995, the postmortem examination on the pilot was conducted by Dr. Steve Haynes at the Rankin County Morgue in Pearl Mississippi. The toxicological examination was negative for drugs and alcohol.

Additional information

The wreckage was released to Mr. Rick Stevens, of Isola, Mississippi.

Aircraft

Registration
N3615K
Reported as
Piper J-3-C65
Category
Airplane
Serial number
22305
Engine
Continental C-85-12, 85 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Thomas A. Tharp
Registered owner
A. D. Tharp
Airworthiness certificate
Standard, Normal
Departed
NONE · Isola, MS

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
21
Certificate
Student
Medical
Class 3, Expired
Seat
Front
Toxicology
Performed
Flight hours
200 total

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 8 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
41 °F, dew point 28 °F
Altimeter
30.00 inHg
Observed at
GWO, 30 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.