MIA95FA089

NTSB accident investigation · Piper PA-22-150 · Staley, NC · March 18, 1995

Accident · FatalField investigationFinal report
Date
March 18, 1995, 16:35 local (21:35 UTC)
Place
Staley, NC
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N7545DPiper PA-22-150
Weather
Visual (VMC) · Day
Status
Completed · report August 23, 1995
Report
Approved by Office Director
FAA report
19950318004289A
Case key
37644

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

The pilot's failure to maintain airspeed (VSO) while maneuvering during a forced landing, resulting in an in-flight loss of control (inadvertent stall), and subsequent in flight collision with terrain. Contributing to the accident was the pilot's inadequate preflight planning/preparation to ensure there was adequate fuel available for the flight, resulting in a total loss of engine power from fuel exhaustion.

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 engine power(total) - nonmechanicalManeuvering
Fluid,fuel - exhaustion
Preflight planning/preparation - inadequatePilot in commandFactor
Forced landingDescent - emergency
Loss of control - in flightManeuvering - turn to landing area (emergency)
Airspeed(vso) - not maintainedPilot in commandCause
Stall - inadvertentPilot in command
In flight collision with terrain/waterDescent - normal
Terrain condition - ground

Analysis

A witness stated he heard a change in engine noise from an airplane flying towards his location. He looked up and saw the airplane descending in a dive estimated at a 45-degree nose-down attitude. The airplane began at right spiraling turn at treetop level, when the nose pitched down vertically, the airplane disappeared from view below the tree line. Just before the airplane collided with the ground, the engine noise quit completely. Examination of airframe, flight controls, engine assembly and accessories revealed no evidence of a precrash failure or malfunction. Both fuel tanks were ruptured. There was no evidence of damage to the vegetation consistent with fuel spillage, and there was no odor of fuel present at the crash site.

Factual narrative

History of flight

On March 18, 1995, about 1635 eastern standard time, a Piper PA-22-150, N7545D, registered to Richard J. Pereira, operating as a 14 CFR Part 91 personal flight, crashed while maneuvering in the vicinity of Staley, North Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was destroyed and the commercial pilot was fatally injured. The flight originated from Piedmont Triad International Airport, Greensboro, North Carolina, about 16 minutes before the accident en route to Siler City, North Carolina.

A witness stated he was working in his garden, when he heard the sound of an airplane descending. He looked towards the northwest, and saw a red and white Piper airplane pull out of a dive, and climb to about 1,000 feet. The airplane was observed in a 45-degree bank, descends to about 200 feet above the trees heading southbound, and pulls up at a 45-degree angle. The airplane leveled off, turned to the east, flew over his house, climbed to about 1,000 feet, and turned to the north. An increase in engine noise was heard, the airplane turned to the west in about a 45-degree to 90-degree bank descending to the south. The airplane rolled out of the turn east bound at about 150 to 200 feet above the ground, pulls up at about a 45-degree to 50-degree angle, and performed the same maneuver two more times. The airplane disappeared from view below the tree line about 4 to 5 miles southwest of his house.

Another witness stated he was building a barn next to his house when he heard a change in engine noise from an airplane flying towards his location. He looked up and observed the airplane descending in a dive estimated to be about 45-degrees nose down. The airplane was observed to begin a right spiraling turn at treetop level, when the nose pitched down vertically, and the airplane disappeared from view below the tree line. Just before the airplane collided with the ground, the engine noise quit completely.

Personnel information

Review of the pilot's logbook revealed his last recorded flight was on August 10, 1994. Approximate total flight time time was obtained through the family from an aircraft insurance renewal questionnaire dated May 4, 1995.

Aircraft information

Information pertaining to aircraft information is contained in NTSB Form 6120.4.

Meteorological information

Visual meteorological conditions prevailed at the time of the accident. (For additional information, see NTSB Form 6120.4).

Wreckage and impact information

The wreckage of N7545D was located in the grass on the east side of Foust Road in the vicinity of Staley, North Carolina. Examination of the crash site revealed the airplane collided with the ground in a nose-down attitude, right wing low, nosed over, and came to rest inverted. The engine was buried about 2 to 3 feet below the ground. The propeller was attached to the propeller flange, and the spinner was crushed and torn. Both propeller blades were bent aft. Slight torsional twisting was present on one propeller blade tip. Both wings were displaced aft with compression damage extending along the leading edge of both wings. The fuselage was compressed aft to the elevators. The left and right fuel tanks were ruptured. The vegetation in the area adjacent to the airplane wreckage showed no evidence of damage consistent with fuel spillage. No odor of fuel was present at the crash scene.

Examination of the airframe, flight controls, propeller, engine assembly and accessories revealed no evidence of a precrash failure or malfunction. All components necessary for flight were present at the crash site. Continuity of the flight control system was confirmed for pitch, roll, and yaw.

Medical and pathological information

Post-mortem examination of the pilot, Richard J. Pereira, was conducted by Dr. Thomas A. Sporn, Assistant Chief Medical Examiner, State Medical Examiners Office, Chapel Hill, North Carolina, on March 19, 1995. The cause of death was severe trauma. Post-mortem toxicology studies of specimens from the pilot were performed by the Armed Forces Institute of Pathology, Washington D.C. These studies were negative for basic, acidic, and neutral drugs.

Test and research

All airports that the pilot was known to frequent were contacted. None reported establishing radio contact or selling aviation fuel to N7545D on the day of the accident. The last reported sale of aviation fuel was on March 11, 1995, in New Bern, North Carolina. The last reported radio contact within the air traffic control system was with Greensboro south departure radar position, when radar services was terminated about 20 miles southeast of Piedmont Triad International airport on the day of the accident.

Additional information

The wreckage was released to Lieutenant Cecil E. Berry, Randolph County Sheriff's Department, Asheboro, North Carolina, on March 19, 1995. The engine was released to Mr. Kenneth J. Honstetter, Guilford Technical Community College Aviation Center, Greensboro, North Carolina, on March 20, 1995.

Aircraft

Registration
N7545D
Reported as
Piper PA-22-150
Category
Airplane
Serial number
22-5276
Airframe hours
2,678
Engine
Lycoming O-320, 150 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Pereira, Richard J.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 1, 1994 · 2 hours before
Departed
GSO · Greensboro, NC
Destination
5W8 · Siler City, NC

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
57
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
4,043 total · 592 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
80° at 9 knots
Visibility
15 statute miles
Lowest ceiling
25,000 ft broken
Temperature
59 °F, dew point 27 °F
Altimeter
30.00 inHg
Observed at
GSO, 28 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.