ATL97LA041

NTSB accident investigation · Piper PA-28R-200 · Winston Salem, NC · February 12, 1997

Accident · No injuriesLimited investigationFinal report
Date
February 12, 1997, 15:45 local (20:45 UTC)
Place
Winston Salem, NC
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N15013Piper PA-28R-200
Weather
Visual (VMC) · Day
Status
Completed · report December 15, 1997
Report
Approved by Office Director
FAA report
19970212003689A
Case key
3823

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 inadequate compensation for wind conditions and failure to maintain directional cntrol of the airplane, which resulted in a ground swerve and collapse of the right main landing gear. The crosswind was a related factor.

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 - on ground/waterLanding - roll
Weather condition - crosswindFactor
Compensation for wind conditions - inadequatePilot in commandCause
Directional control - not maintainedPilot in commandCause
Ground loop/swerve
Main gear collapsedLanding - roll
Landing gear,main gear - overload

Analysis

The flight had been cleared for a touch-and-go landing on runway 4, when shortly after touchdown, the airplane veered off the right side of the runway. The pilot reported that during the landing roll, he experienced some difficulty with the brakes, and the airplane veered off the runway into a grassy area. During the uncontrolled movement of the airplane, the right main landing gear collapsed, and the right wing spar was damaged. A review of the weather data disclosed that the prevailing wind was from 320 degrees at 7 knots. An examination of the airplane failed to disclose a mechanical problem with the brake system.

Factual narrative

On February 12, 1997, at 1545 eastern standard time, a Piper PA-28R-200, N15013, collided with the ground and collapsed the right main landing gear during an attempted landing on runway 04 at the Smith Reynolds Airport in Winston Salem, North Carolina. 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 airplane sustained substantial damage. The pilot was not injured. The flight departed Winston Salem at 1540.

The flight had been cleared for a touch and go landing when shortly after the touch phase of the procedure the airplane veered off the right side of the runway. The pilot reported that during the landing roll, he experienced some difficulty with the brakes, and the airplane veered off the runway into a grassy area. During the uncontrolled movement of the airplane, the right main landing gear collapsed, and the right wing spar was damaged.

A review of the weather data disclosed that, the prevailing winds were 320 degrees at seven knots when the pilot attempted the landing. An examination of the airplane failed to disclose a mechanical problem with the brake system.

Aircraft

Registration
N15013
Reported as
Piper PA-28R-200
Category
Airplane
Serial number
28R-7235318
Airframe hours
1,091
Engine
Lycoming IO-360-C1C, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Mark L. Palmer
Registered owner
Michael D. Shadrick
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 14, 1996 · 100 hours before
Departed
INT
Airport
INT · Smith Reynolds, runway 4, 3,930 × 75 ft, asphalt

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
38
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
138 total · 27 in this make and model · 27 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 7 knots
Visibility
10 statute miles
Lowest ceiling
1,800 ft broken
Temperature
50 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
INT, 1 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.