MIA97LA138

NTSB accident investigation · Piper PA-28-160 · Pickens, SC · April 14, 1997

Accident · Minor injuriesLimited investigationFinal report
Date
April 14, 1997, 18:45 local (22:45 UTC)
Place
Pickens, SC
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N5363WPiper PA-28-160
Weather
Visual (VMC) · Day
Status
Completed · report August 29, 1997
Report
Approved by Office Director
FAA report
19970414005899A
Case key
38263

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 directional control during the takeoff roll from a touch-and-go landing, which resulted in the airplane going off the side of the runway, down an embankment, and into brush/trees.

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/waterTakeoff - roll/run
Touch-and-go - initiatedPilot in command
Directional control - not maintainedPilot in commandCause
Ground loop/swerve
On ground/water encounter with terrain/waterTakeoff - aborted
Terrain condition - drop-off/descending embankment
Terrain condition - high vegetation

Analysis

The student pilot stated that he had completed his fifth touch-and-go landing and was taking off again. He said that just before reaching rotation speed, the right wing dropped down, and the airplane began to roll on the right main and nose landing gear, turning 45 degrees to the left. The aircraft went off the side of the runway, and subsequently, it went down an embankment into trees and brush, where it came to rest. Postcrash examination of the right landing gear strut showed it was extended above 2 inches and still had air pressure and fluid.

Factual narrative

On April 14, 1997, about 1845 eastern daylight time, a Piper PA-28-160, N5363W, registered to a private individual, crashed when control was lost during takeoff at Pickens County Airport, Pickens, South Carolina, while on a Title 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the student-rated pilot received minor injuries. The flight originated from Pickens, the same day, about 1750.

The pilot stated he had completed his fifth touch-and-go landing and was taking off again. Just before reaching rotation speed, the right wing dropped down. The airplane then began to roll on the right main and nose landing gear, and turned 45 degrees to the left. The aircraft went off the side of the runway and he reduced engine power. He did not apply brakes because the aircraft was still on the two wheels. The left main landing gear touched down just about the time the aircraft went down an embankment into trees and brush where it came to rest.

Postcrash examination of the right landing gear strut was performed by two mechanics. The strut was found to be holding air pressure and had no evidence of air leaks. The strut contained 2.5 ounces of hydraulic fluid and was extended above 2 inches. (See attached statements.)

Aircraft

Registration
N5363W
Reported as
Piper PA-28-160
Category
Airplane
Serial number
28-428
Airframe hours
2,884
Engine
Lycoming O-320-B2B, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Chester D. Maynard
Registered owner
Thomas W. Huntsman
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 22, 1996 · 30 hours before
Departed
LQK
Airport
LQK · Pickens County, runway 23, 5,000 × 100 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
48
Certificate
Student
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
17 total · 17 in this make and model · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 4 knots
Visibility
10 statute miles
Lowest ceiling
25,000 ft broken
Temperature
59 °F
Altimeter
30.00 inHg
Observed at
AND, 25 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.