MIA07CA096

NTSB accident investigation · Piper PA-28-180 · Fairmont, WV · May 10, 2007

Accident · No injuriesData collectionFinal report
Date
May 9, 2007, 21:30 local (May 10, 2007, 02:30 UTC)
Place
Fairmont, WV
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N38730Piper PA-28-180
Weather
Visual (VMC) · Night
Status
Completed · report October 31, 2007
Report
Approved by Office Director
Parties
Charleston FAA FSDO
FAA report
20070509832129A
Case key
65760

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 directional control during landing.

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
Directional control - not maintainedPilot in commandCause
On ground/water collision with objectLanding - roll
Object - vasi light/system
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - ravine

Analysis

The pilot stated that he flew a stabilized approach and had a normal touchdown. After touchdown the airplane veered to the left, and he compensated with right rudder but got no response. As the airplane drifted to the left, he increased the right rudder inputs and also used right toe-brake but again got no response. Before exiting the runway he pulled the handbrake while applying hard right toe-brake. The aircraft did slow but didn't turn to the right. After exiting the runway the airplane overran the VASI light system and struck a row of runway lights. After which the airplane impacted an embankment and slid obliquely down the side of it. The airplane then impacted another embankment perpendicular to that one, shearing the nose-wheel, bending the prop and engine-cowl. The airplane then rolled to the left and the wing struck the ground, buckling the inboard side fuel tank bulkhead and partially shearing from the fuselage before it come to a stop. The pilot stated that the airplane's nosewheel steering and brakes performed normally prior to the accident flight. The responding FAA inspector stated that examination of the site indicated that the airplane touchdown point was 25 yards from the end of the runway and 8 yards left of the centerline, and angled directly towards the second VASI light installation. Following the tire tracks it appears that the underside of the left wing impacted the VASI light. The pilot stated to the FAA inspector that there were no mechanical difficulties with the aircraft.

Factual narrative

The pilot stated he flew a stabilized approach and had a normal touchdown. After touchdown the airplane veered to the left; he compensated with right rudder but got no response. As the airplane drifted to the left, he increased the right rudder inputs and also used right toe-brake but again got no response. Before exiting the runway he pulled the handbrake while applying hard right toe-brake. The aircraft did slow but didn't turn to the right. After exiting the runway the airplane overran the VASI light system and struck a row of runway lights. After which the airplane impacted an embankment and slid obliquely down the side of it. The airplane then impacted another embankment perpendicular to that one, shearing the nose-wheel, bending the prop and engine-cowl. The airplane then rolled to the left and the wing struck the ground, buckling the inboard side fuel tank bulkhead and partially shearing from the fuselage before it come to a stop. The pilot stated that the airplane's nose-wheel steering and braking performed normally prior to the accident flight.

The responding FAA inspector stated that examination of the site indicated the airplane's touched down point was 25 yards from the end of the runway and 8 yards left of the centerline, and angled directly towards the second VASI light installation. Following the tire tracks it appears that the underside of the left wing impacted the VASI light. The pilot stated to the FAA inspector that there were no mechanical difficulties with the aircraft.

Aircraft

Registration
N38730
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-7725255
Airframe hours
5,728
Engine
Continental 0-360 A2A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Business · Part 91
Registered owner
Mark Hugh Hefner
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 1, 2007 · 21 hours before
Departed
W22 · Buckhannon, WV
Destination
4G7 · Fairmont, WV
Airport
4G7 · Fairmount Municipal, runway 22, 2,859 × 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
56
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
November 1, 2006
Seat
Left
Flight hours
690 total · 425 in this make and model · 600 as pilot in command · 35 in the last 90 days · 15 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 55 °F
Altimeter
29.95 inHg
Observed at
KCKB, 10 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.

Other investigations on N38730 · 1

Matched to the same aircraft by N-number and date.