ATL05LA001

NTSB accident investigation · Stinson 108 · Ashland, AL · October 2, 2004

Accident · Minor injuriesLimited investigationFinal report
Date
October 2, 2004, 09:00 local (14:00 UTC)
Place
Ashland, AL
Injuries
3 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N40129Stinson 108
Weather
Visual (VMC) · Day
Status
Completed · report June 8, 2005
Report
Approved by Office Director
Parties
Birmingham FSDO-09
FAA report
20041002024869A
Case key
60256

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A total loss of engine power in cruise flight due to the fatigue failure of the No.4 cylinder exhaust valve.

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(partial) - mech failure/malfCruise
Engine assembly,valve,exhaust - fatigueCause
Engine assembly,valve,exhaust - failureCause
Forced landingDescent - emergency
In flight collision with terrain/waterDescent - emergency
Object - tree(s)
Terrain condition - none suitable
Terrain condition - ground

Analysis

The pilot stated they were in cruise flight at 2,500 feet with a private pilot flying the airplane. The engine began to run rough and shudder. The pilot stated, "I have the controls" and the private pilot responded, "you have the controls." The pilot looked for a forced landing area and observed a country road and a field. He completed the emergency checklist and entered a downwind to land on the highway. He turned base and observed power poles, but he could not see any power lines running between the poles and decided to land in the field. He made a left 35-degree turn towards a field and propeller struck a tree, yawed to the left colliding with the ground separating the landing gear and bending the engine firewall. Examination of the engine assembly revealed the exhaust valve in the No.4 cylinder had failed. Examination of the exhaust valve revealed fatigue cracks had propagated from opposite sides of the stem adjacent to the beginning of the radius between the stem and the valve head.

Factual narrative

On October 2, 2004, at 0900 central daylight time, a Stinson 108, N40129, registered to and operated by a private owner, as a 14 CFR Part 91 personal flight collided with trees during a forced landing to unsuitable terrain following a loss of engine power near Ashland, Alabama. Visual meteorological conditions prevailed and no flight plan was filed. The airplane received substantial damage. The airline transport rated pilot, private pilot passenger, and one rear seat passenger reported minor injuries. The remaining rear seat passenger reported no injuries. The flight originated from Birmingham, Alabama on October 2, 2004, at 0835.

The pilot stated they were in cruise flight at 2,500 feet MSL with a private pilot flying the airplane. The engine began to run rough and shudder. The pilot stated, "I have the controls" and the private pilot responded, "you have the controls." The pilot looked for a forced landing area and observed a country road and a field. He completed the emergency checklist and entered a downwind to land on the highway. He turned base and observed power poles, but he could not see any power lines running between the poles and decided to land in the field. He made a left 35-degree turn towards a field and propeller struck a tree, yawed to the left colliding with the ground separating the landing gear and bending the engine firewall.

Examination of the engine assembly revealed the exhaust valve in the No.4 cylinder had failed. The No. 4 cylinder and exhaust valve were forwarded to the NTSB Materials Laboratory for further analysis. Examination of the exhaust valve revealed fatigue cracks had propagated from opposite sides of the stem adjacent to the beginning of the radius between the stem and the valve head.

The No. 4 cylinder and exhaust valve was returned to the registered owner on January 24, 2005.

Aircraft

Registration
N40129
Reported as
Stinson 108
Category
Airplane
Serial number
108-59
Engine
Franklin GA4-150 B3, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
James R. Brandt
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 3, 2004 · 6 hours before
Departed
BHM · Birmingham, AL
Destination
26A · Ashland, AL

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
54
Injuries
Minor
Certificates
Commercial, Airline transport, Flight instructor
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
May 20, 2004
Seat
Right
Flight hours
9,387 total · 55 in this make and model · 7,833 as pilot in command · 74 in the last 90 days · 22 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
7 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 63 °F
Altimeter
30.21 inHg
Observed at
ANB, 29 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.