CHI03LA322

NTSB accident investigation · Stinson 108-3 · Lincoln, NE · September 27, 2003

Accident · Minor injuriesLimited investigationFinal report
Date
September 27, 2003, 15:30 local (20:30 UTC)
Place
Lincoln, NE
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N6624MStinson 108-3
Weather
Visual (VMC) · Day
Status
Completed · report June 2, 2004
Report
Approved by Office Director
Parties
FAA- Lincoln FSDO
FAA report
20030927024739A
Case key
58015

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 total loss of engine power due to the fatigue fracture of the engine accessory gear drive. A factor was the concrete marker.

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 powerCruise
Engine assembly,gear - fatigueCause
Engine assembly,gear - failure,totalCause
Forced landingEmergency descent/landing
On ground/water collision with objectLanding - roll
Object - signFactor
Nose overLanding - roll

Analysis

The airplane sustained substantial damage during a forced landing. The pilot reported that the engine failed at 3,000 feet mean sea level during cruise flight. While on his landing roll on a sod field, the airplane struck a concrete marker and the airplane nosed over. The inspection of the airplane revealed the accessory gear drive was fractured in two pieces and had become dislodged from the crankshaft. A metallurgical examination of the accessory gear drive revealed a fatigue fracture at the key way.

Factual narrative

On September 27, 2003, at 1530 central daylight time, a Stinson 108-3, N6624M, piloted by a commercial pilot, sustained substantial damage when it lost engine power and nosed over while attempting to land in a field 6 nautical miles north-northeast of Lincoln Municipal Airport (LNK), Lincoln, Nebraska. Visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot sustained minor injuries. The flight departed the Fremont Municipal Airport (FET), Fremont, Nebraska, at 1510.

The pilot reported that the engine failed while in cruise flight at 3,000 feet mean sea level. The engine could not be restarted, and a forced landing was made to a sod field. During the landing roll, the airplane struck a concrete marker and nosed over.

A Federal Aviation Administration (FAA) airworthiness inspector examined the airplane. The exam revealed that the accessory gear drive was fractured in two pieces, and had become dislodged from the crankshaft. He reported, "a corrosion spot was observed protruding off of the keyway propagating towards the outside of the gear." Metal shavings were found in the accessory area and in the oil reservoir.

The accessory gear drive was inspected by Engineering Systems Inc., (ESI), Aurora, Illinois, on January 13, 2004. The inspection revealed that a fatigue fracture had initiated at the key way that held the gear on the rotating shaft.

Aircraft

Registration
N6624M
Reported as
Stinson 108-3
Category
Airplane
Serial number
108-4624
Airframe hours
2,137
Engine
Franklin 6A4-165-B3, 165 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Steven P Becker
Registered owner
Steven Becker
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 19, 2002 · 20 hours before
Departed
FET · Fremont, NE
Destination
LNK · Lincoln, NE

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
53
Injuries
Minor
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
March 28, 2003
Seat
Left
Flight hours
2,600 total · 695 in this make and model · 2,440 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
330° at 23 knots, gusting 29
Visibility
10 statute miles
Lowest ceiling
7,000 ft broken
Temperature
64 °F, dew point 30 °F
Altimeter
30.01 inHg
Observed at
LNK, 6 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.