NYC04CA124

NTSB accident investigation · Fraker Mustang II · Wauseon, OH · May 13, 2004

Accident · Minor injuriesData collectionFinal report
Date
May 13, 2004, 11:00 local (15:00 UTC)
Place
Wauseon, OH
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N78KFraker Mustang II
Weather
Visual (VMC) · Day
Status
Completed · report September 1, 2004
Report
Approved by Office Director
Parties
Cleveland, OH
FAA report
20040513012979A
Case key
59232

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

The failure of the drive coupling between the engine and the propeller speed reducer. A factor related to the accident was the pilot's inadequate preflight inspection of the drive coupling.

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.

Propeller failure/malfunctionApproach - vfr pattern - downwind
Aircraft preflight - inadequatePilot in commandFactor
Propeller system/drive assembly - failureCause
Forced landingDescent - emergency
On ground/water encounter with terrain/waterEmergency descent/landing
Terrain condition - crop

Analysis

According to the pilot, while in the traffic pattern, he heard a loud grinding noise, and noted a subsequent loss of airspeed. As the homebuilt airplane descended, the pilot realized that he would not be able to land on the runway, and performed a forced landing to a field. Examination of the wreckage revealed that the drive coupling between the automotive V8 engine and the propeller speed reducer disconnected. Further examination of the coupling revealed that the rivets holding the coupling together failed. The pilot added, "a better inspection of the drive coupling may have caught this problem."

Factual narrative

On May 13, 2004, at 1100 eastern daylight time, a homebuilt Mustang II, N78K, was substantially damaged during a forced landing, after experiencing a loss of propeller control while landing at the Fulton County Airport (USE), Wauseon, Ohio. The certificated private pilot sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under 14 CFR Part 91.

According to the pilot, while in the traffic pattern at USE, he heard a loud grinding noise, and noted a subsequent loss of airspeed. As the airplane descended, the pilot realized that he would not be able to land on the runway, and performed a forced landing to a field.

The airplane was equipped with an automotive V8 engine, which was connected to a propeller speed reducer by a coupling.

Examination of the wreckage by a Federal Aviation Administration (FAA) inspector revealed that the drive coupling was disconnected. Further examination of the coupling revealed that the rivets holding the coupling together failed.

The pilot added, "a better inspection of the drive coupling may have caught this problem."

Aircraft

Registration
N78K
Reported as
Fraker Mustang II
Category
Airplane, amateur-built
Serial number
MII 952
Airframe hours
716
Engine
General Motors 1962 V-8, 170 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Carlton Fraker
Registered owner
Carlton R. Fraker
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · October 2, 2003 · 20 hours before
Departed
7W5 · Napolean, OH
Destination
USE · Wauseon, OH
Airport
USE · Fulton County Airport, runway 27, 3,882 × 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
61
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
May 9, 2002
Seat
Left
Flight hours
1,428 total · 717 in this make and model · 8 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 66 °F
Altimeter
30.07 inHg
Observed at
TOL

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.