CHI05LA158

NTSB accident investigation · Piper PA-28-180 · Allegan, MI · June 25, 2005

Accident · No injuriesLimited investigationFinal report
Date
June 25, 2005, 10:00 local (14:00 UTC)
Place
Allegan, MI
Injuries
5 uninjured
Phase of flight
Standing
Aircraft
N8321WPiper PA-28-180N569SXMartin Sonex
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2005
Report
Approved by Office Director
Parties
Grand Rapids FSDO
Case key
62303

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 inadequate aircraft control by the PA-28-180 pilot while the airplane was stopped.

The inadequate aircraft control by the Piper PA-28-180 pilot while the airplane was stopped.

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/waterStanding - engine(s) operating
Aircraft control - inadequatePilot in commandCause
On ground/water collision with objectStanding - engine(s) operating
Misc eqpt/furnishings,shoulder harness - not installed
On ground/water collision with objectStanding - engine(s) operating
Aircraft control - inadequatePilot of other aircraftCause

Analysis

A Piper PA-28-180 impacted a Martin Sonex on the ground near the taxiway. Both airplanes were awaiting takeoff clearances when the Piper rolled forward and struck the left horizontal stabilizer and elevator of the Sonex. The pilot of the Piper stated that he was holding in position when he became distracted from holding the brakes while leaning across his right seat passenger to secure the entry door. The airplane then rolled and struck the left horizontal stabilizer and elevator of the Martin Sonex with his propeller. He stated that they taxied with the door open because of the extreme heat and lack cabin air circulation.

A Piper PA-28-180 impacted a Martin Sonex on the ground near the taxiway. Both airplanes were awaiting takeoff clearances when the Piper rolled forward and struck the left horizontal stabilizer and elevator of the Sonex. The pilot of the Piper stated that he was holding in position when he became distracted from holding the brakes while leaning across his right seat passenger to secure the entry door. The airplane then rolled and struck the left horizontal stabilizer and elevator of the Martin Sonex with his propeller. He stated that they taxied with the door open because of the extreme heat and lack cabin air circulation.

Factual narrative

On June 25, 2005, at 1410 eastern daylight time, a Piper PA-28-180, N8321W, impacted a Martin Sonex, N569SX, during an on-ground collision at Padgham Field Airport, Allegan, Michigan. Both airplanes were awaiting takeoff clearance when the Piper PA-28-180 rolled forward while stopped on a taxiway and impacted the Martin Sonex. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal/educational flight was a Experimental Aviation Association's Young Eagles program flight. Neither airplane was operating on a flight plan. The airline transport pilot and three passengers aboard the Piper PA-28-180 were uninjured. The pilot aboard the Martin Sonex was uninjured.

The pilot of the Piper PA-28-180 stated that he was holding in position when he became distracted from holding the brakes while leaning across his right seat passenger to secure the entry door. The airplane then rolled and struck the left horizontal stabilizer and elevator of the Martin Sonex with his propeller. He stated that they taxied with the door open because of the extreme heat and lack cabin air circulation.

The 1965 Piper PA-28-180, serial number 28-2496, was registered to the pilot as co-owner on February 27, 2004. The airplane was not certificated nor equipped with shoulder harnesses.

Advisory Circular 91-65, Use of Shoulder Harness in Passenger Seats, states: "...The safety board [National Transportation Safety Board] found that 20 percent of the fatally injured occupants in these accidents could have survived with shoulder harnesses (assuming the seat belt fastened) and 88 percent of the seriously injured could have had significantly less severe injuries with the use of shoulder harnesses. Energy absorbing seats could have benefited 34 percent of the seriously injuries. The safety board concluded that shoulder harness use is the most effective way of reducing fatalities and serious injuries in general aviation accidents."

On June 25, 2005, at 1410 eastern daylight time, a Piper PA-28-180, N8321W, impacted a Martin Sonex, N569SX, during an on-ground collision at Padgham Field Airport, Allegan, Michigan. Both airplanes were awaiting takeoff clearance when the Piper PA-28-180 rolled forward while stopped on a taxiway and impacted the Martin Sonex. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 personal/educational flight was a Experimental Aviation Association's Young Eagles program flight. Neither airplane was operating on a flight plan. The airline transport pilot and three passengers aboard the Piper PA-28-180 were uninjured. The pilot aboard the Martin Sonex was uninjured.

The pilot of the Piper PA-28-180 stated that he was holding in position when he became distracted from holding the brakes while leaning across his right seat passenger to secure the entry door. The airplane then rolled and struck the left horizontal stabilizer and elevator of the Martin Sonex with his propeller. He stated that they taxied with the door open because of the extreme heat and lack cabin air circulation.

The 1965 Piper PA-28-180, serial number 28-2496, was registered to the pilot as co-owner on February 27, 2004. The airplane was not certificated nor equipped with shoulder harnesses.

Advisory Circular 91-65, Use of Shoulder Harness in Passenger Seats, states: "...The safety board [National Transportation Safety Board] found that 20 percent of the fatally injured occupants in these accidents could have survived with shoulder harnesses (assuming the seat belt fastened) and 88 percent of the seriously injured could have had significantly less severe injuries with the use of shoulder harnesses. Energy absorbing seats could have benefited 34 percent of the seriously injuries. The safety board concluded that shoulder harness use is the most effective way of reducing fatalities and serious injuries in general aviation accidents."

Aircraft · 2

Registration
N8321W
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-2496
Airframe hours
3,548
Engine
Lycoming O-360-A3A, 180 horsepower, reciprocating
Damage
Minor damage
Flight
Personal · Part 91
Operator
Richard Martin
Registered owner
John D. Amundson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 1, 2005 · 3 hours before
Departed
35D · Allegan, MI
Destination
35D
Airport
35D · Padgham Field

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.

Registration
N569SX
Reported as
Martin Sonex
Category
Airplane, amateur-built
Engine
reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Departed
35D · Allegan, MI
Destination
35D · Allegan, MI
Airport
35D · Padgham Field

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot, aircraft N8321W
Age
70
Injuries
None
Certificates
Flight instructor, Airline transport
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2
Last flight review
June 1, 2005
Seat
Left
Flight hours
12,780 total · 262 in this make and model · 10,790 as pilot in command · 21 in the last 90 days · 9 in the last 30 days · 3 in the last 24 hours
Role
Pilot, aircraft N569SX
Injuries
None

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 66 °F
Altimeter
30.06 inHg
Observed at
BIV, 18 nm away

FAA reports on this event · 2

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