MIA94LA123

NTSB accident investigation · Piper PA-24-260 · Spring Hill, FL · April 16, 1994

Accident · No injuriesLimited investigationFinal report
Date
April 16, 1994, 08:15 local (12:15 UTC)
Place
Spring Hill, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8572PPiper PA-24-260
Weather
Visual (VMC) · Day
Status
Completed · report December 7, 1994
Report
Approved by Office Director
FAA report
19940416011009A
Case key
37532

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

Unsuitable terrain encountered during a forced landing. Contributing to the accident was the fatigue failure of one of the propeller blade's pitch change knob.

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.

Airframe/component/system failure/malfunctionCruise - normal
Propeller system/accessories,pitch change mech - fatigueFactor
Propeller system/accessories,pitch change mech - failure,totalFactor
Forced landingDescent - emergency
In flight collision with terrain/waterLanding
Terrain condition - uphill
Unsuitable terrain or takeoff/landing/taxi area - encounteredPilot in commandCause

Analysis

During cruise flight the pilot reported a severe vibration. During the forced landing the airplane collided with terrain and came to rest upright. Examination of the propeller revealed that a pitch change knob on one of the propeller blades was failed. Metallurgical examination of the failed pitch change knob revealed that it failed due to fatigue.

Factual narrative

On April 16, 1994, about 0815 eastern daylight time, a Piper PA-24-260, N8572P, registered to Roger L. Millheim, was substantially damaged during a forced landing near the Pilot Country Airport, Spring Hill, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The commercial-rated pilot, the sole occupant, was not injured. The flight originated from the Pilot Country Airport, Spring Hill, Florida, about 7 minutes earlier.

The pilot stated that during cruise flight he felt a severe vibration through the airframe which he attributed to be from the propeller. He attempted a forced landing on a road but during the descent, the airplane collided with the top of a 40-foot-tall dirt embankment. The airplane slid over the top down the other side coming to rest upright.

The propeller was removed for examination which revealed that a pitch change knob on one of the propeller blades was failed. The failed knob and butt end of the propeller blade was sent to the NTSB Metallurgy Laboratory in Washington, DC, for examination.

Metallurgical examination of the failed pitch change knob revealed that it failed due to fatigue.

Review of the aircraft logbooks revealed that the propeller was overhauled on June 28, 1989. At the time of the accident the propeller had accumulated about 397 hours since overhaul.

Aircraft

Registration
N8572P
Reported as
Piper PA-24-260
Category
Airplane
Serial number
24-4029
Airframe hours
4,097
Engine
Lycoming IO-540-D4A5, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Millheim, Roger L.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 24, 1993 · 41 hours before

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
47
Certificate
Commercial
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,865 total · 420 in this make and model · 2,410 as pilot in command · 78 in the last 90 days · 29 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 5 knots
Visibility
12 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 70 °F
Altimeter
30.00 inHg
Observed at
TPA, 21 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.