MIA91LA138

NTSB accident investigation · Piper PA-32-300 · Clearwater, FL · May 9, 1991

Accident · Minor injuriesLimited investigationFinal report
Date
May 9, 1991, 11:00 local (15:00 UTC)
Place
Clearwater, FL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N55653Piper PA-32-300
Weather
Visual (VMC) · Day
Status
Completed · report January 25, 1993
Report
Approved by Office Director
FAA report
19910509014919A
Case key
32864

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

Inadequate annual inspection of the airplane by maintenance personnel who failed to detect a deteriorated oil line. This resulted in oil exhaustion causing the total loss of engine power due to failure of one of the connecting rods. Also inadvertent stall/mush by the pilot.

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(total) - mech failure/malfTakeoff - initial climb
Lubricating system,oil line - deterioratedCause
Maintenance,annual inspection - inadequateOther maintenance personnelCause
Fluid,oil - leak
Fluid,oil - exhaustion
Engine assembly,connecting rod - failure,total
Loss of control - in flightManeuvering - turn to landing area (emergency)
Stall/mush - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water

Analysis

The plt stated the eng was sluggish during the takeoff for the third touch and go landing, followed by a total loss of oil pressure. With insufficient rwy remaining to land he continued to climb & advised the tower of the eng malfunction. He was cleared to land on any rwy but the eng then quit. He initiated a lt turn to return to the arpt. While descending he attempted to correct the nose & lt wing low attitude before impact with the water but stated that the flt controls were unresponsive. The acft was recovered & the eng removed for exam. Exam of the eng revealed a hole in the top of the crankcase near the no. 4 cylinder. The no. 4 cylinder connecting rod was not attached to the crankshaft. The fire sleeves protecting the three oil lines attached to the lt & rt oil coolers were oil soaked. During removal of the fire sleeves, one line broke due to deterioration. The two other lines were examined & found to be deteriorated. The data tags attached to each line indicated that they were manufactured in April 1972.

Aircraft

Registration
N55653
Reported as
Piper PA-32-300
Category
Airplane
Serial number
32-7340131
Airframe hours
3,415
Engine
Lycoming IO-540-K1A5, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Tropicair Pilot'S Club
Registered owner
White, Rodney D.
Last inspection
Annual · November 9, 1990 · 77 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
33
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Toxicology
Performed
Flight hours
287 total · 40 in this make and model · 243 as pilot in command · 30 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 10 knots
Visibility
7 statute miles
Lowest ceiling
2,000 ft broken
Temperature
82 °F, dew point 79 °F
Altimeter
30.00 inHg
Observed at
PIE, 1 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.

Other investigations on N55653 · 1

Matched to the same aircraft by N-number and date.