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Aviation safety reports, made easier to study

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December 1, 1996 · Piper PA-28-180 · N9545J

Sugarloaf Key, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 1, 1996
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury)
Location
Sugarloaf Key, FL
Aircraft
Piper PA-28-180
Tail Number
N9545J
Operator
Edig Executive Aircraft
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
MIA97LA032

While in cruise flight the engine lost power, and the pilot elected to land on a road. As the airplane touched down the left wing struck the brush on the side of the road, veered left, and turned 180 degrees opposite the direction of travel. Witnesses reported seeing black smoke coming from the engine before impact. The airplane's engine was disassembled, and the examination revealed that the No. 3 connecting rod cap had become detached from the crankshaft assembly, resulting in external damage to the engine. In addition, the remaining connecting rod assemblies were found to be incorrectly installed, and the nuts were all found opposite end down. The No. 2 and No. 4 assemblies were found to be loose.

NTSB Probable Cause

a complete loss of engine power due to a disconnected connecting rod cap.

Full Narrative

On December 1, 1996, about 1200 eastern standard time, a Piper PA-28-180, N9545J, registered to a private owner, operating as a Title 14 CFR Part 91, personal flight, crashed during a forced landing near Sugarloaf Key, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was substantially damage. The private pilot received serious injuries, and one passenger received minor injuries. While in cruise flight the pilot noticed a fluctuation in engine rpm. The engine lost power, and the pilot elected to land on a road. As the airplane touched down the left wing struck the brush on the side of the road, veered left, and turned 180 degrees opposite the direction of travel. Witnesses reported seeing black smoke coming from the engine before impact. The airplane's engine was disassembled under the supervision of the FAA, at Certified Engines Inc., Opa-Locka, Florida, on December 12, 1996. The engine examination revealed that the No. 3 connecting rod cap had become detached from the crankshaft assembly, resulting in external damage to the engine. In addition, the FAA inspector stated, the remaining connecting rod assemblies were found to be "incorrectly installed," and the nuts were "all found opposite end down." The No. 2 and No. 4 assemblies were found to be "loose."

Flight

Event TypeAccident
Event Time12:00 EST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-180
Tail NumberN9545J
Aircraft CategoryAir
DamageSubstantial
OperatorEdig Executive Aircraft
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A4A · Reciprocating · 180
Seats0

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury)
Fatal0
Serious1
Minor1
Uninjured0
Total2
Crew 1Age 35 · Third Class

Conditions

ConditionsUnknown
LightDaylight
Wind5 kt
Visibility10 sm
CeilingBroken clouds 4800 ft
Altimeter30.00 inHg
Observation Time16:53
Weather SourceWFAC

Appendix: Source Data