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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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September 1, 1990 · Piper J3C-65 · N70659

Opa-Locka, FL

Overview

Report Status
Probable Cause
Event Type
Accident
Date
September 1, 1990
Injury Outcomes
1 injury (1 minor injury)
Location
Opa-Locka, FL
Aircraft
Piper J3C-65
Tail Number
N70659
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA90LA181

DURING NORMAL CRUISE FLT, THE PLT REPORTED THAT THE RPM WAS DECREASING & THE OIL TEMPERATURE WAS INCREASING. THE ENG THEN SEIZED. WITH POOR FWD VISIBILITY DUE TO OIL COVERING THE WINDSCREEN, HE OVERSHOT THE FIELD HE WAS ATTEMPTING TO LAND IN. THE ACFT COLLIDED WITH A FENCE THEN NOSED OVER. EXAM OF THE ENG REVEALED THAT THE NUMBER 3 CYLINDER CONNECTING ROD END CAP SEPARATED, EXISTED THE CASE & CAME TO REST IN THE OIL SUMP. LYCOMING ENG PERSONNEL STATED THAT THE SEPARATION OF THE ROD CAP WAS DUE TO A LACK OF LUBRICATION WHICH CAUSED THE ROD BOLTS TO STRETCH, LOSING THEIR TORQUE, & ONE OF THE TWO NUTS VIBRATED OFF. THE OTHER ROD BOLT FAILED DUE TO OVERLOAD. THE ENG RECEIVED A TOP OVERHAUL 136 HRS EARLIER & A MAJOR OVERHAUL WAS PERFORMED 2,122 HRS EARLIER. NO DETERMINATION COULD BE MADE AS TO THE REASON FOR THE LACK OF LUBRICATION.

NTSB Probable Cause

ENGINE FAILURE DUE TO LACK OF OIL SUPPLY TO THE NUMBER 3 CYLINDER CONNECTING ROD FOR UNDETERMINED REASONS. THIS ALLOWED THE CONNECTING ROD END CAP TO SEPARATE THROUGH THE CASE RESULTING IN OIL EXHAUSTION.

Full Narrative

DURING NORMAL CRUISE FLT, THE PLT REPORTED THAT THE RPM WAS DECREASING & THE OIL TEMPERATURE WAS INCREASING. THE ENG THEN SEIZED. WITH POOR FWD VISIBILITY DUE TO OIL COVERING THE WINDSCREEN, HE OVERSHOT THE FIELD HE WAS ATTEMPTING TO LAND IN. THE ACFT COLLIDED WITH A FENCE THEN NOSED OVER. EXAM OF THE ENG REVEALED THAT THE NUMBER 3 CYLINDER CONNECTING ROD END CAP SEPARATED, EXISTED THE CASE & CAME TO REST IN THE OIL SUMP. LYCOMING ENG PERSONNEL STATED THAT THE SEPARATION OF THE ROD CAP WAS DUE TO A LACK OF LUBRICATION WHICH CAUSED THE ROD BOLTS TO STRETCH, LOSING THEIR TORQUE, & ONE OF THE TWO NUTS VIBRATED OFF. THE OTHER ROD BOLT FAILED DUE TO OVERLOAD. THE ENG RECEIVED A TOP OVERHAUL 136 HRS EARLIER & A MAJOR OVERHAUL WAS PERFORMED 2,122 HRS EARLIER. NO DETERMINATION COULD BE MADE AS TO THE REASON FOR THE LACK OF LUBRICATION.

Flight

Event TypeAccident
Event Time16:37 EDT
Nearest AirportOpa Locka West (0nm N)
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper J3C-65
Tail NumberN70659
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-235C · Reciprocating · 100
Seats1

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 44 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind130° @ 10 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Observation Time20:55
Weather SourceWFAC

Appendix: Source Data