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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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August 2, 1988 · Beech A36TC · N3707Z

Vega, TX

Overview

Report Status
Preliminary report
Event Type
Accident
Date
August 2, 1988
Injury Outcomes
No injuries (3 uninjured)
Location
Vega, TX
Aircraft
Beech A36TC
Tail Number
N3707Z
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW88LA142

THE AIRPLANE WAS ON A NIGHT CROSS COUNTRY FLIGHT WHEN ENGINE OIL STARTED TO APPEAR ON THE WINDOWS. THE PILOT WAS UNABLE TO GET THE AIRPLANE TO AN AIRPORT BEFORE THE OIL PRESSURE WENT TO ZERO. AFTER LOSS OF OIL PRESSURE, THE ENGINE STARTED TO VIBRATE, AND THE PROPELLER SEPARATED FROM THE ENGINE. WITH NO FORWARD VISIBILITY AND VERY LITTLE SIDE VISIBILITY, THE PILOT MADE A FORCED LANDING ON A HIGHWAY SERVICE ROAD; HOWEVER, DURING THE LANDING ROLL, THE AIRPLANE IMPACTED HIGHWAY SIGNS AND REFLECTORS. THE PILOT SAID THERE WAS A FIRE ON THE HIGHWAY, BEHIND THE AIRPLANE, BUT IT NEVER REACHED THE AIRPLANE. A TEARDOWN OF THE ENGINE REVEALED A FAILURE OF THE CRANKSHAFT THAT WAS INITIATED BY A PRE-EXISTING FATIGUE CRACK. THERE WAS EVIDENCE THAT OPENING OF THE FATIGUE CRACK LED TO GRADUAL LOSS OF LUBRICATING OIL, THEN SEPARATION OF THE PROPELLER.

Full Narrative

THE AIRPLANE WAS ON A NIGHT CROSS COUNTRY FLIGHT WHEN ENGINE OIL STARTED TO APPEAR ON THE WINDOWS. THE PILOT WAS UNABLE TO GET THE AIRPLANE TO AN AIRPORT BEFORE THE OIL PRESSURE WENT TO ZERO. AFTER LOSS OF OIL PRESSURE, THE ENGINE STARTED TO VIBRATE, AND THE PROPELLER SEPARATED FROM THE ENGINE. WITH NO FORWARD VISIBILITY AND VERY LITTLE SIDE VISIBILITY, THE PILOT MADE A FORCED LANDING ON A HIGHWAY SERVICE ROAD; HOWEVER, DURING THE LANDING ROLL, THE AIRPLANE IMPACTED HIGHWAY SIGNS AND REFLECTORS. THE PILOT SAID THERE WAS A FIRE ON THE HIGHWAY, BEHIND THE AIRPLANE, BUT IT NEVER REACHED THE AIRPLANE. A TEARDOWN OF THE ENGINE REVEALED A FAILURE OF THE CRANKSHAFT THAT WAS INITIATED BY A PRE-EXISTING FATIGUE CRACK. THERE WAS EVIDENCE THAT OPENING OF THE FATIGUE CRACK LED TO GRADUAL LOSS OF LUBRICATING OIL, THEN SEPARATION OF THE PROPELLER.

Flight

Event TypeAccident
Event Time23:17 CDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftBeech A36TC
Tail NumberN3707Z
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · TSIO-520-UB · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 35 · First Class

Conditions

ConditionsVMC
LightDark Night
Wind170° @ 15 kt
Visibility25 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data