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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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November 5, 1989 · Piper PA-28-181 · N47759

Laurel, MD

Overview

Report Status
Probable Cause
Event Type
Accident
Date
November 5, 1989
Injury Outcomes
No injuries (2 uninjured)
Location
Laurel, MD
Aircraft
Piper PA-28-181
Tail Number
N47759
Injuries
None
Aircraft Damage
Substantial
NTSB Number
BFO90FA008

SHORTLY AFTER TAKEOFF, THE ACFT LEVELED AT 1500 FT MSL WHERE THE PLT SET POWER AT 2450 RPM. ACCORDING TO THE PLT, SHORTLY AFTERWARD A PARTIAL POWER LOSS OCCURRED. THE PLT UNSUCCESSFULLY TRIED TO REGAIN POWER. HE TURNED BACK TO THE DEPARTURE ARPT AND HE DID A GO-AROUND WHEN THE FIRST APCH WAS TOO HIGH. ACCORDING TO THE PLT, AS HE CIRCLED TO LAND MORE POWER LOSS OCCURRED AND HE WAS UNABLE TO CONTINUE THE FLIGHT. THE PLT MADE A FORCED LANDING ON A HIGHWAY, STRIKING A GUY WIRE DURING THE APCH. EXAMINATION OF THE ENGINE REVEALED THE NUMBER THREE CYL EXHAUST VALVE HEAD SEPARATED. FRAGMENTS OF THE VALVE HEAD WERE FOUND INSIDE THE NUMBER TWO CYL. METALLURGICAL EXAM OF THE VALVE HEAD REVEALED IT WAS EXPOSED TO ABOVE NORMAL TEMP AND THE FRACTURE WAS CONSISTENT WITH OVERSTRESS.

NTSB Probable Cause

LOST OF ENGINE POWER CAUSED BY MATERIAL FAILURE OF THE NUMBER THREE CYLINDER EXHAUST VALVE. THE FAILURE WAS ATTRIBUTED TO EXCESSIVE TEMPERATURE.

Full Narrative

SHORTLY AFTER TAKEOFF, THE ACFT LEVELED AT 1500 FT MSL WHERE THE PLT SET POWER AT 2450 RPM. ACCORDING TO THE PLT, SHORTLY AFTERWARD A PARTIAL POWER LOSS OCCURRED. THE PLT UNSUCCESSFULLY TRIED TO REGAIN POWER. HE TURNED BACK TO THE DEPARTURE ARPT AND HE DID A GO-AROUND WHEN THE FIRST APCH WAS TOO HIGH. ACCORDING TO THE PLT, AS HE CIRCLED TO LAND MORE POWER LOSS OCCURRED AND HE WAS UNABLE TO CONTINUE THE FLIGHT. THE PLT MADE A FORCED LANDING ON A HIGHWAY, STRIKING A GUY WIRE DURING THE APCH. EXAMINATION OF THE ENGINE REVEALED THE NUMBER THREE CYL EXHAUST VALVE HEAD SEPARATED. FRAGMENTS OF THE VALVE HEAD WERE FOUND INSIDE THE NUMBER TWO CYL. METALLURGICAL EXAM OF THE VALVE HEAD REVEALED IT WAS EXPOSED TO ABOVE NORMAL TEMP AND THE FRACTURE WAS CONSISTENT WITH OVERSTRESS.

Flight

Event TypeAccident
Event Time14:19 EST
Nearest Airport1nm E
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-181
Tail NumberN47759
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A4M · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 34 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind140° @ 6 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point61 F / 48
Altimeter30.00 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data