FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

MIA95FA115 · Piper PA-28-180

21 Apr 1995 · Quincy, FL, United States

Piper PA-28-180 · Accident: partial loss of engine power (mechanical failure) during takeoff

From Quincy Municipal Airport (2J9) to LHC · Arlington, TN

Report a problem

Event

NTSB case
MIA95FA115
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
5 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper PA-28-180

Aircraft type
Piper PA-28
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N3995R
Operator
Unknown
Onboard fatalities
Unknown
Route
From Quincy Municipal Airport (2J9)To LHC · Arlington, TN
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Takeoff
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Partial loss of engine power (mechanical failure)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Tree(s)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Engine compartment › Fire
  • Fuel system › Leak
  • Fuel system › Undetermined

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

THE PILOT WAS HEARD TO PERFORM AN ENGINE RUN-UP BEFORE DEPARTURE. THE FLIGHT THEN DEPARTED WITH FULL FUEL TANKS AND ACCORDING TO WITNESSES, CLIMBED TO ABOUT 200-300 FEET ABOVE GROUND LEVEL. A WITNESS NEAR THE CRASH SITE OBSERVED BLACK SMOKE TRAILING THE ENGINE AREA, AND ANOTHER WITNESS HEARD THE ENGINE 'BACKFIRING AND SPUTTERING.' THE AIRPLANE COLLIDED WITH TREES THEN THE GROUND WHILE DESCENDING, AND A POST CRASH FIRE OCCURRED. EXAMINATION OF THE ENGINE COMPARTMENT REVEALED SEVERE (FIRE) DAMAGE TO THE FIREWALL ADJACENT TO THE 2 ELECTRIC FUEL PUMPS AND GASCOLATOR, BUT NO EVIDENCE OF PREIMPACT (INTERNAL) ENGINE FAILURE OR MALFUNCTION WAS FOUND. THE EXAMINATION ALSO REVEALED THAT THE #1 CYLINDER BAFFLE TUBE HAD FAILED CIRCUMFERENTIALLY ALONG A WELD AT THE END PLATE OF THE MUFFLER WITH EVIDENCE OF STRESS CORROSION CRACKING. ALSO, CARBON MONOXIDE WAS DETECTED IN THE PILOT AND TWO OF THE PASSENGERS; ALTHOUGH, NO EVIDENCE OF SOOT DEPOSITION OR BURNING OF THE LARYNX WAS NOTED IN ANY OF THE FIVE OCCUPANTS.

Probable cause

AN UNDETERMINED FUEL SYSTEM PROBLEM THAT RESULTED IN A FUEL LEAK, AN ENGINE COMPARTMENT FIRE, AND A PARTIAL LOSS OF ENGINE POWER. A FACTOR RELATING TO THE ACCIDENT WAS: THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING. AN EXHAUST LEAK FROM THE FRACTURE OF AN IMPROPERLY WELDED BAFFLE TUBE MAY HAVE BEEN THE SOURCE OF IGNITION FOR THE ENGINE COMPARTMENT FIRE.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA95FA115
Event ID
20001207X03337
Case number
MIA95FA115
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: a6b34573baa8e09db9f45aaf6e2c7c18754ca3257af54a131c7f7369eaf8c5d9; retrieved 2026-09-20T23:48:33.806Z.