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ATL97LA009 · Mooney M20K

25 Oct 1996 · AMELIA ISLAND, FL, United States

Mooney M20K · Accident: total loss of engine power (mechanical failure) en route

From 55J to Kissimmee Gateway Airport (ISM)

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Event

NTSB case
ATL97LA009
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
0 · 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

Mooney M20K

Aircraft type
Mooney M20
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
N32DG
Operator
Jack B. Healan, JR · private individual
Onboard fatalities
Unknown
Route
From 55JTo Kissimmee Gateway Airport (ISM), Kissimmee, FL
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
En route · climb to cruise
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
Total 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
Substantial

Cause areas

  • Fuel system, pump › Pressure excessive
  • Ignition system, magneto › Corroded
  • Maintenance, inspection › Inadequate

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

NTSB narrative

During the climb after takeoff, the engine began to run rough, then lost power. According to the pilot, he turned on the boost pump, and the engine quit. The pump was turned off, the engine surged, then quit again. During a forced landing, the airplane struck trees, then came to rest on a street. Postaccident examination of the engine revealed corrosion in the left magneto, which was indicative of moisture contamination of the magneto that may have resulted in a loss of power. Additionally, the engine driven fuel pump pressure was set high, which would have resulted in a rich mixture, when the boost pump was activated. The engine had been equipped with pressure type, Slick Electro Model 6224 magnetos. A service bulletin, applicable to another aircraft manufacturer, had been issued by the magneto manufacturer to inspect the pressurized magnetos each 100 hours for evidence of moisture contamination. The same information was contained in the magneto maintenance and overhaul manual. The airplane was maintained under an annual inspection program, with no intervening 100 hour inspections; 159 hours of flight time had been accumulated since the last annual inspection.

Probable cause

inadequate maintenance/inspection, which resulted in a failure to detect and correct moisture contamination of the left magneto; and/or improper adjustment of the engine fuel pump output, which resulted in excessive fuel pressure.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ATL97LA009
Event ID
20001208X06840
Case number
ATL97LA009
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: 4bdd37fb480ffaa3734f6a19224fe5eca8cf7a5961d634dc01154870f9b58936; retrieved 2026-09-21T12:21:39.041Z.