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ATL84LA293 · Grumman AA5-B

24 Sept 1984 · LUKA, MS, United States

Grumman AA5-B · Accident: partial loss of engine power (mechanical failure) en route

From Almyra Municipal Airport (M73) to Northeast Alabama Regional Airport (GAD)

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Event

NTSB case
ATL84LA293
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

Grumman AA5-B

Aircraft type
Grumman AA5
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
N74107
Operator
Unknown
Onboard fatalities
Unknown
Route
From Almyra Municipal Airport (M73), ALMYRA, ARTo Northeast Alabama Regional Airport (GAD), GASDEN, AL
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 · 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
Partial loss of engine power (mechanical failure)
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

  • Engine assembly, valve, intake › Separation

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

NTSB narrative

DURING NORMAL CRUISE FLIGHT THE NUMBER ONE CYLINDER EXHAUST VALVE HEAD SEPARATED FROM THE VALVE STEM CAUSING A SIGNIFICANT POWER LOSS. THE PILOT SET UP A LANDING APPROACH TO A FARM FIELD. ON FINAL APPROACH THE PILOT NOTICED THAT ROUGH AND RISING TERRAIN EXISTED IN THE FIELD. DURING A SLIGHT RIGHT TURN AT 10 FT ABOVE THE GROUND THE WING CAUGHTIN SOME WEEDS AND THE ACFT GROUND LOOPED. THE REASON FOR THE EXAUST VALVE HEAD SEPARATION COULD NOT BE DETERMINED.

Verbatim NTSB analysis from the NTSB dataset

Sources

NTSB record ATL84LA293
Event ID
20001214X40980
Case number
ATL84LA293
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: 0e8578435ae69b56e5c6e02977170a77498f8f2908424f655c18174a25b30668; retrieved 2026-09-23T19:04:51.609Z.