MIA99LA069 · Beech A36
Beech A36 · Accident: total loss of engine power (mechanical failure) en route
From Charleston International Airport (CHS) to Hilton Head Airport (HXD)
Event
- NTSB case
- MIA99LA069
- 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
Beech A36
- Aircraft type
- Beechcraft 36
- 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
- N4976M
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Charleston International Airport (CHS)To Hilton Head Airport (HXD), Hilton Head, SC
- 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)
- 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, connecting rod › Failure
- Fluid, oil › Exhaustion
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot reported that about 7 minutes after takeoff the airplane's engine lost oil pressure and started to lose oil, followed by a loss of engine power. The airplane started a descent that the pilot could not arrest, and continued to descend at a rate of about 100-200 feet per minute. The pilot then heard, 'a loud bang...a shudder occurred in the engine compartment, and the engine lost power.' The pilot banked the airplane, and headed towards a clearing. The engine compartment appeared to be on fire, and smoke began to enter the cockpit. He elected to make a forced landing in a field. The engine was examined at the crash site, and a hole was noted in the case at the No. 4 cylinder. Oil was observed on the No. 4 cylinder wall, the oil dip stick did not show any oil, and there was evidence that oil had leaked out of the engine. The engine was examined on February 12, 1999, and the examination revealed that oil had leaked at the engine oil filter adapter. In addition, there were more threads showing on one stud than on the other. A torque wrench was used to check torque on the nuts. It was noted that one nut rotated 1 1/2 rotations before reaching the specified torque. The other nut rotated 1 rotation before reaching torque. The oil filter adapter was removed for further examination, and revealed that the gasket was found with a gap at the corner with a opening of about 1/16 of an inch. It was concluded, that the leak caused the engine to exhaust the oil supply, causing the No. 4 cylinder connecting rod to fail, which resulted in a total loss of engine power.
Probable cause
the total loss of engine power caused by an oil leak at the oil filter adapter, resulting in a broken connecting rod, a subsequent forced landing and impact with rough terrain.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA99LA069
- Event ID
- 20001204X00095
- Case number
- MIA99LA069
- 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: b6e2584416b3fb97f0c5fc785ec056bea3eb366efdaa92e5f13285547f4d45fe; retrieved 2026-09-22T15:56:52.702Z.