MIA03LA119 · Piper PA-28R-180
Piper PA-28R-180 · Accident: partial loss of engine power (non-mechanical) during initial climb
From Olive Branch Airport (OLV) to 0M6 · Batesville, MS
Event
- NTSB case
- MIA03LA119
- 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
- Unknown
- 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-28R-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
- N4658J
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Olive Branch Airport (OLV), Olive Branch, MSTo 0M6 · Batesville, MS
- 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
- Initial climb
- 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 (non-mechanical)
- 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
- Pilot in command › Operation with known deficiencies in equipment, attempted
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
After departure from runway 18, about 350 feet above the ground, the pilot reported that the engine "started to sputter." He could not maintain altitude and attempted a forced landing on a taxiway located perpendicular to the departure runway. The airplane struck trees and brush before it impacted with the terrain, approximately 250 feet short of the runway. Examination of the airplane's fuel at the wreckage site revealed the presence of water in the right main fuel tank using water-finding paste. The engine test run revealed that on the initial run the engine would advance to 2,200 rpm and immediately dropped to 1,200 rpm. Examination of the fuel system revealed that the number 4 fuel injector nozzle was 70 percent obstructed with debris, water was found in all the fuel injectors, and the fuel servo screen was found 30 percent obstructed with corrosion. Corrections to the discrepancies were performed, and the engine was tested again with the same results. An examination of the fuel servo revealed that the fuel diaphragm chamber contained deposits of a white milky substance consistent with water contamination in the fuel, and a service bulletin requiring the unit to be overhauled was not complied with. The airplane had flown a total of 11.18 hours since the last annual. The pilot was aware of water infiltration into the right wing fuel tank after heavy rain. The pilot stated on the day of the accident a tablespoon of water was sump from the right wing. The pilot's flight logbook records indicated the accident airplane flew on May 1, 10, and 11 before fueling on May 12, 2003, with 13.7 gallons of 100 LL aviation fuel.
Probable cause
The pilot's operation of the airplane with known deficiencies (water contamination of the fuel) resulting in loss of engine power shortly after takeoff and damage to airframe during the subsequent forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA03LA119
- Event ID
- 20030612X00864
- Case number
- MIA03LA119
- 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: local date, investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2003-06-10.
- API snapshot SHA-256: 59e50a06844d10fbe8969cca319d819037d3a71cf6b4bae07f109dfd96c34d86; retrieved 2026-09-21T19:27:42.973Z.