DFW06CA084 · Piper PA-28-140
Piper PA-28-140 · Accident: partial loss of engine power (non-mechanical) on approach
From Smith Field (SLG) to Grove Regional Airport (GMJ)
Event
- NTSB case
- DFW06CA084
- 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-28-140
- 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
- N5537F
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Smith Field (SLG), Siloam Springs, ARTo Grove Regional Airport (GMJ), Grove, OK
- 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
- Approach · VFR go-around
- 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)
- 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
- Reason for occurrence undetermined
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The 75-hour private pilot/owner planned a simulated low-approach to an open area within his property where he was planning on building a grass airstrip. The pilot reported that he had no intention to land and had planned to execute a go-around and then continue his flight on to his intended destination. As the pilot approached the field to the south, he added one notch of flaps and retarded the throttle to idle. He did not apply carburetor heat. When the airplane was on final approach, at approximately 200 feet above the ground, the pilot added power to initiate the intended go-around; however, there was no response and power did not increase above idle speed. The pilot was unable to maintain altitude and the airplane landed short of the field, colliding with a fence and tree stumps. The pilot stated that when the airplane first touched down, the engine regained full power but, he immediately pulled the power back to idle to prevent further damage. The pilot and the passenger were able to egress the airplane unassisted and were not injured. Both wings were reported to have sustained structural damage. According to the pilot, he had owned the airplane for approximately seven months and had no previous problems with the engine. At the time of the accident, the temperature was reported as 37 degrees Fahrenheit and the dew point was 21 degrees Fahrenheit. The reason for the intermittent loss of engine power could not be determined.
Probable cause
The loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record DFW06CA084
- Event ID
- 20060412X00432
- Case number
- DFW06CA084
- 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, coordinates. 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: e6d1446d1374976439c30a752dc150f5b0a921be9d4e44b0538df28b2b529295; retrieved 2026-09-22T05:04:18.657Z.