MIA00LA007 · Piper PA-28-161
Piper PA-28-161 · Accident: total loss of engine power (non-mechanical) during initial climb
From Cedar Crest Field (1TN0) to John C Tune Airport (JWN)
Event
- NTSB case
- MIA00LA007
- 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
Piper PA-28-161
- 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
- N3013C
- Operator
- Hiram L. Allen · private individual
- Onboard fatalities
- Unknown
- Route
- From Cedar Crest Field (1TN0)To John C Tune Airport (JWN), Nashville, TN
- 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
- Total 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
- Other maintenance personnel › Maintenance, inspection, inadequate
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
After takeoff about 75 feet agl, the engine experienced a total loss of engine power. The pilot landed the airplane on the remaining runway and collided with trees, separating the right wing. Post accident examination of the airplane by an FAA inspector revealed that the gascolator bowl was loose and fuel leakage was noted at the gascolator when the auxiliary fuel pump was turned on. The threaded portion of the bail wire P/N 494 644, was noted to have 2 1/2 failed threads near the top. The gascolator was bypassed, the engine was started and found to operate normally. During the last annual inspection, the gascolator seal was replaced. It was reported by the pilot that on the first takeoff following the annual inspection, the engine experienced a loss of power in an identical manner; an uneventful landing occurred. Following the uneventful landing, the mechanic who performed the annual inspection and the pilot noted that the gascolator seal was not seated properly. A rubber gascolator seal was installed to replace the cork type seal that had been installed during the annual inspection. The airplane had accumulated approximately 3 hours since the annual inspection at the time of the accident.
Probable cause
The inadequate annual inspection of the airplane by the mechanic for his failure to note that the threaded portion of the bail wire had 2 1/2 failed threads which resulted in the inability to keep the gascolator bowl tightly secured. Also his failure to note this condition during replacement of the gascolator seal following a similar loss of engine power on the first takeoff following the annual inspection which was performed approximately 3 hours earlier. A contributing factor to the accident was the unsuitable terrain encountered by the pilot during the forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA00LA007
- Event ID
- 20001212X20010
- Case number
- MIA00LA007
- 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: d96329cf753f3498fb9dc72aa0ffa622f9cecefcea0ffe8c3e772ed1671912df; retrieved 2026-09-21T20:22:15.376Z.