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FTW02LA018 · Piper PA-30

19 Oct 2001 · Ozona, TX, United States

Piper PA-30 · Accident: total loss of engine power (non-mechanical) on approach

From Quahadi Ranch Airport (17XS) to San Angelo Regional Mathis Field (SJT)

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Event

NTSB case
FTW02LA018
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-30

Aircraft type
Piper PA-30
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
N8642Y
Operator
Unknown
Onboard fatalities
Unknown
Route
From Quahadi Ranch Airport (17XS), Lajitas, TXTo San Angelo Regional Mathis Field (SJT), San Angelo, TX
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 pattern final
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)
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
Fuel exhaustion; Wire, transmission
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

  • Fluid, fuel › Exhaustion
  • Pilot in command › Refueling, not performed

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

During dark night light conditions, the pilot landed the airplane on an unlighted runway, taxied to the ramp, boarded the passengers, and taxied for the departure flight. The pilot had not refueled the airplane en route and fuel was not available at this airport. En route at 9,500 msl, the pilot requested and received VFR flight following to the planned refueling destination. Subsequently, the pilot decided to land the airplane for refueling at an en route airport. The pilot reported that he tried to activate the non-towered airport's runway lights and "there were no lights or rotating beacon operating at the airport." After approximately 20-30 minutes of flying over the town and looking for the airport, the left engine lost power, and the pilot feathered the left engine. Subsequently, the right engine lost power. The pilot performed the emergency landing procedures to a vacant lot, and during the approach, the airplane struck power lines. The pilot reported dark night light conditions, clear skies, visibility 30 miles with no restrictions to visibility, and calm wind. No evidence of fuel was found in either the area surrounding the accident site or in the aircraft's fuel tanks. No mechanical discrepancies were found that indicated the engines were incapable of producing power prior to the impact. A preset timer operates the runway lights at the low intensity and the taxiway lights; however, the intensity of the runway lights may be changed when the pilot keys the airplane microphone over the CTAF. Witnesses, the acting airport manager, and the FAA reported the runway lights and the rotating beacon were operational.

Probable cause

The loss of engine power due to fuel exhaustion resulting from the pilot's failure to refuel the airplane. Contributing factors were the lack of suitable terrain for the forced landing and the dark night conditions.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record FTW02LA018
Event ID
20011026X02151
Case number
FTW02LA018
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 2001-10-20.
  • API snapshot SHA-256: ac96081315e62b9678c54a4748a0847eca343a30ec589e850dee0346cb8cbd2e; retrieved 2026-09-21T09:46:02.575Z.