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DFW06CA013 · Hiller UH-12E

22 Oct 2005 · Pasadena, TX, United States

Hiller UH-12E · Accident: total loss of engine power (non-mechanical) en route

From West Houston Airport (KIWS) to Ellington Airport (KEFD)

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Event

NTSB case
DFW06CA013
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

Hiller UH-12E

Aircraft type
Hiller UH-12
Category
Helicopter
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
N909BC
Onboard fatalities
Unknown
Route
From West Houston Airport (KIWS), Houston, TXTo Ellington Airport (KEFD), Houston, 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
En route · 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 (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

  • Fuel system › Exhaustion
  • Pilot in command › Fuel management, inadequate

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

NTSB narrative

The 2,358-hour commercial pilot and his passenger were in cruise flight approximately seven nautical miles north of the airport when the engine lost power. The pilot reported that he entered an autorotation and the helicopter impacted a petroleum coke mound. The helicopter subsequently tumbled down the face of the mound and came to rest on its left side. An FAA inspector performed an on-scene examination of the helicopter. According to the inspector, the helicopter's 46-gallon fuel tank was found to be empty at the accident site. Following the recovery of the wreckage, the inspector tested the fuel tank for leaks and none were found. The inspector stated that the last entry in the maintenance logbooks revealed the Hobbs meter was reading 366.1 hours, and the Hobbs meter at the accident site was reading 369.1 hours. During an interview conducted by the FAA inspector, the mechanic, who performed the last maintenance action prior to the accident flight, revealed that he had removed 44 gallons of fuel from the fuel tank and then placed the same fuel back into the tank after the required maintenance was accomplished. On the day before the accident, the pilot flew to an air show at another nearby airport, from where he flew an unknown number of short flights. Prior to departing the airshow for his home base, the pilot purchased an additional 15 gallons of fuel. On the day of the accident, the pilot flew from DWH to IWS, and then towards his final destination of EFD, when the helicopter lost power. Numerous attempts, albeit unsuccessful, were made by the investigator-in-charge to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) from the pilot.

Probable cause

The pilot's inadequate fuel management, which resulted in fuel exhaustion and a loss of engine power. 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 DFW06CA013
Event ID
20051130X01909
Case number
DFW06CA013
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 2005-10-23.
  • API snapshot SHA-256: 8835286cf9a4a452e76f3df5b6ddc2885a54f8655d2c62abd01fd08036401711; retrieved 2026-09-21T09:01:59.825Z.