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ATL03LA072 · Rotorway 162F

27 Mar 2003 · Greensboro, NC, United States

Rotorway 162F · Accident: loss of engine power en route

From Piedmont Triad International Airport (GSO) to an unrecorded destination

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Event

NTSB case
ATL03LA072
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

Rotorway 162F

Aircraft type
Rotorway 162
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
N92AL
Operator
Unknown
Onboard fatalities
Unknown
Route
From Piedmont Triad International Airport (GSO), Greensboro, NCTo not recorded
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
Loss of engine power
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
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 › Preflight planning/preparation, inadequate

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

NTSB narrative

According to the pilot, he flew around the airstrip for approximately 45 minutes. After several passes over the airstrip, the pilot reported he received an electronic control unit (ECU) failure indication light. When the engine lost power, the pilot entered an autorotation. During the touchdown phase of the autorotation, the helicopter rolled over on the left side. During the examination of the helicopter no fuel was found in the fuel tanks or at the accident site. The ECU's were sent to be bench tested. The test revealed, the last 30 seconds of the flight indicated an increase in the throttle position with a corresponding decrease of engine RPM, with a rapid cycling during the final 12 seconds prior to the engine completely shutting down. The data retrieved from the ECUs revealed the flight prior to the accident lasted 10 minutes with a three-minute ground run. The accident flight was approximately 57 minutes. The pilot stated that the helicopter fuel tank capacity is 14 gallons, and can fly for 2 hours or 180 miles with full fuel. According to the pilot, the helicopter departed with 14 gallons of automotive fuel.

Probable cause

The pilot's inadequate preflight planning of fuel required for flight which resulted in fuel exhaustion, and a complete loss of engine power followed by a forced landing, and a dynamic rollover during the autorotative touchdown.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ATL03LA072
Event ID
20030411X00486
Case number
ATL03LA072
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: 613a330ca69d7126a3ce4978812602ae9c796430e450283aa216eff1fa62c8f4; retrieved 2026-09-22T09:28:19.110Z.