Fuel Exhaustion & Starvation · NTSB CEN10FA385

CESSNA 177B — Owasso, OK

3 fatal Low-time pilot
DateJuly 12, 2010
LocationOwasso, OK
AircraftCESSNA 177B
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceApproach Fuel exhaustion
Pilot age64
Pilot total time314 hrs · Low time
Time in typeUnknown
Fatalities3

Probable cause

The pilot’s failure to maintain adequate airspeed during an engine-out approach to the runway, resulting in an aerodynamic stall and spin. Contributing to the accident was the pilot’s inadequate preflight planning, which resulted in a loss of engine power due to fuel exhaustion.

NTSB findings

  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Personnel issues-Task performance-Inspection-Preflight inspection-Pilot - F
  • Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid management - F

What happened

The pilot and passengers were on the return leg of a cross-country flight. Witnesses reported seeing the airplane approach the airfield in a left turn before losing altitude in a spin. The airplane impacted the ground in a left-wing and nose-low attitude just north and slightly east of the runway. Two witnesses added that the airplane was quiet as it approached the airport; a third witness thought the airplane’s engine was “cutting in-and-out”.

A postaccident examination revealed that both wing tanks were intact and contained no fuel. The grass area underneath each fuel tank did not indicate fuel contamination or fuelblight. The firewall fuel strainer, which sustained impact damage, was absent debris and fuel. The carburetor received impact damage and two of its front attachment bolts were broken. The carburetor’s fuel bowl drain plug was removed and contained only a few drops of fuel. Inspection of the engine and propeller revealed the absence of power signatures. Examination of the engine and airframe revealed no evidence of a mechanical malfunction prior to the accident.

The accident is consistent with the airplane entering a stall/spin as a result of the pilot allowing the airspeed to decay in an attempt to reach the runway in an engine-out situation.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →