Casualties unknown

2013-04-07: Cessna 152 (HK2248) — Barrancabermeja, CO

Barrancabermeja, CO

On April 7, 2013, a Cessna 152 (registration HK2248) was involved in an aviation accident near Barrancabermeja, CO. Investigators recorded the probable cause as: The engine failure was caused by fuel exhaustion during flight, exacerbated by improper flight planning that failed to account for increased fuel consumption due to the aircraft being overweight and operating in a formation-leading role. This summary draws on records from the Aircraft Accident Investigation Group of the Colombian Civil Aviation Authority (GRIAA); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Aircraft Accident Investigation Group of the Colombian Civil Aviation Authority (GRIAA)Primary reportUpdated 1785102594Data APIEditorial standards

A Cessna 152 instructor and student performed an emergency landing in an unprepared field after the engine failed due to fuel exhaustion during a flight training mission.

What happened

On April 7, 2013, a Cessna 152, registration HK-2248 G, was operating as the lead aircraft in a three-plane formation for a flight training mission. The flight, operated by Aeroandes S.A., was traveling from Cartagena toward Barrancabermeja. During the descent phase, approximately 9 nautical miles from the Yarigüies Aerodrome (SKEJ), the student pilot noticed abnormal engine vibrations. The instructor took control of the aircraft and notified the other aircraft in the formation and the control tower of an impending engine failure and an emergency landing in an unprepared field.

While attempting the emergency landing at Finca El Lebrón, approximately 6.5 nautical miles from the aerodrome, the aircraft struck a perimeter wire fence. The impact caused a dynamic rollover, leaving the aircraft in an inverted position. The student pilot was uninjured, while the instructor sustained a minor shoulder injury. Both crew members evacuated the aircraft on their own and were later evacuated by a Colombian Air Force helicopter.

The investigation

The GRIAA investigation focused on the engine, fuel system, and flight planning. Laboratory analysis of fuel samples showed no signs of contamination. A subsequent test of the Lycoming O-320-E2D engine on a test bench confirmed that all components, pressures, and power outputs were within standard operating parameters, ruling out mechanical failure as the cause.

Investigators found that the aircraft was operating with a weight and balance that exceeded the manufacturer's limits. This increased weight resulted in higher drag and required higher power settings to maintain formation speed, which in turn led to increased fuel consumption. Upon inspecting the aircraft after the incident, investigators found only approximately 2 liters of fuel remaining in the distribution lines and wings.

Findings

  • Fuel exhaustion caused the engine to shut down during the flight.
  • The aircraft was operating outside of approved weight and balance parameters, which significantly increased fuel consumption.
  • Inadequate flight planning failed to account for the increased fuel burn rate caused by the heavy load and the requirements of leading a formation.
  • The impact with a fence during the emergency landing caused the aircraft to flip onto its back.

Probable cause

The engine failure was caused by fuel exhaustion during flight, exacerbated by improper flight planning that failed to account for increased fuel consumption due to the aircraft being overweight and operating in a formation-leading role.