Overweight takeoff leads to loss of climb performance in Beechcraft Musketeer

Casualties unknown • TMA EPWR, PL

An aircraft operating a private flight experienced a significant reduction in climb rate due to exceeding maximum takeoff mass during high ambient temperatures.

What happened

On June 16, 2018, a Beechcraft A23-19 Musketeer was scheduled for a private flight from EPBC, carrying a pilot and two passengers, along with luggage. At the time of departure, the ambient temperature was 25°C. During the initial takeoff attempt, the pilot observed an unusually slow rate of climb and aborted the takeoff to perform a secondary inspection of the aircraft. No mechanical defects were found during this inspection.

Upon the second takeoff attempt, the aircraft initially achieved a climb rate of approximately 500 ft/min. However, the aircraft subsequently lost power and the rate of climb decreased significantly. Recognizing the performance degradation, the pilot decided to return to the departure airfield, where the aircraft landed safely without further incident.

The investigation

The investigation focused on the aircraft's performance capabilities under the prevailing environmental conditions. Investigators noted that the pilot had not provided a weight and balance sheet for the flight. Based on the estimated weight of the occupants and luggage, it was determined that the Maximum Takeoff Mass (MTOM) was exceeded by approximately 57.5 kg. Additionally, the investigation examined the impact of the 25°C ambient temperature on the aircraft's engine and aerodynamic performance.

Findings

  • The primary cause of the incident was the exceedance of the MTOM combined with high ambient temperatures, which degraded the aircraft's climb performance.
  • The aircraft was fully fueled with 224 liters of fuel at the time of the event.
  • No mechanical or technical failures were identified in the propulsion system during the post-incident inspection.

Probable cause

The incident was caused by the aircraft operating above its maximum takeoff weight during high ambient temperatures, leading to insufficient climb performance.

Frequently asked questions

What happened in the 2018-06-18 Musketeer Ba23 accident near TMA EPWR, PL?

An aircraft operating a private flight experienced a significant reduction in climb rate due to exceeding maximum takeoff mass during high ambient temperatures.

What aircraft was involved and where did it happen?

The accident on 2018-06-18 involved a Musketeer Ba23, registration SP-FGW, operated by Pilot PPL(A), at TMA EPWR, PL.

What was the probable cause of the accident?

The incident was caused by the aircraft operating above its maximum takeoff weight during high ambient temperatures, leading to insufficient climb performance.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2018-1850/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.

Loading the flight search…

What you can do on Flight Finder

  • Search flights between any two airports with live fares.
  • By aircraft — pick a plane model (e.g. Boeing 787, Airbus A350) and see every route it flies from your origin.
  • Route map — click any airport worldwide to explore its destinations, or draw a radius to find nearby airports.
  • Global aviation safety — aviation accident database, 40,000+ records since 1980, with map and rankings by aircraft and operator.
  • NTSB safety feed — recent U.S. aviation accidents and incidents from the official NTSB CAROL database, updated daily.