Casualties unknown

Piper PA-36-285 Crash During Agricultural Spraying in Ciudad Real (EC-CUU)

Granátula de Calatrava (Ciudad Real), ES

On June 1, 2004, a Piper PA-36-375 (registration EC-CUU) was involved in an aviation accident near Granátula de Calatrava (Ciudad Real), ES. Investigators recorded the probable cause as: The accident was caused by the pilot attempting a takeoff from an unpaved strip that was too short for the aircraft's weight and configuration. The aircraft was overloaded (2,004 kg vs. 1,996 kg max), and the required takeoff distance (approx. This summary draws on records from the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC).

Sourcesthe Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC)Primary reportUpdated 2026-09-13Data APIEditorial standards

On June 1, 2004, a Piper PA-36-285 (EC-CUU) crashed during takeoff from an unpaved strip in Granátula de Calatrava. The aircraft was overloaded for the short runway and failed to gain altitude, striking olive trees. The pilot survived.

Incident Overview

On Tuesday, June 1, 2004, at approximately 08:30 local time, a Piper PA-36-285 Brave with registration EC-CUU crashed while attempting to take off from an unpaved agricultural track in the municipality of Granátula de Calatrava, Ciudad Real. The aircraft was engaged in commercial aerial work, specifically spraying olive trees with a mixture of water and pesticide.

Flight Sequence and Impact

The pilot initiated the takeoff roll on a 500-meter strip. After traveling approximately 400 meters, the aircraft failed to lift off. The pilot activated the emergency dump system, releasing two-thirds of the cargo, but the plane only gained a few meters of altitude before reaching the end of the usable runway. Unable to climb, the pilot released the remaining load. The aircraft drifted right and descended into an olive grove.

The first impact occurred when the right wing struck an olive tree, causing the aircraft to yaw. Subsequent impacts with other trees damaged the horizontal stabilizers, elevator, left main landing gear, and fuselage. The aircraft finally came to rest after rotating 90 degrees to the left. The pilot, a 68-year-old commercial pilot with an estimated 20,000 flight hours, exited the wreckage unharmed.

Investigation Findings

The investigation revealed that the aircraft was overloaded for the short runway. Calculations indicated a total weight of 2,004 kg, exceeding the maximum takeoff weight of 1,996 kg. The required takeoff distance with zero flaps was estimated at 490 meters, which exceeded the available 500-meter strip when accounting for safety margins and surface conditions.

Additionally, there were discrepancies regarding the control yoke. The installed grip did not match any part number in the operator's 1981 parts catalog. The pilot believed a flap switch was mounted on the yoke, but the aircraft manual indicated the flap switch was located on the left console. This confusion may have contributed to the failure to deploy flaps for takeoff, which would have reduced the required runway length.

Probable cause

The accident was caused by the pilot attempting a takeoff from an unpaved strip that was too short for the aircraft's weight and configuration. The aircraft was overloaded (2,004 kg vs. 1,996 kg max), and the required takeoff distance (approx. 490 m) exceeded the available runway length (500 m). Contributing factors included potential confusion over flap deployment due to a non-standard control yoke installation.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2004_028_a_0.pdf. This page is a structured re-presentation; facts and quotes are in the Comision de Investigacion de Accidentes e Incidentes de Aviacion Civil (CIAIAC), Spain - Ministerio de Transportes y Movilidad Sostenible.