15 fatalities

Managua-Las Mercedes Airport Crash: Aircraft Destroyed After Takeoff (YS-09C)

Managua-Augusto Cesar Sandino-Las Mercedes, NicaraguaTakeoff (climb)

On March 5, 1959, a Vickers Viscount (registration YS-09C) operated by TACA International Airlines - Transportes Aéreos Centro Americanos was involved in an aviation accident near Managua-Augusto Cesar Sandino-Las Mercedes, Nicaragua during takeoff. 15 people were killed. Investigators recorded the probable cause as: The accident was caused by the failure of engine number 1 before V2 speed, non-retraction of the landing gear after V2 speed, and the failure of engine number 2 during a climb with insufficient speed, which resulted in a forced left turn, an inverted roll,… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-06-12Data APIEditorial standards

An aircraft crashed in flames 2.4 km from Managua-Las Mercedes Airport shortly after takeoff, killing 15 people. The official investigation could not attribute the accident to a specific mechanical or electrical failure or piloting error.

Accident Overview and Casualties Shortly after departing runway 29 at Managua-Las Mercedes Airport, the aircraft entered its initial climb and banked left. It struck the ground in a field 2.4 km from the airport and caught fire. The impact and post-crash fire destroyed the aircraft. Fifteen people were killed, including two crew members, while four occupants survived. ## Official Investigation Findings The investigating board concluded that the accident involved several factors. The number 1 engine failed at the end of runway 29 during takeoff, before the aircraft reached V2 speed. The landing gear did not retract immediately after the aircraft reached V2 speed. Engine number 2 failed a few seconds later during a climb with insufficient speed to maintain control. This led to a forced left turn that became progressively tighter, causing the aircraft to roll inverted and strike a tree with its left wing. ## Cause Determination The board considered several possible reasons for the engine failures and the non-retraction of the landing gear. However, tests on the aircraft's parts did not provide substantiating evidence or proof supporting any one of those reasons. As a result, the board was unable to positively attribute the accident to any mechanical or electrical failure or to any piloting error.

Probable cause

The accident was caused by the failure of engine number 1 before V2 speed, non-retraction of the landing gear after V2 speed, and the failure of engine number 2 during a climb with insufficient speed, which resulted in a forced left turn, an inverted roll, and impact with a tree. The board could not positively attribute the accident to any mechanical or electrical failure or piloting error.