Descripción del Accidente ASN 15 MAR 2005 Antonov An-26B-100 OB-1778-P - Lima-J Chavez International Airport (LIM)
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Estado:Accident investigation report completed and information captured
Fecha:martes 15 marzo 2005
Hora:07:21
Tipo:Silhouette image of generic AN26 model; specific model in this crash may look slightly different
Antonov An-26B-100
Operador:Aero Transporte SA - ATSA
Registración: OB-1778-P
Numéro de série: 14205
Año de Construcción: 1985
Horas Totales de la Célula:5798
Ciclos:2451
Motores: 2 Ivchenko AI-24VT
Tripulación:Fatalidades: 0 / Ocupantes: 4
Pasajeros:Fatalidades: 0 / Ocupantes: 0
Total:Fatalidades: 0 / Ocupantes: 4
Daños en la Aeronave: Considerable
Consecuencias: Repaired
Ubicación:Lima-J Chavez International Airport (LIM) (   Perú)
Fase: Despegue (TOF)
Naturaleza:Carga
Aeropuerto de Salida:Lima-Jorge Chávez International Airport (LIM/SPIM), Perú
Aeropuerto de Llegada:Andoas-Alferez FAP Alfredo Vladimir Sara Bauer Airport (AOP/SPAS), Perú
Descripción:
The aircraft started the takeoff roll on runway 33 at Lima (LIM). When reaching VR speed (207 km/h) the copilot announced "rotation" and the captain raised the nose of the airplane. At V2 (242 km/h) it reached a positive climb and the undercarriage was raised. From a height of 5 m the airplane began to descend again. It contacted the runway with the tail and skidded for about 200 meters before coming to rest.
It appears that an overweight takeoff was carried out with flaps at 0 degrees instead of 15 degrees.

Probable Cause:

CONCLUSIONS: "The Aviation Accident Investigation Commission of the Ministry of Transportation and Communications, determines on the probable cause(s) of the accident, as follows:
The impact of the aircraft against the ground without loss of control due to the deficient dispatch, planning, execution of the Checklists and CRM of the crew allowing the takeoff and rotation run to start with overweight (25,798kgs) and 0° of flap since for a weight of 25,000kgs corresponded 15 ° of flaps according to the Flight Manual of the aircraft. Likewise, the failure to abort the takeoff when the configuration alarm did not function.
CONTRIBUTING CAUSES:
- The overweight of the aircraft, which was due to the deficient procedure used by the same crew member who performed the functions of dispatcher and navigator in Lima, by not complying with the provisions of the ATSA company's MGO.
- The Checklists that do not conform to the order indicated in the Flight Manual (Annex 3) of the aircraft."

Accident investigation:

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Investigating agency: CIAA Peru
Status: Investigation completed
Duration: 200 days (7 months)
Accident number: CIAA-ACCID-004-2005
Download report: Final report


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Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Lima-Jorge Chávez International Airport to Andoas-Alferez FAP Alfredo Vladimir Sara Bauer Airport as the crow flies is 1024 km (640 miles).

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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