ASN logo
Last updated: 17 October 2021
Statuts:Enquęte Officielle
Date:mardi 21 juin 2016
Heure:14:39
Type/Sous-type:Silhouette image of generic BE20 model; specific model in this crash may look slightly different
Beechcraft 200C Super King Air
Compagnie:AerCaribe Peru
Immatriculation: OB-2104-P
Numéro de série: BL-14
Année de Fabrication: 1980
Heures de vol:8844
Cycles:8329
Moteurs: 2 Pratt & Whitney Canada PT6A-41
Equipage:victimes: 0 / ŕ bord: 3
Passagers:victimes: 0 / ŕ bord: 0
Total:victimes: 0 / ŕ bord: 3
Dégats de l'appareil: Substantiels
Conséquences: Repaired
Lieu de l'accident:Lima-Jorge Chávez International Airport (LIM) (   Pérou)
Phase de vol: A l'atterrissage (LDG)
Nature:Entrainement
Aéroport de départ:Lima-Jorge Chávez International Airport (LIM/SPJC), Pérou
Aéroport de destination:Lima-Jorge Chávez International Airport (LIM/SPJC), Pérou
Détails:
A Beechcraft Super King Air sustained damage in a landing accident at Lima-Jorge Chavez International Airport (LIM), Peru. The aircraft was engaged in a local training flight. After completion of the flight, the aircraft was prepared for landing. The undercarriage was selected down but the indicator lights show the left hand main landing gear was not locked. After fly-by of the control tower, the controller reported that the landing gear was down.
The crew requested holding west of the airport to perform emergency gear unloading procedures. After performing the checklist procedures, the left main gear light still did not show down and locked. After landing, the left undercarriage retracted until the left wing touched the runway and caused the aircraft to leave towards the left side of the main runway at taxiway B.

Probable Cause:

CAUSE
The Aviation Accident Investigation Commission of the Ministry of Transport and Communications, determines as "Cause of the Accident", the following:
"Retraction of the left main gear at the time of landing, due to the absence of a taper pin that did not allow the connection of the electric motor with the torque tube and mechanical actuator for the extension and securing of the main gear, which generated the runway exit (Runway Excursion)".
CONTRIBUTING FACTORS
a. Deficient Quality Control process during the execution of the Phase 3 Inspection to the torque tube, which did not detect the bad installation of the self-tapping nut in the Taper Pin (Taper Pin N°13), which prevented the correct operation of the mechanical chain of motion transmission to properly extend and keep secured the left main train.

Accident investigation:
cover
Investigating agency: CIAA Peru
Status: Investigation completed
Accident number: CIAA-ACCID-007-2016
Download report: Final report

Sources:
» Géstion


Photos

photo of Beechcraft-200C-Super-King-Air-HK-4969
accident date: 21-06-2016
type: Beechcraft 200C Super King Air
registration: HK-4969
 

Video, social media

Plan

Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus ŕ ce jour.
languages: languages

Share