Statuts: | Accident investigation report completed and information captured |
Date: | mercredi 7 juin 2000 |
Heure: | 19:38 |
Type/Sous-type: |  Boeing 767-241ER |
Compagnie: | Varig |
Immatriculation: | PP-VNN |
Numéro de série: | 23803/161 |
Année de Fabrication: | 1987-01-04 (13 years 5 months) |
Heures de vol: | 49134 |
Cycles: | 20212 |
Moteurs: | 2 General Electric CF6-80C2B2 |
Equipage: | victimes: 0 / à bord: 13 |
Passagers: | victimes: 0 / à bord: 178 |
Total: | victimes: 0 / à bord: 191 |
Dégats de l'appareil: | Substantiels |
Conséquences: | Repaired |
Lieu de l'accident: | São Paulo-Guarulhos International Airport, SP (GRU) ( Brésil)
|
Phase de vol: | Au décollage (TOF) |
Nature: | Transport de Passagers Intern. |
Aéroport de départ: | São Paulo-Guarulhos International Airport, SP (GRU/SBGR), Brésil |
Aéroport de destination: | Lima-Jorge Chávez International Airport (LIM/SPIM), Pérou |
Numéro de vol: | 886 |
Détails:Varig Flight 886 to Lima, Peru, experienced an uncontained failure of the HPC stage 3-9 spool in the No. 2 (right) General Electric CF6-80C2B2 engine during takeoff. The flight crew reported that at a speed of about 60 knots, they heard a loud bang. They rejected the takeoff and stopped the airplane on the runway. The copilot opened the right-side cockpit window to look out and advised the pilot that there was a fire around the right main landing gear. The flight crew reported that they then attempted to taxi clear of the fire but stopped the airplane on the runway again when they realized it was the engine that was on fire and ordered an evacuation. Although the flight crew discharged both fire bottles into the No. 2 engine nacelle, the fire continued until it was extinguished by airport fire department personnel.
Probable Cause:
Contributing factors (translated from Portuguese):
Material factor
(1) Design Deficiency - Contributed
The inspection by penetrating liquid, scheduled to be executed on the HPC stage 3-9 spool, failed to ensure the detection of cracks caused by DTF ("Dwell-Time Fatigue"), such as that caused the failure in this accident.
(2) Deficiency manufacturing - Contributed
The HPC stages 3-9 spool failure occurred because the existence of an area of quasi-cleavage, originating from the manufacturing process of the same.
Accident investigation:
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Investigating agency: | CENIPA  |
Status: | Investigation completed |
Duration: | 3 years and 7 months | Accident number: | Final report | Download report: | Final report
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Sources:
» NTSB Safety Recommendation A-00-104
»
FAA Airworthiness Directive 2001-10-07
Opérations de secours
FAA issued 1 Airworthiness Directive
NTSB issued 1 Safety Recommendation
Issued: 09-AUG-2000 | To: FAA | A-00-104 |
IMMEDIATELY ISSUE AN AIRWORTHINESS DIRECTIVE (AD) TO REQUIRE THE EXPEDITIOUS REMOVAL FROM SERVICE OF CF6-50 AND -80 SERIES ENGINES WITH HIGH PRESSURE COMPRESSOR STAGE 3-9 SPOOLS THAT ARE MOST AT RISK OF RUPTURING AND INSPECT THOSE SPOOLS IN ACCORDANCE WITH AD 99-24-15 AND ENGINE MANUAL INSTRUCTIONS. (Closed - Acceptable Action) |
Issued: 21-AUG-2000 | To: | AD 2000-16-12 |
Requiring "...initial ultrasonic and eddy current inspections of certain HPCR stage 3-9 spools for cracks." |
Show all...
Photos

accident date:
07-06-2000type: Boeing 767-241ER
registration: PP-VNN
Plan
Ce plan montre l'aéroport de départ ainsi que la supposée destination du vol. La ligne fixe reliant les deux aéroports n'est pas le plan de vol exact.
La distance entre São Paulo-Guarulhos International Airport, SP et Lima-Jorge Chávez International Airport est de 3463 km (2164 miles).
Accident location: Approximate; accuracy within a few kilometers.
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 à ce jour.