Status: | Accident investigation report completed and information captured |
Datum: | woensdag 7 juni 2000 |
Tijd: | 19:38 |
Type: |  Boeing 767-241ER |
Luchtvaartmaatschappij: | Varig |
Registratie: | PP-VNN |
Constructienummer: | 23803/161 |
Bouwjaar: | 1987-01-04 (13 years 5 months) |
Aantal vlieguren: | 49134 |
Aantal vluchten: | 20212 |
Motoren: | 2 General Electric CF6-80C2B2 |
Bemanning: | slachtoffers: 0 / inzittenden: 13 |
Passagiers: | slachtoffers: 0 / inzittenden: 178 |
Totaal: | slachtoffers: 0 / inzittenden: 191 |
Schade: | Groot |
Gevolgen: | Repaired |
Plaats: | São Paulo-Guarulhos International Airport, SP (GRU) ( Brazilië)
|
Fase: | Start (TOF) |
Soort vlucht: | Internationale lijnvlucht |
Vliegveld van vertrek: | São Paulo-Guarulhos International Airport, SP (GRU/SBGR), Brazilië |
Vliegveld van aankomst: | Lima-Jorge Chávez International Airport (LIM/SPIM), Peru |
Vluchtnummer: | 886 |
Beschrijving: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:
|
Investigating agency: | CENIPA  |
Status: | Investigation completed |
Duration: | 3 years and 7 months | Accident number: | Final report | Download report: | Final report
|
|
Bronnen:
» NTSB Safety Recommendation A-00-104
»
FAA Airworthiness Directive 2001-10-07
Veiligheidsmaatregelen
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...
Foto's

accident date:
07-06-2000type: Boeing 767-241ER
registration: PP-VNN
Kaart
Deze kaart geeft het vliegveld van vetrek weer en de geplande bestemming van de vlucht. De lijn tussen de vliegvelden geeft
niet de exacte vliegroute weer.
De afstand tussen São Paulo-Guarulhos International Airport, SP en Lima-Jorge Chávez International Airport bedraagt 3463 km (2164 miles).
Accident location: Approximate; accuracy within a few kilometers.
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.