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Dec 22, 2016 at 22:28 history tweeted twitter.com/StackAviation/status/812062159345696769
Dec 7, 2016 at 10:07 vote accept Anso Mamachan
Dec 7, 2016 at 10:06 comment added Anso Mamachan Sorry guys i cannot provide image because it is confidential data. There is no sign of FOD though. the bending of the blades is almost same as your first image. I suspect that the abradable coating in rotor path came chipped off (as a large piece, but it cannot be confirmed because the rubbed area doesn't look so) because of any ovality in casing and it might have struck in between blades and rotor path. Total 5 blades got bended. first in the five got more damage and the following ones got less bend.
Nov 28, 2016 at 17:19 answer added DeltaLima timeline score: 5
Nov 28, 2016 at 16:35 comment added Notts90 Also it's worth noting that on some compressor blade tips the leading edge is deliberately bent slight forward. Hence why a picture would be useful.
Nov 28, 2016 at 16:22 comment added DeltaLima And welcome to Aviation.SE, Anso.
Nov 28, 2016 at 16:21 comment added DeltaLima Is it specifically the leading edge of the tip of the blade that is bend forward?
Nov 28, 2016 at 13:00 comment added Notts90 Not a great deal I think is the answer so if you have one it's a bit worrying. How much is it bent by and where (tip/root)? Pictures would be very helpful!
Nov 28, 2016 at 11:42 history edited user14897
edited tags
Nov 28, 2016 at 10:01 comment added Federico also, can you post a picture?
Nov 28, 2016 at 10:01 history edited Federico CC BY-SA 3.0
added 37 characters in body; edited title
Nov 28, 2016 at 9:58 comment added Manu H You should provide more context to ease the reading of your question.
Nov 28, 2016 at 9:53 review First posts
Nov 28, 2016 at 9:58
Nov 28, 2016 at 9:53 history asked Anso Mamachan CC BY-SA 3.0