Oostende Tuesday: An-124 aborts takeoff due engine failure..

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Stratofreighter
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Posts: 22202
Joined: 25 Jan 2006, 08:02
Location: Netherlands

Oostende Tuesday: An-124 aborts takeoff due engine failure..

Post by Stratofreighter »

...see
https://www.aviation24.be/airlines/anto ... t-belgium/

Of course Wiloo "has a field day", now... :roll:
https://twitter.com/wiloo_vzw/status/11 ... 1825570816

http://avherald.com/h?article=4cfcb737&opt=0
Incident: Antonov A124 at Ostend on Nov 26th 2019, rejected takeoff due to engine problem

An Antonov Design Bureau Antonov AN-124-100, registration UR-82072
performing flight ADB-5250 from Ostend (Belgium) to Mazar-i-Sharif (Afghanistan),
was accelerating for takeoff from Ostend's runway 26 at about 19:05L (18:05Z)
when the crew rejected takeoff at high speed (about 110 knots over ground) :shock:
due to a poblem with the #2 engine (D-18T, inboard left hand).

The aircraft slowed safely and returned to the apron.
Engine debris was collected from the runway.
http://avherald.com/h?article=4cfcb737&opt=0
November 2024 update at FokkerNews.nl....
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Stratofreighter
Scramble Master
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Posts: 22202
Joined: 25 Jan 2006, 08:02
Location: Netherlands

Re: Oostende Tuesday: An-124 aborts takeoff due engine failu

Post by Stratofreighter »

http://avherald.com/h?article=4cfcb737&opt=0
last updated Sunday, Mar 22nd 2020 15:54Z

On Mar 11th 2020
the State Aviation Administration of Ukraine released their Airworthiness Directive AD-0890-20
stating that an uncontained engine failure had occurred.

The source of the failure had been the destruction of the 2nd stage disk rim of the intermediate pressure compressor.

The AD requires:

Within a period of 6 months or until an engine time in service will be 250+50 hours (whichever comes first)
after effective date of this AD,

conduct one-time eddy current inspection of the 2nd stage disk dovetails of the intermediate pressure compressor
in accordance with the instructions
of the "Service Bulletin for Inspection No. ISB 18T-72.30-137" of SE "Ivchenko-Progress".

The results of AD implementation shall be sent
to the engine manufacturer JSC MOTOR SICH and the TC holder SE Ivchenko-Progress within 3 working days.

In case if any cracks are detected in the area of 2nd stage disk ovetails of the intermediate pressure compressor
the engine shall be removed from aircraft
and corrective actions in accordance with the instructions of SE Ivchenko-Progress shall be performed.
http://avherald.com/h?article=4cfcb737&opt=0
November 2024 update at FokkerNews.nl....
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