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Airworthiness directives › 2017-06-06

AD 2017-06-06 Airworthiness Directives; Fokker Services B.V. Airplanes

Superseded. This directive was replaced by AD 2019-12-10. Work to the current one.
2018-04-03
2018-02-27
39-18830
FAA-2016-9435
Airframe
2019-12-10

Models named: F28 Mark 0070, Mark 0100. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes, certificated in any category, all serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

This paragraph restates the requirements of paragraph (i) of AD 2012-22-15, with revised compliance language. Within 3 months after December 20, 2012 (the effective date of AD 2012-22-15), revise the maintenance program to incorporate the airworthiness limitations specified in Fokker Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 8, released March 17, 2011. For all tasks and retirement lives identified in Fokker Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 8, released March 17, 2011, the initial compliance times start from the later of the times specified in paragraphs (g)(1) and (g)(2) of this AD, and the repetitive inspections must be accomplished thereafter at the applicable interval specified in Fokker Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 8, released March 17, 2011. Doing the revision required by paragraph (k) of this AD terminates the requirements of this paragraph. (1) Within 3 months after December 20, 2012 (the effective date of AD 2012-22-15). (2) At the time specified in Fokker Report SE-623, “Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,” Issue 8, released March 17, 2011.

Unsafe condition

This AD was prompted by a revision of an airworthiness limitations items (ALI) document, which introduces new and more restrictive maintenance requirements and airworthiness limitations. We are issuing this AD to prevent reduced structural integrity of the airplane.

Affected ADs

(1) This AD replaces AD 2012-22-15, Amendment 39-17252 (77 FR 68063, November 15, 2012) (“AD 2012-22-15”). (2) This AD affects AD 2012-12-07, Amendment 39-17087 (77 FR 37788, June 25, 2012) (“AD 2012-12-07”). (3) This AD affects AD 2008-06-20 R1, Amendment 39-16089 (74 FR 61018, November 23, 2009) (“AD 2008-06-20 R1”).

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1