Airworthiness directives › 2014-07-03
AD 2014-07-03 Airworthiness Directives; Fokker Services B.V. Airplanes
Models named: F.28 Mark 0070, 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 F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
(1) Within 24 months after the effective date of this AD: Install the additional bonding provisions at the locations specified in, and in accordance with, Parts 3, 4, 5, and 6 of the Accomplishment Instructions of Fokker Service Bulletin SBF100-28-069, dated August 17, 2012, which includes the attachments identified in paragraphs (g)(1)(i) through (g)(1)(ix) of this AD. (i) Fokker Drawing W31036, Sheet 001, Issue A, dated November 12, 2012. (ii) Fokker Drawing W69280, Sheet 001, Issue A, dated November 12, 2009. (iii) Fokker Drawing W69350, Sheet 001, Issue A, dated November 12, 2009. (iv) Fokker Drawing W69285, Sheet 001, Issue A, dated November 12, 2009. (v) Fokker Drawing W69200, Sheet 001, Issue A, and Sheets 002 through 004, Issue B, all dated November 12, 2009. (vi) Fokker Drawing W69240, Sheet 001, Issue A, and Sheets 002 through 004, Issue B, all dated November 12, 2009. (vii) Fokker Drawing W69335, Sheet 001, dated November 12, 2009. (viii) Fokker Drawing W69405, Sheet 001, dated November 12, 2009. (ix) Fokker Drawing W69710, Sheet 004, Issue B, dated November 12, 2008. (2) At the next scheduled opening of the fuel tanks after the effective date of this AD, but no later than 84 months after the effective date of this AD, install the additional bonding provisions at the locations specified in, and in accordance with, Parts 1, 2, 7, 8, and 9 of the Accomplishment Instructions of Fokker Service Bulletin SBF100-28-069, dated August 17, 2012, which includes the attachments identified in paragraphs (g)(2)(i) through (g)(2)(ix) of this AD. (i) Fokker Drawing W31036, Sheet 001, Issue A, dated November 12, 2012. (ii) Fokker Drawing W69280, Sheet 001, Issue A, dated November 12, 2009. (iii) Fokker Drawing W69350, Sheet 001, Issue A, dated November 12, 2009. (iv) Fokker Drawing W69285, Sheet 001, Issue A, dated November 12, 2009. (v) Fokker Drawing W69200, Sheet 001, Issue A, and Sheets 002 through 004, Issue B, dated November 12, 2009. (vi) Fokker Drawing W69240, Sheet 001, Issue A, and Sheets 002 through 004, Issue B, dated November 12, 2009. (vii) Fokker Drawing W69335, Sheet 001, dated November 12, 2009. (viii) Fokker Drawing W69405, Sheet 001, dated November 12, 2009. (ix) Fokker Drawing W69710, Sheet 004, Issue B, dated November 12, 2008.
Unsafe condition
This AD was prompted by a design review, which revealed that no controlled bonding provisions are present on a number of critical locations inside the fuel tank or connected to the fuel tank wall. We are issuing this AD to prevent an ignition source in the fuel tank vapor space, which could result in a fuel tank explosion and consequent loss of the airplane.
Affected ADs
None.
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