Airworthiness directives › 2016-12-12
AD 2016-12-12 Airworthiness Directives; Fokker Services B.V. Airplanes
Models named: F.27 Mark 050, 200, 300, 400, 500, 600, 700. 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.27 Mark 050, 200, 300, 400, 500, 600, and 700 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 actions required by paragraph (f)(1) of AD 2008-05-18 R1, with revised table reference. For Model F.27 Mark 050, 200, 300, 400, 500, 600, and 700 airplanes, serial numbers 10102 through 10692 inclusive: Within 3 months after April 16, 2008 (the effective date of AD 2008-05-18, Amendment 39-15412 (73 FR 13071, March 12, 2008)), revise the ALS of the Instructions for Continued Airworthiness to incorporate the limits (inspections, thresholds, and intervals) specified in Fokker 50/60 Fuel Airworthiness Limitation Items (ALI) and Critical Design Configuration Control Limitations (CDCCL) Report SE-671, Issue 2, dated December 1, 2006; or Fokker Service Bulletin SBF27-28-070, Revision 1, dated January 8, 2008; as applicable. For all tasks identified in Fokker 50/60 Fuel Airworthiness Limitation Items (ALI) and Critical Design Configuration Control Limitations (CDCCL) Report SE-671, Issue 2, dated December 1, 2006; or Fokker Service Bulletin SBF27-28-070, Revision 1, dated January 8, 2008; the initial compliance times are as specified in Table 1 to paragraph (g) of this AD, as applicable. The repetitive inspections must be accomplished thereafter at the intervals specified in Fokker 50/60 Fuel Airworthiness Limitation Items (ALI) and Critical Design Configuration Control Limitations (CDCCL) Report SE-671, Issue 2, dated December 1, 2006; or Fokker Service Bulletin SBF27-28-070, Revision 1, dated January 8, 2008; as applicable, except as provided by paragraphs (i) and (n)(1) of this AD. Table 1 to Paragraph ( g ) of This AD—Initial Compliance Times for ALS Revision For— The later of— Model F.27 Mark 050 airplanes: Task 280000-01 102 months after April 16, 2008 (the effective date of AD 2008-05-18, Amendment 39-15412 (73 FR 13071, March 12, 2008)); or 102 months after the date of issuance of the original Dutch standard airworthiness certificate or the date of issuance of the original Dutch export certificate of airworthiness. Model F.27 Mark 050 airplanes: Task 280000-02 30 months after April 16, 2008 (the effective date of AD 2008-05-18, Amendment 39-15412 (73 FR 13071, March 12, 2008)); or 30 months after the date of issuance of the original Dutch standard airworthiness certificate or the date of issuance of the original Dutch export certificate of airworthiness. Model F.27 Mark 200, 300, 400, 500, 600, and 700 airplanes: Task 280000-01 78 months after April 16, 2008 (the effective date of AD 2008-05-18, Amendment 39-15412 (73 FR 13071, March 12, 2008)); or 78 months after the date of issuance of the original Dutch standard airworthiness certificate or the date of issuance of the original Dutch export certificate of airworthiness. Model F.27 Mark 200, 300, 400, 500, 600, and 700 airplanes: Task 280000-02 18 months after April 16, 2008 (the effective date of AD 2008-05-18, Amendment 39-15412 (73 FR 13071, March 12, 2008)); or 18 months after the date of issuance of the original Dutch standard airworthiness certificate or the date of issuance of the original Dutch export certificate of airworthiness.
Unsafe condition
This AD was prompted by the issuance of revised service information to update the Fuel Airworthiness Limitation Items (ALIs) and critical design configuration control limitations (CDCCLs) that address fuel tank system ignition sources. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
Affected ADs
This AD replaces AD 2008-05-18 R1, Amendment 39-16083 (74 FR 57402, November 6, 2009) (“AD 2008-05-18 R1”).
Read the original on the Federal Register →
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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