Federal Aviation Administration (FAA), DOT.
Notice of proposed rulemaking (NPRM).
We propose to supersede Airworthiness Directive (AD) 2012–22–15 for all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes. AD 2012–22–15 currently requires revising the maintenance program to incorporate the limitations, tasks, thresholds, and intervals specified in certain revised Fokker maintenance review board (MRB) documents. Since we issued AD 2012–22–15, we received new revisions of airworthiness limitations items (ALI) documents, which introduce new and more restrictive maintenance requirements and airworthiness limitations. This proposed AD would require revising the maintenance or inspection program to incorporate new maintenance requirements and airworthiness limitations. We are proposing this AD to prevent the unsafe condition on these products.
We must receive comments on this proposed AD by January 30, 2017.
You may send comments by any of the following methods:
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For service information identified in this NPRM, contact Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL Hoofddorp, the Netherlands; telephone: +31 (0)88–6280–350; fax: +31 (0)88–6280–111; email:
You may examine the AD docket on the Internet at
Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1137; fax 425–227–1149.
We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the
We will post all comments we receive, without change, to
On October 30, 2012, we issued AD 2012–22–15, Amendment 39–17252 (77 FR 68063, November 15, 2012) (“AD 2012–22–15”). AD 2012–22–15 requires actions intended to address an unsafe condition on all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes.
Since we issued AD 2012–22–15, we received Fokker Services Engineering Reports that consist of new and more restrictive airworthiness limitations (ALS).
The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive AD 2016–0125, dated June 21, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or “the MCAI”), to correct an unsafe condition for all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes. The MCAI states:
Fokker Services recently published issue 15 of Engineering Report SE–623, containing Airworthiness Limitation Items (ALIs) and Safe Life Items (SLIs). This report is Part 2 of the Airworthiness Limitations Section (ALS Part 2) of the Instructions for Continued Airworthiness, referred to in Section 06, Appendix 1, of the Fokker 70/100 Maintenance Review Board document.
The complete ALS currently consists of:
Part 1—Report SE–473, Certification Maintenance Requirements (CMRs)—reference: EASA AD 2015–0027 [which corresponds to FAA AD 2016–11–22, Amendment 39–18549 (81 FR 36438, June 7, 2016)].
Part 2—Report SE–623, ALIs and SLIs—reference: EASA AD 2014–0224 [which corresponds to FAA AD 2012–22–15], and
Part 3—Report SE–672, Fuel ALIs and CDCCLs—reference: EASA AD 2015–0032 [which corresponds to FAA AD 2016–11–15, Amendment 39–18542 (81 FR 36447, June 7, 2016)].
The instructions contained in those reports have been identified as mandatory actions for continued airworthiness. Failure to accomplish these actions could result in an unsafe condition.
EASA previously issued AD 2014–0224, requiring the actions described in ALS Part 1 (report SE–473 issue 10), Part 2 (report SE–623 issue 13) and Part 3 (report SE–672 issue 4). Since that [EASA] AD was issued, ALS Part 1 was revised (SE–473 issue 11) and EASA issued AD 2015–0027 accordingly. ALS Part 3 was also revised (SE–672 issue 5) and EASA issued AD 2015–0032 accordingly.
For the reasons described above, this [EASA] AD retains part of the requirements of [EASA] AD 2014–0224, which is superseded, and requires implementation of the maintenance actions as specified in ALS Part 2 of the Instructions for Continued Airworthiness, Fokker Services Engineering Report SE–623 at issue 15 (hereafter referred to as `ALS Part 2' in this [EASA] AD).
You may examine the MCAI in the AD docket on the Internet at
Fokker Services B.V. has issued Fokker Services B.V. Engineering Report SE–623, “Fokker 70/100 ALI's and SLI's,” Issue 16, issued June 3, 2016. The service information describes new and more restrictive maintenance requirements and airworthiness limitations. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the
This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design.
This proposed AD would require revisions to certain operator maintenance documents to include new actions (
We estimate that this proposed AD affects 15 airplanes of U.S. registry.
The actions required by AD 2012–22–15, and retained in this proposed AD, take about 1 work-hour per product, at an average labor rate of $85 per work-hour. Based on these figures, the estimated cost of the actions that are
We also estimate that it would take about 1 work-hour per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $1,275, or $85 per product.
Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. “Subtitle VII: Aviation Programs,” describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in “Subtitle VII, Part A, Subpart III, Section 44701: General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.
We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed regulation:
1. Is not a “significant regulatory action” under Executive Order 12866;
2. Is not a “significant rule” under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
49 U.S.C. 106(g), 40113, 44701.
We must receive comments by January 30, 2017.
(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”).
This AD applies to Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes, certificated in any category, all serial numbers.
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
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.
Comply with this AD within the compliance times specified, unless already done.
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 13, released August 25, 2014 (“Fokker Report SE–623, Issue 13”). For all tasks and retirement lives identified in Fokker Report SE–623, Issue 13, 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, Issue 13. Accomplishing 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, Issue 13.
This paragraph restates the requirements of paragraph (j) of AD 2012–22–15, with specific delegation approval language. If any discrepancy, as defined in Fokker Report SE–623, Issue 13, is found during accomplishment of any task specified in Fokker Report SE–623, Issue 13: Within the applicable compliance time specified in Fokker Report SE–623, Issue 13, accomplish the applicable corrective actions in accordance with Fokker Report SE–623, Issue 13.
(1) If no compliance time is identified in Fokker Report SE–623, Issue 13, accomplish the applicable corrective actions before further flight.
(2) If any discrepancy is found and there is no corrective action specified in Fokker Report SE–623, Issue 13: Before further flight, repair using a method approved by the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Fokker Services' EASA Design Organization Approval (DOA).
This paragraph restates the requirements of paragraph (k) of AD 2012–22–15, with a new exception. Except as required by paragraph (k) of this AD, after accomplishing the revision required by paragraph (g) of this AD, no alternative actions (
This paragraph restates the requirements of paragraph (m) of AD 2012–22–15, with revised compliance language. Accomplishing the actions specified in paragraph (g) of this AD terminates the requirements of paragraphs (f)(1) through (f)(5) of AD 2008–06–20 R1.
Within 30 days of the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the ALI instructions specified in Fokker Services B.V. Engineering Report SE–623, “Fokker 70/100 ALI's and SLI's,” Issue 16, issued June 3, 2016 (“Fokker Services B.V. Engineering
(1) The initial compliance times for the tasks specified in Fokker Services B.V. Engineering Report SE–623, Issue 16, are at the later of the applicable compliance times specified in Fokker Services B.V. Engineering Report SE–623, Issue 16, or within 30 days after the effective date of this AD, whichever is later.
(2) If any discrepancy is found, before further flight, repair using a method approved by the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA; or the EASA; or Fokker B.V. Service's EASA DOA.
After the maintenance or inspection program, as applicable, has been revised as required by paragraph (k) of this AD, no alternative actions (
The following provisions also apply to this AD:
(1)
(2)
(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2016–0125, dated June 21, 2016, for related information. You may examine the MCAI on the Internet at
(2) For service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL Hoofddorp, the Netherlands; telephone: +31 (0)88–6280–350; fax: +31 (0)88–6280–111; email: