83 FR 8328 - Airworthiness Directives; Fokker Services B.V. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 39 (February 27, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 39 (February 27, 2018)
| Page Range | 8328-8331 | |
| FR Document | 2018-03430 |
[Federal Register Volume 83, Number 39 (Tuesday, February 27, 2018)] [Rules and Regulations] [Pages 8328-8331] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-03430] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9435; Product Identifier 2016-NM-108-AD; Amendment 39-18830; AD 2017-06-06] RIN 2120-AA64 Airworthiness Directives; Fokker Services B.V. Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are superseding Airworthiness Directive (AD) 2012-22-15, which applied to all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes. AD 2012-22-15 required revising the maintenance program to incorporate the limitations, [[Page 8329]] tasks, thresholds, and intervals specified in certain revised Fokker maintenance review board (MRB) documents. This new AD requires revising the maintenance or inspection program, as applicable, to incorporate new maintenance requirements and airworthiness limitations. This AD was prompted by new and more restrictive airworthiness limitations. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 3, 2018. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 3, 2018. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of December 20, 2012 (77 FR 68063, November 15, 2012). ADDRESSES: For service information identified in this final rule, 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: [email protected]; internet http://www.myfokkerfleet.com. You may view this referenced service information at the FAA, Transport Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9435. Examining the AD Docket You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 9435; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800- 647-5527) is Docket Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227- 1149. SUPPLEMENTARY INFORMATION: Discussion We issued a supplemental notice of proposed rulemaking (SNPRM) to amend 14 CFR part 39 to supersede AD 2012-22-15, Amendment 39-17252 (77 FR 68063, November 15, 2012) (``AD 2012-22-15''). AD 2012-22-15 applied to all Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes. The SNPRM published in the Federal Register on October 19, 2017 (82 FR 48671) (``the SNPRM''). We preceded the SNPRM with a notice of proposed rulemaking (NPRM) that published in the Federal Register on December 16, 2016 (81 FR 91068) (``the NPRM''). The NPRM was prompted by new and more restrictive airworthiness limitations. The NPRM proposed to revise the maintenance or inspection program, as applicable, to incorporate the new and more restrictive airworthiness limitations. The SNPRM proposed to require revising the maintenance or inspection program, as applicable, to incorporate new and more restrictive airworthiness limitations that were issued since the NPRM was released. We are issuing this AD to prevent reduced structural integrity of the airplane. 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 2017-0095, dated May 30, 2017 (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 Engineering Report SE-623 contains the 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 consists of: Part 1--Report SE-473, Certification Maintenance Requirements (CMRs)--ref. 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--ref. EASA AD 2016-0125 [which corresponds to certain requirements in FAA AD 2012-22-15], and Part 3--Report SE-672, Fuel ALIs and CDCCLs--ref. 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 2016-0125, requiring the actions described in ALS Part 2, Report SE-623 at issue 15 and 16. Since that AD was issued, Fokker Services published issue 17 of Report SE-623, containing new and/or more restrictive maintenance tasks. For the reasons described above, this [EASA] AD retains the requirements of AD 2016-0125, 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 17 (hereafter referred to as ``ALS Part 2'' in this [EASA] AD). You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 9435. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the SNPRM or on the determination of the cost to the public. Conclusion We reviewed the available data and determined that air safety and the public interest require adopting this AD as proposed except for minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the SNPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the SNPRM. Related Service Information Under 1 CFR Part 51 Fokker Services B.V. has issued Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue 17, issued April 26, 2017. The service information describes new and more restrictive 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 ADDRESSES. Costs of Compliance We estimate that this AD affects 15 airplanes of U.S. registry. The actions required by AD 2012-22-15, and retained in this 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 required by AD 2012-22-15 is $85 per product. We also estimate that it would take about 1 work-hour per product to [[Page 8330]] comply with the new basic requirements of this AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this AD on U.S. operators to be $1,275, or $85 per product. Authority for This Rulemaking 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order 13132. This AD will 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 that this AD: 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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by removing Airworthiness Directive 2012- 22-15, Amendment 39-17252 (77 FR 68063, November 15, 2012), and adding the following new AD. 2017-06-06 Fokker Services B.V: Amendment 39-18830; Docket No. FAA- 2016-9435; Product Identifier 2016-NM-108-AD. (a) Effective Date This AD is effective April 3, 2018. (b) 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''). (c) Applicability This AD applies to Fokker Services B.V. Model F28 Mark 0070 and Mark 0100 airplanes, certificated in any category, all serial numbers. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/ Maintenance Checks. (e) Reason 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. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Maintenance Program Revision, with Revised Compliance Language 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. (h) Retained Corrective Actions, With Specific Delegation Approval Language 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, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011, is found during accomplishment of any task specified in Fokker Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011: Within the applicable compliance time specified in Fokker Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011, accomplish the applicable corrective actions in accordance with Fokker Report SE- 623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011, except as required by paragraphs (h)(1) and (h)(2) of this AD. (1) If no compliance time is identified in Fokker Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011, 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, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011: Before further flight, contact the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Fokker B.V. Services' EASA Design Organization Approval (DOA); for approved corrective actions, and accomplish those actions before further flight. (i) Retained ``No Alternative Actions or Intervals,'' With a New Exception This paragraph restates the requirements of paragraph (k) of AD 2012-22-15, with a new [[Page 8331]] exception. Except as required by paragraph (k) of this AD, after accomplishing the revision required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (m)(1) of this AD. (j) Retained Method of Compliance With AD 2008-06-20 R1, With Revised Compliance Language This paragraph restates the terminating action specified in 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. (k) New Requirement of This AD: Maintenance or Inspection Program Revision Within 30 days of the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the airworthiness limitations specified in Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue 17, issued April 26, 2017. Accomplishing the revision required by this paragraph terminates the requirements of paragraph (g) of this AD. Accomplishing the revision required by this paragraph also terminates the requirements of paragraph (g) of AD 2012-12-07. (1) The initial compliance times for the tasks specified in Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue 17, issued April 26, 2017, are at the later of the applicable compliance times specified in Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/100 ALI's and SLI's,'' Issue 17, issued April 26, 2017, 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 Section, Transport Standards Branch, FAA; or the EASA; or Fokker B.V. Service's EASA DOA. If approved by the DOA, the approval must include the DOA-authorized signature. (l) No Alternative Actions or Intervals After the maintenance or inspection program, as applicable, has been revised as required by paragraph (k) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an AMOC in accordance with the procedures specified in paragraph (m)(1) of this AD. (m) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (n)(2) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (2) Contacting the Manufacturer: As of the effective date of this AD, for any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or EASA; or Fokker B.V. Services' EASA DOA. If approved by the DOA, the approval must include the DOA-authorized signature. (n) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive AD 2017-0095, dated May 30, 2017, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9435. (2) For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. (o) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (3) The following service information was approved for IBR on April 3, 2018. (i) Fokker Services B.V. Engineering Report SE-623, ``Fokker 70/ 100 ALI's and SLI's,'' Issue 17, issued April 26, 2017. (ii) Reserved. (4) The following service information was approved for IBR on December 20, 2012 (77 FR 68063, November 15, 2012). (i) Fokker Report SE-623, ``Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,'' Issue 8, released March 17, 2011. (ii) Reserved. (5) 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: [email protected]; internet http://www.myfokkerfleet.com. (6) You may view this service information at the FAA, Transport Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (7) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on February 9, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-03430 Filed 2-26-18; 8:45 am] BILLING CODE 4910-13-P
![8328 Federal Register / Vol. 83, No. 39 / Tuesday, February 27, 2018 / Rules and Regulations
(b) Affected ADs (j) Exceptions to Service Information Airframe Section, FAA, Los Angeles ACO
This AD affects AD 2012–18–13 R1, Specifications Branch, 3960 Paramount Boulevard,
Amendment 39–17429 (78 FR 27020, May 9, (1) For purposes of determining Lakewood, CA 90712–4137; phone: 562–627–
2013) (‘‘AD 2012–18–13 R1’’). compliance with the requirements of this AD: 5232; fax: 562–627–5210; email:
Where Boeing Alert Service Bulletin 737– george.garrido@faa.gov.
(c) Applicability 53A1355, dated March 10, 2017, uses the (m) Material Incorporated by Reference
(1) This AD applies to all The Boeing phrase ‘‘the original issue date of this service
Company Model 737–100, –200, –200C, bulletin,’’ this AD requires using ‘‘the (1) The Director of the Federal Register
–300, –400, and –500 series airplanes, effective date of this AD.’’ approved the incorporation by reference
certificated in any category. (2) Although Boeing Alert Service Bulletin (IBR) of the service information listed in this
737–53A1355, dated March 10, 2017, paragraph under 5 U.S.C. 552(a) and 1 CFR
(2) Installation of Supplemental Type
specifies to contact Boeing for repair part 51.
Certificate (STC) ST01219SE (http://rgl.faa.
instructions, and specifies that action as (2) You must use this service information
gov/Regulatory_and_Guidance_Library/
‘‘RC’’ (Required for Compliance), this AD as applicable to do the actions required by
rgstc.nsf/0/EBD1CEC7B301293E86257CB30
requires repair before further flight using a this AD, unless the AD specifies otherwise.
045557A?OpenDocument&Highlight=
method approved in accordance with the (i) Boeing Alert Service Bulletin 737–
st01219se) does not affect the ability to
procedures specified in paragraph (k) of this 53A1355, dated March 10, 2017.
accomplish the actions required by this AD.
AD. (ii) Reserved.
Therefore, for airplanes on which STC
(3) For service information identified in
ST01219SE is installed, a ‘‘change in (k) Alternative Methods of Compliance this AD, contact Boeing Commercial
product’’ alternative method of compliance (AMOCs) Airplanes, Attention: Contractual & Data
(AMOC) approval request is not necessary to (1) The Manager, Los Angeles ACO Branch, Services (C&DS), 2600 Westminster Blvd.,
comply with the requirements of 14 CFR FAA, has the authority to approve AMOCs MC 110–SK57, Seal Beach, CA 90740–5600;
39.17. for this AD, if requested using the procedures telephone 562–797–1717; internet https://
(d) Subject found in 14 CFR 39.19. In accordance with www.myboeingfleet.com.
14 CFR 39.19, send your request to your (4) You may view this service information
Air Transport Association (ATA) of principal inspector or local Flight Standards at the FAA, Transport Standards Branch,
America Code 53, Fuselage. District Office, as appropriate. If sending 2200 South 216th St., Des Moines, WA. For
(e) Unsafe Condition information directly to the manager of the information on the availability of this
certification office, send it to the attention of material at the FAA, call 206–231–3195.
This AD was prompted by an evaluation by the person identified in paragraph (l) of this
the design approval holder (DAH) indicating (5) You may view this service information
AD. Information may be emailed to: 9-ANM- that is incorporated by reference at the
that the gore web lap splices of the aft LAACO-AMOC-Requests@faa.gov.
pressure bulkhead are subject to widespread National Archives and Records
(2) Before using any approved AMOC, Administration (NARA). For information on
fatigue damage (WFD). We are issuing this notify your appropriate principal inspector,
AD to detect and correct cracking in the gore the availability of this material at NARA, call
or lacking a principal inspector, the manager 202–741–6030, or go to: http://
webs, gore web lap splices, and repair webs of the local flight standards district office/
of the aft pressure bulkhead, which could www.archives.gov/federal-register/cfr/ibr-
certificate holding district office. locations.html.
result in possible rapid decompression and (3) An AMOC that provides an acceptable
loss of structural integrity. level of safety may be used for any repair, Issued in Renton, Washington, on February
modification, or alteration required by this 14, 2018.
(f) Compliance
AD if it is approved by the Boeing Michael Kaszycki,
Comply with this AD within the Commercial Airplanes Organization
compliance times specified, unless already Acting Director, System Oversight Division,
Designation Authorization (ODA) that has Aircraft Certification Service.
done. been authorized by the Manager, Los Angeles
ACO Branch, to make those findings. To be [FR Doc. 2018–03600 Filed 2–26–18; 8:45 am]
(g) Required Actions for Group 1 Airplanes
approved, the repair method, modification BILLING CODE 4910–13–P
For airplanes identified as Group 1 in deviation, or alteration deviation must meet
Boeing Alert Service Bulletin 737–53A1355, the certification basis of the airplane, and the
dated March 10, 2017: Within 120 days after approval must specifically refer to this AD. DEPARTMENT OF TRANSPORTATION
the effective date of this AD, inspect the (4) Except as required by paragraph (j)(2)
airplane, using a method approved in of this AD: For service information that Federal Aviation Administration
accordance with the procedures specified in contains steps that are labeled as Required
paragraph (k) of this AD. for Compliance (RC), the provisions of
14 CFR Part 39
(h) Actions Required for Compliance paragraphs (k)(4)(i) and (k)(4)(ii) of this AD
apply. [Docket No. FAA–2016–9435; Product
Except as required by paragraph (j) of this (i) The steps labeled as RC, including Identifier 2016–NM–108–AD; Amendment
AD: For airplanes identified as Group 2 in substeps under an RC step and any figures 39–18830; AD 2017–06–06]
Boeing Alert Service Bulletin 737–53A1355, identified in an RC step, must be done to
dated March 10, 2017, at the applicable times comply with the AD. If a step or substep is RIN 2120–AA64
specified in paragraph 1.E., ‘‘Compliance,’’ of labeled ‘‘RC Exempt,’’ then the RC
Boeing Alert Service Bulletin 737–53A1355, requirement is removed from that step or Airworthiness Directives; Fokker
dated March 10, 2017, do all applicable substep. An AMOC is required for any Services B.V. Airplanes
actions identified as required for compliance deviations to RC steps, including substeps
(‘‘RC’’) in, and in accordance with, the and identified figures. AGENCY: Federal Aviation
Accomplishment Instructions of Boeing Alert (ii) Steps not labeled as RC may be Administration (FAA), Department of
Service Bulletin 737–53A1355, dated March deviated from using accepted methods in Transportation (DOT).
10, 2017. accordance with the operator’s maintenance ACTION: Final rule.
or inspection program without obtaining
(i) Termination of Requirements of
approval of an AMOC, provided the RC steps, SUMMARY: We are superseding
daltland on DSKBBV9HB2PROD with RULES
Paragraph (o) of AD 2012–18–13 R1
including substeps and identified figures, can Airworthiness Directive (AD) 2012–22–
Accomplishment of the initial inspection still be done as specified, and the airplane
for Zone 1, defined in Boeing Alert Service 15, which applied to all Fokker Services
can be put back in an airworthy condition.
Bulletin 737–53A1355, dated March 10, B.V. Model F28 Mark 0070 and Mark
2017, and required by paragraph (h) of this (l) Related Information 0100 airplanes. AD 2012–22–15
AD terminates the requirements of paragraph For more information about this AD, required revising the maintenance
(o) of AD 2012–18–13 R1. contact George Garrido, Aerospace Engineer, program to incorporate the limitations,
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tasks, thresholds, and intervals specified SUPPLEMENTARY INFORMATION: accomplish these actions could result in an
in certain revised Fokker maintenance unsafe condition.
Discussion EASA previously issued AD 2016–0125,
review board (MRB) documents. This
We issued a supplemental notice of requiring the actions described in ALS Part
new AD requires revising the 2, Report SE–623 at issue 15 and 16.
maintenance or inspection program, as proposed rulemaking (SNPRM) to
Since that AD was issued, Fokker Services
applicable, to incorporate new amend 14 CFR part 39 to supersede AD published issue 17 of Report SE–623,
maintenance requirements and 2012–22–15, Amendment 39–17252 (77 containing new and/or more restrictive
airworthiness limitations. This AD was FR 68063, November 15, 2012) (‘‘AD maintenance tasks.
prompted by new and more restrictive 2012–22–15’’). AD 2012–22–15 applied For the reasons described above, this
airworthiness limitations. We are to all Fokker Services B.V. Model F28 [EASA] AD retains the requirements of AD
issuing this AD to address the unsafe Mark 0070 and Mark 0100 airplanes. 2016–0125, which is superseded, and
The SNPRM published in the Federal requires implementation of the maintenance
condition on these products. actions as specified in ALS Part 2 of the
DATES: This AD is effective April 3, Register on October 19, 2017 (82 FR
Instructions for Continued Airworthiness,
2018. 48671) (‘‘the SNPRM’’). We preceded Fokker Services Engineering Report SE–623
The Director of the Federal Register the SNPRM with a notice of proposed at issue 17 (hereafter referred to as ‘‘ALS Part
approved the incorporation by reference rulemaking (NPRM) that published in 2’’ in this [EASA] AD).
of a certain publication listed in this AD the Federal Register on December 16,
You may examine the MCAI in the
as of April 3, 2018. 2016 (81 FR 91068) (‘‘the NPRM’’). The
AD docket on the internet at http://
The Director of the Federal Register NPRM was prompted by new and more
www.regulations.gov by searching for
approved the incorporation by reference restrictive airworthiness limitations.
and locating Docket No. FAA–2016–
of a certain other publication listed in The NPRM proposed to revise the
9435.
this AD as of December 20, 2012 (77 FR maintenance or inspection program, as
68063, November 15, 2012). applicable, to incorporate the new and Comments
ADDRESSES: For service information
more restrictive airworthiness We gave the public the opportunity to
identified in this final rule, contact limitations. The SNPRM proposed to participate in developing this AD. We
Fokker Services B.V., Technical require revising the maintenance or received no comments on the SNPRM or
Services Dept., P.O. Box 1357, 2130 EL inspection program, as applicable, to on the determination of the cost to the
Hoofddorp, the Netherlands; telephone: incorporate new and more restrictive public.
+31 (0)88–6280–350; fax: +31 (0)88– airworthiness limitations that were
issued since the NPRM was released. Conclusion
6280–111; email: technicalservices@
fokker.com; internet http:// We are issuing this AD to prevent We reviewed the available data and
www.myfokkerfleet.com. You may view reduced structural integrity of the determined that air safety and the
this referenced service information at airplane. public interest require adopting this AD
The European Aviation Safety Agency as proposed except for minor editorial
the FAA, Transport Standards Branch,
(EASA), which is the Technical Agent changes. We have determined that these
1601 Lind Avenue SW, Renton, WA. For
for the Member States of the European minor changes:
information on the availability of this
material at the FAA, call 425–227–1221.
Union, has issued EASA Airworthiness • Are consistent with the intent that
Directive AD 2017–0095, dated May 30, was proposed in the SNPRM for
It is also available on the internet at
2017 (referred to after this as the correcting the unsafe condition; and
http://www.regulations.gov by searching
Mandatory Continuing Airworthiness • Do not add any additional burden
for and locating Docket No. FAA–2016–
Information, or ‘‘the MCAI’’), to correct upon the public than was already
9435.
an unsafe condition for all Fokker proposed in the SNPRM.
Examining the AD Docket Services B.V. Model F28 Mark 0070 and
Related Service Information Under 1
You may examine the AD docket on Mark 0100 airplanes. The MCAI states:
CFR Part 51
the internet at http:// Fokker Services Engineering Report SE–
623 contains the Airworthiness Limitation Fokker Services B.V. has issued
www.regulations.gov by searching for
Items (ALIs) and Safe Life Items (SLIs). This Engineering Report SE–623, ‘‘Fokker 70/
and locating Docket No. FAA–2016–
report is Part 2 of the Airworthiness 100 ALI’s and SLI’s,’’ Issue 17, issued
9435; or in person at the Docket
Limitations Section (ALS Part 2) of the April 26, 2017. The service information
Management Facility between 9 a.m. Instructions for Continued Airworthiness, describes new and more restrictive
and 5 p.m., Monday through Friday, referred to in Section 06, Appendix 1, of the airworthiness limitations. This service
except Federal holidays. The AD docket Fokker 70/100 Maintenance Review Board information is reasonably available
contains this AD, the regulatory document.
because the interested parties have
evaluation, any comments received, and The complete ALS consists of:
Part 1—Report SE–473, Certification access to it through their normal course
other information. The address for the
Maintenance Requirements (CMRs)—ref. of business or by the means identified
Docket Office (telephone 800–647–5527)
EASA AD 2015–0027 [which corresponds to in the ADDRESSES.
is Docket Management Facility, U.S.
FAA AD 2016–11–22, Amendment 39–18549
Department of Transportation, Docket (81 FR 36438, June 7, 2016)],
Costs of Compliance
Operations, M–30, West Building Part 2—Report SE–623, ALIs and SLIs—ref. We estimate that this AD affects 15
Ground Floor, Room W12–140, 1200 EASA AD 2016–0125 [which corresponds to airplanes of U.S. registry.
New Jersey Avenue SE, Washington, DC certain requirements in FAA AD 2012–22– The actions required by AD 2012–22–
20590. 15], and 15, and retained in this AD, take about
FOR FURTHER INFORMATION CONTACT: Tom Part 3—Report SE–672, Fuel ALIs and
daltland on DSKBBV9HB2PROD with RULES
1 work-hour per product, at an average
Rodriguez, Aerospace Engineer, CDCCLs—ref. EASA AD 2015–0032 [which
corresponds to FAA AD 2016–11–15,
labor rate of $85 per work-hour. Based
International Section, Transport Amendment 39–18542 (81 FR 36447, June 7, on these figures, the estimated cost of
Standards Branch, FAA, 1601 Lind 2016)]. the actions that are required by AD
Avenue SW, Renton, WA 98057–3356; The instructions contained in those reports 2012–22–15 is $85 per product.
telephone 425–227–1137; fax 425–227– have been identified as mandatory actions for We also estimate that it would take
1149. continued airworthiness. Failure to about 1 work-hour per product to
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![8330 Federal Register / Vol. 83, No. 39 / Tuesday, February 27, 2018 / Rules and Regulations
comply with the new basic List of Subjects in 14 CFR Part 39 2012–22–15), revise the maintenance
requirements of this AD. The average program to incorporate the airworthiness
Air transportation, Aircraft, Aviation limitations specified in Fokker Report SE–
labor rate is $85 per work-hour. Based safety, Incorporation by reference, 623, ‘‘Fokker 70/100 Airworthiness
on these figures, we estimate the cost of Safety. Limitation Items and Safe Life Items,’’ Issue
this AD on U.S. operators to be $1,275, 8, released March 17, 2011. For all tasks and
or $85 per product. Adoption of the Amendment
retirement lives identified in Fokker Report
Authority for This Rulemaking Accordingly, under the authority SE–623, ‘‘Fokker 70/100 Airworthiness
delegated to me by the Administrator, Limitation Items and Safe Life Items,’’ Issue
Title 49 of the United States Code the FAA amends 14 CFR part 39 as 8, released March 17, 2011, the initial
specifies the FAA’s authority to issue follows: compliance times start from the later of the
rules on aviation safety. Subtitle I, times specified in paragraphs (g)(1) and (g)(2)
section 106, describes the authority of PART 39—AIRWORTHINESS of this AD, and the repetitive inspections
the FAA Administrator. ‘‘Subtitle VII: DIRECTIVES must be accomplished thereafter at the
Aviation Programs,’’ describes in more applicable interval specified in Fokker
■ 1. The authority citation for part 39 Report SE–623, ‘‘Fokker 70/100
detail the scope of the Agency’s
continues to read as follows: Airworthiness Limitation Items and Safe Life
authority. Items,’’ Issue 8, released March 17, 2011.
We are issuing this rulemaking under Authority: 49 U.S.C. 106(g), 40113, 44701. Doing the revision required by paragraph (k)
the authority described in ‘‘Subtitle VII, of this AD terminates the requirements of this
Part A, Subpart III, Section 44701: § 39.13 [Amended] paragraph.
General requirements.’’ Under that ■ 2. The FAA amends § 39.13 by (1) Within 3 months after December 20,
section, Congress charges the FAA with removing Airworthiness Directive 2012– 2012 (the effective date of AD 2012–22–15).
promoting safe flight of civil aircraft in 22–15, Amendment 39–17252 (77 FR (2) At the time specified in Fokker Report
air commerce by prescribing regulations 68063, November 15, 2012), and adding SE–623, ‘‘Fokker 70/100 Airworthiness
for practices, methods, and procedures Limitation Items and Safe Life Items,’’ Issue
the following new AD. 8, released March 17, 2011.
the Administrator finds necessary for 2017–06–06 Fokker Services B.V:
safety in air commerce. This regulation Amendment 39–18830; Docket No. (h) Retained Corrective Actions, With
is within the scope of that authority FAA–2016–9435; Product Identifier Specific Delegation Approval Language
because it addresses an unsafe condition 2016–NM–108–AD. This paragraph restates the requirements of
that is likely to exist or develop on (a) Effective Date
paragraph (j) of AD 2012–22–15, with
products identified in this rulemaking specific delegation approval language. If any
action. This AD is effective April 3, 2018. discrepancy, as defined in Fokker Report SE–
This AD is issued in accordance with (b) Affected ADs 623, ‘‘Fokker 70/100 Airworthiness
Limitation Items and Safe Life Items,’’ Issue
authority delegated by the Executive (1) This AD replaces AD 2012–22–15, 8, released March 17, 2011, is found during
Director, Aircraft Certification Service, Amendment 39–17252 (77 FR 68063, accomplishment of any task specified in
as authorized by FAA Order 8000.51C. November 15, 2012) (‘‘AD 2012–22–15’’). Fokker Report SE–623, ‘‘Fokker 70/100
In accordance with that order, issuance (2) This AD affects AD 2012–12–07, Airworthiness Limitation Items and Safe Life
of ADs is normally a function of the Amendment 39–17087 (77 FR 37788, June Items,’’ Issue 8, released March 17, 2011:
Compliance and Airworthiness 25, 2012) (‘‘AD 2012–12–07’’). Within the applicable compliance time
Division, but during this transition (3) This AD affects AD 2008–06–20 R1, specified in Fokker Report SE–623, ‘‘Fokker
Amendment 39–16089 (74 FR 61018, 70/100 Airworthiness Limitation Items and
period, the Executive Director has November 23, 2009) (‘‘AD 2008–06–20 R1’’).
delegated the authority to issue ADs Safe Life Items,’’ Issue 8, released March 17,
applicable to transport category (c) Applicability 2011, accomplish the applicable corrective
actions in accordance with Fokker Report
airplanes to the Director of the System This AD applies to Fokker Services B.V.
SE–623, ‘‘Fokker 70/100 Airworthiness
Oversight Division. Model F28 Mark 0070 and Mark 0100
Limitation Items and Safe Life Items,’’ Issue
airplanes, certificated in any category, all
Regulatory Findings 8, released March 17, 2011, except as
serial numbers.
required by paragraphs (h)(1) and (h)(2) of
We determined that this AD will not (d) Subject this AD.
have federalism implications under Air Transport Association (ATA) of (1) If no compliance time is identified in
Executive Order 13132. This AD will America Code 05, Time Limits/Maintenance Fokker Report SE–623, ‘‘Fokker 70/100
not have a substantial direct effect on Checks. Airworthiness Limitation Items and Safe Life
the States, on the relationship between Items,’’ Issue 8, released March 17, 2011,
(e) Reason accomplish the applicable corrective actions
the national government and the States,
This AD was prompted by a revision of an before further flight.
or on the distribution of power and
airworthiness limitations items (ALI) (2) If any discrepancy is found and there
responsibilities among the various is no corrective action specified in Fokker
document, which introduces new and more
levels of government. restrictive maintenance requirements and Report SE–623, ‘‘Fokker 70/100
For the reasons discussed above, I airworthiness limitations. We are issuing this Airworthiness Limitation Items and Safe Life
certify that this AD: AD to prevent reduced structural integrity of Items,’’ Issue 8, released March 17, 2011:
1. Is not a ‘‘significant regulatory the airplane. Before further flight, contact the Manager,
action’’ under Executive Order 12866; International Section, Transport Standards
2. Is not a ‘‘significant rule’’ under the (f) Compliance Branch, FAA; or the European Aviation
DOT Regulatory Policies and Procedures Comply with this AD within the Safety Agency (EASA); or Fokker B.V.
(44 FR 11034, February 26, 1979); compliance times specified, unless already Services’ EASA Design Organization
done. Approval (DOA); for approved corrective
daltland on DSKBBV9HB2PROD with RULES
3. Will not affect intrastate aviation in
Alaska; and actions, and accomplish those actions before
(g) Retained Maintenance Program Revision,
further flight.
4. Will not have a significant with Revised Compliance Language
economic impact, positive or negative, This paragraph restates the requirements of (i) Retained ‘‘No Alternative Actions or
on a substantial number of small entities paragraph (i) of AD 2012–22–15, with revised Intervals,’’ With a New Exception
under the criteria of the Regulatory compliance language. Within 3 months after This paragraph restates the requirements of
Flexibility Act. December 20, 2012 (the effective date of AD paragraph (k) of AD 2012–22–15, with a new
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![Federal Register / Vol. 83, No. 39 / Tuesday, February 27, 2018 / Rules and Regulations 8331
exception. Except as required by paragraph Office, as appropriate. If sending information Administration (NARA). For information on
(k) of this AD, after accomplishing the directly to the International Section, send it the availability of this material at NARA, call
revision required by paragraph (g) of this AD, to the attention of the person identified in 202–741–6030, or go to: http://
no alternative actions (e.g., inspections) or paragraph (n)(2) of this AD. Information may www.archives.gov/federal-register/cfr/ibr-
intervals may be used unless the actions or be emailed to: 9-ANM-116-AMOC- locations.html.
intervals are approved as an alternative REQUESTS@faa.gov. Before using any
Issued in Renton, Washington, on February
method of compliance (AMOC) in approved AMOC, notify your appropriate
9, 2018.
accordance with the procedures specified in principal inspector, or lacking a principal
paragraph (m)(1) of this AD. inspector, the manager of the local flight Michael Kaszycki,
standards district office/certificate holding Acting Director, System Oversight Division,
(j) Retained Method of Compliance With AD Aircraft Certification Service.
district office.
2008–06–20 R1, With Revised Compliance
(2) Contacting the Manufacturer: As of the [FR Doc. 2018–03430 Filed 2–26–18; 8:45 am]
Language
effective date of this AD, for any requirement BILLING CODE 4910–13–P
This paragraph restates the terminating in this AD to obtain corrective actions from
action specified in paragraph (m) of AD a manufacturer, the action must be
2012–22–15, with revised compliance accomplished using a method approved by
language. Accomplishing the actions the Manager, International Section, Transport
DEPARTMENT OF TRANSPORTATION
specified in paragraph (g) of this AD Standards Branch, FAA; or EASA; or Fokker
terminates the requirements of paragraphs B.V. Services’ EASA DOA. If approved by the
Federal Aviation Administration
(f)(1) through (f)(5) of AD 2008–06–20 R1. DOA, the approval must include the DOA-
authorized signature. 14 CFR Part 97
(k) New Requirement of This AD:
Maintenance or Inspection Program (n) Related Information
Revision [Docket No. 31180; Amdt. No. 3788]
(1) Refer to Mandatory Continuing
Within 30 days of the effective date of this Airworthiness Information (MCAI) EASA
AD, revise the maintenance or inspection Standard Instrument Approach
Airworthiness Directive AD 2017–0095, Procedures, and Takeoff Minimums
program, as applicable, to incorporate the dated May 30, 2017, for related information.
airworthiness limitations specified in Fokker This MCAI may be found in the AD docket
and Obstacle Departure Procedures;
Services B.V. Engineering Report SE–623, on the internet at http://www.regulations.gov Miscellaneous Amendments
‘‘Fokker 70/100 ALI’s and SLI’s,’’ Issue 17, by searching for and locating Docket No.
issued April 26, 2017. Accomplishing the FAA–2016–9435.
AGENCY: Federal Aviation
revision required by this paragraph (2) For more information about this AD, Administration (FAA), DOT.
terminates the requirements of paragraph (g) contact Tom Rodriguez, Aerospace Engineer, ACTION: Final rule.
of this AD. Accomplishing the revision International Section, Transport Standards
required by this paragraph also terminates Branch, FAA, 1601 Lind Avenue SW,
the requirements of paragraph (g) of AD SUMMARY: This rule amends, suspends,
Renton, WA 98057–3356; telephone 425– or removes Standard Instrument
2012–12–07.
227–1137; fax 425–227–1149. Approach Procedures (SIAPs) and
(1) The initial compliance times for the
tasks specified in Fokker Services B.V. (o) Material Incorporated by Reference associated Takeoff Minimums and
Engineering Report SE–623, ‘‘Fokker 70/100 (1) The Director of the Federal Register Obstacle Departure Procedures for
ALI’s and SLI’s,’’ Issue 17, issued April 26, approved the incorporation by reference operations at certain airports. These
2017, are at the later of the applicable (IBR) of the service information listed in this regulatory actions are needed because of
compliance times specified in Fokker paragraph under 5 U.S.C. 552(a) and 1 CFR the adoption of new or revised criteria,
Services B.V. Engineering Report SE–623, part 51.
‘‘Fokker 70/100 ALI’s and SLI’s,’’ Issue 17, or because of changes occurring in the
(2) You must use this service information National Airspace System, such as the
issued April 26, 2017, or within 30 days after as applicable to do the actions required by
the effective date of this AD, whichever is commissioning of new navigational
this AD, unless this AD specifies otherwise.
later. facilities, adding new obstacles, or
(3) The following service information was
(2) If any discrepancy is found, before
approved for IBR on April 3, 2018. changing air traffic requirements. These
further flight, repair using a method changes are designed to provide for the
(i) Fokker Services B.V. Engineering Report
approved by the Manager, International safe and efficient use of the navigable
SE–623, ‘‘Fokker 70/100 ALI’s and SLI’s,’’
Section, Transport Standards Branch, FAA; airspace and to promote safe flight
Issue 17, issued April 26, 2017.
or the EASA; or Fokker B.V. Service’s EASA
DOA. If approved by the DOA, the approval
(ii) Reserved. operations under instrument flight rules
(4) The following service information was at the affected airports.
must include the DOA-authorized signature.
approved for IBR on December 20, 2012 (77
(l) No Alternative Actions or Intervals DATES: This rule is effective February
FR 68063, November 15, 2012).
(i) Fokker Report SE–623, ‘‘Fokker 70/100 27, 2018. The compliance date for each
After the maintenance or inspection
Airworthiness Limitation Items and Safe Life SIAP, associated Takeoff Minimums,
program, as applicable, has been revised as
required by paragraph (k) of this AD, no Items,’’ Issue 8, released March 17, 2011. and ODP is specified in the amendatory
alternative actions (e.g., inspections) or (ii) Reserved. provisions.
intervals may be used unless the actions or (5) For service information identified in The incorporation by reference of
intervals are approved as an AMOC in this AD, contact Fokker Services B.V., certain publications listed in the
accordance with the procedures specified in Technical Services Dept., P.O. Box 1357,
regulations is approved by the Director
paragraph (m)(1) of this AD. 2130 EL Hoofddorp, the Netherlands;
telephone: +31 (0)88–6280–350; fax: +31 of the Federal Register as of February
(m) Other FAA AD Provisions (0)88–6280–111; email: technicalservices@ 27, 2018.
The following provisions also apply to this fokker.com; internet http:// ADDRESSES: Availability of matter
AD: www.myfokkerfleet.com. incorporated by reference in the
(1) Alternative Methods of Compliance (6) You may view this service information amendment is as follows:
daltland on DSKBBV9HB2PROD with RULES
(AMOCs): The Manager, International at the FAA, Transport Standards Branch,
Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA. For For Examination
has the authority to approve AMOCs for this information on the availability of this
AD, if requested using the procedures found material at the FAA, call 425–227–1221. 1. U.S. Department of Transportation,
in 14 CFR 39.19. In accordance with 14 CFR (7) You may view this service information Docket Ops–M30, 1200 New Jersey
39.19, send your request to your principal that is incorporated by reference at the Avenue SE, West Bldg., Ground Floor,
inspector or local Flight Standards District National Archives and Records Washington, DC 20590–0001;
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Document Created: 2018-02-27 01:14:31
Document Modified: 2018-02-27 01:14:31
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective April 3, 2018. | |
| Contact | Tom Rodriguez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227- 1149. | |
| FR Citation | 83 FR 8328 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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