Published 2018-04-06 · Federal Register document 2018-06822
Airworthiness Directives; Fokker Services B.V. Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by interference between certain passenger service unit (PSU) panels, when in the deployed/open position, and the nearby emergency exit door cover. We are issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[99]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-07-11
- Effective date printed in this edition
- 2018-04-23
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD becomes effective April 23, 2018.
Exact source excerpt. Text positions 10420–10487, end exclusive, in the original decoded publication. SHA-256: 167fcf1de25c5b7a9712bd502667402a5ba5cdb666f10b00524553f1fb31ea94
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10487–10516, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Fokker Services B.V. Model F28 Mark 0100
airplanes, certificated in any category, serial numbers 11359,
11361, 11367, 11397, 11404, 11446, 11456, 11460, 11468, 11483,
11490, 11499, 11502, 11515 and 11520.
Exact source excerpt. Text positions 10516–10767, end exclusive, in the original decoded publication. SHA-256: 366e78c5e763cbe83031a2ade74a778fe61308cf09c103b7baa34e5c3887db19
Subject
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
[[Page 14745]]
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Reason
(e) Reason
This AD was prompted by a report of interference between certain
passenger service unit (PSU) panels, when in the deployed/open
position, and the nearby emergency exit door cover. We are issuing
this AD to detect and correct interference between certain PSU
panels and the nearby emergency exit door cover, which could prevent
a complete opening of the overwing emergency exit door, and possibly
obstruct the evacuation of occupants in case of an emergency
landing.
Exact source excerpt. Text positions 10877–11367, end exclusive, in the original decoded publication. SHA-256: f69531eee4998a97cdf7d6a38050de288e5ae0835642fff327b497a26f480186
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11367–11469, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(g) Required Actions
Within 30 days after the effective date of this AD, request
instructions from the Manager, International Section, Transport
Standards Branch, FAA, to address the unsafe condition specified in
paragraph (e) of this AD; and accomplish the actions at the times
specified in, and in accordance with, those instructions. Guidance
can be found in Mandatory Continuing Airworthiness Information
(MCAI) European Aviation Safety Agency (EASA) AD 2017-0113, dated
June 28, 2017.
Exact source excerpt. Text positions 11469–11972, end exclusive, in the original decoded publication. SHA-256: 8ac6ee6d1f4ccf729fb07871b0e832093d85d9a87178ca52b50e9358a36024c2
Alternative Methods of Compliance (AMOCs)
(h) 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 (i)(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.
Exact source excerpt. Text positions 11972–12747, end exclusive, in the original decoded publication. SHA-256: 28bba0bb566ba89c93478c5dc4fa95ee0b89ec77b39587bfff817058f362af81
Related Information
(i) Related Information
(1) Refer to MCAI EASA AD 2017-0113, dated June 28, 2017, for
related information. You may examine the MCAI on the internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2018-0268.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax: 206-231-3226.
Exact source excerpt. Text positions 12747–13213, end exclusive, in the original decoded publication. SHA-256: cea65e572af62f91a2f8e72cfa431a5bb83289a19d647c3de5d1c3aefcfb6e10
Material Incorporated by Reference
(j) Material Incorporated by Reference
None.
Exact source excerpt. Text positions 13213–13264, end exclusive, in the original decoded publication. SHA-256: 9d583edbcf085b1fae94c8be8274ba3ce59b91db7bf15c5f5fd81fff2816eec7
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2018-07-11 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 984c36179ce2237c808541cedec53f6733450922dd5313bee9bd252774e3ead9. Source manifest: 4b1c5f751b1ba1ea8c0d0c6ffe26ab91093a49af77f20b3a6e78871c5720a7ec.
Official source · 2018-04-06
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 83, Number 67 (Friday, April 6, 2018)]
[Rules and Regulations]
[Pages 14743-14745]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-06822]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-0268; Product Identifier 2017-NM-096-AD; Amendment
39-19242; AD 2018-07-11]
RIN 2120-AA64
Airworthiness Directives; Fokker Services B.V. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD requires
contacting the FAA to obtain instructions for addressing the unsafe
condition on these products, and doing the actions specified in those
instructions. This AD was prompted by interference between certain
passenger service unit (PSU) panels, when in the deployed/open
position, and the nearby emergency exit door cover. We are issuing this
AD to address the unsafe condition on these products.
DATES: This AD becomes effective April 23, 2018.
We must receive comments on this AD by May 21, 2018.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
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-2018-
0268; or in person at the Docket Operations office 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 street address for the Docket Operations office
(telephone: 800-647-5527) is in the ADDRESSES section. Comments will be
available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; telephone and fax: 206-231-3226.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA AD
2017-0113, dated June 28, 2017 (referred to after this as the Mandatory
Continuing Airworthiness Information, or ``the MCAI''), to correct an
unsafe condition for certain Fokker Services B.V. Model F28 Mark 0100
airplanes. The MCAI states:
A report was received of an occurrence involving interference
between certain Passenger Service Unit (PSU) panels, Part Number (P/
N) A546011-501 and P/N A546011-503, when in the deployed/open
position, and the nearby emergency exit door cover.
This condition, if not detected and corrected, could prevent a
complete opening of the overwing emergency exit door, possibly
obstructing the evacuation of occupants in case of an emergency
landing.
To address this potential unsafe condition, Fokker Services
published Service Bulletin (SB) SBF100-25-131 (hereafter referred to
as `the SB' in this AD) to provide inspection instructions.
For the reasons described above, this [EASA] AD requires a one-
time inspection to verify that the overwing emergency exit doors can
be fully operated with the PSU-panels in the deployed/opened
position and, depending on findings, accomplishment of applicable
corrective action(s). This [EASA] AD also requires the reporting of
findings.
You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0268.
[[Page 14744]]
FAA's Determination and Requirements of This AD
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. We are
issuing this AD because we evaluated all pertinent information and
determined the unsafe condition exists and is likely to exist or
develop on other products of these same type designs.
FAA's Determination of the Effective Date
Since there are currently no domestic operators of this product, we
find good cause that notice and opportunity for prior public comment
are unnecessary. In addition, for the reasons stated above, we find
that good cause exists for making this amendment effective in less than
30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2018-0268; Product
Identifier 2017-NM-096-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD based on
those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
Costs of Compliance
Currently, there are no affected U.S.-registered airplanes. This AD
requires contacting the FAA to obtain instructions for addressing the
unsafe condition, and doing the actions specified in those
instructions. Based on the actions specified in the MCAI AD, we are
providing the following cost estimates for an affected airplane that is
placed on the U.S. Register in the future:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Inspection................................. 1 work-hour x $85 per hour = $85... $0 $85
Reporting.................................. 1 work-hour x $85 per hour = $85... 0 85
----------------------------------------------------------------------------------------------------------------
We have received no definitive data that would enable us to provide
cost estimates for the on-condition actions specified in this AD.
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 adding the following new airworthiness
directive (AD):
2018-07-11 Fokker Services B.V.: Amendment 39-19242; Docket No. FAA-
2018-0268; Product Identifier 2017-NM-096-AD.
(a) Effective Date
This AD becomes effective April 23, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Fokker Services B.V. Model F28 Mark 0100
airplanes, certificated in any category, serial numbers 11359,
11361, 11367, 11397, 11404, 11446, 11456, 11460, 11468, 11483,
11490, 11499, 11502, 11515 and 11520.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
[[Page 14745]]
(e) Reason
This AD was prompted by a report of interference between certain
passenger service unit (PSU) panels, when in the deployed/open
position, and the nearby emergency exit door cover. We are issuing
this AD to detect and correct interference between certain PSU
panels and the nearby emergency exit door cover, which could prevent
a complete opening of the overwing emergency exit door, and possibly
obstruct the evacuation of occupants in case of an emergency
landing.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 30 days after the effective date of this AD, request
instructions from the Manager, International Section, Transport
Standards Branch, FAA, to address the unsafe condition specified in
paragraph (e) of this AD; and accomplish the actions at the times
specified in, and in accordance with, those instructions. Guidance
can be found in Mandatory Continuing Airworthiness Information
(MCAI) European Aviation Safety Agency (EASA) AD 2017-0113, dated
June 28, 2017.
(h) 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 (i)(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.
(i) Related Information
(1) Refer to MCAI EASA AD 2017-0113, dated June 28, 2017, for
related information. You may examine the MCAI on the internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2018-0268.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone
and fax: 206-231-3226.
(j) Material Incorporated by Reference
None.
Issued in Des Moines, Washington, on March 22, 2018.
Michael Kaszicki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-06822 Filed 4-5-18; 8:45 am]
BILLING CODE 4910-13-P
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