Published 2017-11-27 · Federal Register document 2017-25382
Airworthiness Directives; Fokker Services B.V. Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for certain Fokker Services B.V. Model F.27 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 reports indicating that certain exit signs have a hydrogen isotope that decays over time, causing the signs to lose their brightness. 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 2026-09-03T22:23:54.997910+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2017-90ba553c3b802c53
- Source row
- results[350]
- Raw source SHA-256
- 90ba553c3b802c5316e8d18f30db5da9f7731a87f58278ec2965f199ef4375e9
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2017-24-04
- Effective date printed in this edition
- 2017-12-12
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD becomes effective December 12, 2017.
Exact source excerpt. Text positions 10923–10993, end exclusive, in the original decoded publication. SHA-256: 88d72dffe0ba532956b268089870eeee74ef1338c86f2b829102811dfb438013
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10993–11022, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Fokker Services B.V. Model F.27 airplanes,
certificated in any category, serial numbers 10425 through 10692
inclusive.
Exact source excerpt. Text positions 11022–11186, end exclusive, in the original decoded publication. SHA-256: 3ea70003e31318255dd292f9d937fce3db038a3935b840eb29d9b374ae9dd77e
Subject
(d) Subject
Air Transport Association (ATA) of America Code 11, Placards and
markings.
Exact source excerpt. Text positions 11186–11280, end exclusive, in the original decoded publication. SHA-256: f7ad866ff6b884a348599d64f94c4cdf27fa898e61c5ea0ad63fde703c8bbefe
Reason
(e) Reason
This AD was prompted by reports indicating that certain exit
signs have a hydrogen isotope that decays over time, causing the
signs to lose their brightness. We are issuing this AD to prevent
insufficiently illuminated exit signs, which could possibly prevent
safe evacuation during an emergency and cause injury to occupants.
[[Page 55941]]
Exact source excerpt. Text positions 11280–11644, end exclusive, in the original decoded publication. SHA-256: f831c34c0dcea9ecaf42e6e53a92d3a50950e1357b2aa7e48d450a2462ff39e1
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11644–11746, 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 2012-0238, dated
November 9, 2012.
Exact source excerpt. Text positions 11746–12252, end exclusive, in the original decoded publication. SHA-256: f5ad316b62f34b10af1121ab7f6b7b1e2add822bcc5ba71f5c06e31595c76e9c
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 12252–13027, end exclusive, in the original decoded publication. SHA-256: 28bba0bb566ba89c93478c5dc4fa95ee0b89ec77b39587bfff817058f362af81
Related Information
(i) Related Information
(1) Refer to MCAI EASA AD 2012-0238, dated November 9, 2012, for
related information. You may examine the MCAI on the Internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2017-1095.
(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.
Exact source excerpt. Text positions 13027–13506, end exclusive, in the original decoded publication. SHA-256: f8e055c2b7b74d9a3f723fe757a1880a5c25bfa83b1568773778555f2c9a44c8
Material Incorporated by Reference
(j) Material Incorporated by Reference
None.
Exact source excerpt. Text positions 13506–13557, 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 2017-24-04 · 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: 5fdbf8c3cbe4ec545f7594a1dac95151ce9765d6a6cda80cf433af934f25ce45. Source manifest: 6ada15a47c2ea23f38812063dd5bf966de24a09d8462e9ee9a1be712561cae85.
Official source · 2017-11-27
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 82, Number 226 (Monday, November 27, 2017)]
[Rules and Regulations]
[Pages 55939-55941]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-25382]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-1095; Product Identifier 2012-NM-215-AD; Amendment
39-19108; AD 2017-24-04]
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 F.27 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 reports indicating that certain exit signs have
a hydrogen isotope that decays over time, causing the signs to lose
their brightness. We are issuing this AD to address the unsafe
condition on these products.
DATES: This AD becomes effective December 12, 2017.
We must receive comments on this AD by January 11, 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-2017-
1095; 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, 1601 Lind
Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-
1149.
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
2012-0238, dated November 9, 2012 (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 F.27
airplanes. The MCAI states:
A number of Fokker F.27 aeroplanes have exit signs installed to
locate the emergency exits. A number of these signs are not
electrically powered, but are self-illuminated by means of a
hydrogen isotope known as Tritium. As this isotope decays over time,
these signs will lose their brightness.
To remain compliant with regulations, Tritium exit signs should
be replaced when their brightness has deteriorated below accepted
levels. The established service life for the Tritium powered exit
signs is 7 years. Currently, the F.27 maintenance program does not
include a replacement task for exit signs containing Tritium.
This condition, if not corrected, could result in insufficiently
bright exit signs, possibly preventing safe evacuation during an
emergency, which could result in injury to occupants.
For the reasons described above, this [EASA] AD requires the
replacement of the affected Tritium powered exit signs. Depending on
the aeroplane configuration, the replacement exit signs must be
either photo-luminescent or Tritium powered. In addition, this
[EASA] AD introduces a life limit for the Tritium signs and requires
repetitive maintenance tasks for the photo-luminescent signs. [The
EASA AD provides an option to revise the airplane maintenance
program.]
You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1095.
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
[[Page 55940]]
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 the same type design.
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 reason(s) 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-2017-1095; Product
Identifier 2012-NM-215-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, 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
----------------------------------------------------------------------------------------------------------------
Replacement........................... 1 work-hour x $85 per Unavailable.................. $85
hour = $85.
Inspection............................ 1 work-hour x $85 per $0........................... 85
hour = $85.
Maintenance or inspection program 1 work-hour x $85 per $0........................... 85
revision. hour = $85.
----------------------------------------------------------------------------------------------------------------
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):
2017-24-04 Fokker Services B.V.: Amendment 39-19108; Docket No. FAA-
2017-1095; Product Identifier 2012-NM-215-AD.
(a) Effective Date
This AD becomes effective December 12, 2017.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Fokker Services B.V. Model F.27 airplanes,
certificated in any category, serial numbers 10425 through 10692
inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 11, Placards and
markings.
(e) Reason
This AD was prompted by reports indicating that certain exit
signs have a hydrogen isotope that decays over time, causing the
signs to lose their brightness. We are issuing this AD to prevent
insufficiently illuminated exit signs, which could possibly prevent
safe evacuation during an emergency and cause injury to occupants.
[[Page 55941]]
(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 2012-0238, dated
November 9, 2012.
(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 2012-0238, dated November 9, 2012, for
related information. You may examine the MCAI on the Internet at
http://www.regulations.gov by searching for and locating Docket No.
FAA-2017-1095.
(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.
(j) Material Incorporated by Reference
None.
Issued in Renton, Washington, on November 14, 2017.
Chris Spangenberg,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2017-25382 Filed 11-24-17; 8:45 am]
BILLING CODE 4910-13-P
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