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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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5ed4aee65725fd175e530fdf42ca8ae20683a80d159210582f9b3093d6693119
Text SHA-256
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.