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Published 2020-01-06 · Federal Register document 2019-28467

Airworthiness Directives; Fokker Services B.V. Airplanes

Publication summary

The FAA is adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD was prompted by reports of smoke in the flight deck, in conjunction with the loss of electrical power. This AD requires replacement of affected generator power transfer contactors (GPTCs), essential bus transfer contactors (EBTCs), and auxiliary power transfer contactors (APTCs), as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:04.586324+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2020-f01fbc4d7ab3dbaa
Source row
results[5]
Raw source SHA-256
f01fbc4d7ab3dbaae6a412acd9ff6cece48db77a6a882e46e8f8087200be3837

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2019-25-15
Effective date printed in this edition
2020-02-10
Read 11 complete recorded clauses
Effective Date
(a) Effective Date

    This AD is effective February 10, 2020.

Exact source excerpt. Text positions 8854–8919, end exclusive, in the original decoded publication. SHA-256: 23c8e540cb1a30b381be78b8a47c0408e82e973530fa6bb9a9061b37409845c8

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 8919–8948, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to all Fokker Services B.V. Model F28 Mark 0100 
airplanes, certificated in any category.

Exact source excerpt. Text positions 8948–9078, end exclusive, in the original decoded publication. SHA-256: 00fbb42470dacdab0d01848e7b9fc4a31ccd59652c69328a5e2c8cb98e1724c0

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 24, Electrical 
power.

Exact source excerpt. Text positions 9078–9167, end exclusive, in the original decoded publication. SHA-256: 255ad8dea90f73c6c0904fcd7f65ac20d65a0da0af7ff85531f827e632a9c83d

Reason
(e) Reason

    This AD was prompted by reports of smoke in the flight deck, in 
conjunction with the loss of electrical power. The FAA is issuing 
this AD to address smoke in the flight deck combined with the loss 
of electrical power, which could lead to excessive flightcrew 
workload and injury to the flightcrew.

Exact source excerpt. Text positions 9167–9486, end exclusive, in the original decoded publication. SHA-256: 732c348686fd25194f339292c1c96b88ded56f9f4ad25b2303bff3101ae0065c

Compliance
(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

Exact source excerpt. Text positions 9486–9588, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Requirements
(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, European Union Aviation Safety Agency (EASA) AD 
2019-0120, dated May 29, 2019 (``EASA AD 2019-0120'').

Exact source excerpt. Text positions 9588–9858, end exclusive, in the original decoded publication. SHA-256: 18cc113bec6669a451371cc6e4dae3d1f9a8b2a8f9665e73c14c27dc004db008

Exceptions to EASA AD 2019-0120
(h) Exceptions to EASA AD 2019-0120

    (1) Where EASA AD 2019-0120 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2019-0120 does not apply 
to this AD.

Exact source excerpt. Text positions 9858–10094, end exclusive, in the original decoded publication. SHA-256: f6253a420e35dae6f994ed600b1e03f993501323c52b6940e4308bd4d2319af8

Other FAA AD Provisions
(i) 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 (j) 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: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or EASA; or Fokker 
Services B.V.'s EASA Design Organization Approval (DOA). If approved 
by the DOA, the approval must include the DOA-authorized signature.

Exact source excerpt. Text positions 10094–11354, end exclusive, in the original decoded publication. SHA-256: baced4622ac13d825c66c3d834601f9d7a050f04a33b5bc613ba7e1b78b35a51

Related Information
(j) Related Information

    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; email [email protected].

Exact source excerpt. Text positions 11354–11623, end exclusive, in the original decoded publication. SHA-256: 5026aa69a3f1dc2021ec5efd6fa0e93a8b2f8877640a52d591e848bf9935b459

Material Incorporated by Reference
(k) 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.
    (i) European Union Aviation Safety Agency (EASA) AD 2019-0120, 
dated May 29, 2019.
    (ii) [Reserved]
    (3) For information about EASA AD 2019-0120, contact the EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 
89990 6017; email [email protected]; internet https://www.easa.europa.eu. You may find this EASA AD on the EASA website at 
https://ad.easa.europa.eu.
    (4) You may view this material at the FAA, Transport Standards 
Branch, 2200 South 216th St., Des Moines, WA. For information on the 
availability of this material at the FAA, call 206-231-3195. This 
material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2019-0703.
    (5) You may view this material that is incorporated by reference 
at the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, email 
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 11623–13023, end exclusive, in the original decoded publication. SHA-256: 6a1775c2fcbe654c7d7582ea20fc0d099eec04b7dd635ef8065d4ddf8cb5fd20

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 2019-25-15 · 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: 450a5ae0080f3410f8a555825c4f7c14aea478c3ebfb1bf64dc9454025fe79e3. Source manifest: 8b6628690a5b39599858ab19e476ec6549669e84beb13004d00633714ecb9e6c.

Official source · 2020-01-06

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 85, Number 3 (Monday, January 6, 2020)]
[Rules and Regulations]
[Pages 451-453]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-28467]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0703; Product Identifier 2019-NM-106-AD; Amendment 
39-21014; AD 2019-25-15]
RIN 2120-AA64


Airworthiness Directives; Fokker Services B.V. Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Fokker Services B.V. Model F28 Mark 0100 airplanes. This AD was 
prompted by reports of smoke in the flight deck, in conjunction with 
the loss of electrical power. This AD requires replacement of affected 
generator power transfer contactors (GPTCs), essential bus transfer 
contactors (EBTCs), and auxiliary power transfer contactors (APTCs), as 
specified in a European Union Aviation Safety Agency (EASA) AD, which 
is incorporated by reference. The FAA is issuing this AD to address the 
unsafe condition on these products.

DATES: This AD is effective February 10, 2020.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of February 10, 
2020.

ADDRESSES: For the material incorporated by reference (IBR) in this AD, 
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
telephone +49 221 89990 1000; email [email protected]; internet 
https://www.easa.europa.eu. You may find this IBR material on the EASA 
website at https://ad.easa.europa.eu. You may view this IBR material at 
the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, 
WA. For information on the availability of this material at the FAA, 
call 206-231-3195. It is also available in

[[Page 452]]

the AD docket on the internet at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2019-0703.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0703; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations is 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, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email 
[email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    The EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2019-0120, dated May 29, 2019 
(``EASA AD 2019-0120'') (also referred to as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for all Fokker Services B.V. Model F28 Mark 0100 airplanes.
    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 by adding an AD that would apply to all Fokker Services 
B.V. Model F28 Mark 0100 airplanes. The NPRM published in the Federal 
Register on October 1, 2019 (84 FR 52044). The NPRM was prompted by 
reports of smoke in the flight deck, in conjunction with the loss of 
electrical power. The NPRM proposed to require replacement of affected 
GPTCs, EBTCs, and APTCs, as the most likely cause of the smoke was 
arcing inside one of these affected parts.
    The FAA is issuing this AD to address smoke in the flight deck 
combined with the loss of electrical power, which could lead to 
excessive flightcrew workload and injury to the flightcrew. See the 
MCAI for additional background information.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA received no comments on the NPRM or 
on the determination of the cost to the public.

Conclusion

    The FAA reviewed the relevant data and determined that air safety 
and the public interest require adopting this final rule as proposed, 
except for minor editorial changes. The FAA has determined that these 
minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2019-0120 describes procedures for replacing affected parts 
(GPTCs, EBTCs, and APTCs having part number DHR18-1) with serviceable 
parts. This material 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 section.

Costs of Compliance

    The FAA estimates that this AD affects 4 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
2 work-hours x $85 per hour = $170...........................          $5,400           $5,570          $22,280
----------------------------------------------------------------------------------------------------------------

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.
    The FAA is 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 and 
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    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) Will not affect intrastate aviation in Alaska, and
    (3) 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:

[[Page 453]]

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):

2019-25-15 Fokker Services B.V.: Amendment 39-21014; Docket No. FAA-
2019-0703; Product Identifier 2019-NM-106-AD.

(a) Effective Date

    This AD is effective February 10, 2020.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Fokker Services B.V. Model F28 Mark 0100 
airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 24, Electrical 
power.

(e) Reason

    This AD was prompted by reports of smoke in the flight deck, in 
conjunction with the loss of electrical power. The FAA is issuing 
this AD to address smoke in the flight deck combined with the loss 
of electrical power, which could lead to excessive flightcrew 
workload and injury to the flightcrew.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, European Union Aviation Safety Agency (EASA) AD 
2019-0120, dated May 29, 2019 (``EASA AD 2019-0120'').

(h) Exceptions to EASA AD 2019-0120

    (1) Where EASA AD 2019-0120 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2019-0120 does not apply 
to this AD.

(i) 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 (j) 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: For any requirement in this AD 
to obtain instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or EASA; or Fokker 
Services B.V.'s EASA Design Organization Approval (DOA). If approved 
by the DOA, the approval must include the DOA-authorized signature.

(j) Related Information

    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; email [email protected].

(k) 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.
    (i) European Union Aviation Safety Agency (EASA) AD 2019-0120, 
dated May 29, 2019.
    (ii) [Reserved]
    (3) For information about EASA AD 2019-0120, contact the EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 
89990 6017; email [email protected]; internet https://www.easa.europa.eu. You may find this EASA AD on the EASA website at 
https://ad.easa.europa.eu.
    (4) You may view this material at the FAA, Transport Standards 
Branch, 2200 South 216th St., Des Moines, WA. For information on the 
availability of this material at the FAA, call 206-231-3195. This 
material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2019-0703.
    (5) You may view this material that is incorporated by reference 
at the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, email 
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Des Moines, Washington, on December 12, 2019.
Jeffrey E. Duven,
Director, System Oversight Division, Aircraft Certification Service.
[FR Doc. 2019-28467 Filed 1-3-20; 8:45 am]
BILLING CODE 4910-13-P


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7f895e4a7893db4eb9fad400ae1372540dea3c96bf37ff92c061cbefe178abab
Text SHA-256
450a5ae0080f3410f8a555825c4f7c14aea478c3ebfb1bf64dc9454025fe79e3

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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.