AD 2019-17-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services B.V. | F.28 Mark 0070 | Airworthiness Directives; Fokker Services B.V. Airplanes |
| aircraft | Fokker Services B.V. | F.28 Mark 0100 | Airworthiness Directives; Fokker Services B.V. Airplanes |
Unsafe Condition
cracking of NLG turning tubes, which could lead to NLG turning tube failure, possibly resulting in damage to the airplane and injury to occupants.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
remove the affected parts and replacing them with serviceable parts, inspect (no cracks found, having the correct radius) before installation
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes, all manufacturer serial numbers
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This AD was prompted by reports of cracks on certain nose landing gear (NLG) turning tubes resulting from incorrectly applied repairs. This AD requires removing the affected parts and replacing them with serviceable parts. The FAA is issuing this AD to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Fokker Services B.V. Model F28 Mark 0070 and
0100 airplanes, certificated in any category, all manufacturer
serial numbers.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 84, Number 179 (Monday, September 16, 2019)]
[Rules and Regulations]
[Pages 48563-48565]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2019-19912]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0324; Product Identifier 2019-NM-031-AD; Amendment
39-19726; AD 2019-17-06]
RIN 2120-AA64
Airworthiness Directives; Fokker Services B.V. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This AD
was prompted by reports of cracks on certain nose landing gear (NLG)
turning tubes resulting from incorrectly applied repairs. This AD
requires removing the affected parts and replacing them with
serviceable parts. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective October 21, 2019.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of October 21,
2019.
ADDRESSES: For Fokker 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 <a href="/cdn-cgi/l/email-protection#ff8b9a9c9791969c9e938c9a8d89969c9a8cbf999094949a8dd19c9092"><span class="__cf_email__" data-cfemail="760213151e181f15171a051304001f1513053610191d1d13045815191b">[email protected]</span></a>; internet
<a href="http://www.myfokkerfleet.com">http://www.myfokkerfleet.com</a>. For Safran service information identified
in this final rule, contact Safran Landing Systems, One Carbon Way,
Walton, KY 41094; telephone (859) 525-8583; fax (859) 485-8827;
internet <a href="https://www.safran-landing-systems.com">https://www.safran-landing-systems.com</a>. You may view this
service information 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 on the
internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating
Docket No. FAA-2019-0324.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2019-
0324; 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.
SUPPLEMENTARY INFORMATION:
Discussion
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 0070 and 0100 airplanes. The NPRM published in the
Federal Register on May 14, 2019 (84 FR 21270). The NPRM was prompted
by reports of cracks on certain NLG turning tubes resulting from
incorrectly applied repairs. The NPRM proposed to require removing the
affected parts and replacing them with serviceable parts.
The FAA is issuing this AD to address cracking of NLG turning
tubes, which could lead to NLG turning tube failure, possibly resulting
in damage to the airplane and injury to occupants.
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0037, dated February 19, 2019 (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 0100 airplanes. The MCAI states:
Occurrences have been reported of finding cracks on certain NLG
turning tubes. The subsequent investigation results revealed that
the cracks initiated from an area that is sensitive to fatigue
cracking, which had been subject to incorrectly applied repairs.
This condition, if not detected and corrected, could lead to NLG
turning tube
[[Page 48564]]
failure, possibly resulting in damage to the aeroplane and injury to
occupants.
To address this potential unsafe condition, Fokker Services
published the SB [service bulletin] to provide replacement
instructions, referring to SLS [Safran Landing Systems] SB F100-32-
117 for in-shop inspection.
For the reasons described above, this [EASA] AD requires removal
from service of the affected part and replacement with a serviceable
part.
You may examine the MCAI in the AD docket on the internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2019-
0324.
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 Service Information Under 1 CFR Part 51
Fokker Services B.V. has issued Fokker Service Bulletin SBF100-32-
171, dated November 27, 2018. This service information describes
procedures for removing and replacing affected NLG turning tubes.
Safran Landing Systems has issued Safran Service Bulletin F100-32-
117, dated July 30, 2018. This service information describes procedures
for a magnetic particle or eddy current inspection of NLG turning
tubes.
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 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
----------------------------------------------------------------------------------------------------------------
9 work-hours x $85 per hour = $765........................... $1,282 $2,047 $8,188
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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:
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):
2019-17-06 Fokker Services B.V.: Amendment 39-19726; Docket No.
FAA-2019-0324; Product Identifier 2019-NM-031-AD.
(a) Effective Date
This AD is effective October 21, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Fokker Services B.V. Model F28 Mark 0070 and
0100 airplanes, certificated in any category, all manufacturer
serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
(e) Reason
This AD was prompted by reports of cracks on certain nose
landing gear (NLG) turning tubes resulting from incorrectly applied
repairs. The FAA is issuing this AD to address cracking of NLG
turning tubes, which could lead to NLG turning tube failure,
possibly resulting in damage to the airplane and injury to
occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definitions
(1) An affected part is an NLG turning tube assembly having part
number (P/N) 201456200, 201071202, 201071240, or
[[Page 48565]]
201071241 installed on an NLG unit having a part number identified
in Safran Service Bulletin F100-32-117, dated July 30, 2018.
(2) A serviceable part is an affected part that is new or that,
before installation, has passed an inspection (no cracks found,
having the correct radius), in accordance with the Accomplishment
Instructions of Safran Service Bulletin F100-32-117, dated July 30,
2018.
(h) Replacement
Within 22,000 flight cycles after the effective date of this AD:
Replace the affected parts, with serviceable parts, in accordance
with the Accomplishment Instructions of Fokker Service Bulletin
SBF100-32-171, dated November 27, 2018.
(i) Parts Installation Limitation
As of the effective date of this AD, no person may install, on
any airplane, an affected part, unless it is a serviceable part.
(j) No Reporting Requirement
Although Safran Service Bulletin F100-32-117, dated July 30,
2018, specifies to submit certain information to the manufacturer,
this AD does not include that requirement.
(k) 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 (l)(2) of this AD. Information
may be emailed to: <a href="/cdn-cgi/l/email-protection#81b8acc0cfccacb0b0b7acc0cccec2acd3c4d0d4c4d2d5d2c1e7e0e0afe6eef7"><span class="__cf_email__" data-cfemail="d0e9fd919e9dfde1e1e6fd919d9f93fd829581859583848390b6b1b1feb7bfa6">[email protected]</span></a>. 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 corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Union
Aviation Safety Agency (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.
(l) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2019-0037, dated February 19, 2019, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2019-0324.
(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.
(m) 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) Fokker Service Bulletin SBF100-32-171, dated November 27,
2018.
(ii) Safran Service Bulletin F100-32-117, dated July 30, 2018.
(3) For Fokker 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
<a href="/cdn-cgi/l/email-protection#2e5a4b4d4640474d4f425d4b5c58474d4b5d6e484145454b5c004d4143"><span class="__cf_email__" data-cfemail="e69283858e888f85878a958394908f858395a680898d8d8394c885898b">[email protected]</span></a>; internet <a href="http://www.myfokkerfleet.com">http://www.myfokkerfleet.com</a>.
For Safran service information identified in this final rule,
contact Safran Landing Systems, One Carbon Way, Walton, KY, 41094;
telephone (859) 525-8583; fax (859) 485-8827; internet <a href="https://www.safran-landing-systems.com">https://www.safran-landing-systems.com</a>.
(4) You may view this service information 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.
(5) 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, email <a href="/cdn-cgi/l/email-protection#9ff9fafbedfaf8b1f3faf8fef3dff1feedfeb1f8f0e9"><span class="__cf_email__" data-cfemail="1c7a79786e797b3270797b7d705c727d6e7d327b736a">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Des Moines, Washington, on August 22, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-19912 Filed 9-13-19; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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