82 FR 3217 - Airworthiness Directives; 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 7 (January 11, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 7 (January 11, 2017)
| Page Range | 3217-3219 | |
| FR Document | 2016-31965 |
[Federal Register Volume 82, Number 7 (Wednesday, January 11, 2017)] [Proposed Rules] [Pages 3217-3219] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-31965] [[Page 3217]] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9568; Directorate Identifier 2016-NM-150-AD] RIN 2120-AA64 Airworthiness Directives; 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain 328 Support Services GmbH Model 328-100 airplanes and 328 Support Services GmbH Model 328-300 airplanes. This proposed AD was prompted by reports of broken bonding wires of certain fuel line clamps. This proposed AD would require a one-time inspection of certain fuel line clamps for discrepancies, and replacement of any discrepant clamps. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by February 27, 2017. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. 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. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, contact 328 Support Services GmbH, Global Support Center, P.O. Box 1252, D-82231 Wessling, Federal Republic of Germany; telephone +49 8153 88111 6666; fax +49 8153 88111 6565; email [email protected]; Internet http://www.328support.de. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. 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-2016- 9568; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed 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: Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1175; fax 425-227-1149. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-9568; Directorate Identifier 2016-NM-150-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed 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 proposed AD. Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2016-0169, dated August 17, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain 328 Support Services GmbH Model 328-100 and Model 328-300 airplanes. The MCAI states: Occurrences of broken bonding wires of the fuel line clamps have been reported on Dornier 328-100 and Dornier 328-300 aeroplanes equipped with fuel line clamps Part Number (P/N) 14C02-10A, or P/N 14C02-12A, or P/N 14C02-16A. The affected fuel line clamps have been installed in accordance with the instructions of SB-328-28-490 or SB-328J-28-241 to reduce occurrences of fuel line chafing. The results of the investigation did not identify design deficiency or production failure of the fuel line clamps. It is assumed that the chafing and breaking of the bonding wires are caused either by excessive vibration, misalignment, excessive installation tolerances or mistakes on installation or a combination * * * thereof. This condition, if not detected and corrected, could lead to the loss of bonding function and, in combination with a lightning strike, create a source of ignition in a fuel tank, possibly resulting in a fire or explosion and consequent loss of the aeroplane. To address this unsafe condition, 328 Support Services issued Alert Service Bulletin ASB-328-28-041 for Dornier 328-100 aeroplanes and ASB-328J-28-018 for Dornier 328-300 aeroplanes respectively (hereafter referred to collectively as `the applicable ASB' in this [EASA] AD) providing inspection instructions. For the reason stated above, this [EASA] AD requires a one-time inspection of the fuel line clamps [for discrepancies including damaged, worn, or missing bonding wires, and chafing or incorrect alignment of jet pumps, connection parts, and fuel lines] and, depending on findings, replacement. This [EASA] AD also requires the reporting of all inspection results to the design approval holder. This [EASA] AD is considered an interim action and further [EASA] AD action may follow. You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 9568. Related Service Information Under 1 CFR Part 51 328 Support Services GmbH issued Alert Service Bulletin ASB-328J- 28-018, Revision 1, dated October 13, 2016; and Alert Service Bulletin ASB-328-28-041, Revision 1, dated October 13, 2016. The service information describes a one-time inspection of the fuel line clamps, and replacement of any clamps with worn or missing bonding wires. These documents are distinct since they apply to different airplane models. 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. FAA's Determination and Requirements of This Proposed 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 [[Page 3218]] Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of these same type designs. Costs of Compliance We estimate that this proposed AD affects 35 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspection............................ 8 work-hours x $85 per $0 $680 $23,800 hour = $680. Reporting............................. 1 work-hour x $85 per 0 85 2,975 hour = $85. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary replacements that would be required based on the results of the proposed inspection. We have no way of determining the number of airplanes that might need these replacements. On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Parts cost Cost per product ---------------------------------------------------------------------------------------------------------------- Replacement of discrepant clamps Up to 1 work-hour x Up to $560................ Up to $645. on Model 328-100 airplanes. $85 per hour = $85. Replacement of discrepant clamps Up to 1 work-hour x Up to $588................ Up to $673. on Model 328-300 airplanes. $85 per hour = $85. ---------------------------------------------------------------------------------------------------------------- Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB control number. The control number for the collection of information required by this proposed AD is 2120-0056. The paperwork cost associated with this proposed AD has been detailed in the Costs of Compliance section of this document and includes time for reviewing instructions, as well as completing and reviewing the collection of information. Therefore, all reporting associated with this proposed AD is mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at 800 Independence Ave. SW., Washington, DC 20591, ATTN: Information Collection Clearance Officer, AES-200. 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. Regulatory Findings We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation: 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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH): Docket No. FAA-2016-9568; Directorate Identifier 2016-NM-150- AD. (a) Comments Due Date We must receive comments by February 27, 2017. (b) Affected ADs None. (c) Applicability This AD applies to 328 Support Services GmbH (Type Certificate Previously Held by AvCraft Aerospace GmbH; Fairchild Dornier GmbH; Dornier Luftfahrt GmbH) airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD. [[Page 3219]] (1) Model 328-100 airplanes, on which Dornier 328 Service Bulletin SB-328-28-490, has been incorporated. (2) Model 328-300 airplanes, on which Dornier 328J Service Bulletin SB-328J-28-241, has been incorporated. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Reason This AD was prompted by reports of broken bonding wires of certain fuel line clamps. We are issuing this AD to prevent the loss of bonding function, which, in combination with a lightning strike, could create a source of ignition in a fuel tank, possibly resulting in a fire or explosion and consequent loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection Within 6 months after the effective date of this AD, do a one- time general visual inspection for discrepancies, as identified in, and in accordance with, the Accomplishment Instructions of the service information specified in paragraph (g)(1) or (g)(2) of this AD, as applicable. (1) 328 Support Services GmbH Alert Service Bulletin ASB-328-28- 041, Revision 1, dated October 13, 2016 (Model 328-100 airplanes). (2) 328 Support Services GmbH Alert Service Bulletin ASB-328J- 28-018, Revision 1, dated October 13, 2016 (Model 328-300 airplanes). (h) Replacement of Parts If any discrepancy is found during the inspection required by paragraph (g) of this AD, before further flight, replace the affected clamp in accordance with the Accomplishment Instructions of the service information specified in paragraph (g)(1) or (g)(2) of this AD, as applicable. (i) Reporting At the applicable time specified in paragraph (i)(1) or (i)(2) of this AD, report the inspection results, positive or negative, to 328 Support Services, GmbH, Global Support Center, P.O. Box 1252, D- 82231 Wessling, Federal Republic of Germany; fax +49 8153 88111 6565; email [email protected]. The report must include findings on fuel line clamps, aircraft serial number, total flight hours, and total landings. (1) If the inspection was done on or after the effective date of this AD: Submit the report within 30 days after the inspection. (2) If the inspection was done before the effective date of this AD: Submit the report within 30 days after the effective date of this AD. (j) Credit for Previous Actions This paragraph provides credit for actions required by paragraphs (g) and (h) of this AD, if those actions were performed before the effective date of this AD using the service information specified in paragraph (j)(1) or (j)(2) of this AD. (1) 328 Support Services GmbH Alert Service Bulletin ASB-328-28- 041, dated June 14, 2016. (2) 328 Support Services GmbH Alert Service Bulletin ASB-328J- 28-018, dated June 3, 2016. (k) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1175; fax 425-227-1149. 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 corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or 328 Support Services GmbH's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Reporting Requirements: A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (l) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2016-0169, dated August 17, 2016, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9568. (2) For service information identified in this AD, contact 328 Support Services GmbH, Global Support Center, P.O. Box 1252, D-82231 Wessling, Federal Republic of Germany; telephone +49 8153 88111 6666; fax +49 8153 88111 6565; email [email protected]; Internet http://www.328support.de. You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Issued in Renton, Washington, on December 27, 2016. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-31965 Filed 1-10-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Proposed Rules 3217
DEPARTMENT OF TRANSPORTATION Examining the AD Docket fuel line clamps have been installed in
accordance with the instructions of SB–328–
You may examine the AD docket on 28–490 or SB–328J–28–241 to reduce
Federal Aviation Administration
the Internet at http:// occurrences of fuel line chafing.
www.regulations.gov by searching for The results of the investigation did not
14 CFR Part 39
and locating Docket No. FAA–2016– identify design deficiency or production
[Docket No. FAA–2016–9568; Directorate 9568; or in person at the Docket failure of the fuel line clamps. It is assumed
Identifier 2016–NM–150–AD] Management Facility between 9 a.m. that the chafing and breaking of the bonding
and 5 p.m., Monday through Friday, wires are caused either by excessive
RIN 2120–AA64 vibration, misalignment, excessive
except Federal holidays. The AD docket
installation tolerances or mistakes on
Airworthiness Directives; 328 Support contains this proposed AD, the installation or a combination * * * thereof.
Services GmbH (Type Certificate regulatory evaluation, any comments This condition, if not detected and
Previously Held by AvCraft Aerospace received, and other information. The corrected, could lead to the loss of bonding
GmbH; Fairchild Dornier GmbH; street address for the Docket Operations function and, in combination with a
Dornier Luftfahrt GmbH) Airplanes office (telephone 800–647–5527) is in lightning strike, create a source of ignition in
the ADDRESSES section. Comments will a fuel tank, possibly resulting in a fire or
AGENCY: Federal Aviation be available in the AD docket shortly explosion and consequent loss of the
Administration (FAA), DOT. after receipt. aeroplane.
ACTION: Notice of proposed rulemaking To address this unsafe condition, 328
FOR FURTHER INFORMATION CONTACT:
(NPRM). Support Services issued Alert Service
Todd Thompson, Aerospace Engineer, Bulletin ASB–328–28–041 for Dornier 328–
SUMMARY: We propose to adopt a new International Branch, ANM–116, 100 aeroplanes and ASB–328J–28–018 for
airworthiness directive (AD) for certain Transport Airplane Directorate, FAA, Dornier 328–300 aeroplanes respectively
328 Support Services GmbH Model 1601 Lind Avenue SW., Renton, WA (hereafter referred to collectively as ‘the
98057–3356; telephone 425–227–1175; applicable ASB’ in this [EASA] AD)
328–100 airplanes and 328 Support providing inspection instructions.
Services GmbH Model 328–300 fax 425–227–1149.
For the reason stated above, this [EASA]
airplanes. This proposed AD was SUPPLEMENTARY INFORMATION:
AD requires a one-time inspection of the fuel
prompted by reports of broken bonding Comments Invited line clamps [for discrepancies including
wires of certain fuel line clamps. This damaged, worn, or missing bonding wires,
proposed AD would require a one-time We invite you to send any written and chafing or incorrect alignment of jet
inspection of certain fuel line clamps for relevant data, views, or arguments about pumps, connection parts, and fuel lines] and,
discrepancies, and replacement of any this proposed AD. Send your comments depending on findings, replacement. This
discrepant clamps. We are proposing to an address listed under the [EASA] AD also requires the reporting of all
ADDRESSES section. Include ‘‘Docket No. inspection results to the design approval
this AD to address the unsafe condition holder.
on these products. FAA–2016–9568; Directorate Identifier
2016–NM–150–AD’’ at the beginning of This [EASA] AD is considered an interim
DATES: We must receive comments on action and further [EASA] AD action may
your comments. We specifically invite follow.
this proposed AD by February 27, 2017. comments on the overall regulatory,
ADDRESSES: You may send comments, economic, environmental, and energy You may examine the MCAI in the
using the procedures found in 14 CFR aspects of this proposed AD. We will AD docket on the Internet at http://
11.43 and 11.45, by any of the following consider all comments received by the www.regulations.gov by searching for
methods: closing date and may amend this and locating Docket No. FAA–2016–
• Federal eRulemaking Portal: Go to proposed AD based on those comments. 9568.
http://www.regulations.gov. Follow the We will post all comments we
instructions for submitting comments. Related Service Information Under 1
receive, without change, to http:// CFR Part 51
• Fax: 202–493–2251. www.regulations.gov, including any
• Mail: U.S. Department of personal information you provide. We 328 Support Services GmbH issued
Transportation, Docket Operations, M– will also post a report summarizing each Alert Service Bulletin ASB–328J–28–
30, West Building Ground Floor, Room substantive verbal contact we receive 018, Revision 1, dated October 13, 2016;
W12–140, 1200 New Jersey Avenue SE., about this proposed AD. and Alert Service Bulletin ASB–328–
Washington, DC 20590. 28–041, Revision 1, dated October 13,
• Hand Delivery: Deliver to Mail Discussion 2016. The service information describes
address above between 9 a.m. and 5 The European Aviation Safety Agency a one-time inspection of the fuel line
p.m., Monday through Friday, except (EASA), which is the Technical Agent clamps, and replacement of any clamps
Federal holidays. for the Member States of the European with worn or missing bonding wires.
For service information identified in Union, has issued EASA Airworthiness These documents are distinct since they
this NPRM, contact 328 Support Directive 2016–0169, dated August 17, apply to different airplane models.
Services GmbH, Global Support Center, 2016 (referred to after this as the This service information is reasonably
P.O. Box 1252, D–82231 Wessling, Mandatory Continuing Airworthiness available because the interested parties
Federal Republic of Germany; telephone Information, or ‘‘the MCAI’’), to correct have access to it through their normal
+49 8153 88111 6666; fax +49 8153 an unsafe condition for certain 328 course of business or by the means
88111 6565; email gsc.op@ identified in the ADDRESSES section.
sradovich on DSK3GMQ082PROD with PROPOSALS
Support Services GmbH Model 328–100
328support.de; Internet http:// and Model 328–300 airplanes. The
www.328support.de. You may view this FAA’s Determination and Requirements
MCAI states: of This Proposed AD
referenced service information at the
Occurrences of broken bonding wires of
FAA, Transport Airplane Directorate, the fuel line clamps have been reported on This product has been approved by
1601 Lind Avenue SW., Renton, WA. Dornier 328–100 and Dornier 328–300 the aviation authority of another
For information on the availability of aeroplanes equipped with fuel line clamps country, and is approved for operation
this material at the FAA, call 425–227– Part Number (P/N) 14C02–10A, or P/N in the United States. Pursuant to our
1221. 14C02–12A, or P/N 14C02–16A. The affected bilateral agreement with the State of
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![3218 Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Proposed Rules
Design Authority, we have been notified information and determined an unsafe Costs of Compliance
of the unsafe condition described in the condition exists and is likely to exist or We estimate that this proposed AD
MCAI and service information develop on other products of these same affects 35 airplanes of U.S. registry.
referenced above. We are proposing this type designs. We estimate the following costs to
AD because we evaluated all pertinent comply with this proposed AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Inspection ........................................................ 8 work-hours × $85 per hour = $680 ............. $0 $680 $23,800
Reporting ......................................................... 1 work-hour × $85 per hour = $85 ................. 0 85 2,975
We estimate the following costs to do be required based on the results of the determining the number of airplanes
any necessary replacements that would proposed inspection. We have no way of that might need these replacements.
ON-CONDITION COSTS
Cost per
Action Labor cost Parts cost product
Replacement of discrepant clamps on Model 328– Up to 1 work-hour × $85 per hour = $85 .................. Up to $560 ........ Up to $645.
100 airplanes.
Replacement of discrepant clamps on Model 328– Up to 1 work-hour × $85 per hour = $85 .................. Up to $588 ........ Up to $673.
300 airplanes.
Paperwork Reduction Act General requirements.’’ Under that List of Subjects in 14 CFR Part 39
A federal agency may not conduct or section, Congress charges the FAA with Air transportation, Aircraft, Aviation
sponsor, and a person is not required to promoting safe flight of civil aircraft in safety, Incorporation by reference,
respond to, nor shall a person be subject air commerce by prescribing regulations Safety.
to penalty for failure to comply with a for practices, methods, and procedures
the Administrator finds necessary for The Proposed Amendment
collection of information subject to the
requirements of the Paperwork safety in air commerce. This regulation Accordingly, under the authority
Reduction Act unless that collection of is within the scope of that authority delegated to me by the Administrator,
information displays a current valid because it addresses an unsafe condition the FAA proposes to amend 14 CFR part
OMB control number. The control that is likely to exist or develop on 39 as follows:
number for the collection of information products identified in this rulemaking
action. PART 39—AIRWORTHINESS
required by this proposed AD is 2120–
DIRECTIVES
0056. The paperwork cost associated Regulatory Findings
with this proposed AD has been ■ 1. The authority citation for part 39
detailed in the Costs of Compliance We determined that this proposed AD continues to read as follows:
section of this document and includes would not have federalism implications Authority: 49 U.S.C. 106(g), 40113, 44701.
time for reviewing instructions, as well under Executive Order 13132. This
as completing and reviewing the proposed AD would not have a § 39.13 [Amended]
collection of information. Therefore, all substantial direct effect on the States, on ■ 2. The FAA amends § 39.13 by adding
reporting associated with this proposed the relationship between the national the following new airworthiness
AD is mandatory. Comments concerning Government and the States, or on the directive (AD):
the accuracy of this burden and distribution of power and 328 Support Services GmbH (Type
suggestions for reducing the burden responsibilities among the various Certificate Previously Held by AvCraft
should be directed to the FAA at 800 levels of government. Aerospace GmbH; Fairchild Dornier
Independence Ave. SW., Washington, GmbH; Dornier Luftfahrt GmbH): Docket
For the reasons discussed above, I
DC 20591, ATTN: Information No. FAA–2016–9568; Directorate
certify this proposed regulation: Identifier 2016–NM–150–AD.
Collection Clearance Officer, AES–200.
1. Is not a ‘‘significant regulatory (a) Comments Due Date
Authority for This Rulemaking action’’ under Executive Order 12866;
We must receive comments by February
Title 49 of the United States Code 2. Is not a ‘‘significant rule’’ under the 27, 2017.
specifies the FAA’s authority to issue DOT Regulatory Policies and Procedures
rules on aviation safety. Subtitle I, (b) Affected ADs
sradovich on DSK3GMQ082PROD with PROPOSALS
(44 FR 11034, February 26, 1979);
section 106, describes the authority of None.
the FAA Administrator. ‘‘Subtitle VII: 3. Will not affect intrastate aviation in
Alaska; and (c) Applicability
Aviation Programs,’’ describes in more
4. Will not have a significant This AD applies to 328 Support Services
detail the scope of the Agency’s GmbH (Type Certificate Previously Held by
authority. economic impact, positive or negative, AvCraft Aerospace GmbH; Fairchild Dornier
We are issuing this rulemaking under on a substantial number of small entities GmbH; Dornier Luftfahrt GmbH) airplanes,
the authority described in ‘‘Subtitle VII, under the criteria of the Regulatory certificated in any category, identified in
Part A, Subpart III, Section 44701: Flexibility Act. paragraphs (c)(1) and (c)(2) of this AD.
VerDate Sep<11>2014 19:15 Jan 10, 2017 Jkt 241001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 E:\FR\FM\11JAP1.SGM 11JAP1](https://thefederalregister.org/doc/82_FR_3224/page/2.svg)
![Federal Register / Vol. 82, No. 7 / Wednesday, January 11, 2017 / Proposed Rules 3219
(1) Model 328–100 airplanes, on which (1) 328 Support Services GmbH Alert (2) For service information identified in
Dornier 328 Service Bulletin SB–328–28– Service Bulletin ASB–328–28–041, dated this AD, contact 328 Support Services GmbH,
490, has been incorporated. June 14, 2016. Global Support Center, P.O. Box 1252, D–
(2) Model 328–300 airplanes, on which (2) 328 Support Services GmbH Alert 82231 Wessling, Federal Republic of
Dornier 328J Service Bulletin SB–328J–28– Service Bulletin ASB–328J–28–018, dated Germany; telephone +49 8153 88111 6666;
241, has been incorporated. June 3, 2016. fax +49 8153 88111 6565; email gsc.op@
328support.de; Internet http://
(d) Subject (k) Other FAA AD Provisions
www.328support.de. You may view this
Air Transport Association (ATA) of The following provisions also apply to this service information at the FAA, Transport
America Code 28, Fuel. AD: Airplane Directorate, 1601 Lind Avenue SW.,
(1) Alternative Methods of Compliance Renton, WA. For information on the
(e) Reason (AMOCs): The Manager, International availability of this material at the FAA, call
This AD was prompted by reports of Branch, ANM–116, Transport Airplane 425–227–1221.
broken bonding wires of certain fuel line Directorate, FAA, has the authority to
clamps. We are issuing this AD to prevent the approve AMOCs for this AD, if requested Issued in Renton, Washington, on
loss of bonding function, which, in using the procedures found in 14 CFR 39.19. December 27, 2016.
combination with a lightning strike, could In accordance with 14 CFR 39.19, send your Jeffrey E. Duven,
create a source of ignition in a fuel tank, request to your principal inspector or local Manager, Transport Airplane Directorate,
possibly resulting in a fire or explosion and Flight Standards District Office, as Aircraft Certification Service.
consequent loss of the airplane. appropriate. If sending information directly
to the International Branch, send it to ATTN: [FR Doc. 2016–31965 Filed 1–10–17; 8:45 am]
(f) Compliance
Todd Thompson, Aerospace Engineer, BILLING CODE 4910–13–P
Comply with this AD within the International Branch, ANM–116, Transport
compliance times specified, unless already Airplane Directorate, FAA, 1601 Lind
done. Avenue SW., Renton, WA 98057–3356;
telephone 425–227–1175; fax 425–227–1149. NATIONAL ARCHIVES AND RECORDS
(g) Inspection
Information may be emailed to: 9-ANM-116- ADMINISTRATION
Within 6 months after the effective date of AMOC-REQUESTS@faa.gov. Before using
this AD, do a one-time general visual any approved AMOC, notify your appropriate Information Security Oversight Office
inspection for discrepancies, as identified in, principal inspector, or lacking a principal
and in accordance with, the Accomplishment inspector, the manager of the local flight
Instructions of the service information
32 CFR Part 2004
standards district office/certificate holding
specified in paragraph (g)(1) or (g)(2) of this district office. [FDMS No. NARA–16–0006; Agency No.
AD, as applicable. (2) Contacting the Manufacturer: For any NARA–2017–017]
(1) 328 Support Services GmbH Alert requirement in this AD to obtain corrective
Service Bulletin ASB–328–28–041, Revision
actions from a manufacturer, the action must RIN 3095–AB79
1, dated October 13, 2016 (Model 328–100
be accomplished using a method approved
airplanes).
by the Manager, International Branch, ANM– National Industrial Security Program
(2) 328 Support Services GmbH Alert
116, Transport Airplane Directorate, FAA; or
Service Bulletin ASB–328J–28–018, Revision AGENCY: Information Security Oversight
the European Aviation Safety Agency
1, dated October 13, 2016 (Model 328–300
airplanes).
(EASA); or 328 Support Services GmbH’s Office, National Archives and Records
EASA Design Organization Approval (DOA). Administration (NARA).
(h) Replacement of Parts If approved by the DOA, the approval must
ACTION: Proposed rule.
If any discrepancy is found during the include the DOA-authorized signature.
inspection required by paragraph (g) of this (3) Reporting Requirements: A federal
SUMMARY: The Information Security
AD, before further flight, replace the affected agency may not conduct or sponsor, and a
person is not required to respond to, nor Oversight Office (ISOO) of the National
clamp in accordance with the Archives and Records Administration
Accomplishment Instructions of the service shall a person be subject to a penalty for
information specified in paragraph (g)(1) or failure to comply with a collection of (NARA), proposes to revise the National
(g)(2) of this AD, as applicable. information subject to the requirements of Industrial Security Program (NISP)
the Paperwork Reduction Act unless that Directive. The NISP safeguards
(i) Reporting collection of information displays a current classified information the Federal
At the applicable time specified in valid OMB Control Number. The OMB Government or foreign governments
paragraph (i)(1) or (i)(2) of this AD, report the Control Number for this information release to contractors, licensees,
inspection results, positive or negative, to collection is 2120–0056. Public reporting for
this collection of information is estimated to grantees, and certificate holders. This
328 Support Services, GmbH, Global Support
Center, P.O. Box 1252, D–82231 Wessling, be approximately 5 minutes per response, proposed revision adds provisions
Federal Republic of Germany; fax +49 8153 including the time for reviewing instructions, incorporating executive branch insider
88111 6565; email gsc.op@328support.de. completing and reviewing the collection of threat policy and minimum standards,
The report must include findings on fuel line information. All responses to this collection identifies the Office of the Director of
clamps, aircraft serial number, total flight of information are mandatory. Comments National Intelligence (ODNI) and the
hours, and total landings. concerning the accuracy of this burden and Department of Homeland Security
(1) If the inspection was done on or after suggestions for reducing the burden should (DHS) as new cognizant security
the effective date of this AD: Submit the be directed to the FAA at: 800 Independence
report within 30 days after the inspection. Ave. SW., Washington, DC 20591, Attn: agencies (CSAs), and adds
(2) If the inspection was done before the Information Collection Clearance Officer, responsibilities for all CSAs and non-
effective date of this AD: Submit the report AES–200. CSA departments and agencies (to
within 30 days after the effective date of this reflect oversight functions that are
sradovich on DSK3GMQ082PROD with PROPOSALS
(l) Related Information
AD. already detailed for private sector
(1) Refer to Mandatory Continuing entities in the National Industrial
(j) Credit for Previous Actions Airworthiness Information (MCAI) EASA Security Program Operating Manual
This paragraph provides credit for actions Airworthiness Directive 2016–0169, dated
required by paragraphs (g) and (h) of this AD, August 17, 2016, for related information.
(NISPOM)). The proposed revisions also
if those actions were performed before the This MCAI may be found in the AD docket make other administrative changes to be
effective date of this AD using the service on the Internet at http://www.regulations.gov consistent with recent revisions to the
information specified in paragraph (j)(1) or by searching for and locating Docket No. NISPOM and with updated regulatory
(j)(2) of this AD. FAA–2016–9568. language and style.
VerDate Sep<11>2014 19:15 Jan 10, 2017 Jkt 241001 PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 E:\FR\FM\11JAP1.SGM 11JAP1](https://thefederalregister.org/doc/82_FR_3224/page/3.svg)
Document Created: 2018-02-01 14:59:03
Document Modified: 2018-02-01 14:59:03
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by February 27, 2017. | |
| Contact | Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1175; fax 425-227-1149. | |
| FR Citation | 82 FR 3217 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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