80 FR 64371 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 205 (October 23, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 205 (October 23, 2015)
| Page Range | 64371-64373 | |
| FR Document | 2015-26691 |
[Federal Register Volume 80, Number 205 (Friday, October 23, 2015)] [Proposed Rules] [Pages 64371-64373] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-26691] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-4204; Directorate Identifier 2015-NM-001-AD] RIN 2120-AA64 Airworthiness Directives; Airbus 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 Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes) modified by a particular supplemental type certificate (STC). This proposed AD was prompted by a report of chafing found on the overflow sensor harness of the surge tank, and subsequent contact between the electrical wiring and fuel tank structure. This proposed AD would require a one-time inspection for damage of the outer tank of the overflow sensor harness, and repair if necessary. This proposed AD would also require modification of the sensor harness. We are proposing this AD to prevent chafing of the harness and subsequent contact between the electrical wiring and fuel tank structure, which could result in electrical arcing and a fuel tank explosion. DATES: We must receive comments on this proposed AD by December 7, 2015. 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: 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. For service information identified in this proposed AD, contact Simmonds Precision Products, Inc., A UTC Aerospace Company, 100 Panton Road, [[Page 64372]] Vergennes, Vermont 05491; phone 802-877-2911; fax 802-877-4444; Internet http://www.utcaerospacesystems.com. 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-2015- 4204; 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: Marc Ronell, Aerospace Engineer, Boston Aircraft Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7776; fax: 781-238-7170; email: [email protected]. 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-2015-4204; Directorate Identifier 2015-NM-001-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, issued EASA Airworthiness Directive 2013-0193, dated August 23, 2013 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Airbus Model A300 series airplanes and all Model A300-600 series airplanes. The MCAI corresponds to FAA AD 2015-03-03, Amendment 39-18099 (80 FR 11101, March 2, 2015), which applies to Airbus Model A300 series airplanes and Model A300-600 series airplanes, all serial numbers, except for airplanes modified by supplemental type certificate ST00092BO (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/D41C5AE8E46B4901862574900069E004?OpenDocument&Highlight=st00092bo). In AD 2015-03-03, Amendment 39-18099 (80 FR 11101, March 2, 2015), we explained that airplanes that have had the in-tank fuel quantity system modified by STC ST00092BO cannot accomplish the actions required by AD 2015-03-03 by using Airbus Service Bulletin A300-28-6109, Revision 01, dated December 20, 2013. We also stated that we were considering separate rulemaking to require the procedures and compliance time specified in UTC Aerospace Systems Service Bulletin 300723-28-03 (V-1577), dated October 10, 2014, for airplanes modified by STC ST00092BO. We now have determined that further rulemaking is indeed necessary, and this proposed AD follows from that determination. Related Service Information Under 1 CFR Part 51 UTC Aerospace Systems has issued Service Bulletin 300723-28-03 (V- 1577), Revision 01, dated July 20, 2015. The service information describes procedures for an inspection for damage of the outer tank of the overflow sensor harness, repair, and modification of the sensor harness. 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 of this AD. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of these same type designs. Proposed AD Requirements This proposed AD would require accomplishing the actions specified in the service information described previously. Costs of Compliance We estimate that this proposed AD affects 65 airplanes of U.S. registry. We also estimate that it would take about 3 work-hours per product to comply with the inspections required by this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this inspection proposed by this AD on U.S. operators to be $16,575, or $255 per product. We estimate that it takes about 11 work-hours per product to comply with the modification requirements of this AD. The average labor rate is $85 per work-hour. Required parts cost about $100 per product. Based on these figures, we estimate the cost of this modification on U.S. operators to be $67,275, or $1,035 per product. We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this proposed AD. 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 [[Page 64373]] 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): Airbus: Docket No. FAA-2015-4204; Directorate Identifier 2015-NM- 001-AD. (a) Comments Due Date We must receive comments by December 7, 2015. (b) Affected ADs None. (c) Applicability This AD applies to the Airbus airplanes specified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD; certificated in any category; modified by Simmonds Precision Products, Inc., supplemental type certificate (STC) ST00092BO (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/D41C5AE8E46B4901862v574900069E004?OpenDocument&Highlight=st00092bo). (1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (2) Model A300 B4-605R and B4-622R airplanes. (3) Model A300 F4-605R and F4-622R airplanes. (4) Model A300 C4-605R Variant F airplanes. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Reason This AD was prompted by a report of chafing found on the overflow sensor harness of the surge tank, and subsequent contact between the electrical wiring and fuel tank structure. We are issuing this AD to prevent chafing of the harness and subsequent contact between the electrical wiring and fuel tank structure, which could result in electrical arcing and a fuel tank explosion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) One-Time Inspection and Repair Within 12 months after the effective date of this AD: Do the actions required by paragraphs (g)(1), (g)(2), and (g)(3) of this AD, in accordance with the Accomplishment Instructions of UTC Aerospace Systems Service Bulletin 300723-28-03 (V-1577), Revision 01, dated July 20, 2015. (1) Perform a one-time general visual inspection for damage of the outer tank sensor harness, and if any damage is found on the expando sleeving, before further flight, do a detailed inspection of the underlying wires for exposed conductor wires. If any exposed conductor wire is found, before further flight, replace the outer wing harness assembly. (2) Install new brackets and re-route the surge tank overflow sensor harness. (3) Modify the harness protection. (h) Credit for Previous Actions This paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using UTC Aerospace Systems Service Bulletin 300723- 28-03 (V-1577), dated October 10, 2014. This service information is not incorporated by reference in this AD. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Boston Aircraft Certification Office (ACO) ANE- 150, 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 manager of the ACO, send it to the attention of the person identified in paragraph (j)(1) of this AD. (2) 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. (j) Related Information (1) For more information about this AD, contact Marc Ronell, Aerospace Engineer, Boston ACO, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7776; fax: 781-238-7170; email: [email protected]. (2) For service information identified in this AD, contact Simmonds Precision Products, Inc., A UTC Aerospace Company, 100 Panton Road, Vergennes, Vermont 05491; phone 802-877-2911; fax 802- 877-4444; Internet http://www.utcaerospacesystems.com. 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. Issued in Renton, Washington, on October 15, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-26691 Filed 10-22-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 205 / Friday, October 23, 2015 / Proposed Rules 64371
end October 14, 2015. After receiving a contact Ms. Brenda Edwards at (202) DEPARTMENT OF TRANSPORTATION
request for additional time to prepare 586–2945 or by email:
and submit comments, DOE has decided Brenda.Edwards@ee.doe.gov. Federal Aviation Administration
to reopen the comment period for
submitting comments regarding the RF FOR FURTHER INFORMATION CONTACT: John 14 CFR Part 39
ECS NODA. The comment period is Cymbalsky, U.S. Department of Energy,
Office of Energy Efficiency and [Docket No. FAA–2015–4204; Directorate
reopened through November 6, 2015. Identifier 2015–NM–001–AD]
DATES: DOE will accept comments, data,
Renewable Energy, Building
and information in response to the Technologies Program, EE–5B, 1000 RIN 2120–AA64
NODA received no later than November Independence Avenue SW.,
Washington, DC 20585–0121. Airworthiness Directives; Airbus
6, 2015. Airplanes
Telephone: (202) 287–1692. Email
ADDRESSES: Any comments submitted
must identify the NODA for Energy John.Cymbalsky@ee.doe.govmailto:. AGENCY: Federal Aviation
Conservation Standards for Residential For legal issues, please contact Ms. Administration (FAA), DOT.
Furnaces, and provide docket number Johanna Hariharan, U.S. Department of ACTION: Notice of proposed rulemaking
EERE–2014–BT–STD–0031 and/or Energy, Office of General Counsel, GC– (NPRM).
regulatory information number (RIN) 33, 1000 Independence Avenue SW.,
SUMMARY: We propose to adopt a new
number 1904–AD20. Comments may be Washington, DC 20585–0121.
airworthiness directive (AD) for certain
submitted using any of the following Telephone: (202) 287–6307. Email: Airbus Model A300 B4–600, B4–600R,
methods: Johanna.Hariharan@hq.doe.gov.
1. Federal eRulemaking Portal: and F4–600R series airplanes, and
www.regulations.gov. Follow the SUPPLEMENTARY INFORMATION: On Model A300 C4–605R Variant F
instructions for submitting comments. September 14, 2015, DOE published a airplanes (collectively called Model
2. Email: ResFurnaces2014STD0031@ notice of data availability (NODA) in the A300–600 series airplanes) modified by
ee.doe.gov Include the docket number Federal Register regarding energy a particular supplemental type
EERE–2014–BT–STD–0031 and/or RIN conservation standards for residential certificate (STC). This proposed AD was
1904–AD20 in the subject line of the furnaces (RF ECS NODA). 80 FR 55038. prompted by a report of chafing found
message. The notice requested that interested on the overflow sensor harness of the
3. Mail: Ms. Brenda Edwards, U.S. parties submit written comments by surge tank, and subsequent contact
Department of Energy, Building October 14, 2015. between the electrical wiring and fuel
Technologies Program, Mailstop EE–2J, tank structure. This proposed AD would
DOE received a joint request from the require a one-time inspection for
1000 Independence Avenue SW., American Gas Association (AGA) and
Washington, DC 20585–0121. If damage of the outer tank of the overflow
the American Public Gas Association sensor harness, and repair if necessary.
possible, please submit all items on a
(APGA) requesting additional time to This proposed AD would also require
CD. It is not necessary to include
prepare and submit comments (Docket modification of the sensor harness. We
printed copies.
4. Hand Delivery/Courier: Ms. Brenda No. EERE–2014–BT–STD–0031, AGA/ are proposing this AD to prevent chafing
Edwards, U.S. Department of Energy, APGA, No. 168 at p. 2). In response to of the harness and subsequent contact
Building Technologies Program, 950 this request, DOE is reopening the between the electrical wiring and fuel
L’Enfant Plaza SW., Suite 600, public comment period to allow tank structure, which could result in
Washington, DC 20024. Telephone: interested parties to provide DOE with electrical arcing and a fuel tank
(202) 586–2945. If possible, please written comments and data in response explosion.
submit all items on a CD. It is not to the RF ECS NODA. DATES: We must receive comments on
necessary to include printed copies. DOE will consider any comments in this proposed AD by December 7, 2015.
Docket: The docket, which includes response to the RF ECS NODA received ADDRESSES: You may send comments
Federal Register notices, public meeting by midnight of November 6, 2015, and using the procedures found in 14 CFR
attendee lists and transcripts, deems any comments received by that 11.43 and 11.45, by any of the following
comments, and other supporting time to be timely submitted. methods:
documents/materials, is available for Federal eRulemaking Portal: Go to
review at regulations.gov. All Issued in Washington, DC, on October 15,
http://www.regulations.gov. Follow the
documents in the docket are listed in 2015.
instructions for submitting comments.
the regulations.gov index. However, Kathleen B. Hogan, Fax: (202) 493–2251.
some documents listed in the index, Deputy Assistant Secretary for Energy Mail: U.S. Department of
such as those containing information Efficiency, Energy Efficiency and Renewable Transportation, Docket Operations, M–
that is exempt from public disclosure, Energy. 30, West Building Ground Floor, Room
may not be publicly available. [FR Doc. 2015–27002 Filed 10–22–15; 8:45 am] W12–140, 1200 New Jersey Avenue SE.,
A link to the docket Web page can be BILLING CODE 6450–01–P Washington, DC 20590.
found at: [www.regulations.gov/ Hand Delivery: U.S. Department of
#!docketDetail;D=EERE-2014-BT-STD- Transportation, Docket Operations, M–
0031]. This Web page contains a link to 30, West Building Ground Floor, Room
mstockstill on DSK4VPTVN1PROD with PROPOSALS
the docket for this notice on the W12–140, 1200 New Jersey Avenue SE.,
regulations.gov site. The regulations.gov Washington, DC, between 9 a.m. and 5
Web page contains instructions on how p.m., Monday through Friday, except
to access all documents, including Federal holidays.
public comments, in the docket. For service information identified in
For further information on how to this proposed AD, contact Simmonds
submit a comment or review other Precision Products, Inc., A UTC
public comments and the docket, Aerospace Company, 100 Panton Road,
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![Federal Register / Vol. 80, No. 205 / Friday, October 23, 2015 / Proposed Rules 64373
4. Will not have a significant (f) Compliance Issued in Renton, Washington, on October
economic impact, positive or negative, Comply with this AD within the 15, 2015.
on a substantial number of small entities compliance times specified, unless already Jeffrey E. Duven,
under the criteria of the Regulatory done. Manager, Transport Airplane Directorate,
Flexibility Act. Aircraft Certification Service.
(g) One-Time Inspection and Repair
[FR Doc. 2015–26691 Filed 10–22–15; 8:45 am]
List of Subjects in 14 CFR Part 39 Within 12 months after the effective date
BILLING CODE 4910–13–P
of this AD: Do the actions required by
Air transportation, Aircraft, Aviation paragraphs (g)(1), (g)(2), and (g)(3) of this AD,
safety, Incorporation by reference, in accordance with the Accomplishment
Safety. Instructions of UTC Aerospace Systems
DEPARTMENT OF TRANSPORTATION
Service Bulletin 300723–28–03 (V–1577),
The Proposed Amendment Federal Aviation Administration
Revision 01, dated July 20, 2015.
Accordingly, under the authority (1) Perform a one-time general visual
inspection for damage of the outer tank 14 CFR Part 39
delegated to me by the Administrator,
sensor harness, and if any damage is found [Docket No. FAA–2015–3713; Directorate
the FAA proposes to amend 14 CFR part
on the expando sleeving, before further flight, Identifier 2015–NE–23–AD]
39 as follows: do a detailed inspection of the underlying
wires for exposed conductor wires. If any RIN 2120–AA64
PART 39—AIRWORTHINESS exposed conductor wire is found, before
DIRECTIVES further flight, replace the outer wing harness Airworthiness Directives; Engine
assembly. Alliance Turbofan Engines
■ 1. The authority citation for part 39 (2) Install new brackets and re-route the AGENCY: Federal Aviation
continues to read as follows: surge tank overflow sensor harness.
Administration (FAA), DOT.
Authority: 49 U.S.C. 106(g), 40113, 44701. (3) Modify the harness protection.
ACTION: Notice of proposed rulemaking
(h) Credit for Previous Actions (NPRM).
§ 39.13 [Amended]
This paragraph provides credit for actions
■ 2. The FAA amends § 39.13 by adding required by paragraph (g) of this AD, if those SUMMARY: We propose to adopt a new
the following new airworthiness actions were performed before the effective airworthiness directive (AD) for certain
directive (AD): date of this AD using UTC Aerospace Engine Alliance (EA) GP7270 turbofan
Systems Service Bulletin 300723–28–03 (V– engines. This proposed AD was
Airbus: Docket No. FAA–2015–4204;
Directorate Identifier 2015–NM–001–AD.
1577), dated October 10, 2014. This service prompted by reports of the installation
information is not incorporated by reference of non-conforming honeycomb seals in
(a) Comments Due Date in this AD. the high-pressure compressor (HPC)
We must receive comments by December 7, (i) Alternative Methods of Compliance adjacent to the HPC rotor stage 2 to 5
2015. (AMOCs) spool and stage 7 to 9 spool. This
(b) Affected ADs (1) The Manager, Boston Aircraft proposed AD would require removal
Certification Office (ACO) ANE–150, FAA, and replacement of the affected HPC
None.
has the authority to approve AMOCs for this rotor stage 2 to 5 and stage 7 to 9 spools.
(c) Applicability AD, if requested using the procedures found We are proposing this AD to prevent
This AD applies to the Airbus airplanes in 14 CFR 39.19. In accordance with 14 CFR failure of the HPC rotor stage 2 to 5 and
specified in paragraphs (c)(1), (c)(2), (c)(3), 39.19, send your request to your principal stage 7 to 9 spools, which could lead to
and (c)(4) of this AD; certificated in any inspector or local Flight Standards District uncontained engine failure and damage
category; modified by Simmonds Precision Office, as appropriate. If sending information to the airplane.
Products, Inc., supplemental type certificate directly to the manager of the ACO, send it
DATES: We must receive comments on
(STC) ST00092BO (http://rgl.faa.gov/ to the attention of the person identified in
paragraph (j)(1) of this AD.
this proposed AD by December 22,
Regulatory_and_Guidance_Library/rgstc.nsf/
(2) Before using any approved AMOC, 2015.
0/D41C5AE8E46B4901862v574900069E004
?OpenDocument&Highlight=st00092bo). notify your appropriate principal inspector, ADDRESSES: You may send comments,
(1) Model A300 B4–601, B4–603, B4–620, or lacking a principal inspector, the manager using the procedures found in 14 CFR
and B4–622 airplanes. of the local flight standards district office/ 11.43 and 11.45, by any of the following
(2) Model A300 B4–605R and B4–622R certificate holding district office. methods:
airplanes. (j) Related Information • Federal eRulemaking Portal: Go to
(3) Model A300 F4–605R and F4–622R http://www.regulations.gov. Follow the
airplanes. (1) For more information about this AD,
contact Marc Ronell, Aerospace Engineer, instructions for submitting comments.
(4) Model A300 C4–605R Variant F
airplanes. Boston ACO, FAA, 12 New England • Fax: 202–493–2251.
Executive Park, Burlington, MA 01803; • Mail: U.S. Department of
(d) Subject phone: 781–238–7776; fax: 781–238–7170; Transportation, Docket Operations, M–
Air Transport Association (ATA) of email: marc.ronell@faa.gov. 30, West Building Ground Floor, Room
America Code 28, Fuel. (2) For service information identified in W12–140, 1200 New Jersey Avenue SE.,
this AD, contact Simmonds Precision Washington, DC 20590.
(e) Reason Products, Inc., A UTC Aerospace Company, • Hand Delivery: Deliver to Mail
mstockstill on DSK4VPTVN1PROD with PROPOSALS
This AD was prompted by a report of 100 Panton Road, Vergennes, Vermont 05491; address above between 9 a.m. and 5
chafing found on the overflow sensor harness phone 802–877–2911; fax 802–877–4444;
p.m., Monday through Friday, except
of the surge tank, and subsequent contact Internet http://www.utcaerospace
between the electrical wiring and fuel tank systems.com. You may view this referenced Federal holidays.
structure. We are issuing this AD to prevent service information at the FAA, Transport For service information identified in
chafing of the harness and subsequent Airplane Directorate, 1601 Lind Avenue SW., this proposed AD, contact Engine
contact between the electrical wiring and fuel Renton, WA. For information on the Alliance, 400 Main St., East Hartford,
tank structure, which could result in availability of this material at the FAA, call CT 06108, M/S 169–10, phone: 800–
electrical arcing and a fuel tank explosion. 425–227–1221. 565–0140; email: help24@pw.utc.com;
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Document Created: 2015-12-14 15:32:16
Document Modified: 2015-12-14 15:32:16
| 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 December 7, 2015. | |
| Contact | Marc Ronell, Aerospace Engineer, Boston Aircraft Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7776; fax: 781-238-7170; email: [email protected] | |
| FR Citation | 80 FR 64371 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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