80 FR 19876 - Airworthiness Directives; Dassault Aviation Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 71 (April 14, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 71 (April 14, 2015)
| Page Range | 19876-19878 | |
| FR Document | 2015-08389 |
[Federal Register Volume 80, Number 71 (Tuesday, April 14, 2015)] [Rules and Regulations] [Pages 19876-19878] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-08389] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0825; Directorate Identifier 2015-NM-035-AD; Amendment 39-18138; AD 2015-08-02] RIN 2120-AA64 Airworthiness Directives; Dassault Aviation Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are superseding Airworthiness Directive (AD) 2015-02-04 for certain Dassault Aviation Model MYSTERE-FALCON 50 airplanes. AD 2015- 02-04 required installing two protective plates between the electrical wiring under the glare shield and the engine fire pull handles. This new AD continues to require installing two protective plates between the electrical wiring under the glare shield and the engine fire pull handles. This AD was prompted by our determination that the published version of AD 2015-02-04 incorrectly identified the AD number as ``AD 2014-02-04'' in a certain paragraph. We are issuing this AD to prevent chafing of the electrical wiring, which could result in a short circuit and generation of smoke in the cockpit, potential loss of several functions essential for safe flight, and consequent reduced controllability of the airplane. DATES: This AD becomes effective April 29, 2015. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 6, 2015 (80 FR 5034, January 30, 2015). We must receive comments on this AD by May 29, 2015. ADDRESSES: You may send comments 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 AD, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201- 440-6700; Internet http://www.dassaultfalcon.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- 0825; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. SUPPLEMENTARY INFORMATION: Discussion On January 12, 2015, we issued AD 2015-02-04, Amendment 39-18071 (80 [[Page 19877]] FR 5034, January 30, 2015). AD 2015-02-04 applied to certain Dassault Aviation Model MYSTERE-FALCON 50 airplanes. AD 2015-02-04 was prompted by a report of an untimely and intermittent indication of slat activity due to chafing of the electrical wiring under the glare shield and behind the flight deck front panel. AD 2015-02-04 required installing two protective plates between the electrical wiring under the glare shield and the engine fire pull handles. We issued AD 2015-02-04 to prevent chafing of the electrical wiring, which could result in a short circuit and generation of smoke in the cockpit, potential loss of several functions essential for safe flight, and consequent reduced controllability of the airplane. AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), corresponds to Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) Airworthiness Directive 2014- 0024, dated January 23, 2014. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-0825. Since we issued AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), we have determined that the published version of AD 2015-02-04 incorrectly identified the AD number in the Product Identification line as ``AD 2014-02-04.'' In order to refer to the correct AD number, this AD replaces ``AD 2014-02-04'' with ``AD 2015- 02-04'' in the Product Identification line in the regulatory text. FAA's Determination and Requirements of This AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design. FAA's Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because of the urgency to correct the AD number in the regulatory text to avoid non-compliance. Therefore, we determined that notice and opportunity for prior public comment are unnecessary. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2015-0825; Directorate Identifier 2015-NM-035-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance We estimate that this AD affects 250 airplanes of U.S. registry. The actions required by AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), and retained in this AD are as follows: ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Retained installation from AD 2015- 26 work-hours x $85 per $96 $2,306 $576,500 02-04, Amendment 39-18071 (80 FR hour = $2,210. 5034, January 30, 2015). ---------------------------------------------------------------------------------------------------------------- This AD adds no additional economic burden. 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 AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: 1. Is not a ``significant regulatory action'' under Executive Order 12866; 2. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 3. Will not affect intrastate aviation in Alaska; and 4. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by removing airworthiness directive (AD) [[Page 19878]] 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), and adding the following new AD: 2015-08-02 Dassault Aviation: Amendment 39-18138. Docket No. FAA- 2015-0825; Directorate Identifier 2015-NM-035-AD. (a) Effective Date This AD becomes effective April 29, 2015. (b) Affected ADs This AD replaces AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015). (c) Applicability This AD applies to Dassault Aviation Model MYSTERE-FALCON 50 airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Airplanes with manufacturer serial numbers 5, 7, 27, 30, 34, 36, 78, 132, and 251 through 352 inclusive. (2) Airplanes with manufacturer serial numbers 2 through 250 inclusive, having Honeywell (formerly Allied Signal, Garrett AiResearch) TFE731-40-1C engines modified by Dassault Aviation Service Bulletin F50-280. (d) Subject Air Transport Association (ATA) of America Code 24, Electrical Power. (e) Reason This AD was prompted by a report of an untimely and intermittent indication of slat activity due to chafing of the electrical wiring under the glare shield and behind the flight deck front panel, and also our determination that the published version of AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), incorrectly identified the AD number as ``AD 2014-02-04.'' We are issuing this AD to prevent chafing of the electrical wiring, which could result in a short circuit and generation of smoke in the cockpit, potential loss of several functions essential for safe flight, and consequent reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Installation of Protective Plates, With No Changes This paragraph restates the requirements of paragraph (g) of AD 2015-02-04, Amendment 39-18071 (80 FR 5034, January 30, 2015), with no changes. Within 74 months after March 6, 2015 (the effective date of AD 2015-02-04), install two Rilsan protective plates between the glare shield electrical wiring and the engine fire pull handles, in accordance with the Accomplishment Instructions of Dassault Service Bulletin F50-530, dated November 12, 2013. (h) 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: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; 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. The AMOC approval letter must specifically reference this AD. (2) Contacting the Manufacturer: As of the effective date of this AD, 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 Dassault Aviation's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA- authorized signature. (i) Related Information Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2014-0024, dated January 23, 2014, 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-2015-0825. (j) 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. (3) The following service information was approved for IBR on March 6, 2015, (80 FR 5034, January 30, 2015). (i) Dassault Service Bulletin F50-530, dated November 12, 2013. (ii) Reserved. (4) For service information identified in this AD, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. (5) 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. (6) 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, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on April 6, 2015. John P. Piccola, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-08389 Filed 4-13-15; 8:45 am] BILLING CODE 4910-13-P
![19876 Federal Register / Vol. 80, No. 71 / Tuesday, April 14, 2015 / Rules and Regulations
(i) If the force required to rotate a spherical AgustaWestland, Product Support essential for safe flight, and consequent
bearing in either end of the pitch link is Engineering, Via del Gregge, 100, 21015 reduced controllability of the airplane.
greater than 7.30 N (1.64 pounds force), the Lonate Pozzolo (VA) Italy, ATTN: Maurizio
DATES: This AD becomes effective April
pitch link is unairworthy. D’Angelo; telephone 39–0331–664757; fax 39
(ii) If the force required to rotate the 0331–664680; or at http:// 29, 2015.
spherical bearings in both ends of the pitch www.agustawestland.com/technical- The Director of the Federal Register
link is equal to or less than 7.30 N (1.64 bulletins. approved the incorporation by reference
pounds force), after cleaning the pitch link (4) You may view this service information of a certain publication listed in this AD
rod using aliphatic naphtha or equivalent at FAA, Office of the Regional Counsel, as of March 6, 2015 (80 FR 5034,
and a soft non-metallic bristle brush, visually Southwest Region, 2601 Meacham Blvd., January 30, 2015).
inspect the pitch link rod for a crack in the Room 663, Fort Worth, Texas 76137. For We must receive comments on this
area depicted in Figure 1 of AgustaWestland information on the availability of this AD by May 29, 2015.
Alert BT No. 109–145, 109EP–141, 109K–65, material at the FAA, call (817) 222–5110. ADDRESSES: You may send comments by
109S–065, 109SP–087, or 119–072, all (5) You may view this service information
Revision A, and all dated February 27, 2015, any of the following methods:
that is incorporated by reference at the
as applicable to your model helicopter, using • Federal eRulemaking Portal: Go to
National Archives and Records
a 10x or higher power magnifying glass or by Administration (NARA). For information on http://www.regulations.gov. Follow the
dye penetrant inspection. If there is a crack, the availability of this material at NARA, call instructions for submitting comments.
the pitch link is unairworthy. (202) 741–6030, or go to: http:// • Fax: 202–493–2251.
www.archives.gov/federal-register/cfr/ibr- • Mail: U.S. Department of
(f) Alternative Methods of Compliance
locations.html. Transportation, Docket Operations, M–
(AMOCs)
30, West Building Ground Floor, Room
(1) The Manager, Safety Management Issued in Fort Worth, Texas, on April 6,
2015. W12–140, 1200 New Jersey Avenue SE.,
Group, FAA, may approve AMOCs for this
Washington, DC 20590.
AD. Send your proposal to: Martin Crane, Lance T. Gant,
Aviation Safety Engineer, Safety Management
• Hand Delivery: U.S. Department of
Acting Directorate Manager, Rotorcraft Transportation, Docket Operations, M–
Group, Rotorcraft Directorate, FAA, 2601 Directorate, Aircraft Certification Service.
Meacham Blvd., Fort Worth, Texas 76137; 30, West Building Ground Floor, Room
[FR Doc. 2015–08384 Filed 4–13–15; 8:45 am] W12–140, 1200 New Jersey Avenue SE.,
telephone (817) 222–5110; email
martin.r.crane@faa.gov. BILLING CODE 4910–13–P Washington, DC, between 9 a.m. and 5
(2) For operations conducted under a 14 p.m., Monday through Friday, except
CFR part 119 operating certificate or under Federal holidays.
14 CFR part 91, subpart K, we suggest that DEPARTMENT OF TRANSPORTATION For service information identified in
you notify your principal inspector, or this AD, contact Dassault Falcon Jet,
lacking a principal inspector, the manager of Federal Aviation Administration P.O. Box 2000, South Hackensack, NJ
the local flight standards district office or
certificate holding district office, before 07606; telephone 201–440–6700;
14 CFR Part 39 Internet http://www.dassaultfalcon.com.
operating any aircraft complying with this
AD through an AMOC. [Docket No. FAA–2015–0825; Directorate You may view this referenced service
Identifier 2015–NM–035–AD; Amendment information at the FAA, Transport
(g) Additional Information 39–18138; AD 2015–08–02] Airplane Directorate, 1601 Lind Avenue
The subject of this AD is addressed in SW., Renton, WA. For information on
European Aviation Safety Agency (EASA) RIN 2120–AA64
the availability of this material at the
Emergency AD No. 2015–0035–E, dated FAA, call 425–227–1221.
February 27, 2015. You may view the EASA Airworthiness Directives; Dassault
AD on the Internet at http:// Aviation Airplanes Examining the AD Docket
www.regulations.gov in Docket No. FAA–
2015–0908. AGENCY: Federal Aviation You may examine the AD docket on
Administration (FAA), Department of the Internet at http://
(h) Subject Transportation (DOT). www.regulations.gov by searching for
Joint Aircraft Service Component (JASC) ACTION: Final rule; request for and locating Docket No. FAA–2015–
Code: 6720, Tail Rotor Controls. 0825; or in person at the Docket
comments.
(i) Material Incorporated by Reference Operations office between 9 a.m. and 5
(1) The Director of the Federal Register SUMMARY: We are superseding p.m., Monday through Friday, except
approved the incorporation by reference of Airworthiness Directive (AD) 2015–02– Federal holidays. The AD docket
the service information listed in this 04 for certain Dassault Aviation Model contains this AD, the regulatory
paragraph under 5 U.S.C. 552(a) and 1 CFR MYSTERE–FALCON 50 airplanes. AD evaluation, any comments received, and
part 51. 2015–02–04 required installing two other information. The street address for
(2) You must use this service information protective plates between the electrical the Docket Operations office (telephone
as applicable to do the actions required by wiring under the glare shield and the 800–647–5527) is in the ADDRESSES
this AD, unless the AD specifies otherwise. engine fire pull handles. This new AD section. Comments will be available in
(i) AgustaWestland Alert Bollettino
Tecnico (BT) No. 109–145, Revision A, dated continues to require installing two the AD docket shortly after receipt.
February 27, 2015. protective plates between the electrical FOR FURTHER INFORMATION CONTACT: Tom
(ii) AgustaWestland Alert BT No. 109EP– wiring under the glare shield and the Rodriguez, Aerospace Engineer,
141, Revision A, dated February 27, 2015. engine fire pull handles. This AD was International Branch, ANM–116,
(iii) AgustaWestland Alert BT No. 109K– prompted by our determination that the Transport Airplane Directorate, FAA,
asabaliauskas on DSK5VPTVN1PROD with RULES
65, Revision A, dated February 27, 2015. published version of AD 2015–02–04 1601 Lind Avenue SW., Renton, WA
(iv) AgustaWestland Alert BT No. 109S– incorrectly identified the AD number as 98057–3356; telephone 425–227–1137;
065, Revision A, dated February 27, 2015. ‘‘AD 2014–02–04’’ in a certain
(v) AgustaWestland Alert BT No. 109SP–
fax 425–227–1149.
087, Revision A, dated February 27, 2015.
paragraph. We are issuing this AD to SUPPLEMENTARY INFORMATION:
(vi) AgustaWestland Alert BT No. 119–072, prevent chafing of the electrical wiring,
which could result in a short circuit and Discussion
Revision A, dated February 27, 2015.
(3) For AgustaWestland service generation of smoke in the cockpit, On January 12, 2015, we issued AD
information identified in this AD, contact potential loss of several functions 2015–02–04, Amendment 39–18071 (80
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![Federal Register / Vol. 80, No. 71 / Tuesday, April 14, 2015 / Rules and Regulations 19877
FR 5034, January 30, 2015). AD 2015– number in the Product Identification Comments Invited
02–04 applied to certain Dassault line as ‘‘AD 2014–02–04.’’ In order to
Aviation Model MYSTERE–FALCON 50 refer to the correct AD number, this AD This AD is a final rule that involves
airplanes. AD 2015–02–04 was replaces ‘‘AD 2014–02–04’’ with ‘‘AD requirements affecting flight safety, and
prompted by a report of an untimely 2015–02–04’’ in the Product we did not precede it by notice and
and intermittent indication of slat Identification line in the regulatory text. opportunity for public comment. We
activity due to chafing of the electrical invite you to send any written relevant
FAA’s Determination and Requirements data, views, or arguments about this AD.
wiring under the glare shield and of This AD
behind the flight deck front panel. AD Send your comments to an address
2015–02–04 required installing two This product has been approved by listed under the ADDRESSES section.
protective plates between the electrical the aviation authority of another Include ‘‘Docket No. FAA–2015–0825;
wiring under the glare shield and the country, and is approved for operation Directorate Identifier 2015–NM–035–
engine fire pull handles. We issued AD in the United States. Pursuant to our AD’’ at the beginning of your comments.
2015–02–04 to prevent chafing of the bilateral agreement with the State of We specifically invite comments on the
electrical wiring, which could result in Design Authority, we have been notified overall regulatory, economic,
a short circuit and generation of smoke of the unsafe condition described in the environmental, and energy aspects of
in the cockpit, potential loss of several MCAI and service information this AD. We will consider all comments
functions essential for safe flight, and referenced above. We are issuing this
received by the closing date and may
consequent reduced controllability of AD because we evaluated all pertinent
amend this AD because of those
the airplane. information and determined the unsafe
comments.
condition exists and is likely to exist or
AD 2015–02–04, Amendment 39– We will post all comments we
develop on other products of the same
18071 (80 FR 5034, January 30, 2015), receive, without change, to http://
type design.
corresponds to Mandatory Continuing www.regulations.gov, including any
Airworthiness Information (MCAI) FAA’s Determination of the Effective
personal information you provide. We
European Aviation Safety Agency Date
will also post a report summarizing each
(EASA) Airworthiness Directive 2014– An unsafe condition exists that substantive verbal contact we receive
0024, dated January 23, 2014. You may requires the immediate adoption of this about this AD.
examine the MCAI on the Internet at AD. The FAA has found that the risk to
http://www.regulations.gov by searching the flying public justifies waiving notice Costs of Compliance
for and locating Docket No. FAA–2015– and comment prior to adoption of this
0825. rule because of the urgency to correct We estimate that this AD affects 250
Since we issued AD 2015–02–04, the AD number in the regulatory text to airplanes of U.S. registry.
Amendment 39–18071 (80 FR 5034, avoid non-compliance. Therefore, we The actions required by AD 2015–02–
January 30, 2015), we have determined determined that notice and opportunity 04, Amendment 39–18071 (80 FR 5034,
that the published version of AD 2015– for prior public comment are January 30, 2015), and retained in this
02–04 incorrectly identified the AD unnecessary. AD are as follows:
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Retained installation from AD 2015–02–04, Amend- 26 work-hours × $85 per hour = $96 $2,306 $576,500
ment 39–18071 (80 FR 5034, January 30, 2015). $2,210.
This AD adds no additional economic that is likely to exist or develop on on a substantial number of small entities
burden. products identified in this rulemaking under the criteria of the Regulatory
action. Flexibility Act.
Authority for This Rulemaking
Regulatory Findings List of Subjects in 14 CFR Part 39
Title 49 of the United States Code
specifies the FAA’s authority to issue We determined that this AD will not Air transportation, Aircraft, Aviation
rules on aviation safety. Subtitle I, have federalism implications under safety, Incorporation by reference,
section 106, describes the authority of Executive Order 13132. This AD will Safety.
the FAA Administrator. ‘‘Subtitle VII: not have a substantial direct effect on
Adoption of the Amendment
Aviation Programs,’’ describes in more the States, on the relationship between
the national government and the States, Accordingly, under the authority
detail the scope of the Agency’s
or on the distribution of power and delegated to me by the Administrator,
authority.
responsibilities among the various the FAA amends 14 CFR part 39 as
We are issuing this rulemaking under levels of government. follows:
the authority described in ‘‘Subtitle VII, For the reasons discussed above, I
Part A, Subpart III, Section 44701: certify that this AD: PART 39—AIRWORTHINESS
General requirements.’’ Under that 1. Is not a ‘‘significant regulatory DIRECTIVES
asabaliauskas on DSK5VPTVN1PROD with RULES
section, Congress charges the FAA with action’’ under Executive Order 12866;
promoting safe flight of civil aircraft in 2. Is not a ‘‘significant rule’’ under the ■ 1. The authority citation for part 39
air commerce by prescribing regulations DOT Regulatory Policies and Procedures continues to read as follows:
for practices, methods, and procedures (44 FR 11034, February 26, 1979); Authority: 49 U.S.C. 106(g), 40113, 44701.
the Administrator finds necessary for 3. Will not affect intrastate aviation in
safety in air commerce. This regulation Alaska; and § 39.13 [Amended]
is within the scope of that authority 4. Will not have a significant ■ 2. The FAA amends § 39.13 by
because it addresses an unsafe condition economic impact, positive or negative, removing airworthiness directive (AD)
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![19878 Federal Register / Vol. 80, No. 71 / Tuesday, April 14, 2015 / Rules and Regulations
2015–02–04, Amendment 39–18071 (80 Branch, ANM–116, Transport Airplane www.archives.gov/federal-register/cfr/ibr-
FR 5034, January 30, 2015), and adding Directorate, FAA, has the authority to locations.html.
the following new AD: approve AMOCs for this AD, if requested Issued in Renton, Washington, on April 6,
using the procedures found in 14 CFR 39.19. 2015.
2015–08–02 Dassault Aviation: In accordance with 14 CFR 39.19, send your
Amendment 39–18138. Docket No. request to your principal inspector or local John P. Piccola,
FAA–2015–0825; Directorate Identifier Flight Standards District Office, as Acting Manager, Transport Airplane
2015–NM–035–AD. appropriate. If sending information directly Directorate, Aircraft Certification Service.
(a) Effective Date to the International Branch, send it to ATTN: [FR Doc. 2015–08389 Filed 4–13–15; 8:45 am]
Tom Rodriguez, Aerospace Engineer, BILLING CODE 4910–13–P
This AD becomes effective April 29, 2015.
International Branch, ANM–116, Transport
(b) Affected ADs Airplane Directorate, FAA, 1601 Lind
This AD replaces AD 2015–02–04, Avenue SW., Renton, WA 98057–3356; DEPARTMENT OF TRANSPORTATION
Amendment 39–18071 (80 FR 5034, January telephone 425–227–1137; fax 425–227–1149.
30, 2015). Information may be emailed to: 9-ANM-116- Federal Aviation Administration
AMOC-REQUESTS@faa.gov. Before using
(c) Applicability any approved AMOC, notify your appropriate
principal inspector, or lacking a principal
14 CFR Part 39
This AD applies to Dassault Aviation
Model MYSTERE–FALCON 50 airplanes, inspector, the manager of the local flight [Docket No. FAA–2014–0920; Directorate
certificated in any category, as identified in standards district office/certificate holding Identifier 2014–NM–192–AD; Amendment
paragraphs (c)(1) and (c)(2) of this AD. district office. The AMOC approval letter 39–18135; AD 2015–07–07]
(1) Airplanes with manufacturer serial must specifically reference this AD.
numbers 5, 7, 27, 30, 34, 36, 78, 132, and 251 (2) Contacting the Manufacturer: As of the RIN 2120–AA64
through 352 inclusive. effective date of this AD, for any requirement
(2) Airplanes with manufacturer serial in this AD to obtain corrective actions from Airworthiness Directives; The Boeing
numbers 2 through 250 inclusive, having a manufacturer, the action must be Company Airplanes
Honeywell (formerly Allied Signal, Garrett accomplished using a method approved by AGENCY: Federal Aviation
AiResearch) TFE731–40–1C engines the Manager, International Branch, ANM–
modified by Dassault Aviation Service 116, Transport Airplane Directorate, FAA; or
Administration (FAA), DOT.
Bulletin F50–280. the European Aviation Safety Agency ACTION: Final rule.
(EASA); or Dassault Aviation’s EASA Design
(d) Subject SUMMARY: We are adopting a new
Organization Approval (DOA). If approved by
Air Transport Association (ATA) of the DOA, the approval must include the airworthiness directive (AD) for certain
America Code 24, Electrical Power. DOA-authorized signature. The Boeing Company Model 777–200,
(e) Reason –200LR, –300ER, and 777F series
(i) Related Information airplanes. This AD was prompted by a
This AD was prompted by a report of an Refer to Mandatory Continuing
untimely and intermittent indication of slat
report of a jettison fuel pump that was
Airworthiness Information (MCAI) EASA shut off by the automatic shutoff system
activity due to chafing of the electrical wiring Airworthiness Directive 2014–0024, dated
under the glare shield and behind the flight during the center tank fuel scavenge
January 23, 2014, for related information.
deck front panel, and also our determination process on a short-range flight and a
This MCAI may be found in the AD docket
that the published version of AD 2015–02– on the Internet at http://www.regulations.gov subsequent failure analysis of the fuel
04, Amendment 39–18071 (80 FR 5034, by searching for and locating Docket No. scavenge system. This AD requires
January 30, 2015), incorrectly identified the FAA–2015–0825. making wiring changes, modifying
AD number as ‘‘AD 2014–02–04.’’ We are certain power panels, installing
issuing this AD to prevent chafing of the (j) Material Incorporated by Reference electrical load management system 2
electrical wiring, which could result in a (1) The Director of the Federal Register
short circuit and generation of smoke in the (ELMS2) software, and accomplishing a
approved the incorporation by reference functional test. We are issuing this AD
cockpit, potential loss of several functions (IBR) of the service information listed in this
essential for safe flight, and consequent to prevent extended dry running of the
paragraph under 5 U.S.C. 552(a) and 1 CFR
reduced controllability of the airplane. part 51.
jettison fuel pumps, which can be a
(2) You must use this service information potential ignition source inside the
(f) Compliance
as applicable to do the actions required by main fuel tanks, and consequent fuel
Comply with this AD within the tank fire or explosion in the event that
compliance times specified, unless already this AD, unless this AD specifies otherwise.
(3) The following service information was the jettison pump overheats or has an
done.
approved for IBR on March 6, 2015, (80 FR electrical fault.
(g) Retained Installation of Protective Plates, 5034, January 30, 2015). DATES: This AD is effective May 19,
With No Changes (i) Dassault Service Bulletin F50–530, 2015.
This paragraph restates the requirements of dated November 12, 2013. The Director of the Federal Register
paragraph (g) of AD 2015–02–04, (ii) Reserved.
approved the incorporation by reference
Amendment 39–18071 (80 FR 5034, January (4) For service information identified in
this AD, contact Dassault Falcon Jet, P.O. Box of a certain publication listed in this AD
30, 2015), with no changes. Within 74 as of May 19, 2015.
months after March 6, 2015 (the effective 2000, South Hackensack, NJ 07606;
date of AD 2015–02–04), install two Rilsan telephone 201–440–6700; Internet http:// ADDRESSES: For Boeing service
protective plates between the glare shield www.dassaultfalcon.com. information identified in this AD,
electrical wiring and the engine fire pull (5) You may view this service information contact Boeing Commercial Airplanes,
handles, in accordance with the at the FAA, Transport Airplane Directorate, Attention: Data & Services Management,
asabaliauskas on DSK5VPTVN1PROD with RULES
Accomplishment Instructions of Dassault 1601 Lind Avenue SW., Renton, WA. For P.O. Box 3707, MC 2H–65, Seattle, WA
Service Bulletin F50–530, dated November information on the availability of this 98124–2207; telephone 206–544–5000,
12, 2013. material at the FAA, call 425–227–1221.
(6) You may view this service information
extension 1; fax 206–766–5680; Internet
(h) Other FAA AD Provisions that is incorporated by reference at the https://www.myboeingfleet.com. It is
The following provisions also apply to this National Archives and Records also available on the Internet at http://
AD: Administration (NARA). For information on www.regulations.gov by searching for
(1) Alternative Methods of Compliance the availability of this material at NARA, call and locating Docket No. FAA–2014–
(AMOCs): The Manager, International 202–741–6030, or go to: http:// 0920.
VerDate Sep<11>2014 16:01 Apr 13, 2015 Jkt 235001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\14APR1.SGM 14APR1](https://thefederalregister.org/doc/80_FR_19947/page/3.svg)
Document Created: 2015-12-18 11:10:12
Document Modified: 2015-12-18 11:10:12
| 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 | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD becomes effective April 29, 2015. | |
| Contact | Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. | |
| FR Citation | 80 FR 19876 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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