80 FR 60795 - Airworthiness Directives; Dassault Aviation Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 80, Issue 195 (October 8, 2015)

Page Range		60795-60797
FR Document		2015-25492

We are adopting a new airworthiness directive (AD) for all Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. This AD was prompted by reports of defective fire extinguisher tubes. It was determined the defects were caused by corrosion. This AD requires repetitive general visual inspections of the fire extinguisher tubes for cracking and corrosion, and replacement of any cracked tube with a serviceable tube, if necessary. We are issuing this AD to detect and correct cracking and corrosion in the fire extinguisher tubes, which could impact the capability to extinguish an engine fire, and possibly result in damage to the airplane and injury to the passengers.

Federal Register, Volume 80 Issue 195 (Thursday, October 8, 2015)

[Federal Register Volume 80, Number 195 (Thursday, October 8, 2015)]
[Rules and Regulations]
[Pages 60795-60797]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2015-25492]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 80, No. 195 / Thursday, October 8, 2015 / 
Rules and Regulations

[[Page 60795]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-0934; Directorate Identifier 2014-NM-030-AD; 
Amendment 39-18287; AD 2015-20-08]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G 
airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 
20-C5, 20-D5, 20-E5, and 20-F5 airplanes. This AD was prompted by 
reports of defective fire extinguisher tubes. It was determined the 
defects were caused by corrosion. This AD requires repetitive general 
visual inspections of the fire extinguisher tubes for cracking and 
corrosion, and replacement of any cracked tube with a serviceable tube, 
if necessary. We are issuing this AD to detect and correct cracking and 
corrosion in the fire extinguisher tubes, which could impact the 
capability to extinguish an engine fire, and possibly result in damage 
to the airplane and injury to the passengers.

DATES: This AD becomes effective November 12, 2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-0934; or in person at the 
Docket Management Facility, U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC.

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

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to all Dassault Aviation Model 
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; 
Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-
D5, 20-E5, and 20-F5 airplanes. The NPRM published in the Federal 
Register on May 4, 2015 (80 FR 25254).
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued 
Airworthiness Directive 2013-0299, dated December 19, 2013 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all Dassault Aviation 
Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G 
airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 
20-C5, 20-D5, 20-E5, and 20-F5 airplanes. The MCAI states:

    Several defective extinguisher tubes have been reported on 
certain Dassault Aviation Fan Jet Falcon aeroplanes. The results of 
the investigations concluded that these occurrences were caused by 
corrosion.
    This condition, if not detected and corrected, could impact the 
capability to extinguish an engine fire, possibly resulting in 
damage to the aeroplane and injury to the occupants.
    For the reason described above, this [EASA] AD requires 
repetitive [general visual] inspections [for cracking and corrosion] 
of the fire extinguisher tubes and, depending on findings, the 
replacement of an affected part with a serviceable part (improved 
fire extinguisher tube). It also proposes the replacement of those 
tubes with the ``old Part Number'' (P/N) with a serviceable part 
with the new P/N as a terminating action. In addition, this [EASA] 
AD prohibits installation of an affected tube on an aeroplane.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-0934-0002.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (80 FR 25254, May 4, 2015) 
or on the determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed, except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (80 FR 25254, May 4, 2015) for correcting the unsafe condition; 
and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (80 FR 25254, May 4, 2015).

Costs of Compliance

    We estimate that this AD affects 170 airplanes of U.S. registry.
    We also estimate that it will take about 4 work-hours per product 
to comply with the basic requirements of this AD. The average labor 
rate is $85 per work hour. Based on these figures, we estimate the cost 
of this AD on U.S. operators to be $57,800, or $340 per product.
    We have received no definitive data that will enable us to provide 
cost estimates for the on-condition actions specified in this 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

[[Page 60796]]

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.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-0934; 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 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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:


    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2015-20-08 Dassault Aviation: Amendment 39-18287. Docket No. FAA-
2015-0934; Directorate Identifier 2014-NM-030-AD.

(a) Effective Date

    This AD becomes effective November 12, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Dassault Aviation Model FAN JET FALCON, FAN 
JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 
200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-
F5 airplanes, certificated in any category, all manufacturer serial 
numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire 
protection.

(e) Reason

    This AD was prompted by reports of defective fire extinguisher 
tubes. It was determined the defects were caused by corrosion. We 
are issuing this AD to detect and correct cracking and corrosion in 
the fire extinguisher tubes, which could impact the capability to 
extinguish an engine fire, and possibly result in damage to the 
airplane and injury to the passengers.

(f) Compliance

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

(g) Inspection

    For airplanes identified in paragraphs (g)(1), (g)(2), and 
(g)(3) of this AD: Within 13 months or 450 flight hours, whichever 
occurs first after the effective date of this AD, do a general 
visual inspection of the fire extinguisher tubes for cracking and 
corrosion, in accordance with 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). Repeat the 
inspection thereafter at intervals not to exceed 13 months.
    (1) Model FAN JET FALCON airplanes and Model FAN JET FALCON 
SERIES C, D, E, F, and G airplanes, equipped with any fire 
extinguisher tubes having part numbers MY20791-101, MY20791-101-1, 
MY20791-102, MY20791-102-1, MY20791-117, and MY20791-112.
    (2) Model MYSTERE-FALCON 200 airplanes equipped with any fire 
extinguisher tubes having part numbers M20H791000210B1 and 
M20H791000240B1.
    (3) Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 
airplanes equipped with any fire extinguisher tubes having part 
numbers M20R791101, M20R791101A1, and M20R791102.

(h) Corrective Action

    If, during any inspection required by paragraph (g) of this AD, 
any cracking or corrosion is found, before further flight, replace 
the tube with a serviceable tube having a part number specified in 
Table 1 to paragraph (h) of this AD, as applicable.

                    Table 1 to Paragraph (h) of This AD--Serviceable Fire Extinguisher Tubes
----------------------------------------------------------------------------------------------------------------
               For model--                 Equipped with affected pin--       Replace with serviceable pin--
----------------------------------------------------------------------------------------------------------------
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-101.................  MY20791-101-2.
 D, E, F, and G airplanes.
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-101-1...............  MY20791-101-2.
 D, E, F, and G airplanes.
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-102.................  MY20791-102-2.
 D, E, F, and G airplanes.
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-102-1...............  MY20791-102-2.
 D, E, F, and G airplanes.
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-117.................  MY20791-117n-1.
 D, E, F, and G airplanes.
FAN JET FALCON, FAN JET FALCON SERIES C,   MY20791-112.................  MY20791-112-1.
 D, E, F, and G airplanes.
MYSTERE-FALCON 200 airplanes.............  M20H791000210B1.............  M20H791000210B2.
MYSTERE-FALCON 200 airplanes.............  M20H791000240B1.............  M20H791000240B2.
MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and    M20R791101..................  M20R791101A2.
 20-F5 airplanes.
MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and    M20R791101A1................  M20R791101A3.
 20-F5 airplanes.
MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and    M20R791102..................  M20R791102A2.
 20-F5 airplanes.
----------------------------------------------------------------------------------------------------------------


[[Page 60797]]

(i) Terminating Action for the Repetitive Inspections

    Replacement of an affected tube with a serviceable tube, as 
required by paragraph (h) of this AD, constitutes a terminating 
action for the repetitive inspections required by paragraph (g) of 
this AD.

(j) Parts Installation Prohibition

    As of the effective date of this AD, no person may install a 
tube having a part number identified in paragraphs (g)(1), (g)(2), 
and (g)(3) of this AD, on any airplane.

(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: 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: 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.

(l) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI) 
EASA Airworthiness Directive 2013-0299, dated December 19, 2013, for 
related information. This MCAI may be found in the AD docket on the 
Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-
0934-0002.

(m) Material Incorporated by Reference

    None.

    Issued in Renton, Washington, on September 29, 2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-25492 Filed 10-7-15; 8:45 am]
 BILLING CODE 4910-13-P

60795

Rules and Regulations Federal Register
Vol. 80, No. 195

Thursday, October 8, 2015

This section of the FEDERAL REGISTER 30, West Building Ground Floor, Room You may examine the MCAI in the
contains regulatory documents having general W12–140, 1200 New Jersey Avenue SE., AD docket on the Internet at http://
applicability and legal effect, most of which Washington, DC. www.regulations.gov/
are keyed to and codified in the Code of #!documentDetail;D=FAA-2015-0934-
FOR FURTHER INFORMATION CONTACT: Tom
Federal Regulations, which is published under 0002.
50 titles pursuant to 44 U.S.C. 1510. Rodriguez, Aerospace Engineer,
International Branch, ANM–116, Comments
The Code of Federal Regulations is sold by Transport Airplane Directorate, FAA,
the Superintendent of Documents. Prices of 1601 Lind Avenue SW., Renton, WA We gave the public the opportunity to
new books are listed in the first FEDERAL 98057–3356; telephone 425–227–1137; participate in developing this AD. We
REGISTER issue of each week. fax 425–227–1149. received no comments on the NPRM (80
SUPPLEMENTARY INFORMATION:
FR 25254, May 4, 2015) or on the
determination of the cost to the public.
DEPARTMENT OF TRANSPORTATION Discussion
Conclusion
We issued a notice of proposed
Federal Aviation Administration We reviewed the relevant data and
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would determined that air safety and the
14 CFR Part 39 public interest require adopting this AD
apply to all Dassault Aviation Model
[Docket No. FAA–2015–0934; Directorate FAN JET FALCON, FAN JET FALCON as proposed, except for minor editorial
Identifier 2014–NM–030–AD; Amendment SERIES C, D, E, F, and G airplanes; changes. We have determined that these
39–18287; AD 2015–20–08] Model MYSTERE–FALCON 200 minor changes:
• Are consistent with the intent that
RIN 2120–AA64 airplanes; and Model MYSTERE–
was proposed in the NPRM (80 FR
FALCON 20–C5, 20–D5, 20–E5, and 20–
25254, May 4, 2015) for correcting the
Airworthiness Directives; Dassault F5 airplanes. The NPRM published in
unsafe condition; and
Aviation Airplanes the Federal Register on May 4, 2015 (80
• Do not add any additional burden
FR 25254).
AGENCY: Federal Aviation upon the public than was already
The European Aviation Safety Agency
Administration (FAA), Department of proposed in the NPRM (80 FR 25254,
(EASA), which is the Technical Agent
Transportation (DOT). May 4, 2015).
for the Member States of the European
ACTION: Final rule. Union, has issued Airworthiness Costs of Compliance
Directive 2013–0299, dated December We estimate that this AD affects 170
SUMMARY: We are adopting a new
19, 2013 (referred to after this as the airplanes of U.S. registry.
airworthiness directive (AD) for all
Mandatory Continuing Airworthiness We also estimate that it will take
Model FAN JET FALCON, FAN JET
Information, or ‘‘the MCAI’’), to correct about 4 work-hours per product to
FALCON SERIES C, D, E, F, and G
an unsafe condition for all Dassault comply with the basic requirements of
airplanes; Model MYSTERE–FALCON
Aviation Model FAN JET FALCON, this AD. The average labor rate is $85
200 airplanes; and Model MYSTERE–
FAN JET FALCON SERIES C, D, E, F, per work hour. Based on these figures,
FALCON 20–C5, 20–D5, 20–E5, and 20–
and G airplanes; Model MYSTERE– we estimate the cost of this AD on U.S.
F5 airplanes. This AD was prompted by
FALCON 200 airplanes; and Model operators to be $57,800, or $340 per
reports of defective fire extinguisher
MYSTERE–FALCON 20–C5, 20–D5, 20– product.
tubes. It was determined the defects
E5, and 20–F5 airplanes. The MCAI We have received no definitive data
were caused by corrosion. This AD
states: that will enable us to provide cost
requires repetitive general visual
inspections of the fire extinguisher Several defective extinguisher tubes have estimates for the on-condition actions
tubes for cracking and corrosion, and been reported on certain Dassault Aviation specified in this AD.
Fan Jet Falcon aeroplanes. The results of the
replacement of any cracked tube with a Authority for This Rulemaking
investigations concluded that these
serviceable tube, if necessary. We are occurrences were caused by corrosion.
issuing this AD to detect and correct Title 49 of the United States Code
This condition, if not detected and specifies the FAA’s authority to issue
cracking and corrosion in the fire corrected, could impact the capability to
extinguisher tubes, which could impact extinguish an engine fire, possibly resulting
rules on aviation safety. Subtitle I,
the capability to extinguish an engine in damage to the aeroplane and injury to the section 106, describes the authority of
fire, and possibly result in damage to occupants. the FAA Administrator. ‘‘Subtitle VII:
the airplane and injury to the For the reason described above, this Aviation Programs,’’ describes in more
passengers. [EASA] AD requires repetitive [general detail the scope of the Agency’s
visual] inspections [for cracking and authority.
DATES: This AD becomes effective corrosion] of the fire extinguisher tubes and, We are issuing this rulemaking under
November 12, 2015. depending on findings, the replacement of an the authority described in ‘‘Subtitle VII,
ADDRESSES: You may examine the AD affected part with a serviceable part Part A, Subpart III, Section 44701:
Lhorne on DSK5TPTVN1PROD with RULES

(improved fire extinguisher tube). It also General requirements.’’ Under that
docket on the Internet at http://
proposes the replacement of those tubes with
www.regulations.gov/ the ‘‘old Part Number’’ (P/N) with a
section, Congress charges the FAA with
#!docketDetail;D=FAA-2015-0934; or in serviceable part with the new P/N as a promoting safe flight of civil aircraft in
person at the Docket Management terminating action. In addition, this [EASA] air commerce by prescribing regulations
Facility, U.S. Department of AD prohibits installation of an affected tube for practices, methods, and procedures
Transportation, Docket Operations, M– on an aeroplane. the Administrator finds necessary for

VerDate Sep<11>2014 14:46 Oct 07, 2015 Jkt 238001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\08OCR1.SGM 08OCR1

60796 Federal Register / Vol. 80, No. 195 / Thursday, October 8, 2015 / Rules and Regulations

safety in air commerce. This regulation List of Subjects in 14 CFR Part 39 determined the defects were caused by
is within the scope of that authority corrosion. We are issuing this AD to detect
Air transportation, Aircraft, Aviation and correct cracking and corrosion in the fire
because it addresses an unsafe condition safety, Incorporation by reference,
that is likely to exist or develop on extinguisher tubes, which could impact the
Safety. capability to extinguish an engine fire, and
products identified in this rulemaking
Adoption of the Amendment possibly result in damage to the airplane and
action.
injury to the passengers.
Regulatory Findings Accordingly, under the authority
delegated to me by the Administrator, (f) Compliance
We determined that this AD will not the FAA amends 14 CFR part 39 as Comply with this AD within the
have federalism implications under follows: compliance times specified, unless already
Executive Order 13132. This AD will done.
not have a substantial direct effect on PART 39—AIRWORTHINESS
(g) Inspection
the States, on the relationship between DIRECTIVES
the national government and the States, For airplanes identified in paragraphs
■ 1. The authority citation for part 39 (g)(1), (g)(2), and (g)(3) of this AD: Within 13
or on the distribution of power and
continues to read as follows: months or 450 flight hours, whichever occurs
responsibilities among the various first after the effective date of this AD, do a
levels of government. Authority: 49 U.S.C. 106(g), 40113, 44701. general visual inspection of the fire
For the reasons discussed above, I extinguisher tubes for cracking and
certify that this AD: § 39.13 [Amended]
corrosion, in accordance with a method
1. Is not a ‘‘significant regulatory ■ 2. The FAA amends § 39.13 by adding approved by the Manager, International
action’’ under Executive Order 12866; the following new airworthiness Branch, ANM–116, Transport Airplane
2. Is not a ‘‘significant rule’’ under the directive (AD): Directorate, FAA; or the European Aviation
Safety Agency (EASA); or Dassault Aviation’s
DOT Regulatory Policies and Procedures 2015–20–08 Dassault Aviation:
EASA Design Organization Approval (DOA).
(44 FR 11034, February 26, 1979); Amendment 39–18287. Docket No.
FAA–2015–0934; Directorate Identifier Repeat the inspection thereafter at intervals
3. Will not affect intrastate aviation in not to exceed 13 months.
2014–NM–030–AD.
Alaska; and (1) Model FAN JET FALCON airplanes and
4. Will not have a significant (a) Effective Date Model FAN JET FALCON SERIES C, D, E, F,
economic impact, positive or negative, This AD becomes effective November 12, and G airplanes, equipped with any fire
on a substantial number of small entities 2015. extinguisher tubes having part numbers
under the criteria of the Regulatory MY20791–101, MY20791–101–1, MY20791–
(b) Affected ADs 102, MY20791–102–1, MY20791–117, and
Flexibility Act. None. MY20791–112.
Examining the AD Docket (c) Applicability (2) Model MYSTERE–FALCON 200
airplanes equipped with any fire extinguisher
You may examine the AD docket on This AD applies to Dassault Aviation tubes having part numbers
the Internet at http:// Model FAN JET FALCON, FAN JET FALCON M20H791000210B1 and M20H791000240B1.
www.regulations.gov/ SERIES C, D, E, F, and G airplanes; Model (3) Model MYSTERE–FALCON 20–C5, 20–
#!docketDetail;D=FAA-2015-0934; or in MYSTERE–FALCON 200 airplanes; and
D5, 20–E5, and 20–F5 airplanes equipped
Model MYSTERE–FALCON 20–C5, 20–D5,
person at the Docket Management 20–E5, and 20–F5 airplanes, certificated in
with any fire extinguisher tubes having part
Facility between 9 a.m. and 5 p.m., any category, all manufacturer serial numbers M20R791101, M20R791101A1, and
Monday through Friday, except Federal numbers. M20R791102.
holidays. The AD docket contains this (h) Corrective Action
(d) Subject
AD, the regulatory evaluation, any If, during any inspection required by
comments received, and other Air Transport Association (ATA) of
America Code 26, Fire protection. paragraph (g) of this AD, any cracking or
information. The street address for the corrosion is found, before further flight,
Docket Operations office (telephone (e) Reason replace the tube with a serviceable tube
800–647–5527) is in the ADDRESSES This AD was prompted by reports of having a part number specified in Table 1 to
section. defective fire extinguisher tubes. It was paragraph (h) of this AD, as applicable.

TABLE 1 TO PARAGRAPH (H) OF THIS AD—SERVICEABLE FIRE EXTINGUISHER TUBES
Replace with service-
For model— Equipped with affected pin— able pin—

FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–101 ....................................... MY20791–101–2.
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–101–1 ................................... MY20791–101–2.
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–102 ....................................... MY20791–102–2.
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–102–1 ................................... MY20791–102–2.
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–117 ....................................... MY20791–117n–1.
FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes .. MY20791–112 ....................................... MY20791–112–1.
MYSTERE–FALCON 200 airplanes ..................................................................... M20H791000210B1 .............................. M20H791000210B2.
MYSTERE–FALCON 200 airplanes ..................................................................... M20H791000240B1 .............................. M20H791000240B2.
MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791101 ........................................ M20R791101A2.
MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791101A1 .................................... M20R791101A3.
Lhorne on DSK5TPTVN1PROD with RULES

MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes ................... M20R791102 ........................................ M20R791102A2.

VerDate Sep<11>2014 14:46 Oct 07, 2015 Jkt 238001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\08OCR1.SGM 08OCR1

Federal Register / Vol. 80, No. 195 / Thursday, October 8, 2015 / Rules and Regulations 60797

(i) Terminating Action for the Repetitive FEDERAL TRADE COMMISSION SUMMARY: This rule will allow the U.S.
Inspections Department of Labor (Department) to
Replacement of an affected tube with a 16 CFR Part 4 garnish the disposable wages of non-
serviceable tube, as required by paragraph (h) federal workers who are indebted to the
of this AD, constitutes a terminating action Miscellaneous Rules Department without first obtaining a
for the repetitive inspections required by AGENCY: Federal Trade Commission. court order. It implements the
paragraph (g) of this AD. administrative wage garnishment
ACTION: Final rules; technical correction.
(j) Parts Installation Prohibition provisions contained in the Debt
SUMMARY: The Federal Trade Collection Improvement Act of 1996
As of the effective date of this AD, no
person may install a tube having a part Commission published final rules on (DCIA) in accordance with the
number identified in paragraphs (g)(1), (g)(2), May 6, 2015, revising certain of its rules regulations issued by the Secretary of
and (g)(3) of this AD, on any airplane. of practice. This document makes a the Treasury.
technical correction to those final rules. DATES: This rule is effective October 8,
(k) Other FAA AD Provisions
DATES: Effective October 8, 2015. 2015. Comments must be received
The following provisions also apply to this FOR FURTHER INFORMATION CONTACT: within 30 days of publication, which is
AD: on or before November 9, 2015.
Josephine Liu, Attorney, (202) 326–
(1) Alternative Methods of Compliance
2170, Office of the General Counsel, ADDRESSES: You may submit written
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Federal Trade Commission, 600 comments to the docket using any one
Directorate, FAA, has the authority to Pennsylvania Avenue NW., Washington, of the following methods:
approve AMOCs for this AD, if requested DC 20580. (1) Federal eRulemaking Portal:
using the procedures found in 14 CFR 39.19. SUPPLEMENTARY INFORMATION: This http://www.regulations.gov.
In accordance with 14 CFR 39.19, send your document makes a technical correction (2) Mail: Address comments
request to your principal inspector or local to two cross-references in Rule 4.4(a)(3). concerning this interim rule to Shelia
Flight Standards District Office, as Alexander, Office of Chief Financial
appropriate. If sending information directly List of Subjects in 16 CFR Part 4
Officer, U.S. Department of Labor,
to the International Branch, send it to ATTN: Administrative practice and Frances Perkins Building, Room S4030,
Tom Rodriguez, Aerospace Engineer, procedure, Freedom of information, 200 Constitution Avenue NW.,
International Branch, ANM–116, Transport Public record.
Airplane Directorate, FAA, 1601 Lind
Washington, DC 20210.
Accordingly, 16 CFR part 4 is (3) Email: Comments may also be
Avenue SW., Renton, WA 98057–3356;
corrected by making the following submitted by electronic mail to
telephone 425–227–1137; fax 425–227–1149.
Information may be emailed to: 9-ANM-116-
correcting amendment: alexander.shelia@dol.gov.
AMOC-REQUESTS@faa.gov. Before using Additionally, any comments that
PART 4—MISCELLANEOUS RULES
any approved AMOC, notify your appropriate concern information collection may be
principal inspector, or lacking a principal ■ 1. The authority citation for part 4 sent to the Office of Information and
inspector, the manager of the local flight continues to read as follows: Regulatory Affairs, Attention OMB Desk
standards district office/certificate holding Officer for DOL, Office of Management
district office. The AMOC approval letter Authority: 15 U.S.C. 46, unless otherwise
noted.
and Budget, Room 10235, New
must specifically reference this AD. Executive Office Building, Washington,
(2) Contacting the Manufacturer: For any § 4.4 [Amended] DC 20503.
requirement in this AD to obtain corrective
actions from a manufacturer, the action must ■ 2. In § 4.4, amend the first sentence of FOR FURTHER INFORMATION CONTACT:
be accomplished using a method approved paragraph (a)(3) by removing ‘‘section Shelia Alexander, Office of the Chief
by the Manager, International Branch, ANM– 20(c)(7) of the FTC Act’’ and adding in Financial Officer, (202) 693–4472; or
116, Transport Airplane Directorate, FAA; or its place ‘‘section 20(c)(8) of the FTC Rachel Rikleen, Office of the Solicitor,
the European Aviation Safety Agency Act’’ and by removing ‘‘section 20(c)(8) (202) 693–5702.
(EASA); or Dassault Aviation’s EASA Design of the FTC Act’’ and adding in its place SUPPLEMENTARY INFORMATION:
Organization Approval (DOA). If approved by ‘‘section 20(c)(9) of the FTC Act’’.
the DOA, the approval must include the I. Background
DOA-authorized signature. By direction of the Commission.
Donald S. Clark, Section 31001(o) of the Debt
(l) Related Information
Secretary.
Collection Improvement Act of 1996
Refer to Mandatory Continuing (DCIA), which is codified at 31 U.S.C.
[FR Doc. 2015–25605 Filed 10–7–15; 8:45 am]
Airworthiness Information (MCAI) EASA 3720D, authorizes federal agencies to
BILLING CODE 6750–01–P
Airworthiness Directive 2013–0299, dated use administrative procedure to garnish
December 19, 2013, for related information. the disposable pay of an individual to
This MCAI may be found in the AD docket collect delinquent non-tax debt owed to
on the Internet at http:// DEPARTMENT OF LABOR the United States in accordance with
www.regulations.gov/ regulations promulgated by the
#!documentDetail;D=FAA-2015-0934-0002. Office of the Secretary
Secretary of the Treasury. Wage
(m) Material Incorporated by Reference garnishment is a process whereby an
29 CFR Part 20
None. employer withholds amounts from an
RIN 1290–AA27 employee’s wages and pays those
Issued in Renton, Washington, on amounts to the employee’s creditor
Lhorne on DSK5TPTVN1PROD with RULES

September 29, 2015. Administrative Wage Garnishment pursuant to a withholding order. Under
Jeffrey E. Duven, Procedures the DCIA, agencies may garnish up to
Manager, Transport Airplane Directorate, 15% of a delinquent non-tax debtor’s
AGENCY: Office of the Secretary, Labor.
Aircraft Certification Service. disposable wages. Prior to the
ACTION:Interim final rule with request
[FR Doc. 2015–25492 Filed 10–7–15; 8:45 am] enactment of the DCIA, agencies were
for comments.
BILLING CODE 4910–13–P generally required to obtain a court

VerDate Sep<11>2014 14:46 Oct 07, 2015 Jkt 238001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\08OCR1.SGM 08OCR1

Document Created: 2015-12-15 08:42:58
Document Modified: 2015-12-15 08:42:58

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.
Dates		This AD becomes effective November 12, 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 60795
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

80 FR 60795 - Airworthiness Directives; Dassault Aviation Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 80, Issue 195 (October 8, 2015)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration