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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 al-
    ready 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        REPLACE WITH
                                AFFECTED PIN —       SERVICEABLE PIN —
    ______________________________________________________________________
    FAN JET FALCON,             MY20791-101          MY20791-101-2
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    FAN JET FALCON,             MY20791-101-1        MY20791-101-2
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    FAN JET FALCON,             MY20791-102          MY20791-102-2
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    FAN JET FALCON,             MY20791-102-1        MY20791-102-2
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    FAN JET FALCON,             MY20791-117          MY20791-117n-1
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    FAN JET FALCON,             MY20791-112          MY20791-112-1
    FAN JET FALCON
    SERIES C, D, E,
    F, and G airplanes

    MYSTERE-FALCON 200          M20H791000210B1      M20H791000210B2
    airplanes

    MYSTERE-FALCON 200          M20H791000240B1      M20H791000240B2
    airplanes

    MYSTERE-FALCON              M20R791101           M20R791101A2
    20-C5, 20-D5,
    20-E5, and 20-F5
    airplanes

    MYSTERE-FALCON              M20R791101A1         M20R791101A3
    20-C5, 20-D5,
    20-E5, and 20-F5
    airplanes

    MYSTERE-FALCON              M20R791102           M20R791102A2
    20-C5, 20-D5,
    20-E5, and 20-F5
    airplanes
    ______________________________________________________________________

(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: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Branch, ANM-116,  Transport Airplane Directorate,  FAA, 1601 Lind
Avenue SW, Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149
PREAMBLE 

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 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

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]


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