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2012-12-18 DASSAULT AVIATION: Amendment 39-17098. Docket No. FAA-2012-0265; Directorate Identifier 2010-NM-216-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective July 30, 2012.

(b) AFFECTED ADS

    This AD  supersedes AD  2010-18-03, Amendment  39-16416 (75  FR 51931,
    August 24, 2010).

(c) APPLICABILITY

    This  AD  applies  to Dassault  Aviation  Model  FALCON 7X  airplanes,
    certificated in any category, all serial numbers except those on which
    Dassault Aviation Modification M724 is embodied.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 24: Electrical Power.

(e) REASON

    This AD was  prompted by a  determination that additional  actions are
    necessary to address the  identified unsafe condition. We  are issuing
    this AD  to detect  and correct  a leakage  failure mode  of transient
    voltage suppression  (TVS) diodes  used on  power distribution control
    units  (PDCU) cards  or  generator  control units  (GCU) cards  in the
    primary power  distribution boxes,  which, in  combination with  other
    system  failures,  could  lead  to  loss  of  controllability  of  the
    airplane.

(f) COMPLIANCE

    You  are  responsible  for  having the  actions  required  by  this AD
    performed within  the compliance  times specified,  unless the actions
    have already been done.

(g) RETAINED AIRPLANE FLIGHT MANUAL (AFM) REVISION

    This AFM revision is  retained from AD 2010-18-03,  Amendment 39-16416
    (75 FR 51931, August 24, 2010): Within 30 days after September 8, 2010
    (the effective date of  AD 2010-18-03, revise the  Abnormal Procedures
    and  Limitations  sections of  the  Dassault F7X  AFM  to include  the
    following statement. This may be  done by inserting copies of  this AD
    into the AFM Limitations section and Abnormal Procedures section.

    Upon  display  of  ELEC:BUS MISCONFIG  TIED  in  Crew Alerting  System
    (Abnormal procedure  3-190-20), land  atnearest suitable  airport Upon
    display  of  ELEC:LH  ESS  PWR LO  or  ELEC:LH  ESS  NO PWR  (Abnormal
    procedure 3-190-40), land at nearest suitable airport Upon display  of
    ELEC:RH ESS PWR  LO and ELEC:RH  ESS NO PWR  (Abnormal procedure 3-190
    -45), land at nearest suitable airport

    Upon  display of  HYD:BACKUP PUMP  HI TEMP  (Abnormal procedure  3-250
    -15),  set off  the pump  and if  the backup  pump  is  still rotating
    (green) in  hydraulic synoptic,  descend to  a safe  altitude or below
    15,000 ft

    Caution:  These temporary  amendments  take  precedence over  the same
    procedures displayed through  the Electronic Check  List (ECL) in  the
    aeroplane.

NOTE 1 TO PARAGRAPH (G) OF THIS AD: When a statement identical to that  in
paragraph (g) of this AD has been included in the Limitations section  and
Abnormal  Procedures section  in the  general revisions  of the  AFM,  the
general revisions may be  inserted into the AFM,  and the copy of  this AD
may be removed.

(h) NEW REQUIREMENTS OF THIS AD: TEST THE PDCU AND GCU CARDS

    For airplanes  identified in  Dassault Mandatory  Service Bulletin  7X
    -133, dated December 4, 2009: Within 9 months after the effective date
    of this AD, perform a test of the PDCU and GCU cards to detect  faulty
    components,  in  accordance with  the  Accomplishment Instructions  of
    Dassault Mandatory Service Bulletin 7X-133, dated December 4, 2009. If
    any faulty components  are found, before  further flight, replace  any
    affected  PDCU  or GCU  card,  in accordance  with  the Accomplishment
    Instructions  of  Dassault Mandatory  Service  Bulletin 7X-133,  dated
    December 4, 2009.

(i) OPTIONAL METHOD OF COMPLIANCE

    For airplanes  identified in  Dassault Mandatory  Service Bulletin  7X
    -133, dated December 4,  2009: Accomplishing the actions  specified in
    paragraph (h) of this AD, within 9 months after the effective date  of
    this  AD,  in accordance  with  the service  information  specified in
    paragraphs (i)(1), (i)(2),  and (i)(3) of  this AD, is  acceptable for
    compliance with the actions specified in paragraph (h) of this AD.

(1) Goodrich Service Bulletin 80232190-24-01, dated August 13, 2009.

(2) Goodrich Service Bulletin 80232191-24-01, dated August 13, 2009.

(3) Goodrich Service Bulletin 80232192-24-01, dated August 13, 2009.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Branch, ANM-116, 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,
    Washington 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) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product is airworthy before  it
    is returned to service.

(k) RELATED INFORMATION

    Refer to MCAI European Aviation Safety Agency Airworthiness  Directive
    2010-0073, dated April 15,  2010, and the service  bulletins specified
    in  paragraphs  (k)(1)  through   (k)(4)  of  this  AD,   for  related
    information.

(1) Dassault Mandatory Service Bulletin 7X-133, dated December 4, 2009.

(2) Goodrich Service Bulletin 80232190-24-01, dated August 13, 2009.

(3) Goodrich Service Bulletin 80232191-24-01, dated August 13, 2009.

(4) Goodrich Service Bulletin 80232192-24-01, dated August 13, 2009.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) The  Director  of  the  Federal Register approved the incorporation by
    reference (IBR) of  the following service  information under 5  U.S.C.
    552(a) and 1 CFR part 51.

(2) You  must  use  the  following  service  information to do the actions
    required by this AD, unless  the AD specifies otherwise. (i)  Dassault
    Mandatory Service Bulletin 7X-133, dated December 4, 2009.

(3) If you accomplish the optional actions specified by this AD,  you must
    use the following service information to perform those actions, unless
    the AD specifies otherwise.

(i) Goodrich Service Bulletin 80232190-24-01, dated August 13, 2009.

(ii) Goodrich Service Bulletin 80232191-24-01, dated August 13, 2009.

(iii) Goodrich Service Bulletin 80232192-24-01, dated August 13, 2009.

(4) For  Dassault  service  information  identified  in  this  AD, contact
    Dassault Falcon Jet,  PO Box 2000, South Hackensack, New Jersey 07606;
    telephone  201-440-6700;  Internet  http://www.dassaultfalcon.com. For
    Goodrich service information identified  in this AD, contact  Goodrich
    Corporation,  Power Systems,  1555 Corporate Woods Parkway, Uniontown,
    Ohio  44685-8799;  telephone  330-487-2007;  fax  330-487-1902;  email
    twinsburg.techpubs@goodrich.com; Internet http://www.goodrich.com/Tech
    Pubs.

(5) You may review copies of the service information at the FAA, Transport
    Airplane Directorate,  1601 Lind  Avenue SW.,  Renton, Washington. For
    information on the availability of this material at the FAA, call  425
    -227-1221.

(6) You  may  also  review  copies  of  the  service  information  that is
    incorporated  by  reference  at  the  National  Archives  and  Records
    Administration (NARA).  For information  on the  availability of  this
    material  at   an  NARA   facility,  call   202-741-6030,  or   go  to
    http://www.archives.gov/federal_register/code_of_federal_regulations/i
    br_locations.html.

Issued in Renton, Washington, on June 11, 2012. Kalene C. Yanamura, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

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

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

ACTION: Final rule.

SUMMARY: We are superseding an existing airworthiness directive (AD)
for certain Dassault Aviation Model FALCON 7X airplanes. That AD
currently requires revising the Abnormal Procedures and Limitations
sections of the Dassault F7X Airplane Flight Manual. This new AD
requires a test of the power distribution control units (PDCU) cards
and generator control units (GCU) cards to detect faulty components,
and if any faulty components are found, replacing any affected PDCU or
GCU card. This AD was prompted by a determination that additional
actions are necessary to address the identified unsafe condition. We
are issuing this AD to detect and correct a leakage failure mode of
transient voltage suppression (TVS) diodes used on PDCU cards or GCU
cards in the primary power distribution boxes (PPDB), which, in
combination with other system failures, could lead to loss of
controllability of the airplane.

DATES: This AD becomes effective July 30, 2012.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of July 30, 2012.

ADDRESSES: You may examine the AD docket on the Internet at http://www.
regulations.gov or in person at the 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, Washington 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 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on March 15, 2012 (77
FR 15293), and proposed to supersede AD AD 2010-18-03, Amendment 39-
16416 (75 FR 51931, August 24, 2010).
On August 11, 2010, we issued AD 2010-18-03, Amendment 39-16416 (75
FR 51931, August 24, 2010). That AD required actions intended to
address an unsafe condition on certain Dassault Aviation Model FALCON
7X airplanes. The preamble of AD 2010-18-03 explains that we consider
the requirements of that AD ``interim action'' and are considering
further rulemaking to mandate inspection (testing) of the PDCU and GCU
cards and replacement of faulty cards, as required by European Aviation
Safety Agency AD 2010-0073, dated April 15,
2010. The planned compliance time for those actions would allow enough
time for prior public comment on the merits of those actions. This
proposed AD follows from that determination.
The unsafe condition is a leakage failure mode of TVS diodes used
on PDCU or GCU cards in the PPDB, which, in combination with other
system failures, could lead to loss of controllability of the airplane.
You may obtain further information by examining the MCAI in the AD
docket.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (77 FR 15293, March 15,
2012) or on the determination of the cost to the public.

Conclusion

We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.

Costs of Compliance

We estimate that this AD will affect about 9 products of U.S.
registry.
The actions that are required by AD 2010-18-03, Amendment 39-16416
(75 FR 51931, August 24, 2010), and retained in this AD take about 4
work-hours per product, at an average labor rate of $85 per work hour.
Based on these figures, the estimated cost of the currently required
actions is $340 per product.
We estimate that it would take about 4 work-hours per product to
comply with the new basic requirements of this proposed 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 $3,060, or $340 per
product.
We have received no definitive data that would enable us to provide
cost estimates for the on-condition actions specified in this AD. We
have no way of determining the number of products that may need these
actions.

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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov;
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 the NPRM (75 FR 51931, August 24,
2010), 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.

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 removing airworthiness AD 2010-18-03,
Amendment 39-16416 (75 FR 51931, August 24, 2010), and adding the
following new AD: