
[Federal Register Volume 81, Number 211 (Tuesday, November 1, 2016)]
[Proposed Rules]
[Pages 75757-75758]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-26325]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9303; Directorate Identifier 2016-NM-093-AD]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all 
Dassault Aviation Model FAN JET FALCON airplanes; all Model FAN JET 
FALCON SERIES C, D, E, F, and G airplanes; and all Model MYSTERE-FALCON 
20-C5, 20-D5, 20-E5, and 20-F5 airplanes. This proposed AD was prompted 
by a determination that inspections for discrepancies of the fuselage 
bulkhead are necessary. This proposed AD would require repetitive 
inspections for discrepancies of the fuselage bulkhead, and repair if 
necessary. We are proposing this AD to detect and correct discrepancies 
of the fuselage bulkhead; such discrepancies could result in the 
deterioration and failure of the bulkhead, which could result in rapid 
decompression of the airplane and consequent injury to occupants.

DATES: We must receive comments on this proposed AD by December 16, 
2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

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-2016-
9303; or in person at the Docket Management Facility between 9 a.m. and 
5 p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this proposed AD, the regulatory evaluation, any comments 
received, and other information. The street address for the Docket 
Operations office (telephone: 800-647-5527) is in the ADDRESSES 
section. Comments will be available in the AD docket shortly after 
receipt.

FOR FURTHER INFORMATION CONTACT: 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: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2016-9303; 
Directorate Identifier 2016-NM-093-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2016-0096, dated May 19, 2016 (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 airplanes; all Model FAN JET FALCON SERIES C, D, 
E, F, and G airplanes; and all Model MYSTERE-FALCON 20-C5, 20-D5, 20-
E5, and 20-F5 airplanes. The MCAI states:

    A detailed inspection (DET) of the fuselage bulkhead at frame 
(FR) 33 is established through a subset of inspection/check 
maintenance procedure referenced in the applicable aircraft 
maintenance manual (AMM), task 53-10-0-6 ``MAIN FRAME--INSPECTION/
CHECK'', with periodicity established in Chapter 5-10, at every C-
Check. Failure to accomplish this DET could lead to deterioration of 
the affected structure.
    This condition, if not detected and corrected, could lead to 
bulkhead failure, possibly resulting in a rapid depressurization of 
the aeroplane and consequent injury to occupants.
    For the reasons described above, this [EASA] AD requires 
repetitive DET of the bulkhead at FR33 [for discrepancies, such as 
buckling, deformations, cracks, loose countersinks, scratches, 
dents, and corrosion], and depending on findings, repair of the 
affected structure.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9303.

FAA's Determination and Requirements of This Proposed 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 proposing this AD because we 
evaluated all pertinent information and determined an unsafe condition 
exists and is likely to exist or develop on other products of these 
same type designs.

Costs of Compliance

    We estimate that this proposed AD affects 133 airplanes of U.S. 
registry.
    We also estimate that it would take about 8 work-hours per product 
to

[[Page 75758]]

comply with the 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 proposed AD on U.S. operators to be $90,440, or $680 
per product.
    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this proposed 
AD.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. ``Subtitle VII: Aviation 
Programs,'' describes in more detail the scope of the Agency's 
authority.
    We are issuing this rulemaking under the authority described in 
``Subtitle VII, Part A, Subpart III, Section 44701: General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed 
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    3. Will not affect intrastate aviation in Alaska; and
    4. Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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


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


Sec.  39.13   [Amended]

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

Dassault Aviation: Docket No. FAA-2016-9303; Directorate Identifier 
2016-NM-093-AD.

(a) Comments Due Date

    We must receive comments by December 16, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Dassault Aviation airplanes specified in 
paragraphs (c)(1) and (c)(2) of this AD, certificated in any 
category, all manufacturer serial numbers.
    (1) Model FAN JET FALCON and FAN JET FALCON SERIES C, D, E, F, 
and G airplanes.
    (2) Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 
airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Reason

    This AD was prompted by a determination that inspections for 
discrepancies of the fuselage bulkhead at frame (FR) 33 are 
necessary. We are issuing this AD to detect and correct 
discrepancies of the fuselage bulkhead; such discrepancies could 
result in the deterioration and subsequent failure of the bulkhead, 
which could result in rapid decompression of the airplane and 
consequent injury to occupants.

(f) Compliance

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

(g) Repetitive Inspections

    Before exceeding 5,000 total flight cycles since first flight of 
the airplane, or within 500 flight cycles after the effective date 
of this AD, whichever occurs later: Do a detailed inspection for 
discrepancies of the fuselage bulkhead at FR 33 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. Repeat the inspection thereafter at intervals 
not to exceed 5,000 flight cycles.

(h) Repair

    If any discrepancy is found during any inspection required by 
paragraph (g) of this AD: Before further flight, repair using a 
method approved by the Manager, International Branch, ANM-116, 
Transport Airplane Directorate, FAA; or the EASA; or Dassault 
Aviation's EASA DOA. If approved by the DOA, the approval must 
include the DOA-authorized signature. Repair of an airplane as 
required by this paragraph does not constitute terminating action 
for the repetitive actions required by paragraph (g) of this AD, 
unless specified otherwise in the repair instructions.

(i) 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.
    (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 EASA; 
or Dassault Aviation's EASA DOA. If approved by the DOA, the 
approval must include the DOA-authorized signature.

(j) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI) 
EASA Airworthiness Directive 2016-0096, dated May 19, 2016, 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-2016-9303.

    Issued in Renton, Washington, on October 26, 2016.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-26325 Filed 10-31-16; 8:45 am]
 BILLING CODE 4910-13-P


