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[Federal Register Volume 80, Number 125 (Tuesday, June 30, 2015)]
[Rules and Regulations]
[Pages 37150-37152]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-15860]

[[Page 37150]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-1988; Directorate Identifier 2015-NM-085-AD; 
Amendment 39-18195; AD 2015-13-08]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

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

ACTION: Final rule; request for comments.

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SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Dassault Aviation Model FALCON 2000EX airplanes. This AD requires 
revising the airplane flight manual to include a procedure for 
addressing minimum fan speed rotation (N1) values during stand-alone 
engine anti-ice system operation for engines equipped with certain air 
inlets. This AD was prompted by a quality review of recently delivered 
airplanes which identified a manufacturing deficiency of some engine 
air inlet anti-ice piccolo tubes. We are issuing this AD to detect and 
correct reduced performance of the engine anti-ice protection system, 
leading to ice accretion and ingestion into the engines, which could 
result in dual engine power loss and consequent reduced controllability 
of the airplane.

DATES: This AD becomes effective June 30, 2015.
    We must receive comments on this AD by August 14, 2015.

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: 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.

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-
1988; 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

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Emergency Airworthiness Directive 2015-0102-E, dated June 8, 2015 
(referred to after this as the Mandatory Continuing Airworthiness 
Information, or ``the MCAI''), to correct an unsafe condition for all 
Dassault Aviation Model FALCON 2000EX airplanes. The MCAI states:

    A quality review of recently delivered aeroplanes identified a 
manufacturing deficiency of some engine air inlet anti ice piccolo 
tubes.
    This condition, if not detected and corrected, could lead to 
reduced performance of the engine anti-ice protection system, with 
consequent ice accretion and ingestion, possibly resulting in dual 
engine power loss and reduced control of an aeroplane.
    The Falcon 2000EX Aircraft Flight Manual (AFM) contains a 
procedure 4-200-05, ``Operations in Icing Conditions'', addressing 
minimum fan speed rotation (N1) during combined operation of wing 
anti-ice and engine anti-ice systems. However, the AFM does not 
specify minimum N1 values for stand-alone engine anti-ice system 
operation. The subsequent investigation demonstrated that the 
operation of an engine at or above the minimum N1 value applicable 
for combined wing and engine anti-ice operations, provides efficient 
engine anti ice performance during stand-alone engine anti-ice 
operation, for engines equipped with an air inlet affected by the 
manufacturing deficiency.
    For the reasons described above, this [EASA] AD requires 
amendment of the applicable AFM which can be removed (or is not 
applicable) for aeroplanes having both engine air inlet[s] marked 
``NRK'' on the associated data plate.
    This [EASA] AD is considered to be an interim measure and 
further AD action may follow.

You may examine the MCAI on the Internet at http://www.regulations.gov 
by searching for and locating Docket No. FAA-2015-1988.

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 the 
identified unsafe condition could result in engine inlet ice accretion 
with possible ice separation in volumes beyond engine ingestion 
capability. These conditions could lead to engine damage or engine 
shutdown. Therefore, we determined that notice and opportunity for 
public comment before issuing this AD are impracticable and that good 
cause exists for making this amendment effective in fewer than 30 days.

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-2015-1988; Directorate 
Identifier 2015-NM-085-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 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 AD.

[[Page 37151]]

Costs of Compliance

    We estimate that this AD affects 120 airplanes of U.S. registry.
    We also estimate that it will take about 1 work-hour 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 $10,200, or $85 per product.

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 adding the following new airworthiness 
directive (AD):

2015-13-08 Dassault Aviation: Amendment 39-18195. Docket No. FAA-
2015-1988; Directorate Identifier 2015-NM-085-AD.

(a) Effective Date

    This AD becomes effective June 30, 2015.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Dassault Aviation Model FALCON 2000EX 
airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 30, Ice and Rain 
Protection.

(e) Reason

    This AD was prompted by a quality review of recently delivered 
airplanes which identified a manufacturing deficiency of some engine 
air inlet anti-ice piccolo tubes. We are issuing this AD to detect 
and correct reduced performance of the engine anti-ice protection 
system, leading to ice accretion and ingestion into the engines, 
which could result in dual engine power loss and consequent reduced 
controllability of the airplane.

(f) Compliance

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

(g) Airplane Flight Manual (AFM) Revision

    (1) Within 10 flight cycles after the effective date of this AD: 
Revise the Limitations Section of the Dassault Falcon 2000EX AFM to 
include the statement in figure 1 to this paragraph. This may be 
done by inserting a copy of this AD in the AFM. When a statement 
identical to that in figure 1 to this paragraph has been included 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 from 
the AFM.

[[Page 37152]]

[GRAPHIC] [TIFF OMITTED] TR30JN15.001

    (2) Airplanes on which the air engine inlet on both engines has 
a mark ``NRK'' on the associated data plate are not affected by the 
requirements in paragraph (g)(1) of this AD.

    Note 1 to paragraph (g)(2) of this AD:  Engine air inlets which 
have been refurbished and comply with the design standard are marked 
as ``NRK'' on the air inlet data plate.

(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, 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.

(i) Related Information

    Refer to Mandatory Continuing Airworthiness Information (MCAI) 
EASA Emergency Airworthiness Directive 2015-0102-E, dated June 8, 
2015, for related information. You may examine the MCAI on the 
Internet at http://www.regulations.gov by searching for and locating 
Docket No. FAA-2015-1988.

(j) Material Incorporated by Reference

    None.

    Issued in Renton, Washington, on June 19, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-15860 Filed 6-29-15; 8:45 am]
 BILLING CODE 4910-13-P
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