81 FR 75757 - Airworthiness Directives; Dassault Aviation Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 81, Issue 211 (November 1, 2016)

Page Range		75757-75758
FR Document		2016-26325

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.

Federal Register, Volume 81 Issue 211 (Tuesday, November 1, 2016)

[Federal Register Volume 81, Number 211 (Tuesday, November 1, 2016)]
[Proposed Rules]
[Pages 75757-75758]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2016-26325]


=======================================================================
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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: [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.
    (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

Federal Register / Vol. 81, No. 211 / Tuesday, November 1, 2016 / Proposed Rules 75757

§ 326.4 Reports. airplane and consequent injury to will also post a report summarizing each
The security officer for each occupants. substantive verbal contact we receive
institution shall report at least annually DATES: We must receive comments on about this proposed AD.
to the institution’s board of directors on this proposed AD by December 16, Discussion
the implementation, administration, and 2016.
effectiveness of the security program. The European Aviation Safety Agency
ADDRESSES: You may send comments, (EASA), which is the Technical Agent
PART 391—REGULATIONS using the procedures found in 14 CFR for the Member States of the European
TRANSFERRED FROM THE OFFICE OF 11.43 and 11.45, by any of the following Union, has issued EASA Airworthiness
THRIFT SUPERVISION methods: Directive 2016–0096, dated May 19,
• Federal eRulemaking Portal: Go to 2016 (referred to after this as the
Subpart A—Security Procedures http://www.regulations.gov. Follow the Mandatory Continuing Airworthiness
instructions for submitting comments. Information, or ‘‘the MCAI’’), to correct
■ 3. The authority citation for part 391 • Fax: 202–493–2251. an unsafe condition for all Dassault
is revised to read as follows: • Mail: U.S. Department of
Aviation Model FAN JET FALCON
Authority: 12 U.S.C. 1819(Tenth). Transportation, Docket Operations, M–
airplanes; all Model FAN JET FALCON
30, West Building Ground Floor, Room
SERIES C, D, E, F, and G airplanes; and
Subpart A—[Removed and Reserved] W12–140, 1200 New Jersey Avenue SE.,
all Model MYSTERE–FALCON 20–C5,
Washington, DC 20590.
■ 4. Remove and reserve subpart A 20–D5, 20–E5, and 20–F5 airplanes. The
• Hand Delivery: Deliver to Mail
consisting of §§ 391.1 through 391.5. MCAI states:
address above between 9 a.m. and 5
Dated at Washington, DC, this 19th day of p.m., Monday through Friday, except A detailed inspection (DET) of the fuselage
October, 2016. Federal holidays. bulkhead at frame (FR) 33 is established
By order of the Board of Directors. through a subset of inspection/check
Examining the AD Docket maintenance procedure referenced in the
Federal Deposit Insurance Corporation. applicable aircraft maintenance manual
Robert E. Feldman, You may examine the AD docket on
(AMM), task 53–10–0–6 ‘‘MAIN FRAME—
Executive Secretary.
the Internet at http:// INSPECTION/CHECK’’, with periodicity
www.regulations.gov by searching for established in Chapter 5–10, at every C-
[FR Doc. 2016–26062 Filed 10–31–16; 8:45 am]
and locating Docket No. FAA–2016– Check. Failure to accomplish this DET could
BILLING CODE 6714–01–P
9303; or in person at the Docket lead to deterioration of the affected structure.
Management Facility between 9 a.m. This condition, if not detected and
and 5 p.m., Monday through Friday, corrected, could lead to bulkhead failure,
DEPARTMENT OF TRANSPORTATION except Federal holidays. The AD docket possibly resulting in a rapid depressurization
contains this proposed AD, the of the aeroplane and consequent injury to
Federal Aviation Administration regulatory evaluation, any comments occupants.
For the reasons described above, this
received, and other information. The [EASA] AD requires repetitive DET of the
14 CFR Part 39 street address for the Docket Operations bulkhead at FR33 [for discrepancies, such as
[Docket No. FAA–2016–9303; Directorate office (telephone: 800–647–5527) is in buckling, deformations, cracks, loose
Identifier 2016–NM–093–AD] the ADDRESSES section. Comments will countersinks, scratches, dents, and
be available in the AD docket shortly corrosion], and depending on findings, repair
RIN 2120–AA64 after receipt. of the affected structure.
Airworthiness Directives; Dassault FOR FURTHER INFORMATION CONTACT: Tom You may examine the MCAI in the
Aviation Airplanes Rodriguez, Aerospace Engineer, AD docket on the Internet at http://
International Branch, ANM–116, www.regulations.gov by searching for
AGENCY: Federal Aviation Transport Airplane Directorate, FAA, and locating Docket No. FAA–2016–
Administration (FAA), DOT. 1601 Lind Avenue SW., Renton, WA 9303.
ACTION: Notice of proposed rulemaking 98057–3356; telephone: 425–227–1137;
fax: 425–227–1149. FAA’s Determination and Requirements
(NPRM).
of This Proposed AD
SUPPLEMENTARY INFORMATION:
SUMMARY: We propose to adopt a new This product has been approved by
airworthiness directive (AD) for all Comments Invited the aviation authority of another
Dassault Aviation Model FAN JET We invite you to send any written country, and is approved for operation
FALCON airplanes; all Model FAN JET relevant data, views, or arguments about in the United States. Pursuant to our
FALCON SERIES C, D, E, F, and G this proposed AD. Send your comments bilateral agreement with the State of
airplanes; and all Model MYSTERE– to an address listed under the Design Authority, we have been notified
FALCON 20–C5, 20–D5, 20–E5, and 20– ADDRESSES section. Include ‘‘Docket No. of the unsafe condition described in the
F5 airplanes. This proposed AD was FAA–2016–9303; Directorate Identifier MCAI and service information
prompted by a determination that 2016–NM–093–AD’’ at the beginning of referenced above. We are proposing this
inspections for discrepancies of the your comments. We specifically invite AD because we evaluated all pertinent
fuselage bulkhead are necessary. This comments on the overall regulatory, information and determined an unsafe
asabaliauskas on DSK3SPTVN1PROD with PROPOSALS

proposed AD would require repetitive economic, environmental, and energy condition exists and is likely to exist or
inspections for discrepancies of the aspects of this proposed AD. We will develop on other products of these same
fuselage bulkhead, and repair if consider all comments received by the type designs.
necessary. We are proposing this AD to closing date and may amend this
detect and correct discrepancies of the proposed AD based on those comments. Costs of Compliance
fuselage bulkhead; such discrepancies We will post all comments we We estimate that this proposed AD
could result in the deterioration and receive, without change, to http:// affects 133 airplanes of U.S. registry.
failure of the bulkhead, which could www.regulations.gov, including any We also estimate that it would take
result in rapid decompression of the personal information you provide. We about 8 work-hours per product to

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75758 Federal Register / Vol. 81, No. 211 / Tuesday, November 1, 2016 / Proposed Rules

comply with the basic requirements of the FAA proposes to amend 14 CFR part AD: Before further flight, repair using a
this proposed AD. The average labor 39 as follows: method approved by the Manager,
rate is $85 per work-hour. Based on International Branch, ANM–116, Transport
these figures, we estimate the cost of PART 39—AIRWORTHINESS Airplane Directorate, FAA; or the EASA; or
this proposed AD on U.S. operators to DIRECTIVES Dassault Aviation’s EASA DOA. If approved
be $90,440, or $680 per product. by the DOA, the approval must include the
We have received no definitive data ■ 1. The authority citation for part 39 DOA-authorized signature. Repair of an
that would enable us to provide cost continues to read as follows: airplane as required by this paragraph does
estimates for the on-condition actions not constitute terminating action for the
Authority: 49 U.S.C. 106(g), 40113, 44701.
specified in this proposed AD. repetitive actions required by paragraph (g) of
§ 39.13 [Amended] this AD, unless specified otherwise in the
Authority for This Rulemaking repair instructions.
■ 2. The FAA amends § 39.13 by adding
Title 49 of the United States Code the following new airworthiness (i) Other FAA AD Provisions
specifies the FAA’s authority to issue directive (AD):
rules on aviation safety. Subtitle I, The following provisions also apply to this
Dassault Aviation: Docket No. FAA–2016– AD:
section 106, describes the authority of 9303; Directorate Identifier 2016–NM–
the FAA Administrator. ‘‘Subtitle VII: (1) Alternative Methods of Compliance
093–AD.
Aviation Programs,’’ describes in more (AMOCs): The Manager, International
detail the scope of the Agency’s (a) Comments Due Date Branch, ANM–116, Transport Airplane
authority. We must receive comments by December Directorate, FAA, has the authority to
We are issuing this rulemaking under 16, 2016. approve AMOCs for this AD, if requested
the authority described in ‘‘Subtitle VII, using the procedures found in 14 CFR 39.19.
(b) Affected ADs
Part A, Subpart III, Section 44701: In accordance with 14 CFR 39.19, send your
None. request to your principal inspector or local
General requirements.’’ Under that
section, Congress charges the FAA with (c) Applicability Flight Standards District Office, as
promoting safe flight of civil aircraft in This AD applies to the Dassault Aviation appropriate. If sending information directly
air commerce by prescribing regulations airplanes specified in paragraphs (c)(1) and to the International Branch, send it to ATTN:
for practices, methods, and procedures (c)(2) of this AD, certificated in any category, Tom Rodriguez, Aerospace Engineer,
the Administrator finds necessary for all manufacturer serial numbers. International Branch, ANM–116, Transport
safety in air commerce. This regulation (1) Model FAN JET FALCON and FAN JET Airplane Directorate, FAA, 1601 Lind
FALCON SERIES C, D, E, F, and G airplanes. Avenue SW., Renton, WA 98057–3356;
is within the scope of that authority (2) Model MYSTERE–FALCON 20–C5, 20–
because it addresses an unsafe condition telephone: 425–227–1137; fax: 425–227–
D5, 20–E5, and 20–F5 airplanes.
that is likely to exist or develop on 1149. Information may be emailed to: 9-
products identified in this rulemaking (d) Subject ANM-116-AMOC-REQUESTS@faa.gov.
action. Air Transport Association (ATA) of Before using any approved AMOC, notify
America Code 53, Fuselage. your appropriate principal inspector, or
Regulatory Findings lacking a principal inspector, the manager of
(e) Reason
We determined that this proposed AD the local flight standards district office/
This AD was prompted by a determination certificate holding district office.
would not have federalism implications that inspections for discrepancies of the
under Executive Order 13132. This (2) Contacting the Manufacturer: For any
fuselage bulkhead at frame (FR) 33 are
proposed AD would not have a necessary. We are issuing this AD to detect requirement in this AD to obtain corrective
substantial direct effect on the States, on and correct discrepancies of the fuselage actions from a manufacturer, the action must
the relationship between the national bulkhead; such discrepancies could result in be accomplished using a method approved
Government and the States, or on the the deterioration and subsequent failure of by the Manager, International Branch, ANM–
distribution of power and the bulkhead, which could result in rapid 116, Transport Airplane Directorate, FAA; or
responsibilities among the various decompression of the airplane and the EASA; or Dassault Aviation’s EASA
consequent injury to occupants. DOA. If approved by the DOA, the approval
levels of government.
For the reasons discussed above, I (f) Compliance must include the DOA-authorized signature.
certify this proposed regulation: Comply with this AD within the (j) Related Information
1. Is not a ‘‘significant regulatory compliance times specified, unless already
action’’ under Executive Order 12866; done. Refer to Mandatory Continuing
2. Is not a ‘‘significant rule’’ under the Airworthiness Information (MCAI) EASA
(g) Repetitive Inspections Airworthiness Directive 2016–0096, dated
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); Before exceeding 5,000 total flight cycles May 19, 2016, for related information. This
3. Will not affect intrastate aviation in since first flight of the airplane, or within 500 MCAI may be found in the AD docket on the
flight cycles after the effective date of this Internet at http://www.regulations.gov by
Alaska; and AD, whichever occurs later: Do a detailed
4. Will not have a significant searching for and locating Docket No. FAA–
inspection for discrepancies of the fuselage
economic impact, positive or negative, 2016–9303.
bulkhead at FR 33 using a method approved
on a substantial number of small entities by the Manager, International Branch, ANM– Issued in Renton, Washington, on October
under the criteria of the Regulatory 116, Transport Airplane Directorate, FAA; or 26, 2016.
asabaliauskas on DSK3SPTVN1PROD with PROPOSALS

Flexibility Act. the European Aviation Safety Agency
Dionne Palermo,
(EASA); or Dassault Aviation’s EASA Design
List of Subjects in 14 CFR Part 39 Organization Approval (DOA). If approved by Acting Manager, Transport Airplane
Air transportation, Aircraft, Aviation the DOA, the approval must include the Directorate, Aircraft Certification Service.
safety, Incorporation by reference, DOA-authorized signature. Repeat the [FR Doc. 2016–26325 Filed 10–31–16; 8:45 am]
inspection thereafter at intervals not to
Safety. exceed 5,000 flight cycles.
BILLING CODE 4910–13–P

The Proposed Amendment (h) Repair
Accordingly, under the authority If any discrepancy is found during any
delegated to me by the Administrator, inspection required by paragraph (g) of this

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Document Created: 2016-11-01 02:36:23
Document Modified: 2016-11-01 02:36:23

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		Proposed Rules
Action		Notice of proposed rulemaking (NPRM).
Dates		We must receive comments on this proposed AD by December 16, 2016.
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		81 FR 75757
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

81 FR 75757 - Airworthiness Directives; Dassault Aviation Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 81, Issue 211 (November 1, 2016)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration