## 55362 Federal Register / Vol. 81, No. 161 / Friday, August 19, 2016 / Rules and Regulations

specified in table 1 to paragraphs (i) and (m)(3)(ii) of this AD.

(n) 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: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1405; fax 425–227–1149. Information may be emailed to: 9-ANM-116- AMOC-REQUESTS@faa.gov.

(i) 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.

(ii) AMOCs approved previously for AD 2003–25–07 are approved as AMOCs for the corresponding provisions of paragraph (g) of
this AD.

(iii) AMOCs approved previously for AD 2005–13–39 are approved as AMOCs for the corresponding provisions of paragraph (h) of
this AD.

(2) Contacting the Manufacturer: As of the effective date of this AD, 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 Airbus’s EASA DOA. If approved by the DOA, the approval must include the DOA-authorized signature.

(3) Required for Compliance (RC): If any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are
not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator’s maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC.

(o) Related Information

Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2015–0088R1, including Appendix 01, dated June 2, 2015, 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–2016–4226.

(p) Material Incorporated by Reference

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

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(3) The following service information was approved for IBR on September 23, 2016.

(i) Airbus Service Bulletin A320–27–1243, including Appendix 01, dated March 17,

2015.

(ii) Airbus Service Bulletin A320–27–1244, dated March 5, 2015.

(4) The following service information was approved for IBR on August 9, 2005 (70 FR 38580, July 5, 2005).

(i) Airbus Service Bulletin A320–27–1151, including Appendix 01, dated March 9, 2004.

(ii) Airbus Service Bulletin A320–27–1152, including Appendix 01, dated June 4, 2004.

(5) The following service information was approved for IBR on January 22, 2004 (68 FR 70431, December 18, 2003).

(i) Airbus Service Bulletin A320–27–1135, dated June 29, 2001.

(ii) Reserved. (6) For service information identified in this AD, contact Airbus, Airworthiness Office—EIAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@ airbus.com; Internet http://www.airbus.com.

(7) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221.

(8) You may view this service information that is incorporated by reference at the
National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Renton, Washington, on August

8, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2016–19486 Filed 8–18–16; 8:45 am]

**BILLING CODE 4910–13–P**



### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–8463; Directorate Identifier 2014–NM–226–AD; Amendment**  **39–18612; AD 2016–16–14]**

**RIN 2120–AA64**



### Airworthiness Directives; Airbus **Airplanes**

**AGENCY**

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

**ACTION** 

### : Final rule. **SUMMARY** 

### : We are superseding Airworthiness Directive (AD) 2013–20– 11, for all Airbus Model A318, A319, A320, and A321 series airplanes. AD 2013–20–11 required modifying the passenger emergency oxygen container assembly. This new AD expands the affected group of oxygen containers to include those labeled ‘‘DAe Systems.’’ This AD was prompted by a
determination that the unsafe condition also affects oxygen containers labeled ‘‘DAe Systems.’’ We are issuing this AD to prevent a high temperature oxygen generator and mask from falling down and possibly resulting in an ignition source in the passenger compartment, injury to passengers, and reduced availability of supplemental oxygen.

**DATES** 

### : This AD is effective September

23, 2016.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of December 2, 2013 (78 FR 64162, October 28, 2013).

**ADDRESSES** 

### : For Airbus service information identified in this final rule, contact Airbus, Airworthiness Office— EIAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone: +33 5 61 93 36 96; fax: +33 5 61 93 44 51; email: account.airwortheas@airbus.com; Internet http://
www.airbus.com.

You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. It is also
available on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2015–

8463.

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– 8463; 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 address for the Docket Office (telephone 800–647–5527) is 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 20590.

**FOR FURTHER INFORMATION CONTACT**

### : Sanjay Ralhan, Aerospace Engineer, International Branch, ANM–116,


## 55363 Federal Register / Vol. 81, No. 161 / Friday, August 19, 2016 / Rules and Regulations

Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1405;
fax 425–227–1149.

**SUPPLEMENTARY INFORMATION** 

### :

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2013–20–11, Amendment 39–17617 (78 FR 64162, October 28, 2013) (‘‘AD 2013–20–11’’). AD 2013–20–11 applied to all Model A318, A319, A320, and A321 series airplanes. The NPRM published in the Federal Register on January 20, 2016 (81 FR 3061) (‘‘the NPRM’’). The NPRM was prompted by a determination that the unsafe condition also affects oxygen containers labeled ‘‘DAe Systems.’’ The NPRM proposed to continue to require modifying the passenger emergency oxygen container assembly. The NPRM also proposed to expand the affected group of oxygen containers to include those labeled ‘‘DAe Systems.’’ We are issuing this AD to prevent a high temperature oxygen generator and mask from falling down and possibly resulting in an ignition source in the passenger compartment, injury to passengers, and reduced availability of supplemental oxygen.

The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2014–0207, dated September 16, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition.
The MCAI states:

It was determined that oxygen generators, installed on a specific batch of Type 1 (22 min) passenger emergency oxygen container assemblies, may become detached by extreme pulling of the mask tube at the end of oxygen supply. Investigations revealed that such detachment can be caused by the increase in temperature towards the end of the generator operation, which may weaken the plastic housing in the attachment area of the bracket.

This condition, if not corrected, could make the rivets slip through the plastic housing, causing a ‘hot’ oxygen generator and mask to fall down, possibly resulting in injury to passengers.

To address this potential unsafe condition, EASA issued AD 2012–0055 (later revised) [which corresponds to FAA AD 2013–20–11, Amendment 39–17617 (78 FR 64162, October 28, 2013)] to require modification of the affected oxygen container assemblies. That [EASA] AD also prohibited installation of unmodified containers on any aeroplane as replacement parts.

Since that [EASA] AD was issued, it was
found that the affected containers have not only been marked with company name B/E Aerospace, as was specified, but also, for a brief period, with the former company name DAe Systems.

For the reason described above, this [EASA] AD retains the requirements of EASA AD 2012–0055R1, which is superseded, and expands the affected group of containers to
include those that have the name ‘‘DAe Systems’’ on the identification plate.

This [EASA] AD also clearly separates the serial number (s/n) groups of containers into those manufactured by B/E Aerospace and those manufactured by DAe Systems, for which additional compliance time is provided.



### 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–2015–

8463.

Comments

We gave the public the opportunity to participate in developing this AD. We
received no comments on the NPRM 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 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 for correcting the unsafe condition; and

• Do not add any additional burden upon the public than was already proposed in the NPRM.

Costs of Compliance

We estimate that this AD affects 4 airplanes of U.S. registry.

The actions required by AD 2013–20–
11 and retained in this AD take about 2 work-hours per product, at an average labor rate of $85 per work-hour. Based on these figures, the estimated cost of the actions that are required by AD 2013–20–11 is $170 per product.

We also estimate that it would take about 2 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 $680, or $170 per product.

According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we
have included all available costs in our

cost estimate.

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**

■ 

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

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

**§ 39.13 [Amended]**

■ 

### 2. The FAA amends § 39.13 by removing Airworthiness Directive (AD) 2013–20–11, Amendment 39–17617 (78


## 55364 Federal Register / Vol. 81, No. 161 / Friday, August 19, 2016 / Rules and Regulations

FR 64162, October 28, 2013), and adding the following new AD:

2016–16–14 Airbus: Amendment 39–18612; Docket No. FAA–2015–8463; Directorate
Identifier 2014–NM–226–AD.

(a) Effective Date

This AD is effective September 23, 2016.

(b) Affected ADs

This AD replaces AD 2013–20–11, Amendment 39–17617 (78 FR 64162, October 28, 2013) (‘‘AD 2013–20–11’’).

(c) Applicability

This AD applies to the Airbus airplanes, certificated in any category, specified in paragraphs (c)(1) through (c)(4) of this AD, all
manufacturer serial numbers.

(1) Airbus Model A318–111, –112, –121, and –122 airplanes.

(2) Airbus Model A319–111, –112, –113, –114, –115, –131, –132, and –133 airplanes.

(3) Airbus Model A320–211, –212, –214, –231, –232, and –233 airplanes.

(4) Airbus Model A321–111, –112, –131, –211, –212, –213, –231, and –232 airplanes.

(d) Subject

Air Transport Association (ATA) of America Code 35, Oxygen.

(e) Reason

This AD was prompted by a determination that oxygen generators installed on a certain batch of passenger emergency oxygen container assemblies might become detached by extreme pulling of the mask tube at the end of the oxygen supply causing a high temperature oxygen generator and mask to fall down. This AD was also prompted by a
determination that the unsafe condition affects oxygen containers labeled ‘‘DAe Systems.’’ We are issuing this AD to prevent a high temperature oxygen generator and mask from falling down and possibly resulting in an ignition source in the passenger compartment, injury to passengers, and reduced availability of supplemental

oxygen.
(f) Compliance

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

(g) Retained Oxygen Container Assembly Modification, With Service Information Referenced in a New Paragraph

This paragraph restates the requirements of paragraph (g) of AD 2013–20–11 with service information referenced in a new paragraph. Except as specified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD, within 5,000 flight cycles, or 7,500 flight hours, or 24 months, whichever occurs first, after December 2, 2013 (the effective date of AD 2013–20–11): Modify each type 1 (22 minute) passenger emergency oxygen container assembly installed on an airplane, having a part number (P/N) listed in paragraph (g)(1)(i) of this AD and a serial number (S/N) listed in paragraph (g)(1)(ii) of this AD, in accordance with the Accomplishment Instructions of the applicable Airbus service information specified in paragraphs (k)(1) through (k)(7) of this AD. (1) An oxygen container that has a part number listed in paragraph (g)(1)(i) of this
AD and a serial number as listed in paragraph (g)(1)(ii) of this AD, and that has been modified using the instructions of B/E Aerospace Service Bulletin 1XC22–0100–35– 006, is compliant with the modification requirement of paragraph (g) of this AD.

(i) Oxygen container part numbers listed in paragraphs (g)(1)(i)(A) through (g)(1)(i)(D) of this AD, where xxxxx stands for an alphanumerical value.

(A) 13C22Lxxxxx0100. (B) 13C22Rxxxxx0100. (C) 14C22Lxxxxx0100. (D) 14C22Rxxxxx0100. (ii) Oxygen container serial numbers listed in paragraphs (g)(1)(ii)(A) through (g)(1)(ii)(H) of this AD.

(A) ARBC–0182 to ARBC–9999, inclusive. (B) ARBD–0000 to ARBD–9999, inclusive. (C) ARBE–0000 to ARBE–9999, inclusive. (D) BEBF–0000 to BEBF–9999, inclusive. (E) BEBH–0000 to BEBH–9999, inclusive. (F) BEBK–0000 to BEBK–9999, inclusive. (G) BEBL–0000 to BEBL–9999, inclusive. (H) BEBM–0000 to BEBM–0454, inclusive. (2) Airplanes on which Airbus
Modification 150704 has not been embodied in production are excluded from the requirements of paragraph (g) of this AD, unless an oxygen container with a part number listed in paragraph (g)(1)(i) of this AD and a serial number listed in paragraph (g)(1)(ii) of this AD is installed.

(3) Airplanes on which Airbus
Modification 150704 has been embodied in production and that are not listed by model
and manufacturer serial number in the applicable Airbus service information specified in paragraphs (k)(1) through (k)(7) of this AD; are excluded from the requirements of paragraph (g) of this AD, unless an oxygen container with a part number listed in paragraph (g)(1)(i) of this AD and a serial number listed in paragraph (g)(1)(ii) of this AD is installed.

Note 1 to paragraph (g) of this AD: The oxygen container assemblies listed in paragraph (g)(1)(i) of this AD and paragraph (g)(1)(ii) of this AD are B/E Aerospace products with the mark ‘‘B/E AEROSPACE’’ on the identification plate.

(h) Retained Parts Installation Limitation,
With Service Information Referenced in a New Paragraph

This paragraph restates the requirements of paragraph (h) of AD 2013–20–11 with service information referenced in a new paragraph. As of December 2, 2013 (the effective date of AD 2013–20–11), no person may install, on any airplane, an oxygen container with a part number listed in paragraph (g)(1)(i) of this AD, and serial number listed in paragraph (g)(1)(ii) of this AD, unless the oxygen container has been modified according to the applicable Airbus service information specified in paragraphs (k)(1) through (k)(7)
of this AD.

(i) New Requirement of This AD: Modification of Additional Oxygen

Containers

At the applicable times specified in paragraphs (i)(1) and (i)(2) of this AD: Modify each type 1 (22 minute) passenger emergency oxygen container assembly installed on an airplane, having a part number and a serial number listed in paragraph (j) of this AD, in accordance with the Accomplishment Instructions of the applicable Airbus service information specified in paragraphs (k)(1) through (k)(7) of this AD; except as specified in paragraph (l) of this AD.

(1) For units with ‘‘B/E AEROSPACE’’ on the identification plate and having a part
number and a serial number listed in paragraph (j)(1) of this AD: Within 5,000 flight cycles, or 7,500 flight hours, or 24 months, whichever occurs first after the
effective date of this AD.

(2) For units with ‘‘DAe Systems’’ on the identification plate and having a part number and a serial number listed in paragraph (j)(2) of this AD: Within 2,500 flight cycles, or 3,750 flight hours, or 12 months, whichever
occurs first after the effective date of this AD.

(j) New Part Numbers and Serial Numbers for the Parts Affected by Paragraph (i) of
This AD

Affected parts for the actions required by paragraph (i) of this AD are identified in paragraphs (j)(1) and (j)(2) of this AD.

(1) For oxygen containers with ‘‘B/E AEROSPACE’’ on the identification plate: Units having a part number identified in paragraphs (j)(1)(i) through (j)(1)(iv) of this AD, where part number ‘‘xxxxx’’ stands for any alphanumerical value, and a serial number of BEBM–0455 to BEBM–9999,
inclusive.

(i) 13C22Lxxxxx0100. (ii) 13C22Rxxxxx0100. (iii) 14C22Lxxxxx0100. (iv) 14C22Rxxxxx0100. (2) For oxygen containers with ‘‘DAe Systems’’ on the identification plate: Units having a part number identified in paragraphs (j)(1)(i) through (j)(1)(iv) of this AD, where part number ‘‘xxxxx’’ stands for any alphanumerical value, and a serial number identified in paragraphs (j)(2)(i) through (j)(2)(iv) of this AD.

(i) ARBC–0000 to ARBC–9999 inclusive. (ii) ARBD–0000 to ARBD–9999 inclusive. (iii) ARBE–0000 to BEBE–9999 inclusive. (iv) BEBE–0000 to BEBE–9999 inclusive.

(k) Service Information for the Requirements of Paragraphs (g), (h), (i), and (m) of This AD

Accomplish the requirements specified in paragraphs (g), (h), (i), and (m) of this AD in accordance with the Accomplishment Instructions of the applicable Airbus service information identified in paragraphs (k)(1) through (k)(7) of this AD.

(1) Airbus Service Bulletin A320–35–1049, dated June 15, 2011.

(2) Airbus Service Bulletin A320–35–1053, dated June 15, 2011.

(3) Airbus Service Bulletin A320–35–1054, dated June 15, 2011.

(4) Airbus Service Bulletin A320–35–1055, dated June 15, 2011.

(5) Airbus Service Bulletin A320–35–1056, dated June 15, 2011.

(6) Airbus Service Bulletin A320–35–1057, dated June 15, 2011.

(7) Airbus Service Bulletin A320–35–1058, dated June 15, 2011.


## 55365 Federal Register / Vol. 81, No. 161 / Friday, August 19, 2016 / Rules and Regulations

(l) New Exceptions to the Requirements of Paragraph (i) of This AD

(1) An oxygen container that has a part
number and a serial number listed in paragraph (j) of this AD, and that has been modified as specified in B/E Aerospace Service Bulletin 1XC22–0100–35–006, is compliant with the modification requirement of paragraph (i) of this AD.

(2) Airplanes on which Airbus
Modification 150704 has not been embodied in production are excluded from the requirements of paragraph (i) of this AD, unless an oxygen container with a part number and a serial number listed in paragraph (j) of this AD is installed.

(3) Airplanes on which Airbus

Modification 150704 has been embodied in production and that are not listed by model

and manufacturer serial number in the Airbus service information specified in paragraphs (k)(1) through (k)(7) of this AD, as applicable, are excluded from the requirements of paragraph (i) of this AD, unless an oxygen container with a part and a serial number listed in paragraph (j) of this

AD is installed. (4) Airplanes on which the design of the passenger oxygen container is not Design A, as defined in figure 1 to paragraph (l)(4) of this AD, are excluded from the requirements of paragraph (i) of this AD for that passenger oxygen container.

Note 2 to paragraph (l)(4) of this AD: For ‘‘Design A,’’ the placard on the passenger oxygen container test button is as described in ‘‘Picture A’’ in figure 1 to paragraph (l)(4) of this AD. The mask configuration (‘‘ZZ’’ in ‘‘Picture A’’) is a number, and the test button
is as shown in ‘‘Picture B.’’

**BILLING CODE 4910–13–C**

**BILLING CODE 4910–13–P**

(m) New Requirement of This AD: Parts
Installation Limitation

As of the effective date of this AD, no person may install, on any airplane, an oxygen container with a part number and a serial number listed in paragraph (j) of this AD, unless the oxygen container has been
modified in accordance with the Accomplishment Instructions of the applicable Airbus service information specified in paragraphs (k)(1) through (k)(7)
of this AD.

(n) Other FAA AD Provisions

The following provisions also apply to this

AD:


## 55366 Federal Register / Vol. 81, No. 161 / Friday, August 19, 2016 / Rules and Regulations

(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: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1405; fax 425–227–1149. Information may be emailed to: 9-ANM-116- AMOC-REQUESTS@faa.gov.

(i) 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.

(ii) AMOCs approved previously for AD 2013–20–11 are approved as AMOCs for the corresponding provisions of paragraphs (g) and (h) of this AD.

(2) Contacting the Manufacturer: As of the effective date of this AD, 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 Airbus’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.

(o) Related Information

Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2014–0207, dated September 16, 2014, 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–2015–8463.

(p) Material Incorporated by Reference

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

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(3) The following service information was approved for IBR on December 2, 2013 (78 FR 64162, October 28, 2013).

(i) Airbus Service Bulletin A320–35–1049, dated June 15, 2011.

(ii) Airbus Service Bulletin A320–35–1053, dated June 15, 2011.

(iii) Airbus Service Bulletin A320–35– 1054, dated June 15, 2011.

(iv) Airbus Service Bulletin A320–35– 1055, dated June 15, 2011.

(v) Airbus Service Bulletin A320–35–1056, dated June 15, 2011.

(vi) Airbus Service Bulletin A320–35– 1057, dated June 15, 2011.

(vii) Airbus Service Bulletin A320–35– 1058, dated June 15, 2011.

(4) For service information identified in this AD, contact Airbus, Airworthiness Office—EIAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone: +33 5 61 93 36 96; fax: +33 5 61 93 44 51; email: account.airworth-eas@ airbus.com; Internet http://www.airbus.com.

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

(6) You may view this service information that is incorporated by reference at the
National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Renton, Washington, on August

3, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2016–19481 Filed 8–18–16; 8:45 am]

**BILLING CODE 4910–13–P**



### DEPARTMENT OF TRANSPORTATION

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2016–8843; Directorate Identifier 2016–NM–113–AD; Amendment**  **39–18615; AD 2016–17–02]**

**RIN 2120–AA64**



### Airworthiness Directives; Dassault **Aviation Airplanes**

**AGENCY**

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

**ACTION** 

### : Final rule; request for

comments.

**SUMMARY** 

### : We are adopting a new airworthiness directive (AD) for certain
Dassault Aviation Model FALCON 900EX and FALCON 2000EX airplanes. This AD requires revising the airplane flight manual (AFM) to include procedures to follow when an airplane is operating in icing conditions. This AD also provides optional terminating
action for the AFM revision. This ADwas prompted by a design review of inproduction airplanes that identified a deficiency in certain wing anti-ice system ducting. A deficiency in the wing anti-ice system ducting could lead to undetected, reduced performance of the wing anti-ice system, with potential ice accretion and ingestion, possibly resulting in degraded engine power and degraded handling characteristics of the airplane. We are issuing this AD to ensure the flight crew has procedures for operating an airplane in icing
conditions. **DATES** 

### : This AD becomes effective September 6, 2016.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of September 6, 2016.

We must receive comments on this AD by October 3, 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: 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.

For service information identified in this final rule, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201–440–6700; Internet http://www.dassaultfalcon.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425–227–1221. It is also
available on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2016–

8843.

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– 8843; 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.