83_FR_44627 83 FR 44457 - Airworthiness Directives; Airbus SAS Airplanes

83 FR 44457 - Airworthiness Directives; Airbus SAS Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 170 (August 31, 2018)

Page Range44457-44460
FR Document2018-18736

We are superseding Airworthiness Directive (AD) 2015-02-17, which applied to all Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes. AD 2015-02-17 required revising the electrical emergency configuration procedure in the Emergency Procedures section of the airplane flight manual (AFM) to include procedures for deploying the ram air turbine manually to provide sufficient hydraulic power and avoid constant speed motor/generator (CSM/G) shedding. Since we issued AD 2015-02-17, we have determined that replacement or modification of the two flight warning computers (FWCs) is necessary to address the identified unsafe condition. This AD requires the replacement or modifications of the two FWCs. This AD also removes airplanes from the applicability. We are issuing this AD to address the unsafe condition on these products.

Federal Register, Volume 83 Issue 170 (Friday, August 31, 2018) 
[Federal Register Volume 83, Number 170 (Friday, August 31, 2018)]
[Rules and Regulations]
[Pages 44457-44460]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-18736]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0169; Product Identifier 2017-NM-095-AD; Amendment 
39-19372; AD 2018-17-18]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are superseding Airworthiness Directive (AD) 2015-02-17, 
which applied to all Airbus Model A330-200, A330-200 Freighter, and 
A330-300 series airplanes. AD 2015-02-17 required revising the 
electrical emergency configuration procedure in the Emergency 
Procedures section of the airplane flight manual (AFM) to include 
procedures for deploying the ram air turbine manually to provide 
sufficient hydraulic power and avoid constant speed motor/generator 
(CSM/G) shedding. Since we issued AD 2015-02-17, we have determined 
that replacement or modification of the two flight warning computers 
(FWCs) is necessary to address the identified unsafe condition. This AD 
requires the replacement or modifications of the two FWCs. This AD also 
removes airplanes from the applicability. We are issuing this AD to 
address the unsafe condition on these products.

DATES: This AD is effective October 5, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 5, 
2018.
    The Director of the Federal Register approved the incorporation by 
reference of certain other publications listed in this AD as of 
February 13, 2015 (80 FR 4762, January 29, 2015).

ADDRESSES: For service information identified in this final rule, 
contact Airbus SAS, Airworthiness Office--EAW, Rond-Point Emile 
Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 
96; fax +33 5 61 93 44 51; email [email protected]; 
internet http://www.airbus.com. You may view this referenced service 
information at the FAA, Transport Standards Branch, 2200 South 216th 
St., Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195. It is also available on the 
internet at http://www.regulations.gov by searching for and locating 
Docket No. FAA-2018-0169.

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-2018-
0169; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations (phone: 800-647-
5527) is Docket Operations, 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: Vladimir Ulyanov, Aerospace Engineer, 
International Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3229.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to supersede AD 2015-02-17,

[[Page 44458]]

Amendment 39-18084 (80 FR 4762, January 29, 2015) (``AD 2015-02-17''). 
AD 2015-02-17 applied to all Airbus Model A330-200, A330-200 Freighter, 
and A330-300 series airplanes. The NPRM published in the Federal 
Register on April 16, 2018 (83 FR 16248). The NPRM was prompted by a 
determination that replacement or modification of the two FWCs is 
necessary to address the identified unsafe condition. The NPRM proposed 
to require the replacement or modification of the two FWCs. The NPRM 
also proposed to remove airplanes from the applicability. We are 
issuing this AD to address the identified unsafe condition.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA AD 
2017-0105R1, dated July 17, 2017 (referred to after this as the 
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to 
correct an unsafe condition for all Airbus SAS Model A330-200, A330-200 
Freighter, and A330-300 series airplanes. The MCAI states:

    The Constant Speed Motor/Generator (CSM/G), as installed on 
Airbus A330 aeroplanes, is qualified for an overload condition of 
9.5 kVA [kilovolt-ampere] for 30 minutes. This duration is 
sufficient to perform safe landing and go-around. However, 
electrical load analysis revealed that the hydraulic power might not 
be sufficient to supply the CSM/G during slat/flap extension, when 
only one engine is running.
    This condition, if not corrected, and in conjunction with the 
loss of main system, could lead to a scenario where the crew is not 
clearly warned that the electrical system has switched on the 
battery and thus has a limited duration to support a safe landing.
    To initially address this potential unsafe condition, Airbus 
issued an Aircraft Flight Manual (AFM) Temporary Revision (TR) to 
amend the electrical emergency configuration ``ELEC EMER CONFIG'' 
procedure to require the pilot to deploy the ram air turbine 
manually before setting the Landing Recovery to ``ON'' position, 
which provides sufficient hydraulic power and avoids CSM/G shedding 
under worst-case operational conditions. Consequently, EASA issued 
AD 2014-0273 to require amendment of the AFM by incorporating the 
applicable Airbus TR.
    After finding that [EASA] AD 2014-0273 contained some incorrect 
and incomplete information, EASA issued AD 2014-0281 [which 
corresponds to FAA AD 2015-02-17], retaining the requirements of 
EASA AD 2014-0273, which was superseded, but correcting the 
information related to premod/pre Service Bulletin (SB) or post-mod/
post SB aeroplane configurations.
    Since EASA AD 2014-0281 was issued, in order to improve the 
``ELEC EMER CONFIG'' procedure, Airbus developed modifications to 
install improved FWCs, which is embodied in production through 
Airbus modification (mod) 205228, and to be embodied in service with 
Airbus SB A330-31-3232 * * *.
    For the reasons described above, this [EASA] AD retains the 
requirements of EASA AD 2014-0281, which is superseded, and requires 
installation of a software standard upgrade [or replacement] of the 
two FWCs and removal of the applicable AFM TR once the aeroplane is 
modified.
    Since EASA AD 2017-0105 was issued, it was identified that there 
was no need to require removal of applicable AFM TR, nor 
incorporation of a later AFM revision, as the contents are 
identical. This revised [EASA] AD deletes the requirement of 
paragraph (3) [of EASA AD 2017-0105].
* * * * *
    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-2018-
0169.

Comments

    We gave the public the opportunity to participate in developing 
this final rule. The following presents the comments received on the 
NPRM and the FAA's response to each comment. The Air Line Pilots 
Association, International (ALPA), indicated its support for the NPRM.

Request for Additional Credit

    Delta Air Lines requested that paragraph (l) of the proposed AD, 
``Credit for Previous Actions,'' include Airbus Service Bulletin A330-
31-3232, Revision 01, dated February 14, 2017, as well as Airbus 
Service Bulletin A330-31-3232, dated May 4, 2016.
    We disagree this change is necessary. Paragraph (f) of this AD 
requires compliance with this AD unless already done. Paragraph (j) of 
this AD mandates actions in accordance with Airbus Service Bulletin 
A330-31-3232, Revision 01, dated February 14, 2017. Therefore, as 
specified in paragraph (f) of this AD, having previously accomplished 
the actions specified in Airbus Service Bulletin A330-31-3232, Revision 
01, dated February 14, 2017, means compliance with paragraph (j) of 
this AD has already been established. In paragraph (l) of this AD, we 
give credit to operators that have previously accomplished an earlier 
revision of the required service information identified in paragraph 
(j) of this AD; therefore, as specified in paragraph (l) of this AD, 
having accomplished Airbus Service Bulletin A330-31-3232, dated May 4, 
2016, prior to the effective date of this AD means compliance with 
paragraph (j) of this AD has already been established. We have not 
changed this AD in this regard.

Conclusion

    We reviewed the relevant data, considered the comments received, 
and determined that air safety and the public interest require adopting 
this final rule 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 addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Airbus SAS has issued A330/A340 Airplane Flight Manual (AFM) 
Temporary Revision (TR) TR427, UPDATE OF ELEC--EMER CONFIG PROCEDURE, 
Issue 1.0, dated November 7, 2014; and A330/A340 AFM TR TR428, UPDATE 
OF ELEC--EMER CONFIG PROCEDURE, Issue 1.0, dated November 7, 2014. This 
service information describes updated electrical emergency 
configuration procedures in the AFM. This service information is 
distinct because it applies to airplanes in different configurations.
    Airbus SAS has issued Service Bulletin A330-31-3232, Revision 01, 
including Appendix 01, dated February 14, 2017. This service 
information describes procedures for replacement or modification of the 
FWCs.
    This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    We estimate that this AD affects 105 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

[[Page 44459]]



                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
4 work-hour x $85 per hour = $340............................              $0             $340          $35,700
----------------------------------------------------------------------------------------------------------------

    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 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.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes and 
associated appliances to the Director of the System Oversight Division.

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 removing Airworthiness Directive (AD) 
2015-02-2017, Amendment 39-18084 (80 FR 4762, January 29, 2015), and 
adding the following new AD:

2018-17-18 Airbus SAS: Amendment 39-19372; Docket No. FAA-2018-0169; 
Product Identifier 2017-NM-095-AD.

(a) Effective Date

    This AD is effective October 5, 2018.

(b) Affected ADs

    This AD replaces AD 2015-02-17, Amendment 39-18084 (80 FR 4762, 
January 29, 2015) (``AD 2015-02-17'').

(c) Applicability

    This AD applies to the airplanes identified in paragraphs 
(c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, 
all manufacturer serial numbers, except those airplanes with Airbus 
modification 205228 embodied in production.
    (1) Airbus SAS Model A330-201, -202, -203, -223, and -243 
airplanes.
    (2) Airbus SAS Model A330-223F and -243F airplanes.
    (3) Airbus SAS Model A330-301, -302, -303, -321, -322, -323, -
341, -342, and -343 airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 24, Electrical 
power.

(e) Reason

    This AD was prompted by an electrical load analysis that 
revealed that hydraulic power might not be sufficient to supply the 
constant speed motor/generator (CSM/G) during slat/flap extension 
when only one engine is running and a determination that replacement 
or modification of the two flight warning computers (FWCs) is 
necessary to address the identified unsafe condition. We are issuing 
this AD to prevent such a condition which, in conjunction with the 
loss of the main electrical system, could lead to the scenario where 
the flight crew is not clearly warned that the electrical system has 
switched on the battery and thus has a limited duration that would 
allow a safe landing.

(f) Compliance

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

(g) Retained Airplane Flight Manual (AFM) Revision, With a New 
Exception

    This paragraph restates the requirements of paragraph (g) of AD 
2015-02-17, with a new exception. Except for airplanes identified in 
paragraph (h) of this AD: Within 15 days after February 13, 2015 
(the effective date of AD 2015-02-17), revise the Emergency 
Procedures section of the Airbus A330/A340 AFM to include the 
information in the applicable Airbus temporary revision (TR) 
specified in paragraph (g)(1) or (g)(2) of this AD. This may be done 
by inserting a copy of the applicable TR specified in paragraph 
(g)(1) or (g)(2) of this AD into the AFM. Operate the airplane 
according to the procedures in the applicable TR. When the 
information in the applicable TR has been included in the general 
revisions of the AFM, the general revisions may be inserted into the 
AFM, provided the relevant information in the general revision is 
identical to that in the TR, and the TR may be removed.
    (1) For airplanes in Airbus pre-modification 47930 configuration 
and pre-Airbus Service Bulletin A330-28-3067 configuration: Airbus 
A330/A340 AFM TR TR427, UPDATE OF ELEC--EMER CONFIG PROCEDURE, Issue 
1.0, dated November 7, 2014.
    (2) For airplanes in Airbus post-modification 47930 
configuration or post-Airbus Service Bulletin A330-28-3067 
configuration: Airbus A330/A340 AFM TR TR428, UPDATE OF ELEC--EMER 
CONFIG PROCEDURE, Issue 1.0, dated November 7, 2014.

[[Page 44460]]

(h) New Airplanes Not Affected by the Retained AFM Revision

    Airplanes operated with an AFM that incorporates the information 
in Airbus EMERGENCY PROCEDURES/24-ELECTRICAL POWER/ELEC--EMER CONFIG 
Documentary Unit (DU) 00005218.0001001 (for airplanes in Airbus pre-
modification 47930 configuration and pre-Airbus Service Bulletin 
A330-28-3067 configuration), or DU 00005218.0002001 (for airplanes 
in an Airbus post-modification 47930 configuration or post-Airbus 
Service Bulletin A330-28-3067 configuration), as applicable, are 
compliant with the requirements of paragraph (g) of this AD, 
provided that the applicable DU is not removed from the AFM.

(i) New Definitions

    (1) For the purposes of this AD, an affected FWC is an FWC 
standard lower than T7-0. An FWC that is not affected is an FWC 
standard T7-0 having part number (P/N) LA2E20202T70000, or higher 
standard.
    (2) For the purposes of this AD: Group 1 airplanes are those 
equipped with an affected FWC (as defined in paragraph (i)(1) of 
this AD) as of the effective date of this AD. Group 2 airplanes are 
those equipped with FWCs that are not affected (as defined in 
paragraph (i)(1) of this AD) as of the effective date of this AD.

(j) New Requirement of This AD: FWC Replacement or Modification

    For Group 1 airplanes: Within 24 months after the effective date 
of this AD: Replace or modify an affected FWC with an FWC that is 
not affected, in accordance with the Accomplishment Instructions of 
Airbus Service Bulletin A330-31-3232, Revision 01, including 
Appendix 01, dated February 14, 2017.

(k) Parts Installation Prohibition

    (1) For Group 1 airplanes: After accomplishing the actions 
required by paragraph (j) of this AD, no person may install an 
affected FWC on the modified airplane.
    (2) For Group 2 airplanes: As of the effective date of this AD, 
no person may install an affected FWC on any airplane.

(l) Credit for Previous Actions

    This paragraph provides credit for actions required by paragraph 
(j) of this AD, if those actions were performed before the effective 
date of this AD using Airbus Service Bulletin A330-31-3232, dated 
May 4, 2016.

(m) Other FAA AD Provisions

    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards Branch, 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 Section, send it to the attention of 
the person identified in paragraph (n)(2) of this AD. Information 
may be emailed to: [email protected].
    (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 2015-02-17 are approved as 
AMOCs for the corresponding provisions 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 Section, Transport Standards 
Branch, FAA; or the European Aviation Safety Agency (EASA); or 
Airbus SAS's EASA Design Organization Approval (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.

(n) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2017-0105R1, dated July 17, 2017, 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-2018-0169.
    (2) For more information about this AD, contact Vladimir 
Ulyanov, Aerospace Engineer, International Section, Transport 
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; 
telephone and fax 206-231-3229.
    (3) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (o)(5) and (o)(6) of this AD.

(o) 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 
October 5, 2018.
    (i) Airbus Service Bulletin A330-31-3232, Revision 01, including 
Appendix 01, dated February 14, 2017.
    (ii) Reserved.
    (4) The following service information was approved for IBR on of 
February 13, 2015 (80 FR 4762, January 29, 2015).
    (i) Airbus A330/A340 Airplane Flight Manual (AFM) Temporary 
Revision TR427, UPDATE OF ELEC--EMER CONFIG PROCEDURE, Issue 1.0, 
dated November 7, 2014.
    (ii) Airbus A330/A340 AFM Temporary Revision TR428, UPDATE OF 
ELEC--EMER CONFIG PROCEDURE, Issue 1.0, dated November 7, 2014.
    (5) For service information identified in this AD, contact 
Airbus SAS, Airworthiness Office--EAW, Rond-Point Emile Dewoitine 
No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax 
+33 5 61 93 44 51; email [email protected]; internet 
http://www.airbus.com.
    (6) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (7) 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/ibr-locations.html.

    Issued in Des Moines, Washington, on August 17, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-18736 Filed 8-30-18; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 83, No. 170 / Friday, August 31, 2018 / Rules and Regulations 44457 Conclusion (2) Sideways 6g flight warning computers (FWCs) is This action affects only certain novel (3) Downward 6g necessary to address the identified or unusual design features on the unsafe condition. This AD requires the d. Seats and Seatbelts balloon models specified in these replacement or modifications of the two special conditions. It is not a rule of (1) Each seat and its supporting FWCs. This AD also removes airplanes general applicability and it affects only structure must be designed for an from the applicability. We are issuing the applicant who applied to the FAA occupant mass in accordance paragraph this AD to address the unsafe condition for approval of these features on the (a) of these special conditions and for on these products. airplane. These special conditions are the maximum load factors DATES: This AD is effective October 5, identical in intent to the EASA special corresponding to the specified flight and 2018. conditions, although the formatting has ground load conditions, including the The Director of the Federal Register been altered to meet these special emergency landing conditions approved the incorporation by reference condition requirements. prescribed in paragraph (c) of these of a certain publication listed in this AD special conditions. as of October 5, 2018. List of Subjects in 14 CFR Part 31 (2) Each seat or berth shall be fitted The Director of the Federal Register Aircraft, Aviation safety. with an individual approved seat belt or approved the incorporation by reference The authority citation for these harness. of certain other publications listed in special conditions is as follows: (3) Seat belts installed on the balloon this AD as of February 13, 2015 (80 FR must not fail under flight or ground load 4762, January 29, 2015). Authority: 49 U.S.C. 106(g), 40113, 44701– 44702, 44704. conditions or emergency landing ADDRESSES: For service information conditions in accordance with identified in this final rule, contact The Special Conditions paragraph (c) of these special Airbus SAS, Airworthiness Office— ■ Accordingly, pursuant to the authority conditions, taking into account the EAW, Rond-Point Emile Dewoitine No: delegated to me by the Administrator, geometrical arrangement of the belt 2, 31700 Blagnac Cedex, France; the following special conditions are attachment and the seat. telephone +33 5 61 93 36 96; fax +33 5 issued as part of the type certification Issued in Kansas City, Missouri, on August 61 93 44 51; email account.airworth- basis for Ultramagic S.A. Model M–56, 23, 2018. eas@airbus.com; internet http:// M–56C, M–65, M–65C, M–77, M–77C, Pat Mullen, www.airbus.com. You may view this M–90, M–105, M–120, M–130, M–145, Manager, Small Airplane Standards Branch, referenced service information at the M–160, N–180, N–210, N–250, N–300, Aircraft Certification Service. FAA, Transport Standards Branch, 2200 N–355, N–425, S–70, S–90, S–105, S– [FR Doc. 2018–18885 Filed 8–30–18; 8:45 am] South 216th St., Des Moines, WA. For 130, S–160, T–150, T–180, T–210, V–56, BILLING CODE 4910–13–P information on the availability of this V–65, V–77, V–90, and V–105 balloons material at the FAA, call 206–231–3195. with a basket Model no. CV–08. It is also available on the internet at DEPARTMENT OF TRANSPORTATION http://www.regulations.gov by searching 1. Hot Air Balloon Crashworthiness for and locating Docket No. FAA–2018– Requirements for Seat Installations and Federal Aviation Administration 0169. Restraints for Seated and Restrained Occupants 14 CFR Part 39 Examining the AD Docket a. Occupant Mass You may examine the AD docket on [Docket No. FAA–2018–0169; Product For calculation purposes, it should be Identifier 2017–NM–095–AD; Amendment the internet at http:// assumed the mass of an occupant is at 39–19372; AD 2018–17–18] www.regulations.gov by searching for least 86 kilograms (190 pounds). and locating Docket No. FAA–2018– RIN 2120–AA64 0169; or in person at Docket Operations b. Seats, Safety Belts, and Harnesses between 9 a.m. and 5 p.m., Monday Factor of Safety Airworthiness Directives; Airbus SAS through Friday, except Federal holidays. Airplanes The AD docket contains this final rule, For each seat, safety belt, and harness, its attachment to the structure must be AGENCY: Federal Aviation the regulatory evaluation, any shown, by analysis, tests, or both, to be Administration (FAA), Department of comments received, and other able to withstand the inertia forces Transportation (DOT). information. The address for Docket prescribed in paragraph (c) of these ACTION: Final rule. Operations (phone: 800–647–5527) is special conditions multiplied by a Docket Operations, U.S. Department of fitting factor of 1.33. SUMMARY: We are superseding Transportation, Docket Operations, M– Airworthiness Directive (AD) 2015–02– 30, West Building Ground Floor, Room c. Emergency Landing Conditions— 17, which applied to all Airbus Model W12–140, 1200 New Jersey Avenue SE, General A330–200, A330–200 Freighter, and Washington, DC 20590. The balloon—although it may be A330–300 series airplanes. AD 2015– FOR FURTHER INFORMATION CONTACT: damaged under emergency landing 02–17 required revising the electrical Vladimir Ulyanov, Aerospace Engineer, conditions—must be designed to give emergency configuration procedure in International Section, Transport each occupant every reasonable chance the Emergency Procedures section of the Standards Branch, FAA, 2200 South of avoiding serious injury in a crash airplane flight manual (AFM) to include 216th St., Des Moines, WA 98198; landing—when seat belts provided for procedures for deploying the ram air telephone and fax 206–231–3229. daltland on DSKBBV9HB2PROD with RULES in the design are properly used—and turbine manually to provide sufficient SUPPLEMENTARY INFORMATION: the occupant is subject to the following hydraulic power and avoid constant ultimate inertia forces acting relative to speed motor/generator (CSM/G) Discussion the surrounding structure as well as shedding. Since we issued AD 2015–02– We issued a notice of proposed independently of each other. 17, we have determined that rulemaking (NPRM) to amend 14 CFR (1) Forward 6g replacement or modification of the two part 39 to supersede AD 2015–02–17, VerDate Sep<11>2014 16:04 Aug 30, 2018 Jkt 244001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\31AUR1.SGM 31AUR1

44458 Federal Register / Vol. 83, No. 170 / Friday, August 31, 2018 / Rules and Regulations Amendment 39–18084 (80 FR 4762, correcting the information related to premod/ to operators that have previously January 29, 2015) (‘‘AD 2015–02–17’’). pre Service Bulletin (SB) or post-mod/post accomplished an earlier revision of the AD 2015–02–17 applied to all Airbus SB aeroplane configurations. required service information identified Since EASA AD 2014–0281 was issued, in Model A330–200, A330–200 Freighter, order to improve the ‘‘ELEC EMER CONFIG’’ in paragraph (j) of this AD; therefore, as and A330–300 series airplanes. The procedure, Airbus developed modifications specified in paragraph (l) of this AD, NPRM published in the Federal to install improved FWCs, which is having accomplished Airbus Service Register on April 16, 2018 (83 FR embodied in production through Airbus Bulletin A330–31–3232, dated May 4, 16248). The NPRM was prompted by a modification (mod) 205228, and to be 2016, prior to the effective date of this determination that replacement or embodied in service with Airbus SB A330– AD means compliance with paragraph modification of the two FWCs is 31–3232 * * *. (j) of this AD has already been For the reasons described above, this necessary to address the identified established. We have not changed this [EASA] AD retains the requirements of EASA unsafe condition. The NPRM proposed AD 2014–0281, which is superseded, and AD in this regard. to require the replacement or requires installation of a software standard Conclusion modification of the two FWCs. The upgrade [or replacement] of the two FWCs NPRM also proposed to remove and removal of the applicable AFM TR once We reviewed the relevant data, airplanes from the applicability. We are the aeroplane is modified. considered the comments received, and issuing this AD to address the identified Since EASA AD 2017–0105 was issued, it determined that air safety and the unsafe condition. was identified that there was no need to public interest require adopting this require removal of applicable AFM TR, nor The European Aviation Safety Agency final rule as proposed, except for minor incorporation of a later AFM revision, as the (EASA), which is the Technical Agent contents are identical. This revised [EASA] editorial changes. We have determined for the Member States of the European AD deletes the requirement of paragraph (3) that these minor changes: Union, has issued EASA AD 2017– [of EASA AD 2017–0105]. • Are consistent with the intent that 0105R1, dated July 17, 2017 (referred to * * * * * was proposed in the NPRM for after this as the Mandatory Continuing You may examine the MCAI in the addressing the unsafe condition; and Airworthiness Information, or ‘‘the AD docket on the internet at http:// • Do not add any additional burden MCAI’’), to correct an unsafe condition www.regulations.gov by searching for upon the public than was already for all Airbus SAS Model A330–200, and locating Docket No. FAA–2018– proposed in the NPRM. A330–200 Freighter, and A330–300 0169. series airplanes. The MCAI states: Related Service Information Under 1 Comments CFR Part 51 The Constant Speed Motor/Generator (CSM/G), as installed on Airbus A330 We gave the public the opportunity to Airbus SAS has issued A330/A340 aeroplanes, is qualified for an overload participate in developing this final rule. Airplane Flight Manual (AFM) condition of 9.5 kVA [kilovolt-ampere] for 30 The following presents the comments Temporary Revision (TR) TR427, minutes. This duration is sufficient to received on the NPRM and the FAA’s perform safe landing and go-around. UPDATE OF ELEC—EMER CONFIG response to each comment. The Air Line PROCEDURE, Issue 1.0, dated However, electrical load analysis revealed Pilots Association, International that the hydraulic power might not be November 7, 2014; and A330/A340 sufficient to supply the CSM/G during slat/ (ALPA), indicated its support for the AFM TR TR428, UPDATE OF ELEC— flap extension, when only one engine is NPRM. EMER CONFIG PROCEDURE, Issue 1.0, running. Request for Additional Credit dated November 7, 2014. This service This condition, if not corrected, and in information describes updated electrical conjunction with the loss of main system, Delta Air Lines requested that paragraph (l) of the proposed AD, emergency configuration procedures in could lead to a scenario where the crew is not clearly warned that the electrical system ‘‘Credit for Previous Actions,’’ include the AFM. This service information is has switched on the battery and thus has a Airbus Service Bulletin A330–31–3232, distinct because it applies to airplanes limited duration to support a safe landing. Revision 01, dated February 14, 2017, as in different configurations. To initially address this potential unsafe well as Airbus Service Bulletin A330– Airbus SAS has issued Service condition, Airbus issued an Aircraft Flight 31–3232, dated May 4, 2016. Bulletin A330–31–3232, Revision 01, Manual (AFM) Temporary Revision (TR) to including Appendix 01, dated February We disagree this change is necessary. amend the electrical emergency configuration 14, 2017. This service information ‘‘ELEC EMER CONFIG’’ procedure to require Paragraph (f) of this AD requires compliance with this AD unless already describes procedures for replacement or the pilot to deploy the ram air turbine manually before setting the Landing done. Paragraph (j) of this AD mandates modification of the FWCs. Recovery to ‘‘ON’’ position, which provides actions in accordance with Airbus This service information is reasonably sufficient hydraulic power and avoids CSM/ Service Bulletin A330–31–3232, available because the interested parties G shedding under worst-case operational Revision 01, dated February 14, 2017. have access to it through their normal conditions. Consequently, EASA issued AD Therefore, as specified in paragraph (f) course of business or by the means 2014–0273 to require amendment of the AFM of this AD, having previously identified in the ADDRESSES section. by incorporating the applicable Airbus TR. accomplished the actions specified in Costs of Compliance After finding that [EASA] AD 2014–0273 contained some incorrect and incomplete Airbus Service Bulletin A330–31–3232, information, EASA issued AD 2014–0281 Revision 01, dated February 14, 2017, We estimate that this AD affects 105 [which corresponds to FAA AD 2015–02–17], means compliance with paragraph (j) of airplanes of U.S. registry. retaining the requirements of EASA AD this AD has already been established. In We estimate the following costs to 2014–0273, which was superseded, but paragraph (l) of this AD, we give credit comply with this AD: daltland on DSKBBV9HB2PROD with RULES VerDate Sep<11>2014 16:04 Aug 30, 2018 Jkt 244001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\31AUR1.SGM 31AUR1

Federal Register / Vol. 83, No. 170 / Friday, August 31, 2018 / Rules and Regulations 44459 ESTIMATED COSTS Cost per Cost on U.S. Labor cost Parts cost product operators 4 work-hour × $85 per hour = $340 ............................................................................................ $0 $340 $35,700 According to the manufacturer, some 1. Is not a ‘‘significant regulatory (d) Subject of the costs of this AD may be covered action’’ under Executive Order 12866; Air Transport Association (ATA) of under warranty, thereby reducing the 2. Is not a ‘‘significant rule’’ under the America Code 24, Electrical power. cost impact on affected individuals. We DOT Regulatory Policies and Procedures (e) Reason do not control warranty coverage for (44 FR 11034, February 26, 1979); affected individuals. As a result, we 3. Will not affect intrastate aviation in This AD was prompted by an electrical have included all costs in our cost Alaska; and load analysis that revealed that hydraulic estimate. power might not be sufficient to supply the 4. Will not have a significant constant speed motor/generator (CSM/G) Authority for This Rulemaking economic impact, positive or negative, during slat/flap extension when only one on a substantial number of small entities engine is running and a determination that Title 49 of the United States Code under the criteria of the Regulatory replacement or modification of the two flight specifies the FAA’s authority to issue Flexibility Act. warning computers (FWCs) is necessary to rules on aviation safety. Subtitle I, address the identified unsafe condition. We section 106, describes the authority of List of Subjects in 14 CFR Part 39 are issuing this AD to prevent such a the FAA Administrator. Subtitle VII: Air transportation, Aircraft, Aviation condition which, in conjunction with the Aviation Programs, describes in more safety, Incorporation by reference, loss of the main electrical system, could lead detail the scope of the Agency’s Safety. to the scenario where the flight crew is not authority. clearly warned that the electrical system has Adoption of the Amendment switched on the battery and thus has a We are issuing this rulemaking under the authority described in Subtitle VII, Accordingly, under the authority limited duration that would allow a safe delegated to me by the Administrator, landing. Part A, Subpart III, Section 44701: ‘‘General requirements.’’ Under that the FAA amends 14 CFR part 39 as (f) Compliance section, Congress charges the FAA with follows: Comply with this AD within the promoting safe flight of civil aircraft in compliance times specified, unless already air commerce by prescribing regulations PART 39—AIRWORTHINESS done. for practices, methods, and procedures DIRECTIVES (g) Retained Airplane Flight Manual (AFM) the Administrator finds necessary for ■ 1. The authority citation for part 39 Revision, With a New Exception safety in air commerce. This regulation continues to read as follows: is within the scope of that authority This paragraph restates the requirements of Authority: 49 U.S.C. 106(g), 40113, 44701. paragraph (g) of AD 2015–02–17, with a new because it addresses an unsafe condition exception. Except for airplanes identified in that is likely to exist or develop on § 39.13 [Amended] paragraph (h) of this AD: Within 15 days after products identified in this rulemaking February 13, 2015 (the effective date of AD action. ■ 2. The FAA amends § 39.13 by 2015–02–17), revise the Emergency This AD is issued in accordance with removing Airworthiness Directive (AD) Procedures section of the Airbus A330/A340 authority delegated by the Executive 2015–02–2017, Amendment 39–18084 AFM to include the information in the Director, Aircraft Certification Service, (80 FR 4762, January 29, 2015), and applicable Airbus temporary revision (TR) as authorized by FAA Order 8000.51C. adding the following new AD: specified in paragraph (g)(1) or (g)(2) of this In accordance with that order, issuance 2018–17–18 Airbus SAS: Amendment 39– AD. This may be done by inserting a copy of of ADs is normally a function of the 19372; Docket No. FAA–2018–0169; the applicable TR specified in paragraph Compliance and Airworthiness Product Identifier 2017–NM–095–AD. (g)(1) or (g)(2) of this AD into the AFM. Division, but during this transition Operate the airplane according to the (a) Effective Date procedures in the applicable TR. When the period, the Executive Director has This AD is effective October 5, 2018. information in the applicable TR has been delegated the authority to issue ADs included in the general revisions of the AFM, applicable to transport category (b) Affected ADs the general revisions may be inserted into the airplanes and associated appliances to This AD replaces AD 2015–02–17, AFM, provided the relevant information in the Director of the System Oversight Amendment 39–18084 (80 FR 4762, January the general revision is identical to that in the Division. 29, 2015) (‘‘AD 2015–02–17’’). TR, and the TR may be removed. (c) Applicability (1) For airplanes in Airbus pre- Regulatory Findings This AD applies to the airplanes identified modification 47930 configuration and pre- We determined that this AD will not in paragraphs (c)(1), (c)(2), and (c)(3) of this Airbus Service Bulletin A330–28–3067 have federalism implications under AD, certificated in any category, all configuration: Airbus A330/A340 AFM TR Executive Order 13132. This AD will manufacturer serial numbers, except those TR427, UPDATE OF ELEC—EMER CONFIG not have a substantial direct effect on airplanes with Airbus modification 205228 PROCEDURE, Issue 1.0, dated November 7, the States, on the relationship between embodied in production. 2014. daltland on DSKBBV9HB2PROD with RULES (1) Airbus SAS Model A330–201, –202, (2) For airplanes in Airbus post- the national government and the States, –203, –223, and –243 airplanes. modification 47930 configuration or post- or on the distribution of power and Airbus Service Bulletin A330–28–3067 (2) Airbus SAS Model A330–223F and responsibilities among the various –243F airplanes. configuration: Airbus A330/A340 AFM TR levels of government. (3) Airbus SAS Model A330–301, –302, TR428, UPDATE OF ELEC—EMER CONFIG For the reasons discussed above, I –303, –321, –322, –323, –341, –342, and –343 PROCEDURE, Issue 1.0, dated November 7, certify that this AD: airplanes. 2014. 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44460 Federal Register / Vol. 83, No. 170 / Friday, August 31, 2018 / Rules and Regulations (h) New Airplanes Not Affected by the (i) Before using any approved AMOC, PROCEDURE, Issue 1.0, dated November 7, Retained AFM Revision notify your appropriate principal inspector, 2014. Airplanes operated with an AFM that or lacking a principal inspector, the manager (ii) Airbus A330/A340 AFM Temporary incorporates the information in Airbus of the local flight standards district office/ Revision TR428, UPDATE OF ELEC—EMER EMERGENCY PROCEDURES/24– certificate holding district office. CONFIG PROCEDURE, Issue 1.0, dated ELECTRICAL POWER/ELEC—EMER (ii) AMOCs approved previously for AD November 7, 2014. CONFIG Documentary Unit (DU) 2015–02–17 are approved as AMOCs for the (5) For service information identified in 00005218.0001001 (for airplanes in Airbus corresponding provisions of this AD. this AD, contact Airbus SAS, Airworthiness pre-modification 47930 configuration and (2) Contacting the Manufacturer: As of the Office—EAW, Rond-Point Emile Dewoitine pre-Airbus Service Bulletin A330–28–3067 effective date of this AD, for any requirement No: 2, 31700 Blagnac Cedex, France; configuration), or DU 00005218.0002001 (for in this AD to obtain corrective actions from telephone +33 5 61 93 36 96; fax +33 5 61 airplanes in an Airbus post-modification a manufacturer, the action must be 93 44 51; email account.airworth-eas@ 47930 configuration or post-Airbus Service accomplished using a method approved by airbus.com; internet http://www.airbus.com. Bulletin A330–28–3067 configuration), as the Manager, International Section, Transport (6) You may view this service information applicable, are compliant with the Standards Branch, FAA; or the European at the FAA, Transport Standards Branch, requirements of paragraph (g) of this AD, Aviation Safety Agency (EASA); or Airbus 2200 South 216th St., Des Moines, WA. For provided that the applicable DU is not SAS’s EASA Design Organization Approval information on the availability of this removed from the AFM. (DOA). If approved by the DOA, the approval material at the FAA, call 206–231–3195. must include the DOA-authorized signature. (7) You may view this service information (i) New Definitions (3) Required for Compliance (RC): If any that is incorporated by reference at the (1) For the purposes of this AD, an affected service information contains procedures or National Archives and Records FWC is an FWC standard lower than T7–0. tests that are identified as RC, those Administration (NARA). For information on An FWC that is not affected is an FWC procedures and tests must be done to comply the availability of this material at NARA, call standard T7–0 having part number (P/N) with this AD; any procedures or tests that are 202–741–6030, or go to: http:// LA2E20202T70000, or higher standard. not identified as RC are recommended. Those www.archives.gov/federal-register/cfr/ibr- (2) For the purposes of this AD: Group 1 procedures and tests that are not identified locations.html. airplanes are those equipped with an affected as RC may be deviated from using accepted FWC (as defined in paragraph (i)(1) of this Issued in Des Moines, Washington, on methods in accordance with the operator’s AD) as of the effective date of this AD. Group August 17, 2018. maintenance or inspection program without 2 airplanes are those equipped with FWCs obtaining approval of an AMOC, provided Michael Kaszycki, that are not affected (as defined in paragraph the procedures and tests identified as RC can Acting Director, System Oversight Division, (i)(1) of this AD) as of the effective date of be done and the airplane can be put back in Aircraft Certification Service. this AD. an airworthy condition. Any substitutions or [FR Doc. 2018–18736 Filed 8–30–18; 8:45 am] (j) New Requirement of This AD: FWC changes to procedures or tests identified as BILLING CODE 4910–13–P Replacement or Modification RC require approval of an AMOC. For Group 1 airplanes: Within 24 months (n) Related Information after the effective date of this AD: Replace or (1) Refer to Mandatory Continuing DEPARTMENT OF TRANSPORTATION modify an affected FWC with an FWC that Airworthiness Information (MCAI) EASA AD is not affected, in accordance with the 2017–0105R1, dated July 17, 2017, for related Federal Aviation Administration Accomplishment Instructions of Airbus information. This MCAI may be found in the Service Bulletin A330–31–3232, Revision 01, AD docket on the internet at http:// 14 CFR Part 39 including Appendix 01, dated February 14, www.regulations.gov by searching for and 2017. locating Docket No. FAA–2018–0169. [Docket No. FAA–2018–0361; Product (k) Parts Installation Prohibition (2) For more information about this AD, Identifier 2017–NM–160–AD; Amendment contact Vladimir Ulyanov, Aerospace 39–19373; AD 2018–17–19] (1) For Group 1 airplanes: After accomplishing the actions required by Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th RIN 2120–AA64 paragraph (j) of this AD, no person may install an affected FWC on the modified St., Des Moines, WA 98198; telephone and fax 206–231–3229. Airworthiness Directives; Airbus SAS airplane. (3) Service information identified in this Airplanes (2) For Group 2 airplanes: As of the effective date of this AD, no person may AD that is not incorporated by reference is available at the addresses specified in AGENCY: Federal Aviation install an affected FWC on any airplane. Administration (FAA), Department of paragraphs (o)(5) and (o)(6) of this AD. (l) Credit for Previous Actions Transportation (DOT). (o) Material Incorporated by Reference This paragraph provides credit for actions ACTION: Final rule. required by paragraph (j) of this AD, if those (1) The Director of the Federal Register actions were performed before the effective approved the incorporation by reference SUMMARY: We are adopting a new date of this AD using Airbus Service Bulletin (IBR) of the service information listed in this airworthiness directive (AD) for certain A330–31–3232, dated May 4, 2016. paragraph under 5 U.S.C. 552(a) and 1 CFR Airbus SAS Model A318, A319, and part 51. (m) Other FAA AD Provisions (2) You must use this service information A320 series airplanes, and Model A321– (1) Alternative Methods of Compliance as applicable to do the actions required by 111, –112, –131, –211, –212, –213, –231, (AMOCs): The Manager, International this AD, unless this AD specifies otherwise. –232, –251N, –253N, and –271N Section, Transport Standards Branch, FAA, (3) The following service information was airplanes. This AD was prompted by a has the authority to approve AMOCs for this approved for IBR on October 5, 2018. determination that more restrictive AD, if requested using the procedures found (i) Airbus Service Bulletin A330–31–3232, maintenance requirements and in 14 CFR 39.19. In accordance with 14 CFR Revision 01, including Appendix 01, dated airworthiness limitations are necessary. 39.19, send your request to your principal February 14, 2017. This AD requires revising the daltland on DSKBBV9HB2PROD with RULES inspector or local Flight Standards District (ii) Reserved. maintenance or inspection program, as Office, as appropriate. If sending information (4) The following service information was directly to the International Section, send it approved for IBR on of February 13, 2015 (80 applicable, to incorporate the specified to the attention of the person identified in FR 4762, January 29, 2015). maintenance requirements and paragraph (n)(2) of this AD. Information may (i) Airbus A330/A340 Airplane Flight airworthiness limitations. We are be emailed to: 9-ANM-116-AMOC- Manual (AFM) Temporary Revision TR427, issuing this AD to address the unsafe REQUESTS@faa.gov. UPDATE OF ELEC—EMER CONFIG condition on these products. VerDate Sep<11>2014 16:04 Aug 30, 2018 Jkt 244001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\31AUR1.SGM 31AUR1


Document Created: 2018-08-31 00:53:38
Document Modified: 2018-08-31 00:53:38
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionRules and Regulations
ActionFinal rule.
DatesThis AD is effective October 5, 2018.
ContactVladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229.
FR Citation83 FR 44457 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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