81_FR_21332 81 FR 21263 - Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes

81 FR 21263 - Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 81, Issue 69 (April 11, 2016)

Page Range21263-21266
FR Document2016-07229

We are superseding Airworthiness Directive (AD) 2011-21-06 for all BAE SYSTEMS (Operations) Limited Model 4101 airplanes. AD 2011-21- 06 required revising the maintenance program. This new AD requires a new revision of the maintenance or inspection program. This AD was prompted by a determination that the life limit of certain main landing gear components must be reduced, and certain post-repair inspections of critical structure are necessary. We are issuing this AD to prevent failure of certain structurally significant items, including the main landing gear and nose landing gear, which could result in reduced structural integrity of the airplane; and to prevent fuel vapor ignition sources, which could result in a fuel tank explosion and consequent loss of the airplane.

Federal Register, Volume 81 Issue 69 (Monday, April 11, 2016) 
[Federal Register Volume 81, Number 69 (Monday, April 11, 2016)]
[Rules and Regulations]
[Pages 21263-21266]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2016-07229]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2015-1279; Directorate Identifier 2014-NM-049-AD; 
Amendment 39-18454; AD 2016-07-09]
RIN 2120-AA64


Airworthiness Directives; BAE SYSTEMS (Operations) Limited 
Airplanes

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

ACTION: Final rule.

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[[Page 21264]]

SUMMARY: We are superseding Airworthiness Directive (AD) 2011-21-06 for 
all BAE SYSTEMS (Operations) Limited Model 4101 airplanes. AD 2011-21-
06 required revising the maintenance program. This new AD requires a 
new revision of the maintenance or inspection program. This AD was 
prompted by a determination that the life limit of certain main landing 
gear components must be reduced, and certain post-repair inspections of 
critical structure are necessary. We are issuing this AD to prevent 
failure of certain structurally significant items, including the main 
landing gear and nose landing gear, which could result in reduced 
structural integrity of the airplane; and to prevent fuel vapor 
ignition sources, which could result in a fuel tank explosion and 
consequent loss of the airplane.

DATES: This AD is effective May 16, 2016.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of May 16, 
2016.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of 
November 23, 2011 (76 FR 64788, October 19, 2011).

ADDRESSES: For service information identified in this final rule, 
contact BAE SYSTEMS (Operations) Limited, Customer Information 
Department, Prestwick International Airport, Ayrshire, KA9 2RW, 
Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 
675704; email [email protected]; Internet http://www.baesystems.com/Businesses/RegionalAircraft/index.htm. 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-2015-1279.

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-
1279; 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: Theodore (Todd) Thompson, Aerospace 
Engineer, International Branch, ANM-116, Transport Airplane 
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; 
telephone: 425-227-1175; fax 425-227-1149.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to supersede AD 2011-21-06, Amendment 39-16829 (76 FR 64788, 
October 19, 2011) (``AD 2011-21-06''). AD 2011-21-06 applied to all BAE 
SYSTEMS (Operations) Limited Model 4101 airplanes. The NPRM published 
in the Federal Register on May 8, 2015 (80 FR 26484) (``the NPRM'').
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2014-0043, dated February 21, 2014 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all BAE SYSTEMS 
(Operations) Limited Model 4101 airplanes. The MCAI states:

    The Jetstream J41 Aircraft Maintenance Manual (AMM), includes 
the following chapters:

05-10-10 ``Airworthiness Limitations'',
05-10-20 ``Certification Maintenance Requirements'', and,
05-10-30 ``Critical Design Configuration Control Limitations 
(CDCCL)--Fuel System''.

    The maintenance tasks and limitations contained in these 
chapters have been identified as mandatory actions for continued 
airworthiness and EASA issued AD 2010-0098 [dated May 27, 2010 
(http://ad.easa.europa.eu/ad/2010-0098) which corresponds to FAA AD 
2011-21-06, Amendment 39-16829 (79 FR 64788, October 19, 2011)] to 
require operators to comply with those instructions.
    Since that [EASA] AD was issued, BAE Systems (Operations) Ltd 
issued Revision 37 of the AMM amending Chapter 05-10-10 to revise 
and reduce the life limit of certain main landing gear components. 
In addition, Revision 38 of the AMM was issued to amend Chapters 05-
10-00 and 05-10-10 introducing inspections to be accomplished after 
implementation of some repairs affecting fatigue strength of 
critical structure. Failure to comply with the new and more 
restrictive actions could result in an unsafe condition.
    For the reasons described above, this [EASA] AD, which 
supersedes EASA AD 2010-0098, requires implementation of the 
maintenance requirements and/or airworthiness limitations as 
specified in the defined parts of Chapter 05 of the AMM at Revision 
38.

    The unsafe condition is the failure of certain structurally 
significant items, including the main landing gear and nose landing 
gear, which could result in reduced structural integrity of the 
airplane; and fuel vapor ignition sources, which could result in a fuel 
tank explosion and consequent loss of the airplane. 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-2015-1279.

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.

Explanation of Change to NPRM

    Since we issued the NPRM, we discovered an incorrect reference to 
``paragraph (j)'' in paragraph (i)(3) of the proposed AD. The correct 
reference is to ``paragraph (i),'' and we have changed this AD 
accordingly.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting this AD with the change described 
previously and for minor editorial changes. We have determined that 
these 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.

Related Service Information Under 1 CFR Part 51

    We reviewed Subjects 05-10-10, ``Airworthiness Limitations''; 05-
10-20, ``Certification Maintenance Requirements''; and 05-10-30, 
``Critical Design Configuration Control Limitations (CDCCL)--Fuel 
System''; of Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited J41 AMM, Revision 38, dated September 15, 
2013. This service information describes procedures for inspections of 
structurally significant items and the fuel system. 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.

[[Page 21265]]

Costs of Compliance

    We estimate that this AD affects 4 airplanes of U.S. registry.
    The actions required by AD 2011-21-06, Amendment 39-16829 (76 FR 
64788, October 19, 2011), and retained in this AD take about 1 work-
hour 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 2011-21-06 is $85 per product.
    We also estimate that it would take about 1 work-hour per product 
to comply with the basic requirements of this AD. The average labor 
rate is $85 per work-hour. Based on these figures, we estimate the cost 
of this AD on U.S. operators to be $340, or $85 per product.

Authority for This Rulemaking

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

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Airworthiness Directive (AD) 
2011-21-06, Amendment 39-16829 (76 FR 64788, October 19, 2011), and 
adding the following new AD:

2016-07-09 BAE SYSTEMS (Operations) Limited: Amendment 39-18454. 
Docket No. FAA-2015-1279; Directorate Identifier 2014-NM-049-AD.

(a) Effective Date

    This AD is effective May 16, 2016.

(b) Affected ADs

    This AD replaces AD 2011-21-06, Amendment 39-16829 (76 FR 64788, 
October 19, 2011) (``AD 2011-21-06'').

(c) Applicability

    This AD applies to all BAE SYSTEMS (Operations) Limited Model 
4101 airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 05.

(e) Reason

    This AD was prompted by the need to reduce the life limit of 
certain main landing gear components, and to add certain post-repair 
inspections of critical structure to the maintenance or inspection 
program. We are issuing this AD to prevent failure of certain 
structurally significant items, including the main landing gear and 
nose landing gear, which could result in reduced structural 
integrity of the airplane; and to prevent fuel vapor ignition 
sources, which could result in a fuel tank explosion and consequent 
loss of the airplane.

(f) Compliance

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

(g) Retained Maintenance Program Revision, With No Changes

    This paragraph restates the requirements of paragraph (i) of AD 
2011-21-06, with no changes. Within 90 days after November 23, 2011 
(the effective date of AD 2011-21-06): Revise the maintenance 
program by incorporating Subjects 05-10-10, ``Airworthiness 
Limitations''; 05-10-20, ``Certification Maintenance Requirements''; 
and 05-10-30, ``Critical Design Configuration Control Limitations 
(CDCCL)--Fuel System''; of Chapter 05, ``Airworthiness 
Limitations,'' of the BAE Systems (Operations) Limited Jetstream 
Series 4100 Aircraft Maintenance Manual (AMM), Revision 35, dated 
February 15, 2011. The initial compliance times for the tasks are at 
the applicable times specified in paragraphs (g)(1), (g)(2), and 
(g)(3) of this AD. Doing the actions required by paragraph (i) of 
this AD terminates the requirements of this paragraph.
    (1) For replacement tasks of life limited parts specified in 
Subject 05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited Jetstream Series 4100 AMM, Revision 35, dated February 15, 
2011: Prior to the applicable flight cycles (landings) or flight 
hours (flying hours) on the part specified in the ``Mandatory Life 
Limits'' column in Subject 05-10-10, or within 90 days after 
November 23, 2011 (the effective date of AD 2011-21-06), whichever 
occurs later.
    (2) For structurally significant item tasks specified in Subject 
05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited Jetstream Series 4100 AMM, Revision 35, dated February 15, 
2011: Prior to the accumulation of the applicable flight cycles 
specified in the ``Initial Inspection'' column in Subject 05-10-10, 
or within 90 days after November 23, 2011 (the effective date of AD 
2011-21-06), whichever occurs later.
    (3) For certification maintenance requirements tasks specified 
in Subject 05-10-20, ``Certification Maintenance Requirements,'' of 
Chapter 05, ``Airworthiness Limitations,'' of the BAE Systems 
(Operations) Limited Jetstream Series 4100 AMM, Revision 35, dated 
February 15, 2011: Prior to the accumulation of the applicable 
flight hours specified in the ``Time Between Checks'' column in 
Subject 05-10-20, or within 90 days after November 23, 2011 (the 
effective date of AD 2011-21-06), whichever occurs later; except for 
tasks that specify ``first flight of the day'' in the ``Time Between 
Checks'' column in Subject 05-10-20, the initial compliance time is 
the first flight of the next day after doing the revision required 
by paragraph (g) of this AD, or within 90 days after November 23, 
2011 (the effective date of AD 2011-21-06), whichever occurs later.

(h) Retained Restrictions on Alternative Actions, Intervals, and/or 
CDCCLs, With a New Exception

    This paragraph restates the requirements of paragraph (k) of AD 
2011-21-06, with a new exception. Except as required by paragraph 
(i) of this AD, after accomplishing the revision required by 
paragraph (g) of this AD, no alternative actions (e.g., 
inspections), intervals, and/or CDCCLs may be used unless the 
actions, intervals, and/or CDCCLs are approved as an alternative 
method of compliance (AMOC) in accordance with the procedures 
specified in paragraph (l) of this AD.

[[Page 21266]]

(i) New Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD: Revise the 
maintenance or inspection program, as applicable, by incorporating 
Subjects 05-10-10, ``Airworthiness Limitations''; 05-10-20, 
``Certification Maintenance Requirements''; and 05-10-30, ``Critical 
Design Configuration Control Limitations (CDCCL)--Fuel System''; of 
Chapter 05, ``Airworthiness Limitations,'' of the BAE Systems 
(Operations) Limited J41 AMM, Revision 38, dated September 15, 2013. 
The initial compliance times for the tasks are at the applicable 
times specified in paragraphs (i)(1), (i)(2), and (i)(3) of this AD. 
Doing the actions required by this paragraph terminates the 
requirements of paragraph (g) of this AD.
    (1) For replacement tasks of life limited parts specified in 
Subject 05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the 
applicable flight cycles (landings) or flight hours (flying hours) 
on the part specified in the ``Mandatory Life Limits'' column in 
Subject 05-10-10, or within 90 days after the effective date of this 
AD, whichever occurs later.
    (2) For structurally significant item tasks specified in Subject 
05-10-10, ``Airworthiness Limitations,'' of Chapter 05, 
``Airworthiness Limitations,'' of the BAE Systems (Operations) 
Limited J41 AMM, Revision 38, dated September 15, 2013: Prior to the 
accumulation of the applicable flight cycles specified in the 
``Initial Inspection'' column in Subject 05-10-10, or within 90 days 
after the effective date of this AD, whichever occurs later.
    (3) For certification maintenance requirements tasks specified 
in Subject 05-10-20, ``Certification Maintenance Requirements,'' of 
Chapter 05, ``Airworthiness Limitations,'' of the BAE Systems 
(Operations) Limited J41 AMM, Revision 38, dated September 15, 2013: 
Prior to the accumulation of the applicable flight hours specified 
in the ``Time Between Checks'' column in Subject 05-10-20, or within 
90 days after the effective date of this AD, whichever occurs later; 
except for tasks that specify ``first flight of the day'' in the 
``Time Between Checks'' column in Subject 05-10-20, the initial 
compliance time is the first flight of the next day after doing the 
revision required by paragraph (i) of this AD, or within 90 days the 
effective date of this AD, whichever occurs later.

(j) New Restrictions on Alternative Actions, Intervals, and/or (CDCCLs)

    After the maintenance or inspection program, as applicable, has 
been revised as required by paragraph (i) of this AD, no alternative 
actions (e.g., inspections), intervals, and/or CDCCLs may be used 
unless the actions, intervals, and/or CDCCLs are approved as an AMOC 
in accordance with the procedures specified in paragraph (l) of this 
AD.

(k) Credit for Previous Actions

    This paragraph restates the provisions of paragraph (j) of AD 
2011-21-06. This paragraph provides credit for actions required by 
paragraph (g) of this AD, if those actions were performed before 
November 23, 2011 (the effective date of AD 2011-21-06), in 
accordance with Subjects 05-10-10, ``Airworthiness Limitations''; 
05-10-20, ``Certification Maintenance Requirements''; and 05-10-30, 
``Critical Design Configuration Control Limitations (CDCCL)--Fuel 
System''; of Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited Jetstream Series 4100 AMM, Revision 33, 
dated February 15, 2010; which are not incorporated by reference in 
this AD.

(l) 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: Theodore 
(Todd) Thompson, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
WA 98057-3356; telephone: 425-227-1175; fax 425-227-1149. 
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. The AMOC approval letter must specifically 
reference this AD.
    (ii) AMOCs approved previously for AD 2011-21-06, are not 
approved as AMOCs with this AD.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Branch, ANM-116, Transport Airplane Directorate, FAA; or the 
European Aviation Safety Agency (EASA); or BAE Systems (Operations) 
Limited's EASA Design Organization Approval (DOA). If approved by 
the DOA, the approval must include the DOA-authorized signature.

(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2014-0043, dated February 21, 
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-2015-1279.
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (n)(5) and (n)(6) of this AD.

(n) 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 
May 16, 2016.
    (i) Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited J41 Aircraft Maintenance Manual (AMM), 
Revision 38, dated September 15, 2013. Page 1 of the ``Publications 
Transmittal'' is the only page that shows the revision level of this 
document.
    (A) Subject 05-10-10, ``Airworthiness Limitations.''
    (B) Subject 05-10-20, ``Certification Maintenance 
Requirements.''
    (C) Subject 05-10-30, ``Critical Design Configuration Control 
Limitations (CDCCL)--Fuel System.''
    (ii) Reserved.
    (4) The following service information was approved for IBR on 
November 23, 2011 (76 FR 64788, October 19, 2011).
    (i) Chapter 05, ``Airworthiness Limitations,'' of the BAE 
Systems (Operations) Limited Jetstream Series 4100 AMM, Revision 35, 
dated February 15, 2011. Page 1 of the Publications Transmittal of 
the BAE Systems (Operations) Limited Jetstream Series 4100 AMM is 
the only page that shows the revision level of this document.
    (A) Subject 05-10-10, ``Airworthiness Limitations.''
    (B) Subject 05-10-20, ``Certification Maintenance 
Requirements.''
    (C) Subject 05-10-30, ``Critical Design Configuration Control 
Limitations (CDCCL)--Fuel System.''
    (ii) Reserved.
    (5) For service information identified in this AD, contact BAE 
SYSTEMS (Operations) Limited, Customer Information Department, 
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United 
Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email 
[email protected]; Internet http://www.baesystems.com/Businesses/RegionalAircraft/index.htm.
    (6) 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.
    (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 Renton, Washington, on March 22, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-07229 Filed 4-8-16; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 81, No. 69 / Monday, April 11, 2016 / Rules and Regulations 21263 Adoption of the Amendment (g) Inspect (k) Material Incorporated by Reference (1) Inspect the right wing rib at wing (1) The Director of the Federal Register Accordingly, under the authority station (WS) 140.09 for cracks at the approved the incorporation by reference delegated to me by the Administrator, following compliance times. (IBR) of the service information listed in this the FAA amends part 39 of the Federal (i) For airplanes previously affected by AD paragraph under 5 U.S.C. 552(a) and 1 CFR Aviation Regulations (14 CFR part 39) as 2015–20–13: Within the next 25 hours time- part 51. follows: in-service after (TIS) after October 29, 2015 (2) You must use this service information (the effective date retained from AD 2015– as applicable to do the actions required by PART 39—AIRWORTHINESS 20–13) following the INSTRUCTIONS section this AD, unless the AD specifies otherwise. DIRECTIVES of Piper Aircraft, Inc. Service Bulletin No. (3) The following service information was 1279, dated August 26, 2015, or Piper approved for IBR on April 26, 2016. Aircraft, Inc. Service Bulletin No. 1279A, (i) Piper Aircraft, Inc. Service Bulletin No. ■ 1. The authority citation for part 39 1279A, dated March 3, 2016. continues to read as follows: dated March 3, 2016. (ii) For airplanes new to this AD: Within (ii) Reserved. Authority: 49 U.S.C. 106(g), 40113, 44701. (4) The following service information was the next 25 hours TIS after April 26, 2016 approved for IBR on October 29, 2015 (80 FR (the effective date of this AD) following the § 39.13 [Amended] 61725, October 14, 2015). INSTRUCTIONS section of Piper Aircraft, (i) Piper Aircraft, Inc. Service Bulletin No. ■ 2. The FAA amends § 39.13 by Inc. Service Bulletin No. 1279A, dated March 1279, dated August 26, 2015. removing Airworthiness Directive (AD) 3, 2016. (ii) Reserved. (2) If any crack is detected during the (5) For Piper Aircraft, Inc. service 2015–20–13, Amendment 39–18292 (80 inspection required by paragraph (g)(1) of information identified in this AD, contact FR 61725, October 14, 2015) and adding this AD, before further flight, obtain and the following new AD: Piper Aircraft, Inc., Customer Service, 2926 implement an FAA-approved repair scheme, Piper Drive, Vero Beach, Florida 32960; 2016–07–21 Piper Aircraft, Inc.: approved specifically for this AD. At the telephone: (877) 879–0275; fax: none; email: Amendment 39–18466; Docket No. operator’s discretion, assistance may be customer.service@piper.com; Internet: FAA–2016–5432; Directorate Identifier provided by contacting Piper Aircraft, Inc. at www.piper.com. 2016–CE–009–AD. the address identified in paragraph (k)(5) of (6) You may review the referenced service this AD. information at the FAA, Small Airplane (a) Effective Date (h) Special Flight Permit Directorate, 901 Locust, Kansas City, This AD is effective April 26, 2016. Missouri 64106. For information on the A special flight permit is allowed for this availability of this material at the FAA, call (b) Affected ADs AD per 14 CFR 39.23 for the inspection (816) 329–4148. It is also available on the This AD replaces AD 2015–20–13, required in paragraph (g)(1) of this AD. If a Internet at http://www.regulations.gov by Amendment 39–18292 (80 FR 61725) (‘‘AD crack is found during the inspection required searching for locating Docket No. FAA–2016– 2015–20–13’’). in paragraph (g)(1) of this AD, a special flight 5432. permit is allowed with the following (7) You may view this service information (c) Applicability limitations: that is incorporated by reference at the This AD applies to the following Piper (1) Flight must be planned to the nearest National Archives and Records Aircraft, Inc. airplanes certificated in any location where repairs can be done; Administration (NARA). For information on category. (2) Indicated airspeed must be 120 knots or the availability of this material at NARA, call (1) Airplanes previously affected by AD less for the entire flight; 202–741–6030, or go to: http:// 2015–20–13: Model PA–28–161 airplanes, (3) Bank angle is not to exceed 30 degrees www.archives.gov/federal-register/cfr/ibr- serial numbers (S/Ns) 2842393 through for the entire flight; locations.html. 2842395; Model PA–28–181 airplanes, S/Ns (4) Maximum load factors must be between Issued in Kansas City, Missouri, on March 2843769 through 2843775 and 2843779 +3.0 and ¥1.0 for the entire flight; and 28, 2016. through 2843791; and Model PA–28R–201 (5) Flight must be performed VFR, with no Jacqueline Jambor, airplanes, S/N 2844152. turbulence greater than ‘‘light’’ forecast for (2) Airplanes new to this AD: Model PA– the planned flight route and altitude. Acting Manager, Small Airplane Directorate, 28–161 airplanes, S/Ns 2842010 through Aircraft Certification Service. (i) Alternative Methods of Compliance [FR Doc. 2016–07580 Filed 4–8–16; 8:45 am] 2842392; Model PA–28–181 airplanes, S/Ns (AMOCs) 2843021 through 2843768; and Model PA– BILLING CODE 4910–13–P 28R–201 airplane, S/Ns 2844004 through (1) The Manager, Atlanta ACO, FAA, has 2844151. the authority to approve AMOCs for this AD, if requested using the procedures found in 14 DEPARTMENT OF TRANSPORTATION (d) Subject CFR 39.19. In accordance with 14 CFR 39.19, Joint Aircraft System Component (JASC)/ send your request to your principal inspector Federal Aviation Administration Air Transport Association (ATA) of America or local Flight Standards District Office, as Code 5712, Wing Ribs/Bulkhead. appropriate. If sending information directly 14 CFR Part 39 to the manager of the ACO, send it to the (e) Unsafe Condition attention of the person identified in [Docket No. FAA–2015–1279; Directorate This AD was prompted by reports of cracks paragraph (j) of this AD. Identifier 2014–NM–049–AD; Amendment found in the wing rib on airplanes outside (2) Before using any approved AMOC, 39–18454; AD 2016–07–09] the Applicability, paragraph (c), of AD 2015– notify your appropriate principal inspector, 20–13. The cracks occurred in production or lacking a principal inspector, the manager RIN 2120–AA64 during forming of the wing rib bead radius. of the local flight standards district office/ We are issuing this AD to detect and correct certificate holding district office. Airworthiness Directives; BAE jstallworth on DSK7TPTVN1PROD with RULES cracks in the wing rib, which if not corrected, SYSTEMS (Operations) Limited (j) Related Information could result in reduced structural integrity of Airplanes the wing with consequent loss of control. For more information about this AD, contact Gregory ‘‘Keith’’ Noles, Aerospace AGENCY: Federal Aviation (f) Compliance Engineer, FAA, Atlanta ACO, 1701 Columbia Administration (FAA), Department of Comply with this AD within the Avenue, College Park, Georgia 30337; phone: Transportation (DOT). compliance times specified, unless already (404) 474–5551; fax: (404) 474–5606; email: ACTION: Final rule. done. gregory.noles@faa.gov. VerDate Sep<11>2014 14:13 Apr 08, 2016 Jkt 238001 PO 00000 Frm 00041 Fmt 4700 Sfmt 4700 E:\FR\FM\11APR1.SGM 11APR1

21264 Federal Register / Vol. 81, No. 69 / Monday, April 11, 2016 / Rules and Regulations SUMMARY: We are superseding is Docket Management Facility, U.S. 2010–0098, requires implementation of the Airworthiness Directive (AD) 2011–21– Department of Transportation, Docket maintenance requirements and/or 06 for all BAE SYSTEMS (Operations) Operations, M–30, West Building airworthiness limitations as specified in the defined parts of Chapter 05 of the AMM at Limited Model 4101 airplanes. AD Ground Floor, Room W12–140, 1200 Revision 38. 2011–21–06 required revising the New Jersey Avenue SE., Washington, maintenance program. This new AD DC 20590. The unsafe condition is the failure of requires a new revision of the FOR FURTHER INFORMATION CONTACT: certain structurally significant items, maintenance or inspection program. Theodore (Todd) Thompson, Aerospace including the main landing gear and This AD was prompted by a Engineer, International Branch, ANM– nose landing gear, which could result in determination that the life limit of 116, Transport Airplane Directorate, reduced structural integrity of the certain main landing gear components FAA, 1601 Lind Avenue SW., Renton, airplane; and fuel vapor ignition must be reduced, and certain post-repair WA 98057–3356; telephone: 425–227– sources, which could result in a fuel inspections of critical structure are 1175; fax 425–227–1149. tank explosion and consequent loss of necessary. We are issuing this AD to SUPPLEMENTARY INFORMATION: the airplane. You may examine the prevent failure of certain structurally MCAI in the AD docket on the Internet significant items, including the main Discussion at http://www.regulations.gov by landing gear and nose landing gear, We issued a notice of proposed searching for and locating Docket No. which could result in reduced structural rulemaking (NPRM) to amend 14 CFR FAA–2015–1279. integrity of the airplane; and to prevent part 39 to supersede AD 2011–21–06, Comments fuel vapor ignition sources, which could Amendment 39–16829 (76 FR 64788, result in a fuel tank explosion and October 19, 2011) (‘‘AD 2011–21–06’’). We gave the public the opportunity to consequent loss of the airplane. AD 2011–21–06 applied to all BAE participate in developing this AD. We SYSTEMS (Operations) Limited Model received no comments on the NPRM or DATES: This AD is effective May 16, 4101 airplanes. The NPRM published in on the determination of the cost to the 2016. the Federal Register on May 8, 2015 (80 public. The Director of the Federal Register approved the incorporation by reference FR 26484) (‘‘the NPRM’’). Explanation of Change to NPRM of a certain publication listed in this AD The European Aviation Safety Agency (EASA), which is the Technical Agent Since we issued the NPRM, we as of May 16, 2016. discovered an incorrect reference to The Director of the Federal Register for the Member States of the European Union, has issued EASA Airworthiness ‘‘paragraph (j)’’ in paragraph (i)(3) of the approved the incorporation by reference proposed AD. The correct reference is to of a certain other publication listed in Directive 2014–0043, dated February 21, 2014 (referred to after this as the ‘‘paragraph (i),’’ and we have changed this AD as of November 23, 2011 (76 FR this AD accordingly. 64788, October 19, 2011). Mandatory Continuing Airworthiness ADDRESSES: For service information Information, or ‘‘the MCAI’’), to correct Conclusion identified in this final rule, contact BAE an unsafe condition for all BAE We reviewed the available data and SYSTEMS (Operations) Limited, SYSTEMS (Operations) Limited Model determined that air safety and the Customer Information Department, 4101 airplanes. The MCAI states: public interest require adopting this AD Prestwick International Airport, The Jetstream J41 Aircraft Maintenance with the change described previously Ayrshire, KA9 2RW, Scotland, United Manual (AMM), includes the following and for minor editorial changes. We Kingdom; telephone +44 1292 675207; chapters: have determined that these changes: fax +44 1292 675704; email 05–10–10 ‘‘Airworthiness Limitations’’, • Are consistent with the intent that RApublications@baesystems.com; 05–10–20 ‘‘Certification Maintenance was proposed in the NPRM for Requirements’’, and, Internet http://www.baesystems.com/ correcting the unsafe condition; and 05–10–30 ‘‘Critical Design Configuration Businesses/RegionalAircraft/index.htm. Control Limitations (CDCCL)—Fuel • Do not add any additional burden You may view this referenced service System’’. upon the public than was already information at the FAA, Transport The maintenance tasks and limitations proposed in the NPRM. Airplane Directorate, 1601 Lind Avenue contained in these chapters have been Related Service Information Under 1 SW., Renton, WA. For information on identified as mandatory actions for continued CFR Part 51 the availability of this material at the airworthiness and EASA issued AD 2010– FAA, call 425–227–1221. It is also 0098 [dated May 27, 2010 (http:// We reviewed Subjects 05–10–10, available on the Internet at http:// ad.easa.europa.eu/ad/2010-0098) which ‘‘Airworthiness Limitations’’; 05–10–20, www.regulations.gov by searching for corresponds to FAA AD 2011–21–06, ‘‘Certification Maintenance Amendment 39–16829 (79 FR 64788, October Requirements’’; and 05–10–30, ‘‘Critical and locating Docket No. FAA–2015– 19, 2011)] to require operators to comply 1279. Design Configuration Control with those instructions. Since that [EASA] AD was issued, BAE Limitations (CDCCL)—Fuel System’’; of Examining the AD Docket Chapter 05, ‘‘Airworthiness Systems (Operations) Ltd issued Revision 37 You may examine the AD docket on of the AMM amending Chapter 05–10–10 to Limitations,’’ of the BAE Systems the Internet at http:// revise and reduce the life limit of certain (Operations) Limited J41 AMM, www.regulations.gov by searching for main landing gear components. In addition, Revision 38, dated September 15, 2013. and locating Docket No. FAA–2015– Revision 38 of the AMM was issued to This service information describes 1279; or in person at the Docket amend Chapters 05–10–00 and 05–10–10 procedures for inspections of jstallworth on DSK7TPTVN1PROD with RULES Management Facility between 9 a.m. introducing inspections to be accomplished structurally significant items and the after implementation of some repairs and 5 p.m., Monday through Friday, fuel system. This service information is affecting fatigue strength of critical structure. except Federal holidays. The AD docket Failure to comply with the new and more reasonably available because the contains this AD, the regulatory restrictive actions could result in an unsafe interested parties have access to it evaluation, any comments received, and condition. through their normal course of business other information. The address for the For the reasons described above, this or by the means identified in the Docket Office (telephone 800–647–5527) [EASA] AD, which supersedes EASA AD ADDRESSES section. VerDate Sep<11>2014 14:13 Apr 08, 2016 Jkt 238001 PO 00000 Frm 00042 Fmt 4700 Sfmt 4700 E:\FR\FM\11APR1.SGM 11APR1

Federal Register / Vol. 81, No. 69 / Monday, April 11, 2016 / Rules and Regulations 21265 Costs of Compliance List of Subjects in 14 CFR Part 39 ‘‘Airworthiness Limitations’’; 05–10–20, ‘‘Certification Maintenance Requirements’’; We estimate that this AD affects 4 Air transportation, Aircraft, Aviation and 05–10–30, ‘‘Critical Design Configuration airplanes of U.S. registry. safety, Incorporation by reference, Control Limitations (CDCCL)—Fuel System’’; The actions required by AD 2011–21– Safety. of Chapter 05, ‘‘Airworthiness Limitations,’’ 06, Amendment 39–16829 (76 FR of the BAE Systems (Operations) Limited 64788, October 19, 2011), and retained Adoption of the Amendment Jetstream Series 4100 Aircraft Maintenance in this AD take about 1 work-hour per Accordingly, under the authority Manual (AMM), Revision 35, dated February product, at an average labor rate of $85 delegated to me by the Administrator, 15, 2011. The initial compliance times for the per work-hour. Based on these figures, the FAA amends 14 CFR part 39 as tasks are at the applicable times specified in the estimated cost of the actions that are follows: paragraphs (g)(1), (g)(2), and (g)(3) of this AD. Doing the actions required by paragraph (i) required by AD 2011–21–06 is $85 per of this AD terminates the requirements of this product. PART 39—AIRWORTHINESS paragraph. We also estimate that it would take DIRECTIVES (1) For replacement tasks of life limited about 1 work-hour per product to parts specified in Subject 05–10–10, comply with the basic requirements of ■ 1. The authority citation for part 39 ‘‘Airworthiness Limitations,’’ of Chapter 05, this AD. The average labor rate is $85 continues to read as follows: ‘‘Airworthiness Limitations,’’ of the BAE per work-hour. Based on these figures, Authority: 49 U.S.C. 106(g), 40113, 44701. Systems (Operations) Limited Jetstream we estimate the cost of this AD on U.S. Series 4100 AMM, Revision 35, dated § 39.13 [Amended] February 15, 2011: Prior to the applicable operators to be $340, or $85 per product. ■ 2. The FAA amends § 39.13 by flight cycles (landings) or flight hours (flying Authority for This Rulemaking removing Airworthiness Directive (AD) hours) on the part specified in the Title 49 of the United States Code 2011–21–06, Amendment 39–16829 (76 ‘‘Mandatory Life Limits’’ column in Subject 05–10–10, or within 90 days after November specifies the FAA’s authority to issue FR 64788, October 19, 2011), and 23, 2011 (the effective date of AD 2011–21– rules on aviation safety. Subtitle I, adding the following new AD: 06), whichever occurs later. section 106, describes the authority of 2016–07–09 BAE SYSTEMS (Operations) (2) For structurally significant item tasks the FAA Administrator. ‘‘Subtitle VII: Limited: Amendment 39–18454. Docket specified in Subject 05–10–10, Aviation Programs,’’ describes in more No. FAA–2015–1279; Directorate ‘‘Airworthiness Limitations,’’ of Chapter 05, detail the scope of the Agency’s Identifier 2014–NM–049–AD. ‘‘Airworthiness Limitations,’’ of the BAE authority. Systems (Operations) Limited Jetstream (a) Effective Date Series 4100 AMM, Revision 35, dated We are issuing this rulemaking under This AD is effective May 16, 2016. February 15, 2011: Prior to the accumulation the authority described in ‘‘Subtitle VII, of the applicable flight cycles specified in the Part A, Subpart III, Section 44701: (b) Affected ADs ‘‘Initial Inspection’’ column in Subject 05– General requirements.’’ Under that This AD replaces AD 2011–21–06, 10–10, or within 90 days after November 23, section, Congress charges the FAA with Amendment 39–16829 (76 FR 64788, October 2011 (the effective date of AD 2011–21–06), promoting safe flight of civil aircraft in 19, 2011) (‘‘AD 2011–21–06’’). whichever occurs later. air commerce by prescribing regulations (c) Applicability (3) For certification maintenance for practices, methods, and procedures requirements tasks specified in Subject 05– This AD applies to all BAE SYSTEMS 10–20, ‘‘Certification Maintenance the Administrator finds necessary for (Operations) Limited Model 4101 airplanes, safety in air commerce. This regulation Requirements,’’ of Chapter 05, certificated in any category. ‘‘Airworthiness Limitations,’’ of the BAE is within the scope of that authority (d) Subject Systems (Operations) Limited Jetstream because it addresses an unsafe condition Air Transport Association (ATA) of Series 4100 AMM, Revision 35, dated that is likely to exist or develop on February 15, 2011: Prior to the accumulation products identified in this rulemaking America Code 05. of the applicable flight hours specified in the action. (e) Reason ‘‘Time Between Checks’’ column in Subject Regulatory Findings This AD was prompted by the need to 05–10–20, or within 90 days after November reduce the life limit of certain main landing 23, 2011 (the effective date of AD 2011–21– We determined that this AD will not gear components, and to add certain post- 06), whichever occurs later; except for tasks have federalism implications under repair inspections of critical structure to the that specify ‘‘first flight of the day’’ in the Executive Order 13132. This AD will maintenance or inspection program. We are ‘‘Time Between Checks’’ column in Subject not have a substantial direct effect on issuing this AD to prevent failure of certain 05–10–20, the initial compliance time is the the States, on the relationship between structurally significant items, including the first flight of the next day after doing the main landing gear and nose landing gear, revision required by paragraph (g) of this AD, the national government and the States, which could result in reduced structural or within 90 days after November 23, 2011 or on the distribution of power and (the effective date of AD 2011–21–06), integrity of the airplane; and to prevent fuel responsibilities among the various vapor ignition sources, which could result in whichever occurs later. levels of government. a fuel tank explosion and consequent loss of For the reasons discussed above, I (h) Retained Restrictions on Alternative the airplane. Actions, Intervals, and/or CDCCLs, With a certify that this AD: 1. Is not a ‘‘significant regulatory (f) Compliance New Exception action’’ under Executive Order 12866; Comply with this AD within the This paragraph restates the requirements of 2. Is not a ‘‘significant rule’’ under the compliance times specified, unless already paragraph (k) of AD 2011–21–06, with a new DOT Regulatory Policies and Procedures done. exception. Except as required by paragraph (44 FR 11034, February 26, 1979); (i) of this AD, after accomplishing the (g) Retained Maintenance Program Revision, jstallworth on DSK7TPTVN1PROD with RULES 3. Will not affect intrastate aviation in revision required by paragraph (g) of this AD, With No Changes no alternative actions (e.g., inspections), Alaska; and This paragraph restates the requirements of intervals, and/or CDCCLs may be used unless 4. Will not have a significant paragraph (i) of AD 2011–21–06, with no the actions, intervals, and/or CDCCLs are economic impact, positive or negative, changes. Within 90 days after November 23, approved as an alternative method of on a substantial number of small entities 2011 (the effective date of AD 2011–21–06): compliance (AMOC) in accordance with the under the criteria of the Regulatory Revise the maintenance program by procedures specified in paragraph (l) of this Flexibility Act. incorporating Subjects 05–10–10, AD. VerDate Sep<11>2014 14:13 Apr 08, 2016 Jkt 238001 PO 00000 Frm 00043 Fmt 4700 Sfmt 4700 E:\FR\FM\11APR1.SGM 11APR1

21266 Federal Register / Vol. 81, No. 69 / Monday, April 11, 2016 / Rules and Regulations (i) New Maintenance or Inspection Program paragraph provides credit for actions paragraph under 5 U.S.C. 552(a) and 1 CFR Revision required by paragraph (g) of this AD, if those part 51. Within 90 days after the effective date of actions were performed before November 23, (2) You must use this service information this AD: Revise the maintenance or 2011 (the effective date of AD 2011–21–06), as applicable to do the actions required by inspection program, as applicable, by in accordance with Subjects 05–10–10, this AD, unless this AD specifies otherwise. incorporating Subjects 05–10–10, ‘‘Airworthiness Limitations’’; 05–10–20, (3) The following service information was ‘‘Airworthiness Limitations’’; 05–10–20, ‘‘Certification Maintenance Requirements’’; approved for IBR on May 16, 2016. ‘‘Certification Maintenance Requirements’’; and 05–10–30, ‘‘Critical Design Configuration (i) Chapter 05, ‘‘Airworthiness and 05–10–30, ‘‘Critical Design Configuration Control Limitations (CDCCL)—Fuel System’’; Limitations,’’ of the BAE Systems Control Limitations (CDCCL)—Fuel System’’; of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Systems (Operations) Limited (Operations) Limited J41 Aircraft of Chapter 05, ‘‘Airworthiness Limitations,’’ Maintenance Manual (AMM), Revision 38, of the BAE Systems (Operations) Limited J41 Jetstream Series 4100 AMM, Revision 33, dated February 15, 2010; which are not dated September 15, 2013. Page 1 of the AMM, Revision 38, dated September 15, ‘‘Publications Transmittal’’ is the only page 2013. The initial compliance times for the incorporated by reference in this AD. that shows the revision level of this tasks are at the applicable times specified in (l) Other FAA AD Provisions document. paragraphs (i)(1), (i)(2), and (i)(3) of this AD. Doing the actions required by this paragraph The following provisions also apply to this (A) Subject 05–10–10, ‘‘Airworthiness terminates the requirements of paragraph (g) AD: Limitations.’’ of this AD. (1) Alternative Methods of Compliance (B) Subject 05–10–20, ‘‘Certification (1) For replacement tasks of life limited (AMOCs): The Manager, International Maintenance Requirements.’’ parts specified in Subject 05–10–10, Branch, ANM–116, Transport Airplane (C) Subject 05–10–30, ‘‘Critical Design ‘‘Airworthiness Limitations,’’ of Chapter 05, Directorate, FAA, has the authority to Configuration Control Limitations (CDCCL)— ‘‘Airworthiness Limitations,’’ of the BAE approve AMOCs for this AD, if requested Fuel System.’’ Systems (Operations) Limited J41 AMM, using the procedures found in 14 CFR 39.19. (ii) Reserved. Revision 38, dated September 15, 2013: Prior In accordance with 14 CFR 39.19, send your (4) The following service information was to the applicable flight cycles (landings) or request to your principal inspector or local approved for IBR on November 23, 2011 (76 flight hours (flying hours) on the part Flight Standards District Office, as FR 64788, October 19, 2011). specified in the ‘‘Mandatory Life Limits’’ appropriate. If sending information directly (i) Chapter 05, ‘‘Airworthiness column in Subject 05–10–10, or within 90 to the International Branch, send it to ATTN: Limitations,’’ of the BAE Systems days after the effective date of this AD, Theodore (Todd) Thompson, Aerospace Engineer, International Branch, ANM–116, (Operations) Limited Jetstream Series 4100 whichever occurs later. AMM, Revision 35, dated February 15, 2011. (2) For structurally significant item tasks Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; Page 1 of the Publications Transmittal of the specified in Subject 05–10–10, telephone: 425–227–1175; fax 425–227–1149. BAE Systems (Operations) Limited Jetstream ‘‘Airworthiness Limitations,’’ of Chapter 05, ‘‘Airworthiness Limitations,’’ of the BAE Information may be emailed to: 9-ANM-116- Series 4100 AMM is the only page that shows Systems (Operations) Limited J41 AMM, AMOC-REQUESTS@faa.gov. the revision level of this document. Revision 38, dated September 15, 2013: Prior (i) Before using any approved AMOC, (A) Subject 05–10–10, ‘‘Airworthiness to the accumulation of the applicable flight notify your appropriate principal inspector, Limitations.’’ cycles specified in the ‘‘Initial Inspection’’ or lacking a principal inspector, the manager (B) Subject 05–10–20, ‘‘Certification column in Subject 05–10–10, or within 90 of the local flight standards district office/ Maintenance Requirements.’’ days after the effective date of this AD, certificate holding district office. The AMOC (C) Subject 05–10–30, ‘‘Critical Design whichever occurs later. approval letter must specifically reference Configuration Control Limitations (CDCCL)— (3) For certification maintenance this AD. Fuel System.’’ requirements tasks specified in Subject 05– (ii) AMOCs approved previously for AD (ii) Reserved. 10–20, ‘‘Certification Maintenance 2011–21–06, are not approved as AMOCs (5) For service information identified in Requirements,’’ of Chapter 05, with this AD. this AD, contact BAE SYSTEMS (Operations) ‘‘Airworthiness Limitations,’’ of the BAE (2) Contacting the Manufacturer: For any Limited, Customer Information Department, Systems (Operations) Limited J41 AMM, requirement in this AD to obtain corrective Prestwick International Airport, Ayrshire, Revision 38, dated September 15, 2013: Prior actions from a manufacturer, the action must KA9 2RW, Scotland, United Kingdom; to the accumulation of the applicable flight be accomplished using a method approved telephone +44 1292 675207; fax +44 1292 hours specified in the ‘‘Time Between by the Manager, International Branch, ANM– 675704; email RApublications@ Checks’’ column in Subject 05–10–20, or 116, Transport Airplane Directorate, FAA; or baesystems.com; Internet http:// within 90 days after the effective date of this the European Aviation Safety Agency AD, whichever occurs later; except for tasks (EASA); or BAE Systems (Operations) www.baesystems.com/Businesses/ that specify ‘‘first flight of the day’’ in the Limited’s EASA Design Organization RegionalAircraft/index.htm. ‘‘Time Between Checks’’ column in Subject Approval (DOA). If approved by the DOA, (6) You may view this service information 05–10–20, the initial compliance time is the the approval must include the DOA- at the FAA, Transport Airplane Directorate, first flight of the next day after doing the authorized signature. 1601 Lind Avenue SW., Renton, WA. For revision required by paragraph (i) of this AD, information on the availability of this (m) Related Information material at the FAA, call 425–227–1221. or within 90 days the effective date of this AD, whichever occurs later. (1) Refer to Mandatory Continuing (7) You may view this service information Airworthiness Information (MCAI) EASA that is incorporated by reference at the (j) New Restrictions on Alternative Actions, Airworthiness Directive 2014–0043, dated National Archives and Records Intervals, and/or (CDCCLs) February 21, 2014, for related information. Administration (NARA). For information on After the maintenance or inspection This MCAI may be found in the AD docket the availability of this material at NARA, call program, as applicable, has been revised as on the Internet at http://www.regulations.gov 202–741–6030, or go to: http:// required by paragraph (i) of this AD, no by searching for and locating Docket No. www.archives.gov/federal-register/cfr/ibr- alternative actions (e.g., inspections), FAA–2015–1279. locations.html. intervals, and/or CDCCLs may be used unless (2) Service information identified in this jstallworth on DSK7TPTVN1PROD with RULES the actions, intervals, and/or CDCCLs are AD that is not incorporated by reference is Issued in Renton, Washington, on March approved as an AMOC in accordance with available at the addresses specified in 22, 2016. the procedures specified in paragraph (l) of paragraphs (n)(5) and (n)(6) of this AD. Michael Kaszycki, this AD. Acting Manager, Transport Airplane (n) Material Incorporated by Reference (k) Credit for Previous Actions Directorate, Aircraft Certification Service. (1) The Director of the Federal Register This paragraph restates the provisions of approved the incorporation by reference [FR Doc. 2016–07229 Filed 4–8–16; 8:45 am] paragraph (j) of AD 2011–21–06. This (IBR) of the service information listed in this BILLING CODE 4910–13–P VerDate Sep<11>2014 14:13 Apr 08, 2016 Jkt 238001 PO 00000 Frm 00044 Fmt 4700 Sfmt 9990 E:\FR\FM\11APR1.SGM 11APR1


Document Created: 2016-04-09 00:11:27
Document Modified: 2016-04-09 00:11:27
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 May 16, 2016.
ContactTheodore (Todd) Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-1175; fax 425-227-1149.
FR Citation81 FR 21263 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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