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2014-07-10 BALLONBAU WORNER GMBH:
Amendment 39-17824; Docket No. FAA-2014-0041; Directorate Identifier 2013-CE-053-AD.

(a) EFFECTIVE DATE

    This airworthiness directive (AD) becomes effective May 27, 2014.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Ballonbau Worner GmbH Model NL-280/STU, NL-380/STU,
    NL-510/STU,  NL-640/STU,  NL-840/STU,  and  NL-1000/STU  balloons, all
    serial numbers, certificated in any category.

(d) SUBJECT

    Air  Transport  Association  of  America  (ATA)  Code 5:  Time Limits/
    Maintenance Checks.

(e) REASON

    This AD was prompted by mandatory continuing airworthiness information
    (MCAI)  originated  by an  aviation  authority of  another  country to
    identify and correct an unsafe  condition on an aviation product.  The
    MCAI describes  the unsafe  condition as  current inspection intervals
    are no longer adequate to ensure timely detection of deterioration  or
    damage. If this condition is  uncorrected, it could result in  reduced
    structural integrity of the balloon.

(f) ACTIONS AND COMPLIANCE

    Unless  already  done, do  the  actions in  paragraphs  (f)(1) through
    (f)(4) of this AD:

(1) Before  further  flight after May 27, 2014 (the effective date of this
    AD), complete all inspections  and maintenance tasks described  in the
    Chapter  5,   Annual  Inspection,   in  the   Ballonbau  Worner   GmbH
    Instructions for  Continued Airworthiness,  Gas Balloon  Model NL-STU,
    Issue 1, pages 44 through 53  and 55 through 69,  dated November 2013,
    and page 54 dated December 2013.

(2) If any discrepancies are found during the inspection required in para-
    graph (f)(1) of this AD,  before further flight, repair as  applicable
    following  Chapter 6,  Standard Repair  Procedures,  in  the Ballonbau
    Worner  GmbH  Instructions for  Continued  Airworthiness, Gas  Balloon
    Model NL-STU, Issue 1, dated November 2013.

(3) If on May 27, 2014 (the effective date of this AD),  a balloon has al-
    ready exceeded the threshold compliance time for the porosity test  as
    defined  in  Sections  5.1.1.4, 5.1.2.4  and 5.1.3.4  of Chapter  5 in
    Ballonbau Worner  GmbH Instructions  for Continued  Airworthiness, Gas
    Balloon Model NL-STU, Issue 1, pages 44 through 53 and 55 through  69,
    dated November 2013, and page 54 dated December 2013, within 3  months
    after  May 27,  2014 (the  effective date  of this  AD),  conduct  the
    porosity  test  following  Sections 5.1.1.4,  5.1.2.4  and  5.1.3.4 of
    Chapter  5  in  Ballonbau  Worner  GmbH  Instructions  for   Continued
    Airworthiness, Gas Balloon Model NL-STU, Issue 1, pages 44 through  53
    and 55  through 69,  dated November  2013, and  page 54 dated December
    2013.

(4) After May 27, 2014 (the effective date of this AD), do all inspections
    and  necessary  repairs   following  Technische  Mitteilung   (English
    translation:  Technical  Note)  Ballonbau  Worner  GmbH EASA.BA.009-6,
    dated November  7, 2013;  and Ballonbau  Worner GmbH  Instructions for
    Continued Airworthiness, Gas  Balloon Model NL-STU,  Issue 1, pages  1
    through 6, 8 through 16, 18, 20 through 34, 36 through 40, 42  through
    53, and 55 through 82, dated  November 2013; and pages 7, 17,  19, 35,
    41, and 54, dated December 2013.

Note  1  to  paragraph  (f)  of  this  AD:   Pilots  may  only  accomplish
preventative maintenance limited to those items identified in 14 CFR  Part
43, Appendix A.

(g) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative  Methods  of  Compliance  (AMOCs):  The Manager, Standards
    Office,  FAA,  has the authority to approve AMOCs for this AD,  if re-
    quested using the procedures found in 14 CFR 39.19.  Send  information
    to  ATTN: Karl Schletzbaum,  Aerospace Engineer,  FAA,  Small Airplane
    Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106;  tele-
    phone: (816) 329-4123;  fax: (816) 329-4090;  email: karl.schletzbaum@
    faa.gov.  Before using any approved AMOC on  any airplane to which the
    AMOC applies,  notify your appropriate principal inspector (PI) in the
    FAA Flight Standards District Office (FSDO),  or  lacking  a PI,  your
    local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective
    actions from a manufacturer or other source, use these actions if they
    are FAA-approved.  Corrective actions  are considered  FAA-approved if
    they are approved by the State of Design Authority (or their delegated
    agent). You are required to assure the product is airworthy before  it
    is returned to service.

(h) RELATED INFORMATION

    Refer to  MCAI European  Aviation Safety  Agency (EASA)  AD No.:  2013
    -0293R1, dated  December 17, 2013,  for  related information.  You may
    examine  the  MCAI  on  the Internet at: http://www.regulations.gov/#!
    documentDetail;D=FAA-2014-0041-0002.

(i) 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 the AD specifies otherwise.

(i) Technische Mitteilung (English translation:  Technical Note) Ballonbau
    Worner GmbH EASA.BA.009-6, dated November 7, 2013.

(ii) Ballonbau Worner GmbH Instructions for  Continued Airworthiness,  Gas
     Balloon Model NL-STU, Issue 1, pages  1 through 6, 8 through 16,  18,
     20 through 34, 36 through 40, 42 through 53, and 55 through 82, dated
     November 2013; and pages  7, 17, 19, 35,  41, and 54,  dated December
     2013.

(3) For  Ballonbau Worner GmbH service information identified  in this AD,
    contact  Ballonbau Worner GmbH,  Zirbelstrasse 57c,  D-86154 Augsburg,
    Germany;  telephone: +49 821 4504060;  fax: +49 821 419641;  Internet:
    www.ballonbau.de.

(4) You  may  view  this  service information at the FAA,  Small  Airplane
    Directorate, 901 Locust, Kansas City, Missouri 64106.  For information
    on the availability of this material at the FAA, call (816) 329-4148.

(5) 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 Kansas City, Missouri, on April 4, 2014. Earl Lawrence, Manager,
Small Airplane Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Karl  Schletzbaum,  Aerospace  Engineer,
FAA,  Small  Airplane  Directorate, 901  Locust,  Room  301, Kansas  City,
Missouri 64106;  telephone: (816) 329-4123;  fax:  (816) 329-4090;  email:
karl.schletzbaum@faa.gov.
PREAMBLE 

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

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for
Ballonbau Worner GmbH Models NL-280/STU, NL-380/STU, NL-510/STU,
NL-640/STU, NL-840/STU, and NL-1000/STU balloons. This AD results from
mandatory continuing airworthiness information (MCAI) issued by an
aviation authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as current inspection intervals are no longer adequate to
ensure timely detection of deterioration or damage. We are issuing this
AD to require actions to address the unsafe condition on these
products.

DATES: This AD is effective May 27, 2014.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of May 27, 2014.

ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov by searching for and locating Docket No. FAA-2014-
0041; or in person at Document 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 service information identified in this AD, contact Ballonbau
Worner GmbH, Zirbelstrasse 57c, D-86154 Augsburg, Germany;
telephone: +49 821 4504060; fax: +49 821 419641; Internet:
www.ballonbau.de. You may view this referenced service information at
the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the FAA,
call (816) 329-4148.

FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4123; fax: (816) 329-4090; email:
karl.schletzbaum@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to adding an AD that would apply to Ballonbau Worner GmbH
Model NL-280/STU, NL-380/STU, NL-510/STU, NL-640/STU, NL-840/STU, and
NL-1000/STU airplane. The NPRM was published in the Federal Register on
January 31, 2014 (79 FR 5319). The NPRM proposed to correct an unsafe
condition for the specified products and was based on mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country. The MCAI states:

The results of an analysis of NL-STU maintenance data revealed
that the current inspection intervals are no longer adequate to
ensure timely detection of deterioration or damage, which could
affected the structural integrity of the balloon.
This condition, if not detected and corrected, could lead to
failure of balloon components or envelope, possibly resulting in
loss of the balloon.
To address this potential unsafe condition, Ballonbau
Worner developed new, more detailed and descriptive
Instructions for Continued Airworthiness (at the same time separated
from the Flight Manual) and issued Technische Mitteilung/Technical
Note EASA.BA.009-6 to inform all operators.
For the reasons described above, EASA issued AD 2013-0293 to
require compliance with the updated Instructions for Continued
Airworthiness. This AD is revised to extend the compliance time for
the initial porosity test, for balloons which have already exceeded
the relevant threshold.

The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0041-0002.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 5319, January 31,
2014) or on the determination of the cost to the public.

Conclusion

We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (79 FR 5319, January 31, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 5319, January 31, 2014).

Costs of Compliance

We estimate that this AD will affect 6 products of U.S. registry.
The scope of the inspections may vary depending on the condition of the
balloon. We have no way of knowing how extensive an inspection may be
necessary for each balloon. The scope of damage found in the
inspections could vary significantly from balloon to balloon. We have
no way of determining how much damage may be found on each balloon or
the cost to repair damaged parts on each balloon or the number of
balloons that may require repair.

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 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.

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-2014-
0041; 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 the NPRM, the regulatory evaluation, any comments received,
and other information. The street address for the Docket Office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by adding the following new AD: