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2014-20-12 ALEXANDRIA AIRCRAFT LLC:
Amendment 39-17985; Docket No. FAA-2014-0438; Directorate Identifier 2014-CE-015-AD.

(a) EFFECTIVE DATE

    This AD is effective November 12, 2014.

(b) AFFECTED ADS

    This  AD  supersedes  AD 75-20-06,  Amendment  39-2372  (40 FR  43484,
    September 22, 1975, ("AD 75-20-06")).

(c) APPLICABILITY

    This  AD  applies  to   Alexandria  Aircraft  LLC  (type   certificate
    previously held by Bellanca Aircraft Corp., Viking Aviation, Inc., and
    Bellanca,  Inc.)  Models  14-19-3A, 17-30,  17-30A, 17-31,  17-31A, 17
    -31ATC, and 17-31TC airplanes, all serial numbers (S/Ns), certificated
    in any category.

(d) SUBJECT

    Joint Aircraft System Component (JASC)/Air Transport Association (ATA)
    of America Code 53, Fuselage.

(e) UNSAFE CONDITION

    This AD was prompted by reports  that cracks are still being found  in
    the vertical side fuselage tube (fuselage station 7) in the area  near
    the upper fuselage  longeron on airplanes  that have had  Bellanca Kit
    SK1234789-0004  installed,  which  is  a  terminating  action  for the
    repetitive inspections required in AD 75-20-06. We are issuing this AD
    to detect  and correct  cracks in  either vertical  side fuselage tube
    (F.S.  7),  which  is  adjacent  to  the  horizontal  stabilizer carry
    -through, in  the area  near the  upper fuselage  longeron to  prevent
    failure of the horizontal stabilizer. This failure could cause reduced
    structural integrity of the fuselage and result in loss of control.

(f) COMPLIANCE

    Comply  with  this  AD  within  the  compliance  times  specified   in
    paragraphs (g) through (h) of this AD, unless already done.

(g) INSPECTION

(1) Models 14-19-3A and 17-31A, S/Ns 32-15 through 76-32-163; Models 17-30
    and 17-30A, S/Ns  30263 through 76-30811;  and Models 17-31,  17-31TC,
    and  17-31ATC,  S/Ns  30004,  and  31004  through  76-31124 (airplanes
    previously affected by  AD 75-20-06): Within  the next 100  hours time
    -in-service (TIS) after the  last inspection completed by  AD 75-20-06
    or within the next 25 hours TIS after November 12, 2014 (the effective
    date of this AD), whichever occurs later, and repetitively  thereafter
    at intervals  not to  exceed 100  hours TIS,  visually inspect the aft
    fuselage truss for cracks as  specified in paragraph 4. INSPECTION  of
    Alexandria Aircraft LLC Bellanca Service Letter 85, Revision B,  dated
    April 8, 2004.

(2) Models 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31ATC,  and  17-31TC
    airplanes, all  S/Ns not  referenced in  paragraph (g)(1)  of this  AD
    (airplanes not previously affected by AD 75-20-06): Before or upon the
    accumulation of 300 hours  TIS or within the  next 25 hours TIS  after
    November 12, 2014  (the effective date  of this AD),  whichever occurs
    later,  and repetitively  thereafter at  intervals not  to exceed  100
    hours  TIS,  visually  inspect the  aft fuselage  truss for  cracks as
    specified  in  paragraph  4.  INSPECTION  of  Alexandria  Aircraft LLC
    Bellanca Service Letter 85, Revision B, dated April 8, 2004.

(h) REPLACEMENT

    If  cracks  are found  during  any inspection  required  by paragraphs
    (g)(1)  and (g)(2)  of this  AD,  before  further flight,  replace the
    cracked  parts  with  FAA-approved  zero-time  parts  as  specified in
    paragraph 5. REPAIR of Alexandria Aircraft LLC Bellanca Service Letter
    85, Revision B, dated April 8, 2004.

(i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, Chicago Aircraft Certification Office (ACO), 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 manager  of the ACO, send  it to the attention  of the
    person identified in paragraph (j) of this AD.

(2) 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.

(3) AMOCs  approved  for  AD  75-20-06,  Amendment  39-2372  (40 FR 43484,
    September 22, 1975)  are not approved  as AMOCs for  the corresponding
    provisions of this AD.

(j) RELATED INFORMATION

    For  more  information  about  this  AD,  Steven  Rosenfeld, Aerospace
    Engineer, FAA,  Chicago ACO,  2300 East  Devon Avenue,  Room 107,  Des
    Plaines, IL 60018; phone: (847) 294-7030; fax: (847) 294-7834;  email:
    steven.rosenfeld@faa.gov.

(k) 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) Alexandria Aircraft LLC Bellanca Service Letter 85, Revision B,  dated
    April 8, 2004.

(ii) Reserved.

(3) For Alexandria Aircraft LLC service information identified in this AD,
    contact Alexandria Aircraft LLC,  2504 Aga Drive, Alexandria, MN 5630;
    phone: (320) 763-4088;  fax: (320) 763-4095;  Internet:  www.bellanca-
    aircraft.com; email: partsales@bellanca-aircraft.com.

(4) You  may  view  this  service  information  at  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 September 26, 2014. Kelly A. Broadway,
Acting Manager, Small Airplane Directorate, Aircraft Certification Service

FOR FURTHER INFORMATION CONTACT:  Steven  Rosenfeld,  Aerospace  Engineer,
FAA,  Chicago Aircraft Certification Office,  2300 East Devon Avenue, Room
107, Des Plaines, IL 60018;  phone: (847) 294-7030;  fax:  (847) 294-7834;
email: steven.rosenfeld@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0438; Directorate Identifier 2014-CE-015-AD;
Amendment 39-17985; AD 2014-20-12]
RIN 2120-AA64

Airworthiness Directives; Alexandria Aircraft LLC Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: We are superseding Airworthiness Directive (AD) 75-20-06 for
certain Alexandria Aircraft LLC (type certificate previously held by
Bellanca Aircraft Corp., Viking Aviation, Inc., and Bellanca, Inc.)
Models 14-19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31ATC, and 17-31TC
airplanes. AD 75-20-06 required repetitively inspecting the aft
fuselage structure near the top of the vertical side tubing, which
connects the horizontal stabilizer carry-through to the upper fuselage
longeron, for cracks and installing the manufacturer's service repair
kit as a terminating action for the repetitive inspections to repair
any cracks found. Since we issued AD 75-20-06, we have determined that
installing the service kit has not prevented cracks from occurring. We
have also determined that all affected airplane serial numbers should
be included in the Applicability section. This AD requires continued
repetitive inspections of the aft fuselage structure near the top of
the vertical side tubing for cracks and making all necessary
replacements of cracked parts. This AD also adds additional serial
number airplanes to the Applicability section. We are issuing this AD
to correct the unsafe condition on these products.

DATES: This AD is effective November 12, 2014 November 12, 2014.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 12,
2014.

ADDRESSES: For service information identified in this AD, contact
Alexandria Aircraft LLC, 2504 Aga Drive, Alexandria, MN 5630; phone:
(320) 763-4088; fax: (320) 763-4095; Internet: www.bellanca-
aircraft.com; email: aircraft.com">partsales@bellanca-aircraft.com. 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.

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-
0438; 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 (phone: 800-647-
5527) is 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 FURTHER INFORMATION CONTACT
: Steven Rosenfeld, Aerospace Engineer,
FAA, Chicago Aircraft Certification Office, 2300 East Devon Avenue,
Room 107, Des Plaines, IL 60018; phone: (847) 294-7030; fax: (847) 294-
7834; email: steven.rosenfeld@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 75-20-06, Amendment 39-2372 (40 FR 43484,
September 22, 1975, (``AD 75-20-06''). AD 75-20-06 applied to certain
Alexandria Aircraft LLC (type certificate previously held by Bellanca
Aircraft Corp., Viking Aviation, Inc., and Bellanca, Inc.) Models 14-
19-3A, 17-30, 17-30A, 17-31, 17-31A, 17-31ATC, and 17-31TC airplanes.
The NPRM published in the Federal Register on July 2, 2014 (79 FR
37679). The NPRM was prompted by reports that cracks are still being
found in the vertical side fuselage tube (F.S. 7) in the area near the
upper fuselage longeron on airplanes that have had Bellanca Kit
SK1234789-0004 installed, which is a terminating action for the
repetitive inspections required in AD 75-20-06. The NPRM proposed to
retain the inspection requirements of AD 75-20-06, remove the
terminating action allowed in AD 75-20-06, and change the applicability
to include all serial numbers. We are issuing this AD to correct the
unsafe condition on these products.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 37679, July 2,
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 this AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (79 FR 37679, July 2, 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 37679, July 2, 2014).

Costs of Compliance

We estimate that this AD affects 847 airplanes of U.S. registry.

We estimate the following costs to comply with this AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S.
operators
Inspecting the horizontal stabilizer fuselage attachment tube and carry-thru tube support bracket (retained actions from AD 75-20-06). 1 work-hour x $85 per hour = $85
Not applicable
$85 $71,995

We estimate the following costs to do any necessary replacements
that will be required based on the results of the inspection. We have
no way of determining the number of aircraft that might need these
replacements:

On-Condition Costs

Action
Labor cost
Parts cost
Cost per
product
Replacement of the horizontal stabilizer fuselage attachment tube and carry-thru tube support bracket. 30 work-hours x $85 per hour = $2,550 $575 $3,125

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 have 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 DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by removing Airworthiness Directive (AD)
75-20-06, Amendment 39-2372 (40 FR 43484, September 22, 1975), and
adding the following new AD: