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2017-04-01 GULFSTREAM AEROSPACE CORPORATION: Amendment 39-18796; Docket No. FAA-2016-9191; Directorate Identifier 2016-NM-106-AD.
(a) EFFECTIVE DATE

    This AD is effective March 28, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to  Gulfstream Aerospace Corporation Model GVI air-
    planes, certificated in any category, serial numbers 6001 through 6164
    inclusive.

Note 1 to paragraph (c) of this AD:  Model GVI airplanes are also referred
to by marketing designations G650 and G650ER.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 27; Flight controls.

(e) UNSAFE CONDITION

    This AD  was prompted  by a  report indicating  that there  are design
    deficiencies in the  software used for  monitoring the disconnect  for
    the  flight control  computer (FCC)-hosted  flight controls  actuation
    main  ram  linear  variable  differential  transducer  (LVDT).  We are
    issuing this AD to prevent undetected actuation of the main ram  LVDT.
    Undetected actuation  of the  main ram  LVDT, if  not corrected, could
    result in mechanical  failure of the  flight control surface  actuator
    mechanism  under  force fight  (the  actuator is  working  against the
    intended  load  forces),  causing  primary  surface  hardover, spoiler
    hardover, and loss of control of the airplane.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) SOFTWARE UPDATE FOR FCC

    Within  24 months  after the  effective date  of this  AD,  do  an FCC
    software update, in accordance  with the Modification Instructions  of
    Gulfstream G650 Aircraft  Service Change 037,  Revision A, dated  June
    28, 2016;  or Gulfstream G650ER Aircraft Service Change 037,  Revision
    A, dated June 28, 2016; as applicable.

(h) REPORTING NOT REQUIRED

    Although Gulfstream G650 Aircraft Service Change 037 Revision A, dated
    June 28, 2016;  and Gulfstream  G650ER Aircraft  Service  Change  037,
    Revision A, dated June 28, 2016; specify to submit certain information
    to the manufacturer, this AD does not require that action.

(i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, Atlanta 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 in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(j) RELATED INFORMATION

    For more information about this AD,  contact Myles Jalalian, Aerospace
    Engineer,  Systems and Equipment Branch,  ACE-119A,  FAA, Atlanta ACO,
    1701 Columbia Avenue, College Park, GA 30337; phone: 404-474-5572; fax
    404-474-5606; email: Myles.Jalalian@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) Gulfstream G650 Aircraft Service Change 037 Revision A, dated June 28,
    2016.

(ii) Gulfstream G650ER Aircraft Service Change 037, Revision A, dated June
     28, 2016.

(3) For  service information  identified  in this AD,  contact  Gulfstream
    Aerospace  Corporation,  Technical Publications Dept.,  P.O. Box 2206,
    Savannah, GA 31402-2206;  telephone: 800-810-4853;  fax: 912-965-3520;
    email: pubs@gulfstream.com; Internet http://www.gulfstream.com/product
    _support/technical_pubs/pubs/index.htm.

(4) You  may  view  this  service information at 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.

(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  Renton,  Washington,  on  February 2, 2017.  Michael Kaszycki,
Acting  Manager,  Transport Airplane  Directorate,  Aircraft Certification
Service.

FOR  FURTHER  INFORMATION  CONTACT:  Myles Jalalian,  Aerospace  Engineer,
Systems and Equipment Branch, ACE-119A, FAA Atlanta Aircraft Certification
Office (ACO), 1701 Columbia Avenue, College Park, GA 30337; phone: 404-474
-5572; fax: 404-474-5606; email: Myles.Jalalian@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-9191; Directorate Identifier 2016-NM-106-AD;
Amendment 39-18796; AD 2017-04-01]
RIN 2120-AA64

Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Gulfstream Aerospace Corporation Model GVI airplanes. This AD was
prompted by a report indicating that there are design deficiencies in
the software used for monitoring the disconnect for the flight control
computer (FCC)-hosted flight controls actuation main ram linear
variable differential transducer (LVDT). This AD requires an update of
the FCC software. We are issuing this AD to address the unsafe
condition on these products.

DATES: This AD is effective March 28, 2017.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 28, 2017.

ADDRESSES: For service information identified in this final rule,
contact Gulfstream Aerospace Corporation, Technical Publications Dept.,
P.O. Box 2206, Savannah, GA 31402-2206; telephone: 800-810-4853; fax:
912-965-3520; email: pubs@gulfstream.com; Internet: http://www.gulfstream.com/product_support/technical_pubs/pubs/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-2016-9191.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2016-
9191; 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 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: Myles Jalalian, Aerospace Engineer,
Systems and Equipment Branch, ACE-119A, FAA, Atlanta Aircraft
Certification Office (ACO), 1701 Columbia Avenue, College Park, GA
30337; phone: 404-474-5572; fax: 404-474-5606; email:
Myles.Jalalian@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Gulfstream
Aerospace Corporation Model GVI airplanes. The NPRM published in the
Federal Register on November 15, 2016 (81 FR 80009). The NPRM was
prompted by a report indicating that there are design deficiencies in
the software used for monitoring the disconnect for the FCC-hosted
flight controls actuation main ram LVDT. The NPRM proposed to require
an update of the FCC software. We are issuing this AD to prevent
undetected actuation of the main ram LVDT. Undetected actuation of the
main ram LVDT, if not corrected, could result in mechanical failure of
the flight control surface actuator mechanism under force fight (the
actuator is working against the intended load forces), causing primary
surface hardover, spoiler hardover, and loss of control of the
airplane.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion

We reviewed the 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 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 Gulfstream G650 Aircraft Service Change Number 037,
Revision A, dated June 28, 2016; and Gulfstream G650ER Aircraft Service
Change Number 037, Revision A, dated June 28, 2016. The service
information describes procedures for doing an update of the FCC
software. This service information is distinct because it applies to
different airplanes. 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 90 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
Software update 57 work-hours x $85 per hour = $4,845
$9,126
$13,971
$1,257,390

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.

Regulatory Findings

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 adding the following new airworthiness
directive (AD):