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2017-21-04 GULFSTREAM AEROSPACE LP (TYPE CERTIFICATE PREVIOUSLY HELD BY ISRAEL AIRCRAFT INDUSTRIES, LTD.):
Amendment 39-19075; Docket No. FAA-2017-0692; Product Identifier 2017-NM-043-AD.

(a) EFFECTIVE DATE

    This AD is effective November 27, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to  Gulfstream Aerospace LP Model Gulfstream G150 air-
    planes,  certificated in any category,  serial numbers 201 through 318
    inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 52, Doors.

(e) REASON

    This AD was prompted by a report indicating  that  the  main  entrance
    door (MED)  opened during  flight, and  by the  determination that the
    "CABIN DOOR UNLOCK" crew alerting system (CAS) message may  extinguish
    before the handle latch pin is  fully engaged. We are issuing this  AD
    to prevent  the MED  from opening  during flight,  which could lead to
    structural damage and loss of control of the airplane.

(f) COMPLIANCE

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

(g) RIGGING PROCEDURE

    Within 12 months after the effective date of this AD:  Do  an  updated
    rigging procedure for adjustment of the MED microswitch, in accordance
    with  the  Accomplishment  Instructions  of  Gulfstream  G150  Service
    Bulletin 150-52-188, dated January 15, 2016.

(h) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Section, Transport Standards Branch, FAA, has the authority to approve
    AMOCs for this AD, if requested  using the procedures found in 14  CFR
    39.19. In  accordance with  14 CFR  39.19, send  your request  to your
    principal  inspector  or  local Flight  Standards District  Office, as
    appropriate.  If  sending information  directly  to the  International
    Section,  send  it  to  the  attention  of  the  person  identified in
    paragraph (i)(2)  of this  AD. Information  may be  emailed to: 9-ANM-
    116-AMOC-REQUESTS@faa.gov. 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.

(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
    Section,  Transport  Standards  Branch,  FAA;  or  the  Civil Aviation
    Authority  of Israel  (CAAI); or  the CAAI's  authorized Designee.  If
    approved  by  the  CAAI  Designee,  the  approval  must  include   the
    Designee's authorized signature.

(i) RELATED INFORMATION

(1) Refer  to  Mandatory Continuing Airworthiness Information  (MCAI) CAAI
    Airworthiness Directive  ISR-I-52-2017-03-28,  dated  January 3, 2017,
    for related information. This  MCAI may be found  in the AD docket  on
    the  Internet  at  http://www.regulations.gov  by  searching  for  and
    locating Docket No. FAA-2017-0692.

(2) For more information about this AD,  contact Tom Rodriguez,  Aerospace
    Engineer, International Section, Transport Standards Branch, FAA, 1601
    Lind Avenue SW., Renton, WA 98057-3356;  telephone  425-227-1137;  fax
    425-227-1149.

(j) 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.

(i) Gulfstream G150 Service Bulletin 150-52-188, dated January 15, 2016.

(ii) Reserved.

(3) For  service information identified  in  this  AD,  contact Gulfstream
    Aerospace Corporation,  P.O. Box 2206, Mail Station D-25, 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 the FAA,  Transport Standards
    Branch, 1601 Lind Avenue SW, Renton, WA. For information on the avail-
    ability 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 October 11, 2017. Jeffrey E Duven, Direc-
tor, System Oversight Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Inter-
national Section,  Transport Standards Branch,  FAA, 1601 Lind Avenue SW.,
Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0692; Product Identifier 2017-NM-043-AD;
Amendment 39-19075; AD 2017-21-04]
RIN 2120-AA64

Airworthiness Directives; Gulfstream Aerospace LP (Type
Certificate Previously Held by Israel Aircraft Industries, Ltd.)
Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Gulfstream Aerospace LP Model Gulfstream G150 airplanes. This AD was
prompted by a report indicating that the main entrance door (MED)
opened during flight, and by the determination that the ``CABIN DOOR
UNLOCK'' crew alerting system (CAS) message may extinguish before the
handle latch pin is fully engaged. This AD requires accomplishing an
updated rigging procedure for the adjustment of the MED microswitch. We
are issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective November 27, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 27,
2017.

ADDRESSES: For service information identified in this final rule,
contact Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station
D-25, 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
Standards Branch, 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-2017-0692.

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-2017-
0692; 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 street 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: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 1601 Lind
Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-
1149.

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 LP Model Gulfstream G150 airplanes. The NPRM published in the
Federal Register on July 17, 2017 (82 FR 32656) (``the NPRM'').
The Civil Aviation Authority of Israel (CAAI), which is the
aviation authority for Israel, has issued Israeli Airworthiness
Directive ISR-I-52-2017-03-28, dated January 3, 2017 (referred to after
this as the Mandatory Continuing Airworthiness Information, or ``the
MCAI''), to correct an unsafe condition for certain Gulfstream
Aerospace LP Model Gulfstream G150 airplanes. The MCAI states:

[The purpose of the Israeli AD is] to improve the Main Entrance
Door (MED) microswitch adjustment procedure so that the locking
indication will be extinguished when the door handle is locked.

The required actions include accomplishing an updated rigging
procedure for the adjustment of the MED microswitch. The unsafe
condition is the in-flight opening of the MED, which could lead to
structural damage and loss of control 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-2017-0692.

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

Gulfstream Aerospace LP has issued Gulfstream G150 Service Bulletin
150-52-188, dated January 15, 2016. The service information describes
an updated rigging procedure for the adjustment of the MED microswitch.
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 65 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
MED microswitch adjustment 6 work-hours x $85 per hour = $510 $3 $513 $33,345

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes to
the Director of the System Oversight Division.

Regulatory Findings

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

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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):