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PROPOSED AD GULFSTREAM AEROSPACE LP (FORMERLY ISRAEL AIRCRAFT INDUSTRIES, LTD.): Docket No. FAA-2009-1028; Directorate Identifier 2009-NM-188-AD.
COMMENTS DUE DATE

(a) We must receive comments by December 21, 2009.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD applies to Gulfstream Aerospace LP Model Gulfstream  G150 air-
    planes; certificated in any  category; serial numbers 201  through 233
    inclusive.

SUBJECT

(d) Air Transport Association (ATA) of America Code 25: Equipment/Furnish-
    ings.

REASON

(e) The mandatory continuing airworthiness information (MCAI) states:

IAI  Company  Flammability  tests revealed  that  the  baggage compartment
rubber seals manufactured by Gumiyan  are not compliant with FAR  [Federal
Aviation Regulation] 25, Appendix F, Part I requirements.

The  unsafe condition  is potential  ignition of  the baggage  compartment
rubber seals, which could lead to a larger fire. Required actions  include
inspecting to determine the manufacturer of the baggage compartment rubber
seals and replacing the  baggage compartment rubber seals  manufactured by
Gumiyan, with seals manufactured by Rubbercraft.

ACTIONS AND COMPLIANCE

(f) Unless already done, do the following actions.

(1) Within 12 months after the effective date of this AD, inspect  baggage
    compartment  seals for  manufacturer identification  at Station  12247
    around AFT liner location, at Station 10884 around FWD liner location,
    and at Station 10844 floor  panel adjacent to FWD line,  in accordance
    with the  Accomplishment Instructions  of Gulfstream  Service Bulletin
    150-25-055, dated October 28, 2008.

(2) If during the inspection required by paragraph (f)(1) of this AD,  all
    three seals are found to  be imprinted Rubbercraft, no further  action
    is required by this AD.

(3) If during the inspection required  by paragraph (f)(1) of this AD  any
    seal is found  to be imprinted  Gumiyan, or any  imprint is illegible,
    replace  the affected  seals before  further flight  with  Rubbercraft
    manufactured seals, in accordance with the Accomplishment Instructions
    of Gulfstream Service Bulletin 150-25- 055, dated October 28, 2008.

FAA AD DIFFERENCES

NOTE 1: This  AD differs  from the  MCAI  and/or  service  information  as
follows: No differences.

OTHER FAA AD PROVISIONS

(g) 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. Send  information to  Attn:  Mike
    Borfitz, Aerospace Engineer, International Branch, ANM-116,  Transport
    Airplane Directorate, FAA, 1601  Lind Avenue, SW., Renton,  Washington
    98057-3356; telephone (425) 227-2677; fax (425) 227-1149. Before using
    any approved AMOC  on any airplane  to which the  AMOC applies, notify
    your  principal  maintenance  inspector  (PMI)  or  principal avionics
    inspector (PAI),  as appropriate,  or lacking  a principal  inspector,
    your local Flight Standards District Office. The AMOC approval  letter
    must specifically reference this AD.

(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.

(3) Reporting Requirements: For any reporting  requirement in this AD, un-
    der  the provisions  of the  Paperwork  Reduction  Act, the  Office of
    Management and  Budget (OMB)  has approved  the information collection
    requirements and has assigned OMB Control Number 2120- 0056.

RELATED INFORMATION

(h) Refer to Civil Aviation Authority of Israel (CAAI)  Airworthiness Dir-
    ective 25-04-05-09R1, dated November 12, 2008; and Gulfstream  Service
    Bulletin 150-25-055, dated October 28, 2008; for related  information.

Issued in Renton, Washington, on October 28, 2009. Stephen P. Boyd, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by December 21, 2009.
PREAMBLE 
DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

14 CFR Part 39

[Docket  No.  FAA-2009-1028;  Directorate  Identifier  2009-NM-188-AD] RIN
2120-AA64

AIRWORTHINESS DIRECTIVES; Gulfstream  Aerospace  LP Model  Gulfstream G150
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose  to adopt a  new airworthiness directive  (AD) for the
products listed above. This proposed AD results from 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:  IAI   Company
Flammability  tests revealed  that the  baggage compartment  rubber  seals
manufactured  by  Gumiyan are  not  compliant with  FAR  [Federal Aviation
Regulation] 25, Appendix F, Part I requirements.

The  unsafe condition  is potential  ignition of  the baggage  compartment
rubber seals, which  could lead to  a larger fire.  The proposed AD  would
require  actions  that  are  intended  to  address  the  unsafe  condition
described in the MCAI.

DATES: We must receive comments on this proposed AD by December 21, 2009.

ADDRESSES: You may send comments by any of the following methods:

Federal eRulemaking Portal: Go to  http://www.regulations.gov.  Follow the
instructions for submitting comments.

Fax: (202) 493-2251.

Mail: U.S.  Department of  Transportation, Docket  Operations, M-30,  West
Building  Ground  Floor,  Room  W12-140,  1200  New  Jersey  Avenue,  SE.,
Washington, DC 20590.

Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30,
West Building  Ground Floor,  Room W12-40,  1200 New  Jersey Avenue,  SE.,
Washington, DC, between 9 a.m.  and 5 p.m., Monday through  Friday, except
Federal holidays.

For service information identified in this proposed AD, contact Gulfstream
Aerospace Corporation, P.O. Box 2206, Mail Station D-25, Savannah, Georgia
31402-2206;    telephone    800-810-4853;    fax    912-965-3520;   e-mail
pubs@gulfstream.com; Internet   http://www.gulfstream.com/product_support/
technical_pubs/pubs/index.htm.  You may  review copies  of the  referenced
service information at the FAA, Transport Airplane Directorate, 1601  Lind
Avenue, SW., Renton,  Washington. For information  on the availability  of
this material at the FAA, call 425-227-1221 or 425-227-1152.

EXAMINING THE AD DOCKET

You may examine the AD docket  on the Internet at  http://www.regulations.
gov; or in  person at the  Docket Operations office  between 9 a.m.  and 5
p.m.,  Monday  through  Friday, except  Federal  holidays.  The AD  docket
contains  this  proposed  AD,  the  regulatory  evaluation,  any  comments
received,  and  other  information.  The  street  address  for  the Docket
Operations office (telephone (800) 647-5527) is in the ADDRESSES  section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace  Engineer, Inter-
national Branch, ANM-116, Transport  Airplane Directorate, FAA, 1601  Lind
Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-2677;  fax
(425) 227-1149.

SUPPLEMENTARY INFORMATION:

COMMENTS INVITED

We invite you to send any written relevant data, views, or arguments about
this  proposed AD.  Send your  comments to  an address  listed under   the
ADDRESSES  section.   Include  "Docket   No.  FAA-2009-1028;   Directorate
Identifier  2009-NM-188-AD"  at  the   beginning  of  your  comments.   We
specifically  invite  comments   on  the  overall   regulatory,  economic,
environmental, and energy  aspects of this  proposed AD. We  will consider
all comments received by the closing  date and may amend this proposed  AD
based on those comments.

We have lengthened the 30-day comment period for proposed ADs that address
MCAI  originated by  aviation authorities  of other  countries to  provide
adequate  time  for interested  parties  to submit  comments.  The comment
period  for  these  proposed  ADs  is  now  typically  45  days,  which is
consistent with the comment period for domestic transport ADs.

We  will  post  all  comments  we  receive,  without  change,  to  http://
www.regulations.gov, including  any personal  information you  provide. We
will also  post a  report summarizing  each substantive  verbal contact we
receive about this proposed AD.

DISCUSSION

The  Civil Aviation  Authority of  Israel (CAAI),  which is  the  aviation
authority for  Israel, has  issued CAAI  Airworthiness Directive  25-04-05
-09R1, dated November 12, 2008 (referred to after this as "the MCAI"),  to
correct an unsafe condition for the specified products. The MCAI states:

IAI  Company  Flammability  tests revealed  that  the  baggage compartment
rubber seals manufactured by Gumiyan  are not compliant with FAR  [Federal
Aviation Regulation] 25, Appendix F, Part I requirements.

The  unsafe condition  is potential  ignition of  the baggage  compartment
rubber seals, which could lead to a larger fire. Required actions  include
inspecting to determine the manufacturer of the baggage compartment rubber
seals and replacing the  baggage compartment rubber seals  manufactured by
Gumiyan, with seals  manufactured by Rubbercraft.  You may obtain  further
information by examining the MCAI in the AD docket.

RELEVANT SERVICE INFORMATION

Gulfstream  Aerospace LP  has issued  Service Bulletin  150-25-055,  dated
October 28, 2008.  The actions described  in this service  information are
intended to correct the unsafe condition identified in the MCAI.

FAA'S DETERMINATION AND REQUIREMENTS OF THIS PROPOSED AD

This  product  has been  approved  by the  aviation  authority of  another
country, and is approved for  operation in the United States.  Pursuant to
our bilateral agreement with the  State of Design Authority, we  have been
notified  of  the  unsafe  condition described  in  the  MCAI  and service
information  referenced  above.  We  are  proposing  this  AD  because  we
evaluated all  pertinent information  and determined  an unsafe  condition
exists and is  likely to exist  or develop on  other products of  the same
type design.

DIFFERENCES BETWEEN THIS AD AND THE MCAI OR SERVICE INFORMATION

We have reviewed the MCAI and related service information and, in general,
agree with their substance.  But we might have  found it necessary to  use
different words from those in the MCAI to ensure the AD is clear for  U.S.
operators and is enforceable. In making these changes, we do not intend to
differ substantively from the information provided in the MCAI and related
service information.

We might also have proposed different actions in this AD from those in the
MCAI in order to follow FAA policies. Any such differences are highlighted
in a NOTE within the proposed AD.

COSTS OF COMPLIANCE

Based on the service information, we estimate that this proposed AD  would
affect about 33 products of U.S. registry. We also estimate that it  would
take about 10 work-hours per product to comply with the basic requirements
of this proposed AD. The average labor rate is $80 per work-hour. Required
parts would cost about $0 per product. Where the service information lists
required parts costs that are covered under warranty, we have assumed that
there will be  no charge for  these costs. As  we do not  control warranty
coverage for affected  parties, some parties  may incur costs  higher than
estimated  here. Based  on these  figures, we  estimate  the  cost of  the
proposed AD on U.S. operators to be $26,400, or $800 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 proposed AD would not have federalism implications
under Executive Order 13132. This proposed AD would 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 proposed regulation:

1. Is not a "significant regulatory action" under Executive Order 12866;

2. Is not a "significant rule" under the DOT Regulatory Policies and Proc-
   edures (44 FR 11034, February 26, 1979); and

3. 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.

We prepared a regulatory evaluation of the estimated costs to comply  with
this proposed AD and placed it in the AD docket.

LIST OF SUBJECTS IN 14 CFR PART 39

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

THE PROPOSED AMENDMENT

Accordingly, under the authority delegated to me by the Administrator, the
FAA proposes to amend 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: