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PROPOSED AD EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Docket No. FAA-2008-0416; Directorate Identifier 2007-NM-297-AD.
COMMENTS DUE DATE

(a) We must receive comments by May 29, 2008.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD applies to EMBRAER Model EMB-135BJ airplanes, certificated  in
    any category, serial numbers  145363, 145412, 145462, 145484,  145495,
    145505,  145516,  145528,  145540,  145549,  145555,  145586,  145591,
    145625,  145637,  145642,  145644,  145678,  145686,  145699,  145706,
    145711,  145717,  145730,  145770,  145775,  145780,  145789,  145796,
    14500802, and 14500809.

SUBJECT

(d) Air Transport Association (ATA) of America Code 27: Flight Controls.

REASON

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

It has been found the occurrence of cable guard pins not installed in  the
aileron control system, which may  lead to jamming of the  aileron control
cables, reducing the aircraft controllability.

The  corrective actions  include inspecting  for possible  absence of  the
cable  guard pins  in the  aileron control  system inside  the wings,  and
installing new ones bearing the same part number.

ACTIONS AND COMPLIANCE

(f) Within 270 calendar days after  the effective date of this AD,  unless
    already done, do the following actions.

(1) Do  a detailed  inspection with  the aid  of a  borescope for possible
    absence of the cable guard  pins in the aileron control  system inside
    the wings.

(i) If any cable guard  pin having part number (P/N)  NAS427K8, NAS427K28,
    or NAS427K36 is  missing in the  internal part of  the left and  right
    halfwing spar boxes, before further flight, install a new one  bearing
    the  same part  number, in  accordance with  EMBRAER Service  Bulletin
    145LEG-27-0023, dated January 24, 2006.

(ii) If any  cable  guard  pin  P/N  NAS427K26 is  missing in  the aileron
     control cable pulleys in the  internal part of the wing  leading edge
     III, before further flight, remove the corresponding leading edge and
     install  a new  cable  guard  pin bearing  the same  part number,  in
     accordance  with  EMBRAER  Service  Bulletin  145LEG-27-0023,   dated
     January 24, 2006.

FAA AD DIFFERENCES

NOTE: This AD differs from the MCAI and/or service information as follows:

The  MCAI  includes  airplanes  in  addition  to  those  specified  in the
applicability of  this AD.  Those airplanes  are not  included in  this AD
because they are modified by Supplemental Type Certificates (STC) that are
not  FAA-approved.  This AD  includes  only the  U.S.  certified airplanes
identified in the referenced service information.

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: Sanjay
    Ralhan, Aerospace Engineer,  International Branch, ANM-116,  Transport
    Airplane Directorate,  FAA, 1601  Lind Avenue  SW., Renton, Washington
    98057-3356; telephone (425) 227-1405; fax (425) 227-1149. 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 ensure the product is airworthy before  it
    is returned to service.

(3) Reporting Requirements: For  any  reporting  requirement in  this  AD,
    under 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 MCAI Brazilian Airworthiness Directive 2006-07-01,  effective
    July 31,  2006; and  EMBRAER Service  Bulletin 145LEG-27-  0023, dated
    January 24, 2006; for related information.

Issued in  Renton, Washington,  on April  18, 2008.  Ali Bahrami, Manager,
Transport Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by May 29, 2008.
PREAMBLE 
DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

14 CFR Part 39

[Docket  No.  FAA-2008-0416;  Directorate  Identifier  2007-NM-297-AD] RIN
2120-AA64

AIRWORTHINESS DIRECTIVES; Empresa Brasileira de Aeronautica S.A. (EMBRAER)
Model EMB-135BJ 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:

It has been found the occurrence of cable guard pins not installed in  the
aileron control system, which may  lead to jamming of the  aileron control
cables, reducing the aircraft controllability.

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 May 29, 2008.

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.

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: Sanjay Ralhan, Aerospace Engineer, Inter-
national Branch, ANM-116, Transport  Airplane Directorate, FAA, 1601  Lind
Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1405;  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-2008-0416;   Directorate
Identifier  2007-NM-297-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  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 Agencia Nacional de  Avia[ccedil][atilde]o Civil (ANAC), which  is the
aviation  authority  for   Brazil,  has  issued   Brazilian  Airworthiness
Directive 2006-07-01, effective July 31,  2006 (referred to after this  as
"the MCAI"), to  correct an unsafe  condition for the  specified products.
The MCAI states:

It has been found the occurrence of cable guard pins not installed in  the
aileron control system, which may  lead to jamming of the  aileron control
cables, reducing the aircraft controllability.

The  corrective actions  include inspecting  for possible  absence of  the
cable  guard pins  in the  aileron control  system inside  the wings,  and
installing new ones bearing the  same part number. You may  obtain further
information by examining the MCAI in the AD docket.

RELEVANT SERVICE INFORMATION

EMBRAER  has issued  Service Bulletin  145LEG-27-0023, dated  January  24,
2006. 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 13 products of U.S. registry. We also estimate that it  would
take about 2 work-hours per product to comply with the basic  requirements
of this proposed AD. The average labor rate is $80 per work-hour. Based on
these figures, we estimate the cost  of the proposed AD on U.S.  operators
to be $2,080, or $160 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
   Procedures (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, 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: