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PROPOSED AD EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Docket No. FAA-2008-0194; Directorate Identifier 2007-NM-263-AD.
COMMENTS DUE DATE

(a) We must receive comments by May 27, 2008.

AFFECTED ADS

(b) None.

APPLICABILITY

(c) This AD applies to all EMBRAER Model EMB-135BJ airplanes, certificated
    in any category.

NOTE 1:  This  AD  requires  revisions  to  certain  operator  maintenance
documents to include new inspections. Compliance with these inspections is
required by  14 CFR  91.403(c). For  airplanes that  have been  previously
modified,  altered,  or   repaired  in  the   areas  addressed  by   these
inspections, the operator  may not be  able to accomplish  the inspections
described  in the  revisions. In  this situation,  to comply  with 14  CFR
91.403(c), the operator must request approval for an alternative method of
compliance  according to  paragraph (g)  of this  AD.  The  request should
include a  description of  changes to  the required  inspections that will
ensure the continued operational safety of the airplane.

SUBJECT

(d) Air Transport Association (ATA) of America Code 28: Fuel.

REASON

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

    Fuel system  reassessment,  performed  according to  RBHA-E88/SFAR-88,
    requires the inclusion of new maintenance tasks in the Critical Design
    Configuration  Control  Limitations  (CDCCL) and  in  the  Fuel System
    Limitations (FSL), necessary to preclude ignition sources in the  fuel
    system. * * *

    The  corrective  action  is  revising  the  Airworthiness  Limitations
    Section (ALS) of the Instructions for Continued Airworthiness (ICA) to
    incorporate new limitations for fuel tank systems.

ACTIONS AND COMPLIANCE

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

(1) The term  "MPG," as  used in  this AD,  means  the  EMBRAER Legacy  BJ
    Maintenance Planning Guide (MPG) MPG-1483, Revision 5, dated March 22,
    2007.

(2) Before December  16, 2008, revise  the ALS of  the ICA to  incorporate
    Section A2.5.2,  Fuel System  Limitation Items,  of Appendix  2 of the
    MPG. For all tasks identified in  Section A2.5.2 of Appendix 2 of  the
    MPG,  the initial  compliance times  start from  the applicable  times
    specified in Table 1 of  this AD; and the repetitive  inspections must
    be accomplished thereafter at the interval specified in section A2.5.2
    of Appendix 2 of the MPG, except as provided by paragraphs (f)(4)  and
    (g) of this AD.

                                TABLE 1.--INITIAL INSPECTIONS
------------------------------------------------------------------------------------------------
                                                  COMPLIANCE TIME  (WHICHEVER OCCURS LATER)
   REFERENCE NO.           DESCRIPTION       -------------------------------------------------
                                                     THRESHOLD               GRACE PERIOD
------------------------------------------------------------------------------------------------
28-11-00-720-001-A00..  Functionally Check       Before the accumulation  Within 90 days after
                         critical bonding         of 30,000 total flight   the effective date of
                         integrity of selected    hours.                   this AD.
                         conduits inside the
                         wing tank, Fuel Pump
                         and FQIS connectors at
                         tank wall by
                         conductivity
                         measurements.
28-13-01-720-002-A00..  Functionally Check Aft   Before the accumulation  Within 90 days after
                         Fuel tank critical       of 30,000 total flight   the effective date of
                         bonding integrity of     hours.                   this AD.
                         Fuel Pump, FQGS and
                         Low Level SW
                         connectors at tank
                         wall by conductivity
                         measurements.
28-15-04-720-001-A00..  Functionally Check Fwd   Before the accumulation  Within 90 days after
                         Fuel tank critical       of 30,000 total flight   the effective date of
                         bonding integrity of     hours.                   this AD.
                         Fuel Pump, FQGS and
                         Low Level SW
                         connectors at tank
                         wall by conductivity
                         measurements.
28-21-01-220-001-A00..  Inspect Wing Electric    Before the accumulation  Within 90 days after
                         Fuel Pump Connector.     of 10,000 total flight   the effective date of
                                                  hours.                   this AD.
28-23-03-220-001-A00..  Inspect Pilot Valve      Before the accumulation  Within 90 days after
                         harness inside the       of 20,000 total flight   the effective date of
                         conduit.                 hours.                   this AD.
28-23-04-220-001-A00..  Inspect Vent Valve       Before the accumulation  Within 90 days after
                         harness inside the       of 20,000 total flight   the effective date of
                         conduit.                 hours.                   this AD.
28-41-01-720-001-A00..  Functionally Check Fuel  Before the accumulation  Within 90 days after
                         Conditioning Unit        of 10,000 total flight   the effective date of
                         (FCU).                   hours.                   this AD.
28-41-03-220-001-A00..  Inspect FQIS harness     Before the accumulation  Within 90 days after
                         for clamp and wire       of 20,000 total flight   the effective date of
                         jacket integrity.        hours.                   this AD.
28-46-02-220-001-A00..  Aft Fuel Tank Internal   Before the accumulation  Within 90 days after
                         Inspection: FQGS         of 20,000 total flight   the effective date of
                         harness and Low Level    hours.                   this AD.
                         SW harness for clamp
                         and wire jacket
                         integrity.
28-46-04-220-001-A00..  Fwd Fuel Tank Internal   Before the accumulation  Within 90 days after
                         Inspection: FQGS         of 20,000 total flight   the effective date of
                         harness and Low Level    hours.                   this AD.
                         SW harness for clamp
                         and wire jacket
                         integrity.
28-46-05-720-001-A00..  Functionally Check       Before the accumulation  Within 90 days after
                         Auxiliary Fuel           of 10,000 total flight   the effective date of
                         Conditioning Unit        hours.                   this AD.
                         (FCU).
------------------------------------------------------------------------------------------------

(3) Before December 16, 2008, or  within 90 days after the effective  date
    of this  AD, whichever  occurs first,  revise the  ALS of  the ICA  to
    incorporate  items  1,  2,  and 3  of  Section  A2.4,  Critical Design
    Configuration Control Limitation (CDCCL), of Appendix 2 of the MPG.

(4) After  accomplishing the  actions specified  in paragraphs  (f)(2) and
    (f)(3) of this AD,  no alternative inspections, inspection  intervals,
    or CDCCLs may be used unless the inspections, intervals, or CDCCLs are
    part of a later revision of Appendix 2 of the MPG that is approved  by
    the Manager, ANM-116, FAA, or ANAC (or its delegated agent); or unless
    the inspections, intervals, or  CDCCLs are approved as  an alternative
    method  of  compliance  (AMOC)  in  accordance  with  the   procedures
    specified in paragraph (g) of this AD.

FAA AD DIFFERENCES

NOTE 2: This  AD differs  from  the  MCAI  and/or  service information  as
follows:

(1) The MCAI specifies a compliance date of "Before December 31, 2008" for
    doing  the  ALI revisions.  We  have already  issued  regulations that
    require operators to  revise their maintenance/inspection  programs to
    address  fuel  tank  safety  issues.  The  compliance  date  for these
    regulations  is  December  16,   2008.  To  provide  for   coordinated
    implementation of  these regulations  and this  AD, we  are using this
    same compliance date in this AD.

(2) The MCAI specifies a compliance time of 180 days to revise the ALS  of
    the ICA to incorporate items 1, 2, and 3 of Section A2.4 of Appendix 2
    of the MPG. This AD requires a  compliance time of 90 days to do  this
    revision. This difference has been coordinated with ANAC.

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, 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 assure 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  Brazilian  Airworthiness  Directive  2007-08-01,  effective
    September 27, 2007; and Sections A2.5.2, Fuel System Limitation Items,
    and A2.4, Critical Design Configuration Control Limitation (CDCCL), of
    Appendix 2 of the MPG; for related information.

Issued in  Renton, Washington,  on April  30, 2008.  Ali Bahrami, Manager,
Transport Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by May 27, 2008.
PREAMBLE 
DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

14 CFR Part 39

[Docket No. FAA-2008-0194; Directorate Identifier 2007-NM-263-AD]
RIN 2120-AA64

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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Supplemental notice of proposed rulemaking (NPRM); reopening of
comment period.

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

SUMMARY: We are  revising an earlier  NPRM for the  products listed above.
This action revises the earlier NPRM by expanding the scope. 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:

Fuel  system  reassessment,   performed   according   to  RBHA-E88/SFAR-88
(Regulamento  Brasileiro  de  Homologacao  Aeronautica  88/Special Federal
Aviation Regulation  No. 88),  requires the  inclusion of  new maintenance
tasks in the Critical Design Configuration Control Limitations (CDCCL) and
in  the  Fuel System  Limitations  (FSL), necessary  to  preclude ignition
sources in the fuel system. * * *

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 27, 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,
International 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-2008-0194;   Directorate
Identifier  2007-NM-263-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

We proposed to amend 14 CFR part 39 with an earlier NPRM for the specified
products, which was published in the Federal Register on February 21, 2008
(73 FR 9500).  That earlier NPRM  proposed to require  actions intended to
address the unsafe condition for the products listed above.

Since that earlier  NPRM was issued,  we have determined  that for certain
airplanes the initial  compliance times for  doing the tasks  specified in
paragraph (f)(2) of  the earlier NPRM  must be reduced.  That earlier NPRM
resulted  from   Brazilian  Airworthiness   Directive  2007-08-01,   dated
September 27, 2007 (referred to after this as "the MCAI").

The MCAI does not provide an initial compliance time for doing the  tasks.
In the earlier  NPRM we proposed  an initial compliance  time that started
from the effective date of the AD; or the date of issuance of the original
Brazilian standard airworthiness  certificate or the  date of issuance  of
the  original  Brazilian export  certificate  of airworthiness;  whichever
occurs later. Although unstated in  the MCAI, we have determined  that the
intent of the MCAI  is for the initial  compliance time to start  from the
initial delivery date of the  airplane in order to address  the identified
unsafe condition  in a  timely manner.  We have  also revised  the initial
compliance times for clarity by providing a threshold and grace period for
each task. We  have revised this  supplemental NPRM by  adding Table 1  to
specify the initial compliance times for each task. You may obtain further
information by examining the MCAI in the AD docket.

COMMENTS

We have considered the following comments received on the earlier NPRM.

REQUEST TO CLARIFY COMPLIANCE TIMES

EMBRAER requests that we revise the NPRM to enable operators to comply  if
replacement  parts  are  not immediately  available.  EMBRAER  states that
paragraph  (section)  A2.5.1  of  Appendix  2  of  the  EMBRAER  Legacy BJ
Maintenance Planning  Guide (MPG)  MPG-1483, Revision  5, dated  March 22,
2007, contains  provisions to  allow operators  to implement  the required
fuel  system  limitation  inspections in  a  more  timely manner.  EMBRAER
therefore requests that we revise the NPRM to include paragraph A2.5.1  of
the MPG.

We do not agree  with the request to  include MPG paragraph A2.5.1,  which
describes deferring the first mandatory inspections to the next "C"  check
(5,000 flight hours).  However, as described  previously, we have  revised
paragraph  (f)(2)  of  the  supplemental  NPRM  to  clarify  the   initial
compliance times.  With these  revised compliance  times, there  should be
sufficient spare  parts. In  addition, if  an operator  decides that  more
compliance time is needed, the operator may request an alternative  method
of  compliance  (AMOC)  in   accordance  with  paragraph  (g)(1)   of  the
supplemental NPRM.

CLARIFICATION OF INCREASED COSTS

The original NPRM specified that  about 37 airplanes would be  affected by
that proposed action. We have determined that about 49 airplanes would  be
affected by this proposed action, and have revised the Costs of Compliance
accordingly in this supplemental NPRM.

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.

Certain changes described above expand the scope of the earlier NPRM. As a
result, we  have determined  that it  is necessary  to reopen  the comment
period to provide additional opportunity for the public to comment on this
proposed AD.

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 49 products of U.S. registry. We also estimate that it  would
take about 1 work-hour per  product to comply with the  basic requirements
of this 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
$3,920, or $80 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: