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PROPOSED AD EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Docket No. FAA-2008-0483; Directorate Identifier 2008-NM-006-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-135 airplanes and Model  EMB-145,
    -145ER,  -145MR,  -145LR,   -145XR,  -145MP,  and   -145EP  airplanes;
    certificated in  any category;  having serial  numbers 145002  through
    145362, 145364 through 145590, and 145592 through 14500987.

SUBJECT

(d) Air  Transport  Association (ATA)  of America  Code 30:  Ice and  Rain
    Protection.

REASON

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

It has been found  the occurrence of smoke  in the flight deck  originated
from Pitot 1/2  and TAT 1/2  current sensor relays  and [their] respective
sockets, caused by poor electrical contacts between those relays and their
sockets.

The unsafe condition is that smoke  in the flight deck may interfere  with
the  flightcrew's  ability  to operate  the  airplane.  Corrective actions
include inspecting for damage of the Pitot 1 and 2 and TAT 1 and 2 current
sensor relays  and sockets;  and, as  applicable, replacing  the A1 and C1
electrical  contacts  of  the  sockets  and  reidentifying  the   sockets,
replacing the  sockets, and  replacing current  sensor relays.  Damage may
include melted points or stuck material of the silicone gasket,  incorrect
shape  of the  current sensor  relay/sockets, discoloration  of  contacts,
loose pin-type  contacts, cracking  or loose  material of  the polish  and
sealant of the bases,  contaminants of the current  sensor relays/sockets,
and  stuck material  or roughness  of the  surface of  the current  sensor
relay/pin-type contact.

ACTIONS AND COMPLIANCE

(f) Within 2,500  flight hours or  24 months after  the effective date  of
    this AD, whichever occurs first, unless already done, do the following
    actions in accordance with the Accomplishment Instructions of  Embraer
    Service  Bulletin  145-30-0052,  dated  August  2,  2007;  or  Service
    Bulletin 145LEG-30-0019, dated August 28, 2007; as applicable. Do  all
    applicable replacements and re-identification before further flight.

(1) Perform a detailed inspection of the Pitot 1 (K0053), Pitot 2 (K0054),
    TAT 1 (K0064),  and TAT 2  (K0494) current sensor  relays for possible
    damage  caused  by  overheating  in  their  contacts,  enclosure,  and
    finishing material.

(i) If no  damage is found  on a current  sensor relay, that  relay may be
    reinstalled.

(ii) If any damage is found  on a current sensor relay, replace  the relay
     with a new relay having the same part number (P/N) CS500- 060-D4A.

(2) Perform  a  detailed  inspection  on the  Pitot  1 (XK0053),  Pitot  2
    (XK0054),  TAT  1  (XK0064),  and TAT  2  (XK0494)  relay  sockets for
    possible damage  caused by  overheating in  their contacts, enclosure,
    and finishing material.

(i) If no damage is found on a socket, replace electrical contacts A1  and
    C1  of  the socket  with  new contacts  having  P/N M39029/92-536;  re
    -identify  the  socket  from  P/N  S500-9140  to  S500-9140-A;  and re
    -identify the socket electrical code from XK0053, XK0054, XK0064,  and
    XK0494, to XK1243, XK1242, XK1245, and XK1244, respectively.

(ii) If any  damage is found  on a socket,  replace the socket  with a new
     socket having P/N S500-9140-A or S500-9216.

NOTE 1: For the  purpose of this AD,  a detailed inspection (DET)  is: "An
intensive  examination of  a specific  item, installation  or assembly  to
detect damage,  failure or  irregularity. Available  lighting is  normally
supplemented with a direct source of good lighting at an intensity  deemed
appropriate. Inspection aids such as mirrors, magnifying lenses, etc., may
be  necessary. Surface  cleaning and  elaborate access  procedures may  be
required."

FAA AD DIFFERENCES

NOTE 2: 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: 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 MCAI Brazilian Airworthiness Directive 2007-11-04R1,  effect-
    ive December  21, 2007;  Embraer Service  Bulletin 145-30-0052,  dated
    August 2,  2007; and  Embraer Service  Bulletin 145LEG-30-0019,  dated
    August 28, 2007; 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-2008-0483; Directorate Identifier 2008-NM-006-AD]
RIN 2120-AA64

AIRWORTHINESS DIRECTIVES; Empresa Brasileira de Aeronautica S.A. (EMBRAER)
Model  EMB-135  Airplanes,  and Model  EMB-145,  -145ER,  -145MR,  -145LR,
-145XR, -145MP, and -145EP 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 smoke  in the flight deck  originated
from Pitot 1/2  and TAT 1/2  current sensor relays  and [their] respective
sockets, caused by poor electrical contacts between those relays and their
sockets.

The unsafe condition is that smoke  in the flight deck may interfere  with
the flightcrew's ability  to operate the  airplane. 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-2008-0483;   Directorate
Identifier  2008-NM-006-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 2007-11-04R1,  effective December  21, 2007  (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 smoke  in the flight deck  originated
from Pitot 1/2  and TAT 1/2  current sensor relays  and [their] respective
sockets, caused by poor electrical contacts between those relays and their
sockets.

The unsafe condition is that smoke  in the flight deck may interfere  with
the  flightcrew's  ability  to operate  the  airplane.  Corrective actions
include inspecting for damage of the Pitot 1 and 2 and TAT 1 and 2 current
sensor relays  and sockets;  and, as  applicable, replacing  the A1 and C1
electrical  contacts  of  the  sockets  and  reidentifying  the   sockets,
replacing the  sockets, and  replacing current  sensor relays.  Damage may
include melted points or stuck material of the silicone gasket,  incorrect
shape  of the  current sensor  relay/sockets, discoloration  of  contacts,
loose pin-type  contacts, cracking  or loose  material of  the polish  and
sealant of the bases,  contaminants of the current  sensor relays/sockets,
and  stuck material  or roughness  of the  surface of  the current  sensor
relay/pin-type contact.  You may  obtain further  information by examining
the MCAI in the AD docket.

RELEVANT SERVICE INFORMATION

Embraer has issued Service Bulletin 145-30-0052, dated August 2, 2007; and
Service  Bulletin  145LEG-30-0019,  dated  August  28,  2007.  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 704 products of U.S. registry. We also estimate that it would
take about 8 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 $450,560, or $640 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: