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PROPOSED AD EMPRESA BRASILERIA DE AERONAUTICA S.A. (EMBRAER): Docket No. FAA-2012-0441; Directorate Identifier 2012-CE-011-AD.
(a) COMMENTS DUE DATE

We must receive comments by June 8, 2012.

(b) AFFECTED ADS

None.

(c) APPLICABILITY

This AD applies to the  following Empresa Brasileria de  Aeronautica  S.A.
(EMBRAER) Model EMB-505 airplanes certificated in any category.

(1) Group 1: Serial  numbers  (S/Ns)  50500030,  50500033  thru  50500037,
    50500039, 50500040, 50500044, and 50500046.

(2) Group  2: S/Ns  5050004 thru  50500029, 50500031,  50500032, 50500038,
    50500041 thru  50500043, 50500045,  50500047 thru  50500059, 50500061,
    50500063, 50500065 thru 50500068, 50500070, 50500074, and 50500075.

(3) Group 3: S/N 50500072.

(4) Group 4: S/Ns 50500069, 50500071, and 50500073.

(d) SUBJECT

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

(e) REASON

This AD  was prompted  by 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 an inadequate amount of drain holes in the primary
control surfaces (rudder,  elevator, aileron) and  their tab surfaces  may
allow water to accumulate in the control surfaces. We are issuing this  AD
to prevent unbalanced flight control surfaces and reduced flutter margins,
which could result in loss of control of the airplane.

(f) ACTIONS AND COMPLIANCE

Unless already done, do the following actions:

(1) Group 1 airplanes specified in paragraph (c)(1) of this AD:

(i) Within the next 100 hours time-in-service after the effective date  of
    this AD or within the next 3 calendar months after the effective  date
    of this AD,  whichever occurs first,  visually inspect the  right-hand
    (RH)  and left-hand  (LH) ailerons  lower skin  for the  existence of
    required drain holes.

(ii) Before  further flight  after the  inspections required  in paragraph
     (f)(1)(i) of this AD, if the required drain holes do not exist, drill
     the drain holes.

(iii) Within  the next  24 months  after the  effective date  of this  AD,
      rework  the  ailerons,  ailerons  trim-tabs,  ailerons  horn  cover,
      rudder, rudder trim-tab,  elevators and elevators  auto-tab surfaces
      by drilling additional drain holes.

(iv) Do  the actions  required in  paragraphs (f)(1)(i)  and (f)(1)(ii) of
     this AD following the  Accomplishment Instructions in EMBRAER  Phenom
     Service Bulletin No. 505-57-0003, dated November 16, 2011.

(v) Do the actions required in paragraph (f)(1)(iii) of this AD  following
    Part I of  the Accomplishment Instructions  in EMBRAER Phenom  Service
    Bulletin No. 505-57-0002, dated February 13, 2012.

(2) Group 2 airplanes specified in paragraph (c)(2) of this AD:

Within the next 24 months after the effective date of this AD, rework  the
ailerons, ailerons  trim-tabs, ailerons  horn cover,  rudder, rudder  trim
-tab, elevators  and elevators  auto-tab surfaces  by drilling  additional
drain holes. Do the modifications  following Part I of the  Accomplishment
Instructions in  EMBRAER Phenom  Service Bulletin  No. 505-57-0002,  dated
February 13, 2012.

(3) Group 3 airplanes specified in paragraph (c)(3) of this AD:

(i) Within the next 24 months after the effective date of this AD,  rework
    the rudder, rudder trim-tab, elevators and elevators auto-tab surfaces
    by drilling additional drain holes.

(ii) Within  the  next 24  months after  the  effective  date of  this AD,
     inspect the ailerons for the existence of required drain holes.

(iii) Before further  flight after the  inspections required in  paragraph
      (f)(3)(ii) of  this AD,  if the  required drain  holes do not exist,
      drill the drain holes.

(iv) Do the actions required  in paragraph (f)(3)(i) of this  AD following
     Part II of the Accomplishment Instructions in EMBRAER Phenom  Service
     Bulletin No. 505-57-0002, dated February 13, 2012.

(v) Do the  actions required in  paragraphs (f)(3)(ii) and  (f)(3)(iii) of
    this  AD  following  Part II  of  the  Accomplishment Instructions  in
    EMBRAER Phenom  Service Bulletin  No. 505-57-0004,  dated February 16,
    2012.

(4) Group 4 airplanes specified in paragraph (c)(4) of this AD:

(i) Within the next 24 months after the effective date of this AD, inspect
    the  ailerons, elevators,  and rudder  for the  existence of  required
    drain holes.

(ii) Before  further  flight after  the inspection  required in  paragraph
     (f)(4)(i) of this AD, if the required drain holes do not exist, drill
     the drain holes.

(iii) Do the  actions required in  paragraphs (f)(4)(i) and  (f)(4)(ii) of
      this  AD  following Part  I  of the  Accomplishment  Instructions in
      EMBRAER Phenom Service Bulletin No. 505-57-0004, dated February  16,
      2012.

(g) OTHER FAA AD PROVISIONS

The following provisions also apply to this AD:

(1) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS): The Manager, Standards Off-
    ice, 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:
    Jim Rutherford, Aerospace  Engineer, FAA, Small  Airplane Directorate,
    901 Locust, Room  301, Kansas City,  Missouri 64106; telephone:  (816)
    329-4165; fax: (816)  329-4090; email: jim.rutherford@faa.gov.  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, a
    federal  agency  may not  conduct  or sponsor,  and  a person  is  not
    required to respond to, nor shall a person be subject to a penalty for
    failure to  comply with  a collection  of information  subject to  the
    requirements of the Paperwork Reduction Act unless that collection  of
    information  displays  a current  valid  OMB Control  Number.  The OMB
    Control Number  for this  information collection  is 2120-0056. Public
    reporting  for  this  collection of  information  is  estimated to  be
    approximately 5 minutes per response, including the time for reviewing
    instructions, completing and reviewing the collection of  information.
    All  responses  to  this  collection  of  information  are  mandatory.
    Comments concerning the  accuracy of this  burden and suggestions  for
    reducing the burden should be directed to the FAA at: 800 Independence
    Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance
    Officer, AES-200.

(h) RELATED INFORMATION

Refer  to  MCAI  Agencia  Nacional  de  Aviacao  Civil  (ANAC)   Brazilian
Airworthiness Directive 2012-03-01, dated  March 20, 2012; EMBRAER  Phenom
Service Bulletin No. 505-57-0002, dated February 13, 2012; EMBRAER  Phenom
Service Bulletin  No. 505-57-0003,  dated November  16, 2011;  and EMBRAER
Phenom  Service Bulletin  No. 505-57-0004,  dated February  16, 2012,  for
related information. For service  information related to this  AD, contact
Empresa  Brasileira  de  Aeronautica  S.A.  (EMBRAER),  Phenom Maintenance
Support, Av. Brigadeiro  Faria Lima, 2170,  Sao Jose dos  Campos--SP, CEP:
12227-901--P.O.  Box   36/2,  BRASIL;   fax  ++55   12  3927-2619;   email
phenom.reliability@embraer.com.br;  Internet:  http://www.embraer.com. You
may review copies of the referenced service information at the FAA,  Small
Airplane  Directorate,  901  Locust,  Kansas  City,  Missouri  64106.  For
information on the  availability of this  material at the  FAA, call (816)
329-4148.

Issued in Kansas  City, Missouri, on  April 18, 2012.  John Colomy, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by June 8, 2012.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2012-0441; Directorate Identifier 2012-CE-011-AD]
RIN 2120-AA64

Airworthiness Directives; Empresa Brasileria de
Aeronautica S.A. (EMBRAER) Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Empresa Brasileria de Aeron[aacute]utica S.A. (EMBRAER) Model
EMB-505 airplanes. 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 an
inadequate amount of drain holes in the primary control surfaces
(rudder, elevator, and aileron) and their tab surfaces may allow water
to accumulate in the control surfaces. This condition could cause
unbalanced flight control surfaces and reduced flutter margins, which
could result in loss of control of the airplane. We are issuing this
proposed AD to require actions to address the unsafe condition on these
products.

DATES: We must receive comments on this proposed AD by June 8, 2012.

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 W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.

For service information identified in this proposed AD, contact
Empresa Brasileira de Aeronautica S.A. (EMBRAER), Phenom Maintenance
Support, Av. Brigadeiro Faria Lima, 2170, S[atilde]o Jos[eacute] dos
Campos--SP, CEP: 12227-901--P.O. Box 36/2, BRASIL; fax ++55 12 3927-
2619; email phenom.reliability@embraer.com.br; Internet: http://www.embraer.com.
You may review copies of the referenced service
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas
City, Missouri 64106. For information on the availability of this
material at the FAA, call (816) 329-4148.

Examining the AD Docket


You may examine the AD docket on the Internet at http://www.regulations.gov;
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 proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket 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: Jim Rutherford, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email:
jim.rutherford@faa.gov.

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-2012-0441;
Directorate Identifier 2012-CE-011-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 because of those comments.

We will post all comments we receive, without change, to http://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 Aviacao Civil (ANAC),
which is the aviation authority for Brazil, has issued Brazilian
Airworthiness Directive 2012-03-01, dated March 20, 2012 (referred to
after this as "the MCAI"), to correct an unsafe condition for the
specified products. The MCAI states:

It has been found that certain regions of the rudder, elevator,
ailerons, and their tabs surfaces does not present adequate drainage
capacity to avoid water accumulation inside of these control
surfaces. Internal water accumulation may lead to flight control
surfaces unbalancing possibly reducing the flutter margins, which
could result in loss of airplane control.

The MCAI requires visually inspecting the control surfaces (rudder,
elevator, and aileron) and their tab surfaces for the existence of
required drain holes and modifying the control surfaces by drilling
drain holes. You may obtain further information by examining the MCAI
in the AD docket.

Relevant Service Information


EMBRAER has issued Phenom Service Bulletin No. 505-57-0002, dated
February 13, 2012; Phenom Service Bulletin No. 505-57-0003, dated
November 16, 2011; and Phenom Service Bulletin No. 505-57-0004, dated
February 16, 2012. The actions described in this service information
are intended to correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of the 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 this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this
AD because we evaluated all information and determined the unsafe
condition exists and is likely to exist or develop on other products of
the same type design.

Costs of Compliance


We estimate that this proposed AD will affect 38 products of U.S. registry.

We also estimate that it would take from .5 work-hour to 2 work-
hours per product for 10 of the affected airplanes to comply with the
basic inspection requirements of this proposed AD. The average labor
rate is $85 per work-hour.

Based on these figures, we estimate the cost of the proposed
inspection on U.S. operators to be from $425 to $1,700, or $42.50 to
$170 per product.

In addition, we estimate that any necessary follow-on actions would
take from 2 work-hours to 38 work-hours and require parts costing $50,
for a cost from $220 to $3,280 per product. We have no way of
determining the number of products that may need these actions.

We also estimate that it would take from 19 work-hours to 27 work-
hours per product for 36 of the affected airplanes to comply with basic
modification requirements of this proposed AD. The average labor rate
is $85 per work-hour. Required parts would cost about $100 per product.

Based on these figures, we estimate the cost of the proposed
modification on U.S. operators to be from $61,740, to $86,220, or
$1,715 to $2,395 per product.

According to the manufacturer, some of the costs of this proposed
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

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),

(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.

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: