Back to publication catalog

Published 2010-10-14 · Federal Register document 2010-25283

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-500 Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued 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:

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:33.146842+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2010-a7267cd3a71dbd26
Source row
results[332]
Raw source SHA-256
a7267cd3a71dbd2645583c8a673df65e4a7fa9360a96e3be0de5b81f9d68c9a0

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2010-21-15
Effective date printed in this edition
2010-11-18
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This airworthiness directive (AD) becomes effective November 
18, 2010.

Exact source excerpt. Text positions 7983–8080, end exclusive, in the original decoded publication. SHA-256: 854899afb8d779eec3c95a24634149d906a8d1efa565e04b1cf94eff04137844

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 8080–8109, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to Model EMB-500 airplanes, serial numbers 
50000005 through 50000134, 50000136, 50000137, and 50000139 through 
50000165, certificated in any category.

Exact source excerpt. Text positions 8109–8302, end exclusive, in the original decoded publication. SHA-256: ff1a4cd16fa89e799d026c33ea8e37c15f1d456927517d6e91fd0f589ea014cd

Subject
Subject

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

Exact source excerpt. Text positions 8302–8390, end exclusive, in the original decoded publication. SHA-256: 730778f9e234ed027c76ce087f72dcb19faf46092fde1c738867499d67434334

Reason
Reason

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

    It has been found that certain regions of the elevators, 
elevators trim tabs, and ailerons do not present drain holes to 
avoid water accumulation inside of these flight 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.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

The MCAI requires you to drill new drain holes in the elevators, 
elevators trim tabs, and ailerons surfaces.

Exact source excerpt. Text positions 8390–9174, end exclusive, in the original decoded publication. SHA-256: 49f5e6ad5955cdd9c2b0fb63c97825696be14139fb2604b175c4da375fc5f5f2

Actions and Compliance
Actions and Compliance

    (f) Unless already done, within the next 24 calendar months 
after November 18, 2010 (the effective date of this AD), rework the 
elevators, elevators trim tabs, and ailerons surfaces by drilling 
additional drain holes in them following Empresa Brasileira de 
Aeron[aacute]utica S.A. (EMBRAER) Service Bulletin 500-57-0001, 
dated April 28, 2010.

FAA AD Differences

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

Exact source excerpt. Text positions 9174–9669, end exclusive, in the original decoded publication. SHA-256: 3a82094fed74d331dce4e51adc15f9e35cc9c8e77555fc4a7d4864f202290fc7

Other FAA AD Provisions
Other FAA AD Provisions

    (g) The following provisions also apply to this AD:

[[Page 63050]]

    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, 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: Karl Schletzbaum, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090. 
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 (44 
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has 
approved the information collection requirements and has assigned 
OMB Control Number 2120-0056.

Exact source excerpt. Text positions 9669–11060, end exclusive, in the original decoded publication. SHA-256: 6cf7f24df0f168edb7e4ec9a02ba33f1194d6d4cc58e088a007affc7f6315787

Related Information
Related Information

    (h) Refer to MCAI Ag[ecirc]ncia Nacional de 
Avia[ccedil][atilde]o Civil--Brazil (ANAC), AD No.: 2010-07-01, 
dated August 9, 2010; and Empresa Brasileira de Aeron[aacute]utica 
S.A. (EMBRAER) Service Bulletin 500-57-0001, dated April 28, 2010, 
for related information.

Exact source excerpt. Text positions 11060–11357, end exclusive, in the original decoded publication. SHA-256: c6e3d9541fdbe613cdb233abb10308393bd761a2ef7bec33b985a493723aebb7

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use Empresa Brasileira de Aeron[aacute]utica S.A. 
(EMBRAER) Service Bulletin 500-57-0001, dated April 28, 2010, to do 
the actions required by this AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
EMBRAER Empresa Brasileira de Aeron[aacute]utica S.A., Phenom 
Maintenance Support, Av. Brig. Farina Lima, 2170, Sao Jose dos 
Campos--SP, CEP: 12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12 
3927-5383; fax: ++55 12 3927-2610; E-mail: 
[email protected]; Internet: http://www.embraer.com.br.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Exact source excerpt. Text positions 11357–12757, end exclusive, in the original decoded publication. SHA-256: 8f1f979bb290cd9d60d6153bc148a86495b680a55d418d502155b441b74e714c

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2010-21-15 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 8627be883705898a5d681c2a4ec445955b4c4f9608c016814649cd979fc098ee. Source manifest: 59548d44293f2402142e882a4941d7482540e64782ea9d591bb7af72d39ce711.

Official source · 2010-10-14

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 75, Number 198 (Thursday, October 14, 2010)]
[Rules and Regulations]
[Pages 63048-63050]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-25283]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0754 Directorate Identifier 2010-CE-039-AD; 
Amendment 39-16475; AD 2010-21-15]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-500 Airplanes

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

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued 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 that certain regions of the elevators, 
elevators trim tabs, and ailerons do not present drain holes to 
avoid water accumulation inside of these flight 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.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective November 18, 2010.
    On November 18, 2010, the Director of the Federal Register approved 
the incorporation by reference of certain publications listed in this 
AD.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at Document Management Facility, U.S. 
Department of Transportation, Docket Operations, M-30, West Building 
Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 
20590.

FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on August 3, 2010 (75 
FR 45558). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been found that certain regions of the elevators, 
elevators trim tabs, and ailerons do

[[Page 63049]]

not present drain holes to avoid water accumulation inside of these 
flight 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.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

The MCAI requires you to drill new drain holes in the elevators, 
elevators trim tabs, and ailerons surfaces. You may obtain further 
information by examining the MCAI in the AD docket.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD as proposed.

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 required 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 AD.

Costs of Compliance

    We estimate that this AD will affect 78 products of U.S. registry. 
We also estimate that it will take about 18 work-hours per product to 
comply with the basic requirements of this AD. The average labor rate 
is $85 per work-hour. Required parts will cost about $128 per product.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $129,324 or $1,658 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 AD will not have federalism implications 
under Executive Order 13132. This AD will 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 AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866;
    (2) Is not a ``significant rule'' under 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 AD and placed it in the AD Docket.

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 the NPRM, 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.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

2010-21-15 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-16475; Docket No. FAA-2010-0754; Directorate Identifier 
2010-CE-039-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective November 
18, 2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Model EMB-500 airplanes, serial numbers 
50000005 through 50000134, 50000136, 50000137, and 50000139 through 
50000165, certificated in any category.

Subject

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

Reason

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

    It has been found that certain regions of the elevators, 
elevators trim tabs, and ailerons do not present drain holes to 
avoid water accumulation inside of these flight 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.
    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in 
the indicated time limit.

The MCAI requires you to drill new drain holes in the elevators, 
elevators trim tabs, and ailerons surfaces.

Actions and Compliance

    (f) Unless already done, within the next 24 calendar months 
after November 18, 2010 (the effective date of this AD), rework the 
elevators, elevators trim tabs, and ailerons surfaces by drilling 
additional drain holes in them following Empresa Brasileira de 
Aeron[aacute]utica S.A. (EMBRAER) Service Bulletin 500-57-0001, 
dated April 28, 2010.

FAA AD Differences

    Note:  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:

[[Page 63050]]

    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, 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: Karl Schletzbaum, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090. 
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 (44 
U.S.C. 3501 et seq.), 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 Ag[ecirc]ncia Nacional de 
Avia[ccedil][atilde]o Civil--Brazil (ANAC), AD No.: 2010-07-01, 
dated August 9, 2010; and Empresa Brasileira de Aeron[aacute]utica 
S.A. (EMBRAER) Service Bulletin 500-57-0001, dated April 28, 2010, 
for related information.

Material Incorporated by Reference

    (i) You must use Empresa Brasileira de Aeron[aacute]utica S.A. 
(EMBRAER) Service Bulletin 500-57-0001, dated April 28, 2010, to do 
the actions required by this AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
EMBRAER Empresa Brasileira de Aeron[aacute]utica S.A., Phenom 
Maintenance Support, Av. Brig. Farina Lima, 2170, Sao Jose dos 
Campos--SP, CEP: 12227-901--PO Box: 38/2, BRASIL, telephone: ++55 12 
3927-5383; fax: ++55 12 3927-2610; E-mail: 
[email protected]; Internet: http://www.embraer.com.br.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

    Issued in Kansas City, Missouri, on September 30, 2010.
John R. Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-25283 Filed 10-13-10; 8:45 am]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:12:55.719530+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
273b76f0b1bb1cf0229e11aba7e9cb537a3b72fae03615823e95c7cea194fdd4
Text SHA-256
8627be883705898a5d681c2a4ec445955b4c4f9608c016814649cd979fc098ee

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.