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Published 2008-09-08 · Federal Register document E8-19850

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 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) 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:

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2008-e9cf118935fdae82
Source row
results[351]
Raw source SHA-256
e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2008-18-01
Effective date printed in this edition
2008-10-14
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This airworthiness directive (AD) becomes effective October 
14, 2008.

Exact source excerpt. Text positions 7331–7427, end exclusive, in the original decoded publication. SHA-256: 856fceaae4d6feec45bf75f4ff6729583b6c7a025cee6170edab4a3627037be5

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 7427–7456, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes, having 
serial numbers (S/N) 17000002, 17000004 through 17000013, and 
17000015 through 17000154; and Model ERJ 190-100 STD, -100 LR, -100 
IGW, -100 ECJ, -200 STD, -200 LR, and -200 IGW airplanes, having S/N 
19000002, 19000004, and 19000006 through 19000060; certificated in 
any category.

Exact source excerpt. Text positions 7456–7892, end exclusive, in the original decoded publication. SHA-256: b19ed2ba049b9710d9fd5215ea98087192bedd56817f171d92c88fc71d0bc90b

Subject
Subject

    (d) Air Transport Association (ATA) of America Code 21: Air 
Conditioning.

Exact source excerpt. Text positions 7892–7981, end exclusive, in the original decoded publication. SHA-256: fd79c1b49743a5eaefec1ae6baa2f7b90b4257646b4d37c6d81958aa6918f3c5

Reason
Reason

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

    It has been found cases where the pressure equalization valve 
was not installed in the left-hand bulkhead blowout panel, on the 
forward and/or aft cargo compartments, thus affecting the 
effectiveness of fire detection, containment and suppression.

Corrective actions include inspecting for the presence of pressure 
equalization valves and, if necessary, installing pressure 
equalization valves.

Exact source excerpt. Text positions 7981–8471, end exclusive, in the original decoded publication. SHA-256: 6b7d6912b19f3d8e365111e13e212aa177eb7c49240dfb0d2fd7697ee929ca57

Actions and Compliance
Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Within 500 flight hours after the effective date of this AD, 
perform a general visual inspection on the left-hand bulkhead 
blowout panel of both the forward and aft cargo compartments to 
determine whether the pressure equalization valves, part number (P/
N) 120-48865-003, are installed. If both pressure equalization 
valves are installed in their respective blowout panels, no 
additional action is required by this AD.
    (2) If any valve is not installed, within 700 flight hours after 
the effective date of this AD, install valve P/N 120-48865-003, in 
accordance with the Accomplishment Instructions of EMBRAER Service 
Bulletin 170-21-0032 or 190-21-0019, both dated August 10, 2007; as 
applicable.

    Note 1: For the purpose of this AD, a general visual inspection 
(GVI) is: ``A visual examination of an interior or exterior area, 
installation or assembly to detect obvious damage, failure or 
irregularity. This level of inspection is made from within touching 
distance, unless otherwise specified. A mirror may be necessary to 
enhance visual access to all exposed surfaces in the inspection 
area. This level of inspection is made under normally available 
lighting conditions such as daylight, hangar lighting, flashlight or 
drop-light, and may require removal or opening of access panels or 
doors. Stands, ladders or platforms may be required to gain 
proximity to the area being checked.''

FAA AD Differences

    Note 2: This AD differs from the MCAI and/or service information 
as follows: No differences.

Exact source excerpt. Text positions 8471–10095, end exclusive, in the original decoded publication. SHA-256: 2bdece117275fc7e57ebc1a30b0b51387a1b25646d10a5b5bb6a09f5ea6c6394

Other FAA AD Provisions
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: 
Kenny Kaulia, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate,

[[Page 51912]]

FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone 
(425) 227-2848; 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.

Exact source excerpt. Text positions 10095–11538, end exclusive, in the original decoded publication. SHA-256: 3152dbb597e71b2d2a421dbc7c26cce123005b5a7a3adea7521f2f80b1433704

Related Information
Related Information

    (h) Refer to MCAI Brazilian Airworthiness Directives 2007-11-01 
and 2007-11-02, both effective December 12, 2007; and EMBRAER 
Service Bulletins 170-21-0032 and 190-21-0019, both dated August 10, 
2007; for related information.

Exact source excerpt. Text positions 11538–11793, end exclusive, in the original decoded publication. SHA-256: fe49268191bad9ab57f6f7b9551dda0a27dc578bfe614c169c418e30a6f79e0b

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 170-21-0032, dated 
August 10, 2007; or EMBRAER Service Bulletin 190-21-0019, dated 
August 10, 2007; as applicable; 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 
Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343--CEP 
12.225, Sao Jose dos Campos--SP, Brazil.
    (3) You may review copies at the FAA, Transport Airplane 
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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/cfr/ibr-locations.html.

Exact source excerpt. Text positions 11793–12739, end exclusive, in the original decoded publication. SHA-256: 8502610c5a79965c98d9dcc6cc2871792528ab0503573013ff2e03c4f05d9a9b

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 2008-18-01 · 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: ac2110315d99d714a3dd5f9fb7102b1cd1ed6e62bc81f85ed4e41da0bc0a4f9d. Source manifest: fc21e10b09977d1f579d98c5bbcb780da1231ecf188d98bd9b55653ccc73b9fa.

Official source · 2008-09-08

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 73, Number 174 (Monday, September 8, 2008)]
[Rules and Regulations]
[Pages 51910-51912]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-19850]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0562; Directorate Identifier 2008-NM-010-AD; 
Amendment 39-15658; AD 2008-18-01]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model ERJ 170 and ERJ 190 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) 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 cases where the pressure equalization valve 
was not installed in the left-hand bulkhead blowout panel, on the 
forward and/or aft cargo compartments, thus affecting the 
effectiveness of fire detection, containment and suppression.

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

DATES: This AD becomes effective October 14, 2008.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of October 14, 
2008.

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

FOR FURTHER INFORMATION CONTACT: Kenny Kaulia, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-2848; fax (425) 227-1149.

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 May 20, 2008 (73 FR 
29085). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been found cases where the pressure equalization valve 
was not installed in the left-hand bulkhead blowout panel, on the 
forward and/or aft cargo compartments, thus affecting the 
effectiveness of fire detection, containment and suppression.

Corrective actions include inspecting for the presence of pressure 
equalization valves and, if necessary, installing pressure equalization 
valves. 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.

[[Page 51911]]

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 our FAA policies. Any such differences 
are highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect about 101 products of U.S. 
registry. We also estimate that it will 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 this AD to the U.S. operators to be $8,080, 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 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 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 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 Operations office 
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 Operations 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:

2008-18-01 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-15658. Docket No. FAA-2008-0562; Directorate Identifier 
2008-NM-010-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective October 
14, 2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes, having 
serial numbers (S/N) 17000002, 17000004 through 17000013, and 
17000015 through 17000154; and Model ERJ 190-100 STD, -100 LR, -100 
IGW, -100 ECJ, -200 STD, -200 LR, and -200 IGW airplanes, having S/N 
19000002, 19000004, and 19000006 through 19000060; certificated in 
any category.

Subject

    (d) Air Transport Association (ATA) of America Code 21: Air 
Conditioning.

Reason

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

    It has been found cases where the pressure equalization valve 
was not installed in the left-hand bulkhead blowout panel, on the 
forward and/or aft cargo compartments, thus affecting the 
effectiveness of fire detection, containment and suppression.

Corrective actions include inspecting for the presence of pressure 
equalization valves and, if necessary, installing pressure 
equalization valves.

Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Within 500 flight hours after the effective date of this AD, 
perform a general visual inspection on the left-hand bulkhead 
blowout panel of both the forward and aft cargo compartments to 
determine whether the pressure equalization valves, part number (P/
N) 120-48865-003, are installed. If both pressure equalization 
valves are installed in their respective blowout panels, no 
additional action is required by this AD.
    (2) If any valve is not installed, within 700 flight hours after 
the effective date of this AD, install valve P/N 120-48865-003, in 
accordance with the Accomplishment Instructions of EMBRAER Service 
Bulletin 170-21-0032 or 190-21-0019, both dated August 10, 2007; as 
applicable.

    Note 1: For the purpose of this AD, a general visual inspection 
(GVI) is: ``A visual examination of an interior or exterior area, 
installation or assembly to detect obvious damage, failure or 
irregularity. This level of inspection is made from within touching 
distance, unless otherwise specified. A mirror may be necessary to 
enhance visual access to all exposed surfaces in the inspection 
area. This level of inspection is made under normally available 
lighting conditions such as daylight, hangar lighting, flashlight or 
drop-light, and may require removal or opening of access panels or 
doors. Stands, ladders or platforms may be required to gain 
proximity to the area being checked.''

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: 
Kenny Kaulia, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate,

[[Page 51912]]

FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone 
(425) 227-2848; 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 Directives 2007-11-01 
and 2007-11-02, both effective December 12, 2007; and EMBRAER 
Service Bulletins 170-21-0032 and 190-21-0019, both dated August 10, 
2007; for related information.

Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 170-21-0032, dated 
August 10, 2007; or EMBRAER Service Bulletin 190-21-0019, dated 
August 10, 2007; as applicable; 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 
Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343--CEP 
12.225, Sao Jose dos Campos--SP, Brazil.
    (3) You may review copies at the FAA, Transport Airplane 
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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/cfr/ibr-locations.html.

    Issued in Renton, Washington, on August 18, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E8-19850 Filed 9-5-08; 8:45 am]
BILLING CODE 4910-13-P


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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:28:08.280489+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Text SHA-256
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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.

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