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Published 2007-06-14 · Federal Register document E7-11201

Airworthiness Directives; Empresa Brasileira Aeronautica S.A. (EMBRAER) Model ERJ 170 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 2026-09-03T22:23:23.906952+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2007-daaa03e810180273
Source row
results[232]
Raw source SHA-256
daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2007-12-18
Effective date printed in this edition
2007-07-19
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This airworthiness directive (AD) becomes effective July 19, 
2007.

Exact source excerpt. Text positions 9402–9495, end exclusive, in the original decoded publication. SHA-256: 8db789295bd540ff7b9e13d6105ae59a289b524e7aed10a92349eba925a46a83

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 9495–9524, 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; 
certificated in any category; serial numbers 17000005 through 
17000013, 17000015, 17000016, 17000018 through 17000116, 17000118, 
and 17000119.

Exact source excerpt. Text positions 9524–9814, end exclusive, in the original decoded publication. SHA-256: 67a960cbdea160671b8c6c4e4f98cf89020c609ab2387a59dc99c2168633d1eb

Subject
Subject

    (d) Fuel.

Exact source excerpt. Text positions 9814–9838, end exclusive, in the original decoded publication. SHA-256: 62c347cf944ea48ddb54adc56d55671dcec6357270b0b511dd2505c78c8d310b

Reason
Reason

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

    It has been found that the fuel quantity probes harnesses 
installed in the left and right wing stub tanks on some Embraer ERJ-
170( ) aircraft models may not be protected in accordance with RBHA/
FAR (Regulamento Brasileiro de Homologac[atilde] to 
Aeron[aacute]utica/Federal Aviation Regulation) 25.981(a) and (b) 
requirements.

    The unsafe condition is potential ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could 
result in fuel tank explosions and consequent loss of the airplane. 
The MCAI requires inspection of the fuel quantity probes harnesses 
and correct reassembly if necessary.

Exact source excerpt. Text positions 9838–10565, end exclusive, in the original decoded publication. SHA-256: 44db887ad77ca2be39675227bb8eea1f302d7e2e0a8c2e80b8d48e70fab879c7

Actions and Compliance
Actions and Compliance

    (f) Within 6,000 flight hours after the effective date of this 
AD, unless already done, make an inspection in the fuel quantity 
probes harnesses installed on both wings and reassemble them, as 
applicable, as described in EMBRAER Service Bulletin 170-28-0011, 
dated April 26, 2006.

FAA AD Differences

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

Exact source excerpt. Text positions 10565–10997, end exclusive, in the original decoded publication. SHA-256: 93204acb2275341ca591c694c785048d164cbc846c7c1abb51da722db81c39e3

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, FAA, Transport Airplane Directorate, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. Send information to ATTN: Todd 
Thompson, Aerospace Engineer; International Branch, ANM-116, FAA, 
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; telephone (425) 227-1175; 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 10997–12425, end exclusive, in the original decoded publication. SHA-256: 6af54bb3e5cc45b01eba6be76bd378c49d5d56bfb586990919b42020fe90d70a

Related Information
Related Information

    (h) Refer to MCAI Brazilian Airworthiness Directive 2007-01-02, 
effective January 15, 2007; and EMBRAER Service Bulletin 170-28-
0011, dated April 26, 2006; for related information.

Exact source excerpt. Text positions 12425–12634, end exclusive, in the original decoded publication. SHA-256: 8754c595cb984900a76e61eeccb761f778cb8577b4ff056953c5a69c3336ea1b

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 170-28-0011, dated 
April 26, 2006, 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 12634–13499, end exclusive, in the original decoded publication. SHA-256: b932e141515b842069ca656e93bddddb6f6c10cdaaa3b7911b5fdacdad8a2000

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 2007-12-18 · 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: 61aa3c995dd5a1884b0f975fbdd56cef15026d6dc63f6b600e68aca5805d5301. Source manifest: 23aeb6d0ff8723cabdee1e6f5de6ed044bc0383e9d056dcd44a7fc9e15b27b40.

Official source · 2007-06-14

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 72, Number 114 (Thursday, June 14, 2007)]
[Rules and Regulations]
[Pages 32773-32774]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-11201]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 72, No. 114 / Thursday, June 14, 2007 / Rules 
and Regulations

[[Page 32773]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27753; Directorate Identifier 2007-NM-022-AD; 
Amendment 39-15096; AD 2007-12-18]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira Aeronautica S.A. 
(EMBRAER) Model ERJ 170 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 that the fuel quantity probes harnesses 
installed in the left and right wing stub tanks on some Embraer ERJ-
170( ) aircraft models may not be protected in accordance with RBHA/
FAR (Regulamento Brasileiro de Homologac[atilde]o 
Aeron[aacute]utica/Federal Aviation Regulation) 25.981(a) and (b) 
requirements.

    The unsafe condition is potential ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could result 
in fuel tank explosions and consequent loss of the airplane. We are 
issuing this AD to require actions to correct the unsafe condition on 
these products.

DATES: This AD becomes effective July 19, 2007.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of July 19, 
2007.

ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. 
Department of Transportation, 400 Seventh Street, SW., Nassif Building, 
Room PL-401, Washington, DC.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-1175; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Streamlined Issuance of AD

    The FAA is implementing a new process for streamlining the issuance 
of ADs related to MCAI. This streamlined process will allow us to adopt 
MCAI safety requirements in a more efficient manner and will reduce 
safety risks to the public. This process continues to follow all FAA AD 
issuance processes to meet legal, economic, Administrative Procedure 
Act, and Federal Register requirements. We also continue to meet our 
technical decision-making responsibilities to identify and correct 
unsafe conditions on U.S.-certificated products.
    This AD references the MCAI and related service information that we 
considered in forming the engineering basis to correct the unsafe 
condition. The AD contains text copied from the MCAI and for this 
reason might not follow our plain language principles.

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 April 5, 2007 (72 FR 
16747). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been found that the fuel quantity probes harnesses 
installed in the left and right wing stub tanks on some Embraer ERJ-
170( ) aircraft models may not be protected in accordance with RBHA/
FAR (Regulamento Brasileiro de Homologac[atilde]o 
Aeron[aacute]utica/Federal Aviation Regulation) 25.981(a) and (b) 
requirements.

    The unsafe condition is potential ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could result 
in fuel tank explosions and consequent loss of the airplane. The MCAI 
requires inspection of the fuel quantity probes harnesses and correct 
reassembly if necessary. 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 our FAA policies. Any such differences 
are highlighted in a Note within the AD.

Costs of Compliance

    We estimate that this AD will affect 76 products of U.S. registry. 
We also estimate that it will take about 27 work-hours 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 $164,160, or $2,160 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

[[Page 32774]]

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://dms.dot.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:

2007-12-18 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-15096. Docket No. FAA-2007-27753; Directorate 
Identifier 2007-NM-022-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective July 19, 
2007.

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; 
certificated in any category; serial numbers 17000005 through 
17000013, 17000015, 17000016, 17000018 through 17000116, 17000118, 
and 17000119.

Subject

    (d) Fuel.

Reason

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

    It has been found that the fuel quantity probes harnesses 
installed in the left and right wing stub tanks on some Embraer ERJ-
170( ) aircraft models may not be protected in accordance with RBHA/
FAR (Regulamento Brasileiro de Homologac[atilde] to 
Aeron[aacute]utica/Federal Aviation Regulation) 25.981(a) and (b) 
requirements.

    The unsafe condition is potential ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could 
result in fuel tank explosions and consequent loss of the airplane. 
The MCAI requires inspection of the fuel quantity probes harnesses 
and correct reassembly if necessary.

Actions and Compliance

    (f) Within 6,000 flight hours after the effective date of this 
AD, unless already done, make an inspection in the fuel quantity 
probes harnesses installed on both wings and reassemble them, as 
applicable, as described in EMBRAER Service Bulletin 170-28-0011, 
dated April 26, 2006.

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:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. Send information to ATTN: Todd 
Thompson, Aerospace Engineer; International Branch, ANM-116, FAA, 
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; telephone (425) 227-1175; 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 2007-01-02, 
effective January 15, 2007; and EMBRAER Service Bulletin 170-28-
0011, dated April 26, 2006; for related information.

Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 170-28-0011, dated 
April 26, 2006, 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 June 1, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E7-11201 Filed 6-13-07; 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 2026-10-09T03:37:54.494995+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
85a297d5777c8e6b5cbc66d5e710b22fbfe46b199336d4719c131342416654aa
Text SHA-256
61aa3c995dd5a1884b0f975fbdd56cef15026d6dc63f6b600e68aca5805d5301

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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.