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Published 2007-10-16 · Federal Register document E7-20222

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ 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[376]
Raw source SHA-256
daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2007-21-12
Effective date printed in this edition
2007-11-20
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This airworthiness directive (AD) becomes effective November 
20, 2007.

Exact source excerpt. Text positions 7847–7944, end exclusive, in the original decoded publication. SHA-256: 3c12ba770576165dbad784c08e616f08d4970cbe96150266ae3b360c19ac12c9

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 7944–7973, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to EMBRAER Model EMB-135BJ airplanes, 
certificated in any category; as identified in EMBRAER Service 
Bulletin 145LEG-28-0016, Revision 01, dated June 27, 2005.

Exact source excerpt. Text positions 7973–8175, end exclusive, in the original decoded publication. SHA-256: da29eac5deb807a5a3f382afaeef8d8590dc719f66b5ed7c3dca374c5a583ac6

Subject
Subject

    (d) Air Transport Association (ATA) of America Code 28: Fuel.

Exact source excerpt. Text positions 8175–8251, end exclusive, in the original decoded publication. SHA-256: 564a3b0bb8d7b5a1810f3275157fec0cd09c337ce3688635ce34abdf3119127f

Reason
Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    It has been found cases in which some wiring harnesses were not 
protected in accordance with SFAR-88 (Special Federal Aviation 
Regulation No. 88) requirements.
    The potential of ignition sources, in combination with flammable 
fuel vapors, could result in fuel tank explosions and consequent 
loss of the airplane. The corrective action includes installing heat 
shrinkable sleeves on the inspection and refueling panel 
illumination lights wiring, and installing nipples on the terminal 
lugs to protect the wire terminals.

Exact source excerpt. Text positions 8251–8869, end exclusive, in the original decoded publication. SHA-256: 17ca2fa0696ac9f75d4f1fa0f42d0ffe253270093a85516651f4b6c35663a577

Actions and Compliance
Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Within 5,000 flight hours after the effective date of this 
AD, install heat shrinkable sleeves on the inspection and refueling 
panel illumination lights wiring, and install nipples on the 
terminal lugs to protect the wire terminals, in accordance with the 
detailed instructions and procedures in EMBRAER Service Bulletin 
145LEG-28-0016, Revision 01, dated June 27, 2005.
    (2) Actions done before the effective date of this AD in 
accordance with EMBRAER Service Bulletin 145LEG-28-0016, dated March 
8, 2004, are acceptable for compliance with the corresponding 
actions of this AD.

FAA AD Differences

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

Exact source excerpt. Text positions 8869–9665, end exclusive, in the original decoded publication. SHA-256: 97ab67ba1af623c2e726d5d1eae524c7d5ca666c44a663c878f3aaf43f7b97f7

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: Dan 
Rodina, Aerospace Engineer, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 
98057-3356; telephone (425) 227-2125; 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

[[Page 58504]]

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 9665–11106, end exclusive, in the original decoded publication. SHA-256: ec8209243367f61ccb27d8154a918a9d3f6d4c71a8586627149896f9dba0c589

Related Information
Related Information

    (h) Refer to MCAI Brazilian Airworthiness Directive 2006-07-02, 
effective August 21, 2006, and EMBRAER Service Bulletin 145LEG-28-
0016, Revision 01, dated June 27, 2005, for related information.

Exact source excerpt. Text positions 11106–11329, end exclusive, in the original decoded publication. SHA-256: 4b055609dd36527dc97607434550171ee9fb6c5c1f608876d61aa0b577fa13cb

Material Incorporated by Reference
Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 145LEG-28-0016, 
Revision 01, dated June 27, 2005, 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, Sa~o 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 11329–12210, end exclusive, in the original decoded publication. SHA-256: 1a36e22f5df5ddd7d6d557c2d06e36d106684bed712bd9efa6a1f40745a1324b

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 2007-21-12 · 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: a2e18124540a33c9e12460a05c3d95ff147ea1406cd276bc44e45096376bd2e1. Source manifest: 63bc1a2dff11d7d4c56288571a7483e75c2ef3e1e84d99019724a0651787ec25.

Official source · 2007-10-16

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 199 (Tuesday, October 16, 2007)]
[Rules and Regulations]
[Pages 58502-58504]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-20222]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28909; Directorate Identifier 2007-NM-135-AD; 
Amendment 39-15230; AD 2007-21-12]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-135BJ 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 in which some wiring harnesses were not 
protected in accordance with SFAR-88 (Special Federal Aviation 
Regulation No. 88) requirements.

    The potential of ignition sources, 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 November 20, 2007.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of November 20, 
2007.

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: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-2125; 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 August 8, 2007 (72 
FR 44435). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been found cases in which some wiring harnesses were not 
protected in accordance with SFAR-88 (Special Federal Aviation 
Regulation No. 88) requirements.

    The potential of ignition sources, in combination with flammable 
fuel vapors, could result in fuel tank explosions and consequent loss 
of the airplane. The corrective action includes installing heat 
shrinkable sleeves on the inspection and refueling panel illumination 
lights wiring, and installing nipples on the terminal lugs to protect 
the wire terminals. 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

[[Page 58503]]

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 about 8 products of U.S. 
registry. We also estimate that it will take about 6 work-hours per 
product to comply with the basic requirements of this AD. The average 
labor rate is $80 per work-hour. Required parts will cost about $32 per 
product. Where the service information lists required parts costs that 
are covered under warranty, we have assumed that there will be no 
charge for these parts. As we do not control warranty coverage for 
affected parties, some parties may incur costs higher than estimated 
here. Based on these figures, we estimate the cost of this AD to the 
U.S. operators to be $4,096, or $512 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:

2007-21-12 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-15230. Docket No. FAA-2007-28909; Directorate 
Identifier 2007-NM-135-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective November 
20, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to EMBRAER Model EMB-135BJ airplanes, 
certificated in any category; as identified in EMBRAER Service 
Bulletin 145LEG-28-0016, Revision 01, dated June 27, 2005.

Subject

    (d) Air Transport Association (ATA) of America Code 28: Fuel.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    It has been found cases in which some wiring harnesses were not 
protected in accordance with SFAR-88 (Special Federal Aviation 
Regulation No. 88) requirements.
    The potential of ignition sources, in combination with flammable 
fuel vapors, could result in fuel tank explosions and consequent 
loss of the airplane. The corrective action includes installing heat 
shrinkable sleeves on the inspection and refueling panel 
illumination lights wiring, and installing nipples on the terminal 
lugs to protect the wire terminals.

Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Within 5,000 flight hours after the effective date of this 
AD, install heat shrinkable sleeves on the inspection and refueling 
panel illumination lights wiring, and install nipples on the 
terminal lugs to protect the wire terminals, in accordance with the 
detailed instructions and procedures in EMBRAER Service Bulletin 
145LEG-28-0016, Revision 01, dated June 27, 2005.
    (2) Actions done before the effective date of this AD in 
accordance with EMBRAER Service Bulletin 145LEG-28-0016, dated March 
8, 2004, are acceptable for compliance with the corresponding 
actions of this AD.

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, 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: Dan 
Rodina, Aerospace Engineer, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 
98057-3356; telephone (425) 227-2125; 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

[[Page 58504]]

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 2006-07-02, 
effective August 21, 2006, and EMBRAER Service Bulletin 145LEG-28-
0016, Revision 01, dated June 27, 2005, for related information.

Material Incorporated by Reference

    (i) You must use EMBRAER Service Bulletin 145LEG-28-0016, 
Revision 01, dated June 27, 2005, 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, Sa~o 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 October 5, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E7-20222 Filed 10-15-07; 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 2026-10-09T03:35:30.274606+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
43862453aca96fc2eb30216de5df5753afcb0334e3b8658e680d14737250da8b
Text SHA-256
a2e18124540a33c9e12460a05c3d95ff147ea1406cd276bc44e45096376bd2e1

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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.

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