Published 2007-06-14 · Federal Register document E7-11202
Airworthiness Directives; Aerospatiale Model ATR42 and ATR72 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 airworthiness authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as electrical arcing due to chafing between a bonding cable and electrical wires in the 120 VU (volt unit) electrical harness, causing the loss of some instruments and loss of one hydraulic circuit pressure (i.e., loss of pressure of one hydraulic circuit). We are issuing this AD to require actions to correct the unsafe condition on these products.
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[233]
- Raw source SHA-256
- daaa03e81018027354d93b79e2a5f918dd4e1ce116086c5ab24f0dfd782528aa
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2007-12-20
- Effective date printed in this edition
- 2007-07-19
Read 8 complete recorded clauses
Effective Date
Effective Date
(a) This airworthiness directive (AD) becomes effective July 19,
2007.
Exact source excerpt. Text positions 9723–9816, end exclusive, in the original decoded publication. SHA-256: 8db789295bd540ff7b9e13d6105ae59a289b524e7aed10a92349eba925a46a83
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 9816–9845, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to Model ATR42-200, -300, -320, and -500
airplanes; all serial numbers up to manufacturer serial number (MSN)
643 inclusive; and Model ATR72-101, -102, -201, -202, -211, -212,
and -212A airplanes, all serial numbers up to MSN 728 inclusive,
except MSN 723 and 725; certificated in any category.
Exact source excerpt. Text positions 9845–10184, end exclusive, in the original decoded publication. SHA-256: 5641377a40f0097e5b04c72722334597c1738f0d28460b0908069d7bc07e8490
Reason
Reason
(d) The mandatory continuing airworthiness information (MCAI)
states that recently an ATR 42 suffered electrical arcing, causing
the loss of some instruments and loss of one hydraulic circuit
pressure (i.e., loss of pressure of one hydraulic circuit) due to
chafing between a bonding cable and electrical wires in the 120 VU
(volt unit) electrical harness. The investigation showed that a
tubular support had been deformed and therefore impaired the spacing
among electrical harness, supports, and cables; the harness was not
correctly attached; the size of the harness was increased by
addition of cables (for Service Bulletins (SB) or customer
modifications embodiments); and the bonding cable was not correctly
installed. The MCAI mandates an inspection of the ATR 42 and ATR 72
fleet for correct installation of the bonding cable and restoring
correct installation of the bonding cable if necessary.
Exact source excerpt. Text positions 10184–11114, end exclusive, in the original decoded publication. SHA-256: 93b200aaf0dcfcc0ac084f9d7d293321434ecc526724977ea1209c1cbedc3377
Actions and Compliance
Actions and Compliance
(e) Unless already done, do the following actions. Within 3
months after the effective date of this AD: Inspect the harness
installation in the 120 VU electrical harness and, as applicable,
restore correct installation of the bonding cable, in accordance
with the instructions given by Avions de Transport
[[Page 32780]]
Regional Service Bulletins ATR42-92-0012 (for Model ATR42 airplanes)
and ATR72-92-1013 (for Model ATR72 airplanes), both dated July 4,
2006; or Revision 01, both dated December 7, 2006; as applicable.
FAA AD Differences
Note: This AD differs from the MCAI and/or service information
as follows: No differences.
Exact source excerpt. Text positions 11114–11790, end exclusive, in the original decoded publication. SHA-256: 0309508043c8395bc99bed3492ca584772b28a77dd9fb15f6492057894ca798a
Other FAA AD Provisions
Other FAA AD Provisions
(f) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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: Tom Rodriguez, Aerospace Engineer,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 227-1137; 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 11790–13116, end exclusive, in the original decoded publication. SHA-256: 7f3d66e0752abdddf3b15025d10fb8a93ccaa5f41af5515734bfc4fce4a8bd6a
Related Information
Related Information
(g) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2006-0283, dated September 14, 2006; and the Avions de
Transport Regional Service Bulletins specified in Table 1 of this AD
for related information.
Table 1.--Related Service Information
------------------------------------------------------------------------
Avions de transport regional
service bulletin Revision level Date
------------------------------------------------------------------------
ATR42-92-0012................ Original........ July 4, 2006.
ATR42-92-0012................ 01.............. December 7, 2006.
ATR72-92-1013................ Original........ July 4, 2006.
ATR72-92-1013................ 01.............. December 7, 2006
------------------------------------------------------------------------
Exact source excerpt. Text positions 13116–13997, end exclusive, in the original decoded publication. SHA-256: bf739e2515aae4d8c2ffa6f0d2ad24f46b500a567085fbc79646f1b0f38849e7
Material Incorporated by Reference
Material Incorporated by Reference
(h) You must use the applicable Avions de Transport Regional
Service Bulletins specified in Table 2 of this AD 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
Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03,
France.
(3) You may review copies at the FAA, Transport Airplane
Directorate, 1601 Lind Ave., 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.
Table 2.--Material Incorporated by Reference
------------------------------------------------------------------------
Avions de transport regional
service bulletin Revision level Date
------------------------------------------------------------------------
ATR42-92-0012................ Original........ July 4, 2006.
ATR42-92-0012................ 01.............. December 7, 2006.
ATR72-92-1013................ Original........ July 4, 2006.
ATR72-92-1013................ 01.............. December 7, 2006
------------------------------------------------------------------------
Exact source excerpt. Text positions 13997–15485, end exclusive, in the original decoded publication. SHA-256: 34c9e5faf882b04ab753541c1297d7be3bb215dd890fce99e35ca7b599351a60
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 2007-12-20 · 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.
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Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 8b0be0fc35e2c8facb2aff09ec8f43e1c331f6ea9d26f23cea338113f2ccb842. Source manifest: b5b2685f146d5824cabfad7a7f3d6f681351394b02e8d2f6e4bc6ac6fcc5c550.
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 32778-32780]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-11202]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27358; Directorate Identifier 2006-NM-270-AD;
Amendment 39-15098; AD 2007-12-20]
RIN 2120-AA64
Airworthiness Directives; Aerospatiale Model ATR42 and ATR72
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 airworthiness authority
of another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as electrical
arcing due to chafing between a bonding cable and electrical wires in
the 120 VU (volt unit) electrical harness, causing the loss of some
instruments and loss of one hydraulic circuit pressure (i.e., loss of
pressure of one hydraulic circuit). 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 certain publications 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: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1137; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
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 allow 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.
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 March 2, 2007 (72 FR
9475). That NPRM proposed to require inspecting the harness
installation in the 120 VU (volt unit) electrical harness and, as
applicable, restoring correct installation of the bonding cable. The
MCAI states that recently an ATR 42 suffered electrical arcing, causing
the loss of some instruments and loss of one hydraulic circuit pressure
(i.e., loss of pressure of one hydraulic circuit) due to chafing
between a bonding cable and electrical wires in the 120 VU electrical
harness. The investigation showed that a tubular support had been
deformed and therefore impaired the spacing among electrical harness,
supports, and cables; the harness was not correctly attached; the size
of the harness was increased by addition of cables (for Service
Bulletins (SB) or customer modifications embodiments); and the bonding
cable was not correctly installed. The MCAI mandates an inspection of
the ATR 42 and ATR 72 fleet for correct installation of the bonding
cable and restoring correct installation of the bonding cable if
necessary.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received.
Request To Include Revised Service Bulletins
Avions de Transport Regional (ATR) states that in the NPRM
reference is made to Avions de Transport Regional
[[Page 32779]]
Service Bulletins ATR42-92-0012 and ATR72-92-1013, both dated July 4,
2006. ATR notes that this corresponds to the original issue of both
service bulletins, and adds that those bulletins have been revised to
add a reference to European Aviation Safety Agency Airworthiness
Directive 2006-0283. ATR states that nothing else has been changed, and
suggests that the AD reference Avions de Transport Regional Service
Bulletins ATR42-92-0012 and ATR72-92-1013, both Revision 01, both dated
December 7, 2006.
We agree to reference Revision 01 of the service bulletins in the
AD. We have reviewed Revision 01 of the service bulletins, and the
procedures are essentially the same as those in the original issues, as
noted by ATR. We have changed paragraphs (e) and (g) of this AD to
specify Revision 01 of the service bulletins.
Conclusion
We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD with the change described previously. We determined that this change
will not increase the economic burden on any operator or increase the
scope of the AD.
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 a U.S. court of
law. 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 described in a separate paragraph of the AD. These requirements, if
any, take precedence over the actions copied from the MCAI.
Costs of Compliance
Based on the service information, we estimate that this AD affects
about 53 products of U.S. registry. We also estimate that it takes
about 1 work-hour per product to comply with this AD. The average labor
rate is $80 per work-hour. Based on these figures, we estimate the cost
of the inspection on U.S. operators to be $4,240, 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 that 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://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:
2007-12-20 Aerospatiale: Amendment 39-15098. Docket No. FAA-2007-
27358; Directorate Identifier 2006-NM-270-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective July 19,
2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model ATR42-200, -300, -320, and -500
airplanes; all serial numbers up to manufacturer serial number (MSN)
643 inclusive; and Model ATR72-101, -102, -201, -202, -211, -212,
and -212A airplanes, all serial numbers up to MSN 728 inclusive,
except MSN 723 and 725; certificated in any category.
Reason
(d) The mandatory continuing airworthiness information (MCAI)
states that recently an ATR 42 suffered electrical arcing, causing
the loss of some instruments and loss of one hydraulic circuit
pressure (i.e., loss of pressure of one hydraulic circuit) due to
chafing between a bonding cable and electrical wires in the 120 VU
(volt unit) electrical harness. The investigation showed that a
tubular support had been deformed and therefore impaired the spacing
among electrical harness, supports, and cables; the harness was not
correctly attached; the size of the harness was increased by
addition of cables (for Service Bulletins (SB) or customer
modifications embodiments); and the bonding cable was not correctly
installed. The MCAI mandates an inspection of the ATR 42 and ATR 72
fleet for correct installation of the bonding cable and restoring
correct installation of the bonding cable if necessary.
Actions and Compliance
(e) Unless already done, do the following actions. Within 3
months after the effective date of this AD: Inspect the harness
installation in the 120 VU electrical harness and, as applicable,
restore correct installation of the bonding cable, in accordance
with the instructions given by Avions de Transport
[[Page 32780]]
Regional Service Bulletins ATR42-92-0012 (for Model ATR42 airplanes)
and ATR72-92-1013 (for Model ATR72 airplanes), both dated July 4,
2006; or Revision 01, both dated December 7, 2006; as applicable.
FAA AD Differences
Note: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(f) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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: Tom Rodriguez, Aerospace Engineer,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 227-1137; 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
(g) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2006-0283, dated September 14, 2006; and the Avions de
Transport Regional Service Bulletins specified in Table 1 of this AD
for related information.
Table 1.--Related Service Information
------------------------------------------------------------------------
Avions de transport regional
service bulletin Revision level Date
------------------------------------------------------------------------
ATR42-92-0012................ Original........ July 4, 2006.
ATR42-92-0012................ 01.............. December 7, 2006.
ATR72-92-1013................ Original........ July 4, 2006.
ATR72-92-1013................ 01.............. December 7, 2006
------------------------------------------------------------------------
Material Incorporated by Reference
(h) You must use the applicable Avions de Transport Regional
Service Bulletins specified in Table 2 of this AD 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
Aerospatiale, 316 Route de Bayonne, 31060 Toulouse, Cedex 03,
France.
(3) You may review copies at the FAA, Transport Airplane
Directorate, 1601 Lind Ave., 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.
Table 2.--Material Incorporated by Reference
------------------------------------------------------------------------
Avions de transport regional
service bulletin Revision level Date
------------------------------------------------------------------------
ATR42-92-0012................ Original........ July 4, 2006.
ATR42-92-0012................ 01.............. December 7, 2006.
ATR72-92-1013................ Original........ July 4, 2006.
ATR72-92-1013................ 01.............. December 7, 2006
------------------------------------------------------------------------
Issued in Renton, Washington, on June 1, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-11202 Filed 6-13-07; 8:45 am]
BILLING CODE 4910-13-P
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