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Docket ID: [Docket No. FAA-2007-28377; Directorate Identifier 2007-NM-063-AD]
RIN ID: RIN 2120-AA64
SUBJECT CATEGORY: Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes
DOCUMENT SUMMARY: We are revising an earlier NPRM for the products listed above. This action revises the earlier NPRM by expanding the scope. This proposed 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:
Periodic operational check of the firewall hydraulic shutoff
valves, made during routine maintenance, has revealed that the
failure rate of that component is significantly higher than
expected. Such a dormant failure, when combined with further
possible failures, such as engine fire, may lead to an unacceptable reduction of safety margins.
The unsafe condition is failure of the firewall hydraulic shutoff
valve, which, in combination with an engine fire, could result in loss
of hydraulic pressure or spread of an engine fire beyond the firewall.
The proposed AD would require actions that are intended to address the
unsafe condition described in the MCAI.
SUMMARY: Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes,
We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA2007 28377; Directorate Identifier 2007NM063AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments.
We will post all comments we receive, without change, to http:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD.
We proposed to amend 14 CFR part 39 with an earlier NPRM for the specified products, which was published in the Federal Register on June 25, 2007 (72 FR 34648). That earlier NPRM proposed to require actions intended to address the unsafe condition for the products listed above.
Since that NPRM was issued, we added Model 190200 STD, 200 LR, and 200 IGW airplanes to the U.S. type certificate data sheet (TCDS). We determined that this model is also affected by the identified unsafe condition. We revised paragraph (c) of this supplemental NPRM to include this model. In addition, we revised the Costs of Compliance paragraph of this supplemental NPRM to include additional U.S. registered airplanes of this model.
In addition, Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC), which is the aviation authority for Brazil, has issued Brazilian Airworthiness Directives 20070201R1 and 20070202R1, both effective August 27, 2007 (referred to after this as ``the MCAI''), to correct an unsafe condition for the specified products. The revised MCAI adds a reference to hydraulic shutoff valve, P/N 9752875. (This reference is explained in a comment from EMBRAER, which is discussed below.) The MCAI states:
Periodic operational check of the firewall hydraulic shutoff
valves, made during routine maintenance, has revealed that the
failure rate of that component is significantly higher than
expected. Such a dormant failure, when combined with further
possible failures, such as engine fire, may lead to an unacceptable reduction of safety margins.
The unsafe condition is failure of the firewall hydraulic shutoff
valve, which, in combination with an engine fire, could result in loss
of hydraulic pressure or spread of an engine fire beyond the firewall.
The MCAI requires repetitive operational checks of the firewall
hydraulic shutoff valve, and if necessary, replacement of the valve.
You may obtain further information by examining the MCAI in the AD docket.
EMBRAER has issued Service Bulletins 170290013 and 190290008, both Revision 01, both dated July 24, 2007. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI.
We have considered the following comments received on the earlier NPRM.
EMBRAER requests that we add P/N 9752875 to the applicability statement. EMBRAER states that P/N 9752873 (specified in the original NPRM) is reidentified to P/N 9752875 without any changes in its design when doing the actions of EMBRAER Service Bulletins 170290015 and 190290011, both dated May 11, 2007 (these service bulletins were not referenced in the NPRM).
We agree to add a reference to the new part number to this supplemental NPRM since hydraulic shutoff valves having that part number are subject to the identified unsafe condition. As discussed previously, ANAC has issued revised MCAI to address this new part number. Accordingly, we have revised paragraphs (c) and (f) of this supplemental NPRM to include a reference to P/N 9752875.
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service information
[[Page 36292]]
referenced above. We are proposing this AD because we evaluated all
pertinent information and determined an unsafe condition exists and is
likely to exist or develop on other products of the same type design.
Certain changes described above expand the scope of the earlier
NPRM. As a result, we have determined that it is necessary to reopen
the comment period to provide additional opportunity for the public to comment on this proposed 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 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 proposed different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a NOTE within the proposed AD.
Based on the service information, we estimate that this proposed AD would affect about 145 products of U.S. registry. We also estimate that it would take about 1 workhour per product to comply with the basic requirements of this proposed AD. The average labor rate is $80 per workhour. Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $11,600, or $80 per product, per inspection cycle.
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.
We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed regulation:
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 proposed AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety. The Proposed Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows: PART 39AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
2. The FAA amends Sec. 39.13 by adding the following new AD:
Empresa Brasileira De Aeronautica S.A. (EMBRAER): Docket No. FAA 200728377; Directorate Identifier 2007NM063AD.
Comments Due Date
(a) We must receive comments by July 21, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model ERJ 170100 LR, 100 STD,
100 SE, 100 SU, 200 LR, 200 STD, and 200 SU airplanes; and Model
ERJ 190100 STD, 100 LR, 100 IGW, 200 STD, 200 LR, and 200 IGW
airplanes; equipped with firewall hydraulic shutoff valves having part number (P/N) 9752873 or P/N 9752875.
Subject
(d) Air Transport Association (ATA) of America Code 29: Hydraulic power.
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:
Periodic operational check of the firewall hydraulic shutoff
valves, made during routine maintenance, has revealed that the
failure rate of that component is significantly higher than
expected. Such a dormant failure, when combined with further
possible failures, such as engine fire, may lead to an unacceptable reduction of safety margins.
The unsafe condition is failure of the firewall hydraulic shutoff
valve, which, in combination with an engine fire, could result in
loss of hydraulic pressure or spread of an engine fire beyond the
firewall. The MCAI requires repetitive operational checks of the
firewall hydraulic shutoff valve, and if necessary, replacement of the valve.
Actions and Compliance
(f) Unless already done, within the next 600 flight hours after
the effective date of this AD, perform an operational test for
proper operation of the firewall hydraulic shutoff valves P/N
9752873 or P/N 9752875, as applicable, in accordance with the
applicable service bulletin listed in Table 1 of this AD. If the
valve does not operate properly, before further flight, replace the
faulty hydraulic shutoff valve with another one bearing P/N 9752873
or P/N 9752875. Repeat the test thereafter at intervals that do not exceed 600 flight hours.
Note 1: For the purpose of this AD, an operational check is: ``A task to determine that an item is fulfilling its intended purpose. The check does not require quantitative tolerances. This is a failure finding task.''
EMBRAER Service Bulletin Revision level Date
170290013..................... Original.......... December 13, 2006.
170290013..................... 01................ July 24, 2007.
190290008..................... Original.......... December 13, 2006. [[Page 36293]]
190290008..................... 01................ July 24, 2007. 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, ANM
116, International Branch, 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: Sanjay
Ralhan, Aerospace Engineer, International Branch, ANM116, FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington 980573356; telephone (425) 2271405; fax (425) 2271149.
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 FAAapproved. Corrective actions are considered
FAAapproved 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 200702
01R1 and 20070202R1, both effective August 27, 2007; and the
service information listed in Table 2 of this AD for related information.
EMBRAER Service Bulletin Revision level Date 170290013..................... Original.......... December 13, 2006. 170290013..................... 01................ July 24, 2007. 190290008..................... Original.......... December 13, 2006. 190290008..................... 01................ July 24, 2007.
Issued in Renton, Washington, on June 12, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E814476 Filed 62508; 8:45 am]
BILLING CODE 491013P
FOR FURTHER INFORMATION CONTACT Sanjay Ralhan, Aerospace Engineer, International Branch, ANM116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 980573356; telephone (425) 2271405; fax (425) 2271149.
14 CFR Part 39 40 CFR Part 52 14 CFR Part 71 33 CFR Part 165 50 CFR Part 679 26 CFR Part 1 40 CFR Part 180 47 CFR Part 73 50 CFR Part 17 33 CFR Part 117 44 CFR Part 67 50 CFR Part 648 14 CFR Part 97 33 CFR Part 100 40 CFR Part 63 50 CFR Part 622 26 CFR Part 301 39 CFR Part 111 40 CFR Part 300 50 CFR Part 660 44 CFR Part 65 40 CFR Parts 52 and 81 40 CFR Part 271 47 CFR Part 64 50 CFR Part 665 47 CFR Part 76 50 CFR Part 229 14 CFR Part 23 14 CFR Part 25 21 CFR Part 522