80 FR 42007 - Airworthiness Directives; Honeywell International Inc. Turboprop Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 136 (July 16, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 136 (July 16, 2015)
| Page Range | 42007-42010 | |
| FR Document | 2015-16587 |
[Federal Register Volume 80, Number 136 (Thursday, July 16, 2015)] [Rules and Regulations] [Pages 42007-42010] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-16587] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23706; Directorate Identifier 2006-NE-03-AD; Amendment 39-18177; AD 2015-12-04] RIN 2120-AA64 Airworthiness Directives; Honeywell International Inc. Turboprop Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. ----------------------------------------------------------------------- SUMMARY: The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Honeywell International Inc. TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -5AB, -5B, - 6, -6A, -10, -10AV, -10GP, -10GT, -10P, -10R, -10T, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, -11U, -12JR, -12UA, -12UAR, and -12UHR turboprop engines with certain Honeywell part numbers (P/Ns) of Woodward fuel control unit (FCU) assemblies, installed. The AD number in the document headings is incorrect. Additionally, the Amendment number in the regulatory text is incorrect. This document corrects these two errors. In all other respects, the original document remains the same. DATES: This final rule is effective on July 22, 2015. The effective date of AD 2015-12-04, Amendment 39-18177 (80 FR 34534, June 17, 2015) remains July 22, 2015. ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.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 this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562- 627-5246; fax: 562-627-5210; email: [email protected]. SUPPLEMENTARY INFORMATION: AD 2015-12-04, Amendment 39-18177, 80 FR 34534, June 17, 2015), requires initial and repetitive dimensional inspections of the affected fuel control drives and insertion of certain airplane operating procedures into the applicable flight manuals. As published, the AD number in the document headings is incorrect. Additionally, the Amendment number in the regulatory text of AD 2015- 12-04 is incorrect. No other part of the final rule has been changed. The effective date of AD 2015-12-04 remains July 22, 2015. Correction of Non-Regulatory Text In the Federal Register of June 17, 2015, AD 2015-12-04; Amendment 39-18177 (80 FR 34534) is corrected as follows: On page 34534, in the 2nd column, on line 6, change ``2014-12-04'' to ``2015-12-04''. Correction of Regulatory Text Sec. 39.13 [Corrected] 0 2. The FAA amends Sec. 39.13 by removing airworthiness directive (AD) 2006-15-08, Amendment 39-14688 (71 FR 41121, July 20, 2006), and adding the following new AD: 2015-12-04 Honeywell International Inc.: Amendment 39-18177; Docket No. FAA-2006-23706; Directorate Identifier 2006-NE-03-AD. (a) Effective Date This AD is effective August 20, 2015. (b) Affected ADs This AD replaces AD 2006-15-08, Amendment 39-14688 (71 FR 41121, July 20, 2006). (c) Applicability This AD applies to all Honeywell International Inc. TPE331-1, - 2, -2UA, -3U, -3UW, -5, -5A, -5AB, -5B, -6, -6A, -10, -10AV, -10GP, -10GT, -10P, -10R, -10T, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, - 11U, -12JR, -12UA, -12UAR, and -12UHR turboprop engines with Honeywell part numbers (P/Ns) for Woodward fuel control unit (FCU) assemblies listed in Table 1 to paragraph (c) of this AD, installed. Table 1 to Paragraph (c)--Affected FCU Assembly P/Ns ---------------------------------------------------------------------------------------------------------------- Group No. Engine FCU Assembly P/Ns ---------------------------------------------------------------------------------------------------------------- 1.......................... TPE331-1, -2, and -2UA......... P/N 869199-13, -20, -21, -22, -23, -24, -25, -26, 27, -28, -29, -31, -32, -33, -34, and -35. [[Page 42008]] 2 *........................ TPE331-1, -2, and -2UA......... P/N 869199-9, -10, -11, -12, -14, -16, -17, and - 18. 3.......................... TPE331-3U, -3UW, -5, -5A, -5AB, P/N 893561-7, -8, -9, -10, -11, -14, -15, -16, - -5B, -6, -6A, -10AV, -10GP, - 20, -26, -27, and -29; or 10GT, -10P, and -10T. P/N 897770-1, -3, -7, -9, -10, -11, -12, -14, -15, -16, -25, -26, and -28. 4 *........................ TPE331-3U, -3UW, -5, -5B, -6, - P/N 893561-4, -5, -12, and -13 or P/N 897770-5, - 6A, and -10T. 8, and -13. 5.......................... TPE331-10, -10R, -10U, -10UA, - P/N 897375-2, -3, -4, -5, -8, -9, -10, -11, -12, - 10UF, -10UG, -10UGR, -10UR, - 13, -14, -15, -16, -17, -19, -21, -24, -25, -26, 11U, -12JR, -12UA, -12UAR, and and -27; or -12UHR. P/N 897780-1, -2, -3, -4, -5, -6, -7, -8, -9, -10, -11, -14, -15, -16, -17, -18, -19, -20, -21, -22, -23, -24, -25, -26, -27, -30, -32, -34, -36, -37, and -38; or P/N 893561-17, -18, and -19. ---------------------------------------------------------------------------------------------------------------- * New/added FCU assembly P/Ns (d) Unsafe Condition We are issuing this AD to prevent failure of the fuel control drive that could result in damage to the engine and airplane. (e) Compliance Comply with this AD within the compliance times specified, unless already done. (1) Inspection of Engines With FCU Assembly P/Ns in Groups 2 and 4 For FCU assembly P/Ns in Groups 2 and 4 listed in Table 1 to paragraph (c) of this AD: (i) At the next scheduled inspection of the fuel control drive, or within 500 hours-in-service (HIS) after the effective date of this AD, whichever occurs first, inspect the fuel control drive for wear. (ii) Thereafter, re-inspect the fuel control drive within every 1,000 HIS since-last-inspection (SLI). (2) Inspection of Engines With FCU Assembly P/Ns in Groups 1, 3, and 5 For FCU assembly P/Ns in Groups 1, 3, or 5 listed in Table 1 to paragraph (c) of this AD: (i) If on the effective date of this AD the FCU assembly has 950 or more HIS SLI, inspect the fuel control drive for wear within 50 HIS from the effective date of this AD. (ii) If on the effective date of this AD the FCU assembly has fewer than 950 HIS SLI, inspect the fuel control drive for wear before reaching 1,000 HIS. (iii) Thereafter, re-inspect the fuel control drive for wear within every 1,000 HIS SLI. (3) Airplane Operating Procedures Within 60 days after the effective date of this AD, insert the information in Figure 1 to paragraph (e) of this AD, into the Emergency Procedures Section of the Airplane Flight Manual (AFM), Pilot Operating Handbook (POH), and the Manufacturer's Operating Manual (MOM). [[Page 42009]] [GRAPHIC] [TIFF OMITTED] TR16JY15.000 (f) Optional Terminating Action Replacing the affected FCU assembly with an FAA-approved FCU assembly P/N not listed in this AD is terminating action for the initial and repetitive inspections required by this AD, and for inserting the information in Figure 1 to paragraph (e) of this AD into the AFM, POH, and MOM. (g) Definitions For the purposes of this AD: (1) The ``fuel control drive'' is a series of mating splines located between the fuel pump and fuel control governor. (2) The fuel control drive consists of four drive splines: the fuel pump internal spline, the fuel control external ``quill shaft'' spline, and the stub shaft internal and external splines. (h) Alternative Methods of Compliance (AMOCs) The Manager, Los Angeles Aircraft Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. (i) Related Information (1) For more information about this AD, contact Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562-627-5246; fax: 562-627-5210; email: [email protected]. (2) Information pertaining to operating recommendations for affected engines after a fuel control drive failure is contained in Honeywell International Inc., Operating Information Letter (OIL) OI331-12R6, dated May 26, 2009, for multi-engine airplanes; and in OIL OI331-18R4, dated May 26, 2009, for single-engine airplanes. Information on fuel control drive inspection can be found in Section 72-00-00 of the applicable TPE331 maintenance manuals. These Honeywell International Inc., OILs and the TPE331 maintenance manuals, which are not incorporated by reference in this AD, can be obtained from Honeywell International Inc., using the contact information in paragraph (i)(3) of this AD. (3) For service information identified in this AD, contact Honeywell International Inc., 111 S. 34th Street, Phoenix, AZ 85034- 2802; Internet: https://myaerospace.honeywell.com/wps/portal/!ut; phone: 800-601-3099. (4) You may view this service information at the FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. (j) Material Incorporated by Reference None. [[Page 42010]] Issued in Burlington, Massachusetts, on June 26, 2015. Ann C. Mollica, Acting Directorate Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 2015-16587 Filed 7-15-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 136 / Thursday, July 16, 2015 / Rules and Regulations 42007
principal inspector, or lacking a principal DEPARTMENT OF TRANSPORTATION FAA, Transport Airplane Directorate,
inspector, the manager of the local flight 3960 Paramount Blvd., Lakewood, CA
standards district office/certificate holding Federal Aviation Administration 90712–4137; phone: 562–627–5246; fax:
district office. The AMOC approval letter 562–627–5210; email: joseph.costa@
must specifically reference this AD. 14 CFR Part 39
(2) Contacting the Manufacturer: For any
faa.gov.
requirement in this AD to obtain corrective [Docket No. FAA–2006–23706; Directorate SUPPLEMENTARY INFORMATION: AD 2015–
actions from a manufacturer, the action must Identifier 2006–NE–03–AD; Amendment 39– 12–04, Amendment 39–18177, 80 FR
be accomplished using a method approved 18177; AD 2015–12–04] 34534, June 17, 2015), requires initial
by the Manager, International Branch, ANM– and repetitive dimensional inspections
116, Transport Airplane Directorate, FAA; or RIN 2120–AA64
of the affected fuel control drives and
the European Aviation Safety Agency
(EASA); or Airbus’s EASA Design
Airworthiness Directives; Honeywell insertion of certain airplane operating
Organization Approval (DOA). If approved by International Inc. Turboprop Engines procedures into the applicable flight
the DOA, the approval must include the manuals.
AGENCY: Federal Aviation As published, the AD number in the
DOA-authorized signature.
Administration (FAA), DOT. document headings is incorrect.
(i) Related Information ACTION: Final rule; correction. Additionally, the Amendment number
Refer to Mandatory Continuing in the regulatory text of AD 2015–12–04
Airworthiness Information (MCAI) EASA SUMMARY: The FAA is correcting an
is incorrect.
Airworthiness Directive 2014–0191, dated airworthiness directive (AD) that
No other part of the final rule has
August 29, 2014, for related information. published in the Federal Register. That
This MCAI may be found in the AD docket been changed.
AD applies to all Honeywell
on the Internet at http:// The effective date of AD 2015–12–04
International Inc. TPE331–1, –2, –2UA,
www.regulations.gov/ remains July 22, 2015.
–3U, –3UW, –5, –5A, –5AB, –5B, –6,
#!documentDetail;D=FAA-2015-0086-0003.
–6A, –10, –10AV, –10GP, –10GT, –10P, Correction of Non-Regulatory Text
(j) Material Incorporated by Reference –10R, –10T, –10U, –10UA, –10UF, In the Federal Register of June 17,
(1) The Director of the Federal Register –10UG, –10UGR, –10UR, –11U, –12JR, 2015, AD 2015–12–04; Amendment 39–
approved the incorporation by reference –12UA, –12UAR, and –12UHR 18177 (80 FR 34534) is corrected as
(IBR) of the service information listed in this turboprop engines with certain follows:
paragraph under 5 U.S.C. 552(a) and 1 CFR Honeywell part numbers (P/Ns) of
part 51. On page 34534, in the 2nd column, on
Woodward fuel control unit (FCU) line 6, change ‘‘2014–12–04’’ to ‘‘2015–
(2) You must use this service information assemblies, installed. The AD number in
as applicable to do the actions required by 12–04’’.
the document headings is incorrect.
this AD, unless this AD specifies otherwise.
Additionally, the Amendment number Correction of Regulatory Text
(i) Airbus Service Bulletin A310–71–2038,
including Appendices 01 and 02, dated April in the regulatory text is incorrect. This
§ 39.13 [Corrected]
8, 2014. document corrects these two errors. In
(ii) Reserved. all other respects, the original document ■ 2. The FAA amends § 39.13 by
(3) For service information identified in remains the same. removing airworthiness directive (AD)
this AD, contact Airbus SAS, Airworthiness DATES: This final rule is effective on July 2006–15–08, Amendment 39–14688 (71
Office—EAW, 1 Rond Point Maurice FR 41121, July 20, 2006), and adding the
22, 2015. The effective date of AD 2015–
Bellonte, 31707 Blagnac Cedex, France; following new AD:
telephone +33 5 61 93 36 96; fax +33 5 61 12–04, Amendment 39–18177 (80 FR
93 44 51; email account.airworth-eas@ 34534, June 17, 2015) remains July 22, 2015–12–04 Honeywell International Inc.:
airbus.com; Internet http://www.airbus.com. 2015. Amendment 39–18177; Docket No.
(4) You may view this service information FAA–2006–23706; Directorate Identifier
ADDRESSES: You may examine the AD
at the FAA, Transport Airplane Directorate, 2006–NE–03–AD.
docket on the Internet at http://
1601 Lind Avenue SW., Renton, WA. For www.regulations.gov; or in person at the (a) Effective Date
information on the availability of this
Docket Management Facility between 9 This AD is effective August 20, 2015.
material at the FAA, call 425–227–1221.
(5) You may view this service information a.m. and 5 p.m., Monday through
(b) Affected ADs
that is incorporated by reference at the Friday, except Federal holidays. The AD
docket contains this AD, the regulatory This AD replaces AD 2006–15–08,
National Archives and Records
evaluation, any comments received, and Amendment 39–14688 (71 FR 41121, July 20,
Administration (NARA). For information on
2006).
the availability of this material at NARA, call other information. The address for the
202–741–6030, or go to: http:// Docket Office (phone: 800–647–5527) is (c) Applicability
www.archives.gov/federal-register/cfr/ibr- Document Management Facility, U.S. This AD applies to all Honeywell
locations.html. Department of Transportation, Docket International Inc. TPE331–1, –2, –2UA, –3U,
Issued in Renton, Washington, on July 2, Operations, M–30, West Building –3UW, –5, –5A, –5AB, –5B, –6, –6A, –10,
2015. Ground Floor, Room W12–140, 1200 –10AV, –10GP, –10GT, –10P, –10R, –10T,
Jeffrey E. Duven, New Jersey Avenue SE., Washington, –10U, –10UA, –10UF, –10UG, –10UGR,
DC 20590. –10UR, –11U, –12JR, –12UA, –12UAR, and
Manager, Transport Airplane Directorate,
–12UHR turboprop engines with Honeywell
Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: part numbers (P/Ns) for Woodward fuel
[FR Doc. 2015–17202 Filed 7–15–15; 8:45 am] Joseph Costa, Aerospace Engineer, Los control unit (FCU) assemblies listed in Table
BILLING CODE 4910–13–P Angeles Aircraft Certification Office, 1 to paragraph (c) of this AD, installed.
tkelley on DSK3SPTVN1PROD with RULES
TABLE 1 TO PARAGRAPH (C)—AFFECTED FCU ASSEMBLY P/NS
Group No. Engine FCU Assembly P/Ns
1 ..................... TPE331–1, –2, and –2UA ........................ P/N 869199–13, –20, –21, –22, –23, –24, –25, –26, –27, –28, –29, –31, –32, –33,
–34, and –35.
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![42010 Federal Register / Vol. 80, No. 136 / Thursday, July 16, 2015 / Rules and Regulations
Issued in Burlington, Massachusetts, on Internet: http://www.gippsaero.com/ received no comments on the NPRM (74
June 26, 2015. customer-support/technical- FR 21193, April 17, 2015) or on the
Ann C. Mollica, publications.aspx. You may view this determination of the cost to the public.
Acting Directorate Manager, Engine and referenced service information at the
Propeller Directorate, Aircraft Certification
Conclusion
FAA, Small Airplane Directorate, 901
Service. Locust, Kansas City, Missouri 64106. We reviewed the relevant data and
[FR Doc. 2015–16587 Filed 7–15–15; 8:45 am] For information on the availability of determined that air safety and the
BILLING CODE 4910–13–P this material at the FAA, call (816) 329– public interest require adopting the AD
4148. It is also available on the Internet as proposed except for minor editorial
at http://www.regulations.gov by changes. We have determined that these
DEPARTMENT OF TRANSPORTATION searching for and locating Docket No. minor changes:
FAA–2014–1123. • Are consistent with the intent that
Federal Aviation Administration was proposed in the NPRM (74 FR
FOR FURTHER INFORMATION CONTACT:
Doug Rudolph, Aerospace Engineer, 21193, April 17, 2015) for correcting the
14 CFR Part 39 unsafe condition; and
FAA, Small Airplane Directorate, 901
[Docket No. FAA–2014–1123; Directorate Locust, Room 301, Kansas City, • Do not add any additional burden
Identifier 2014–CE–037–AD; Amendment Missouri 64106; telephone: (816) 329– upon the public than was already
[39–18209; AD 2015–06–02 R1] 4059; fax: (816) 329–4090; email: proposed in the NPRM (74 FR 21193,
doug.rudolph@faa.gov. April 17, 2015).
RIN 2120–AA64
SUPPLEMENTARY INFORMATION: Relative Service Information Under 1
Airworthiness Directives; GA 8 Airvan CFR Part 51
(Pty) Ltd Airplanes Discussion
We reviewed GippsAero Mandatory
We issued a notice of proposed Service Bulletin SB–GA8–2014–115,
AGENCY: Federal Aviation rulemaking (NPRM) to amend 14 CFR
Administration (FAA), Department of Issue 1, dated October 6, 2014. The
part 39 to add an AD that would apply service bulletin describes procedures for
Transportation (DOT). to GA 8 Airvan (Pty) Ltd Model GA8– inspecting the orientation of the engine
ACTION: Final rule. TC320 airplanes. The NPRM was isolator mounts to verify proper
published in the Federal Register on installation, re-installing if necessary,
SUMMARY: We are revising an April 17, 2015 (74 FR 21193), and
airworthiness directive (AD) 2015–06– and installing steel washers on the
proposed to revise AD 2015–06–02, forward side of each side of the engine
02 for GA 8 Airvan (Pty) Ltd Model Amendment 39–18120 (80 FR 14810;
GA8–TC320 airplanes. This AD results isolator mounts. This service
March 20, 2015). information is reasonably available
from mandatory continuing The NPRM proposed to correct an
airworthiness information (MCAI) because the interested parties have
unsafe condition for the specified access to it through their normal course
issued by an aviation authority of products and was based on mandatory
another country to identify and correct of business or by the means identified
continuing airworthiness information in the ADDRESSES section of this AD.
an unsafe condition on an aviation originated by an airworthiness authority
product. The MCAI describes the unsafe of another country. The MCAI states Costs of Compliance
condition as missing required engine that:
mount fire seal washers, which could We estimate that this AD will affect
reduce the engine retention capability in A recent review of the engine mount 13 products of U.S. registry. We also
the event of a fire. We are issuing this installation on the GA8–TC 320 aircraft has estimate that it would take about 5
highlighted the omission of engine mount work-hours per product to comply with
AD to require actions to address the fire seal washers during the assembly
unsafe condition on these products. the basic requirements of this AD. The
process. average labor rate is $85 per work-hour.
DATES: This AD is effective August 20, The current engine mount configuration
Required parts would cost about $10 per
2015. does not meet the certification basis for the
aircraft, specifically regulation 23.865 of the product.
The Director of the Federal Register
approved the incorporation by reference Federal Aviation Regulations of the United Authority for This Rulemaking
States of America, where engine mounts
of a certain other publication listed in Title 49 of the United States Code
located in designated fire zones are required
this AD as of April 24, 2015 (80 FR to be suitably shielded so that they are specifies the FAA’s authority to issue
14810, March 20, 2015). capable of withstanding the effects of a fire. rules on aviation safety. Subtitle I,
ADDRESSES: You may examine the AD The Gippsland Aeronautics GA8–TC 320 section 106, describes the authority of
docket on the Internet at http:// aircraft require the installation of an the FAA Administrator. ‘‘Subtitle VII:
www.regulations.gov by searching for approved steel washer at each of the engine Aviation Programs,’’ describes in more
and locating Docket No. FAA–2014– mount locations to address a potential risk of detail the scope of the Agency’s
reduced engine retention capability in the
1123; or in person at the Docket authority.
event of a fire.
Management Facility, U.S. Department This AD, AD/GA8/8 Amdt 1, amends the We are issuing this rulemaking under
of Transportation, Docket Operations, applicability statement to be inclusive of the the authority described in ‘‘Subtitle VII,
M–30, West Building Ground Floor, affected aircraft serial number range. Part A, Subpart III, Section 44701:
Room W12–140, 1200 New Jersey The MCAI can be found in the AD General requirements.’’ Under that
Avenue SE., Washington, DC 20590. docket on the Internet at: http:// section, Congress charges the FAA with
For service information identified in www.regulations.gov/ promoting safe flight of civil aircraft in
tkelley on DSK3SPTVN1PROD with RULES
this AD, contact GA 8 Airvan (Pty) Ltd, #!documentDetail;D=FAA-2014-1123- air commerce by prescribing regulations
c/o GippsAero Pty Ltd, Attn: Technical 0007. for practices, methods, and procedures
Services, P.O. Box 881, Morwell the Administrator finds necessary for
Victoria 3840, Australia; telephone: + 61 Comments safety in air commerce. This regulation
03 5172 1200; fax: +61 03 5172 1201; We gave the public the opportunity to is within the scope of that authority
email: techpubs@gippsaero.com; participate in developing this AD. We because it addresses an unsafe condition
VerDate Sep<11>2014 16:14 Jul 15, 2015 Jkt 235001 PO 00000 Frm 00024 Fmt 4700 Sfmt 4700 E:\FR\FM\16JYR1.SGM 16JYR1](https://thefederalregister.org/doc/80_FR_42143/page/4.svg)
Document Created: 2015-12-15 13:13:45
Document Modified: 2015-12-15 13:13:45
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; correction. | |
| Dates | This final rule is effective on July 22, 2015. The effective date of AD 2015-12-04, Amendment 39-18177 (80 FR 34534, June 17, 2015) remains July 22, 2015. | |
| Contact | Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562- 627-5246; fax: 562-627-5210; email: [email protected] | |
| FR Citation | 80 FR 42007 | |
| RIN Number | 2120-AA64 |
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