Airworthiness Directives; Liberty Aerospace Incorporated Model XL-2 Airplanes, 20265-20268 [2010-8596]
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Federal Register / Vol. 75, No. 74 / Monday, April 19, 2010 / Rules and Regulations
actions to the affected customers and
clearly advise them, in writing, that
such actions will void the FDIC’s
guarantee with respect to the swept,
transferred, or reclassified funds.
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■ 5. Amend § 370.7 by revising
paragraphs (b) and (c) to read as follows:
§ 370.7 Assessment for the Transaction
Account Guarantee program.
WReier-Aviles on DSKGBLS3C1PROD with RULES
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(b) Initiation of assessments.
Beginning on November 13, 2008 each
eligible entity that does not opt out of
the transaction account guarantee
program on or before December 5, 2008
will be required to pay the FDIC
assessments on all deposit amounts in
noninterest-bearing transaction accounts
calculated in accordance with paragraph
(c) of this section.
(c) Amount of assessment.
(1) Except as provided in paragraphs
(c)(2) and (c)(3) of this section any
eligible entity that does not opt out of
the transaction account guarantee
program shall pay quarterly an
annualized 10 basis point assessment on
any deposit amounts exceeding the
existing deposit insurance limit of
$250,000, as reported on its quarterly
Consolidated Reports of Condition and
Income, Thrift Financial Report, or
Report of Assets and Liabilities of U.S.
Branches and Agencies of Foreign Banks
(each, a ‘‘Call Report’’) in any
noninterest-bearing transaction accounts
(as defined in § 370.2(h)), including any
such amounts swept from a noninterestbearing transaction account into an
noninterest-bearing savings deposit
account as provided in § 370.4(c).
(2) For the period after December 31,
2009 through and including June 30,
2010, each participating entity that does
not opt out of the transaction account
guarantee program in accordance with
§ 370.5(c)(2) shall pay quarterly a fee
based upon its Risk Category rating. The
amount of the fee for each such entity
is equal to the annualized, TAG
assessment rate for the entity multiplied
by the amount of the deposits held in
noninterest-bearing transaction accounts
(as defined in § 370.2(h) and including
any amounts swept from a noninterestbearing transaction account into an
noninterest-bearing savings deposit
account as provided in § 370.4(c)) that
exceed the existing deposit insurance
limit of $250,000, as reported on the
entity’s most recent quarterly Call
Report.
(3) Beginning on July 1, 2010, each
participating entity that does not opt out
of the transaction account guarantee
program shall pay quarterly a fee based
upon its Risk Category rating. The
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amount of the fee for each such entity
is equal to the annualized, TAG
assessment rate for the entity multiplied
by the aggregate amount of the deposits
held in noninterest-bearing transaction
accounts (as defined in § 370.2(h) and
including any amounts swept from a
noninterest-bearing transaction account
into an noninterest-bearing savings
deposit account as provided in
§ 370.4(c)) that exceed the existing
deposit insurance limit of $250,000,
calculated based upon the average daily
balances in such accounts as reported
on the entity’s most recent quarterly
Call Report.
(4) The annualized TAG assessment
rates are as follows:
(i) 15 basis points, for the portion of
each quarter in which the entity is
assigned to Risk Category I;
(ii) 20 basis points, for the portion of
each quarter in which the entity is
assigned to Risk Category II; and
(iii) 25 basis points, for the portion of
each quarter in which the entity is
assigned to either Risk Category III or
Risk Category IV.
(5) The amount to be reported for each
noninterest-bearing transaction account
as the average daily balance is the total
dollar amount held in such account that
exceeds $250,000 for each calendar day
during the quarter divided by the
number of calendar days in the quarter.
For those days that an office of the
reporting institution is closed (e.g.,
Saturdays, Sundays, or holidays), the
amounts outstanding from the previous
business day should be used. The total
number of accounts to be reported
should be calculated on the same basis.
Documentation supporting the amounts
used in the calculation of the average
daily balance amounts must be retained
and be readily available upon request by
the FDIC or the institution’s primary
Federal regulator. In addition, all
institutions that do not opt of the
transaction account guarantee program
must establish procedures to gather the
necessary daily data beginning July 1,
2010.
(6) An entity’s Risk Category is
determined in accordance with the
FDIC’s risk-based premium system
described in 12 CFR part 327. The
assessments provided in this paragraph
(c) shall be in addition to an
institution’s risk-based assessment
imposed under Part 327.
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By order of the Board of Directors.
Dated at Washington, DC, this 13th day of
April, 2010.
PO 00000
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Federal Deposit Insurance Corporation.
Robert E. Feldman,
Executive Secretary.
[FR Doc. 2010–8911 Filed 4–16–10; 8:45 am]
BILLING CODE 6714–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0329; Directorate
Identifier 2009–CE–020–AD; Amendment
39–16264; AD 2009–08–05 R1]
RIN 2120–AA64
Airworthiness Directives; Liberty
Aerospace Incorporated Model XL–2
Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are correcting the address,
telephone, and fax information for the
reporting requirement in Airworthiness
Directive (AD) 2009–08–05, which
applies to certain Liberty Aerospace
Incorporated Model XL–2 airplanes. AD
2009–08–05 currently requires
repetitively inspecting the exhaust
muffler for cracks, replacing the exhaust
muffler when cracks are found, and
reporting the results of the inspections
to the FAA. Since AD 2009–08–05
became effective, the FAA’s Atlanta
Aircraft Certification Office (ACO)
moved, which has caused the office
personnel problems in receiving fax and
mailed copies of the inspection result
reports. This document corrects the
mailing address, telephone number, and
fax information of the Atlanta ACO.
DATES: This final rule is effective April
19, 2010. The compliance date of this
AD is April 20, 2009, which is the same
as the effective date of AD 2009–08–05.
As of April 20, 2009 (74 FR 16117,
April 9, 2009), the Director of the
Federal Register approved the
incorporation by reference of Liberty
Aerospace, Inc. Service Document
Critical Service Bulletin (CSB) CSB–09–
001, Revision Level B, Revised on
March 18, 2009.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at
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:
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Federal Register / Vol. 75, No. 74 / Monday, April 19, 2010 / Rules and Regulations
—Corey Spiegel, Aerospace Engineer,
Atlanta Aircraft Certification Office,
1701 Columbia Avenue, College Park,
Georgia 30337; telephone: (404) 474–
5574; facsimile: (404) 474–5606;
e-mail: corey.spiegel@faa.gov; or
—Cindy Lorenzen, Aerospace Engineer,
Atlanta Aircraft Certification Office,
1701 Columbia Avenue, College Park,
Georgia 30337; telephone: (404) 474–
5524; facsimile: (404) 474–5606;
e-mail: cindy.lorenzen@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On April 3, 2009, we issued AD 2009–
08–05, Amendment 39–15878 (74 FR
16117, April 9, 2009), to require
repetitively inspecting the exhaust
muffler for cracks, replacing the exhaust
muffler when cracks are found, and
reporting the results of the inspections
to the FAA.
Since AD 2009–08–05 became
effective, the FAA’s Atlanta Aircraft
Certification Office (ACO) moved,
which has caused the office personnel
problems in receiving fax and mailed
copies of the inspection result reports.
Consequently, the FAA sees a need to
correct the mailing address, telephone
number, and fax information of the
Atlanta ACO in AD 2009–08–05 to
assure that the inspection results are
received and reviewed to help assure
the continued operational safety of the
affected airplanes. Thus, the FAA is
revising the AD to incorporate the
language discussed above and to add the
amendment to section 39.13 of the
Federal Aviation Regulations (14 CFR
39.13).
Since this action only corrects the
address, telephone number, and fax
information for the reporting
requirement and does not require any
additional actions over that originally
required by AD 2009–08–05, it has no
adverse economic impact and imposes
no additional burden on any person
than was already required. Therefore,
the FAA has determined that prior
notice and opportunity for public
comment are unnecessary.
§ 39.13
List of Subjects in 14 CFR Part 39
Applicability
(c) This AD applies to Model XL–2
airplanes, serial numbers 0007, 0009, and
subsequent, that are certificated in any
category.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
■
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by
removing Airworthiness Directive (AD)
2009–08–05, Amendment 39–15878 (74
FR 16117, April 9, 2009), and adding
the following new AD:
■
2009–08–05 R1 Liberty Aerospace
Incorporated: Amendment 39–16264;
Docket No. FAA–2009–0329; Directorate
Identifier 2009–CE–020–AD.
Effective Date
(a) This final rule is effective April 19,
2010. The compliance date of this AD is
April 20, 2009, which is the same as the
effective date of AD 2009–08–05.
Affected ADs
(b) This AD revises AD 2009–08–05.
Unsafe Condition
(d) This AD is the result of reports that
eight cracks have been found in the exhaust
muffler during maintenance and service
inspections. We are issuing this AD to detect
and correct cracks in the exhaust muffler,
which could result in carbon monoxide
entering the cabin heating system. This
condition could lead to incapacitation of the
pilot.
Compliance
(e) To address this problem, you must do
the following, unless already done:
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Actions
Compliance
Procedures
(1) Inspect the following:
(i) The exhaust muffler for cracks. There
are two different exhaust systems available for the affected airplanes. They are:
(A) Standard exhaust system, part
number (P/N) DEL200201–002 that
incorporates
muffler
P/N
DEL200201–101; and
(B) Reduced sound exhaust system,
P/N DEL200201–003 that incorporates muffler P/N 200201–104.
(ii) The tail pipe and the tail pipe opening
in the lower cowl for a 0.5-inch minimum
clearance.
(iii) Inspect the propeller for proper propeller clocking position.
(2) As a result of the inspections required in
paragraphs (e)(1)(ii) and (e)(1)(iii) of this AD:
(i) If the clearance between the tail pipe
and the tail pipe opening is less than the
required 0.5-inch minimum, trim the
lower cowl as needed to achieve the
minimum clearance.
(ii) If there is a discrepancy in the propeller
clocking position, remove and reinstall
the propeller at the correct position.
Initially inspect within the next 10 hours timein-service (TIS) after April 20, 2009 (the effective date of AD 2009–08–05) or at the
next annual inspection, whichever occurs
first. Repetitively inspect the exhaust muffler thereafter as specified in paragraph
(e)(5) of this AD.
Follow Liberty Aerospace, Inc. Service Document Critical Service Bulletin (CSB) CSB–
09–001, Revision Level B, Revised on
March 18, 2009.
Before further flight after the inspection required in paragraph (e)(1) of this AD.
As specified in Liberty Aerospace, Inc. Service Document Critical Service Bulletin
(CSB) CSB–09–001, Revision Level B, Revised on March 18, 2009.
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Federal Register / Vol. 75, No. 74 / Monday, April 19, 2010 / Rules and Regulations
20267
Actions
Compliance
Procedures
(3) As a result of the initial inspection required
in paragraph (e)(1)(i) of this AD or any repetitive inspection required in paragraph (e)(5)
of this AD, if a crack is found, replace the exhaust muffler.
(i) The manufacturer will provide the replacement exhaust system.
(ii) A reduced sound exhaust system may
be replaced with a standard exhaust system.
(iii) Installing a reduced sound exhaust system as a replacement part also requires
installing a bypass SCAT tube and a ‘‘Do
Not Use’’ placard on or near the heater
knob.
(4) If the airplane is equipped with a reduced
sound exhaust system and no cracks are
found during the initial inspection required in
paragraph (e)(1) of this AD, install a bypass
SCAT tube and a ‘‘Do Not Use’’ placard on
or near the heater knob.
(5) If no cracks are found in the exhaust muffler
during the initial inspection required in paragraph (e)(1) of this AD or if the exhaust muffler was replaced as required in paragraph
(e)(3) of this AD, repetitively inspect thereafter at the intervals specified in paragraphs
(e)(5)(i), (e)(5)(ii), and (e)(5)(iii) of this AD.
Before further flight after the initial inspection
required in paragraph (e)(1) of this AD and
before further flight after any repetitive inspection required in paragraph (e)(5) of this
AD.
Follow Liberty Aerospace, Inc. Service Document Critical Service Bulletin (CSB) CSB–
09–001, Revision Level B, Revised on
March 18, 2009.
Within the next 10 hours TIS after April 20,
2009 (the effective date of AD 2009–08–
05).
Follow Liberty Aerospace, Inc. Service Document Critical Service Bulletin (CSB) CSB–
09–001, Revision Level B, Revised on
March 18, 2009.
(i) For airplanes equipped with a standard exhaust system and the optional bypass
SCAT tube has not been installed, repetitively inspect thereafter every 25 hours TIS
or every 12 months, whichever occurs first.
(ii) For airplanes equipped with a standard exhaust system and the optional bypass
SCAT tube has been installed, repetitively
inspect thereafter every 50 hours TIS or
every 12 months, whichever occurs first.
(iii) For airplanes equipped with a reduced
sound exhaust system and the required bypass SCAT tube has been installed, repetitively inspect thereafter every 50 hours TIS
or every 12 months, whichever occurs first.
Within 10 days after each inspection required
by this AD.
Follow Liberty Aerospace, Inc. Service Document Critical Service Bulletin (CSB) CSB–
09–001, Revision Level B, Revised on
March 18, 2009.
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(6) Report the results of the following inspections required in this AD to the FAA.
(i) Initial inspection required in paragraph
(e)(1) of this AD.
(ii) Repetitive inspections required in paragraph (e)(5) of this AD only if cracks are
found.
(iii) The Office of Management and Budget
(OMB) approved the information collection requirements contained in this regulation under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C.
3501 et seq.) and assigned OMB Control
Number 2120–0056.
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Use the form (Figure 1 of this AD) and submit
it to FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park,
Georgia 30337; fax: (404) 474–5606; e-mail
corey.spiegel@faa.gov.
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Federal Register / Vol. 75, No. 74 / Monday, April 19, 2010 / Rules and Regulations
AD 2009–08–05 R1 Inspection Report
Airplane Serial Number
Airplane Tach Hours at time of inspection
Propeller type (circle one)
MT
Sensenich
Exhaust Type (circle one)
Standard
Reduced Sound
Is Exhaust Cracked? (circle one)
YES
NO
Did lower cowl require trimming at the tail pipe opening? (circle one)
Not applicable after initial inspection
YES
NO
Did the propeller clocking position need to be corrected? (circle one)
Not applicable after initial inspection.
YES
NO
Propeller Tach Hours at time of inspection
Were any other discrepancies noticed during the inspection?
Name:
Telephone and/or e-mail address:
Date:
Send report to: Corey Spiegel, Aerospace Engineer, Atlanta ACO,
1701 Columbia Avenue, College Park, Georgia 30337;
facsimile: (404) 474–5606; e-mail: corey.spiegel@faa.gov.
Figure 1
Special Flight Permit
(f) Under 14 CFR part 39.23, we are
limiting the special flight permits for this AD
by the following conditions:
(1) The cabin heat turned off; and
(2) The fresh air vents are open.
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Alternative Methods of Compliance
(AMOCs)
(g) The Manager, Atlanta Aircraft
Certification Office (ACO), 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: Corey
Spiegel, Aerospace Engineer, Atlanta ACO,
1701 Columbia Avenue, College Park,
Georgia 30337. 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.
Material Incorporated by Reference
(h) You must use Liberty Aerospace, Inc.
Service Document Critical Service Bulletin
(CSB) CSB–09–001, Revision Level B,
Revised on March 18, 2009, to do the actions
required by this AD, unless the AD specifies
otherwise.
(1) On April 20, 2009 (74 FR 16117, April
9, 2009), the Director of the Federal Register
previously 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 Liberty Aerospace, 100
Aerospace Drive, Melbourne, Florida 32901;
telephone: (321) 752–0332 or (800) 759–5953;
fax: (321) 752–0377; Internet: https://
www.libertyaircraft.com.
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(3) You may review copies of the service
information incorporated by reference for
this AD at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas
City, Missouri 64106. For information on the
availability of this material at the Central
Region, call (816) 329–3768.
(4) You may also review copies of the
service information incorporated by reference
for this AD 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: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Issued in Kansas City, Missouri, on April
7, 2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2010–8596 Filed 4–16–10; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
DEPARTMENT OF HEALTH AND
HUMAN SERVICES
Food and Drug Administration
21 CFR Part 522
[Docket No. FDA–2010–N–0002]
Implantation or Injectable Dosage
Form New Animal Drugs; Change of
Sponsor; Propofol
AGENCY:
Food and Drug Administration,
HHS.
ACTION:
Final rule.
SUMMARY: The Food and Drug
Administration (FDA) is amending the
animal drug regulations to reflect a
change of sponsor for a new animal drug
application (NADA) from Intervet, Inc.,
to Teva Animal Health, Inc.
DATES: This rule is effective April 19,
2010.
FOR FURTHER INFORMATION CONTACT:
David R. Newkirk, Center for Veterinary
Medicine (HFV–100), Food and Drug
Administration, 7500 Standish Pl.,
Rockville, MD 20855, 240–276–8307, email: david.newkirk@fda.hhs.gov.
SUPPLEMENTARY INFORMATION: Intervet,
Inc., 56 Livingston Ave., Roseland, NJ
07068, has informed FDA that it has
transferred ownership of, and all rights
and interest in, approved NADA 141–
070 for RAPINOVET (propofol), an
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]]>Agencies
[Federal Register Volume 75, Number 74 (Monday, April 19, 2010)]
[Rules and Regulations]
[Pages 20265-20268]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-8596]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0329; Directorate Identifier 2009-CE-020-AD;
Amendment 39-16264; AD 2009-08-05 R1]
RIN 2120-AA64
Airworthiness Directives; Liberty Aerospace Incorporated Model
XL-2 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are correcting the address, telephone, and fax information
for the reporting requirement in Airworthiness Directive (AD) 2009-08-
05, which applies to certain Liberty Aerospace Incorporated Model XL-2
airplanes. AD 2009-08-05 currently requires repetitively inspecting the
exhaust muffler for cracks, replacing the exhaust muffler when cracks
are found, and reporting the results of the inspections to the FAA.
Since AD 2009-08-05 became effective, the FAA's Atlanta Aircraft
Certification Office (ACO) moved, which has caused the office personnel
problems in receiving fax and mailed copies of the inspection result
reports. This document corrects the mailing address, telephone number,
and fax information of the Atlanta ACO.
DATES: This final rule is effective April 19, 2010. The compliance date
of this AD is April 20, 2009, which is the same as the effective date
of AD 2009-08-05.
As of April 20, 2009 (74 FR 16117, April 9, 2009), the Director of
the Federal Register approved the incorporation by reference of Liberty
Aerospace, Inc. Service Document Critical Service Bulletin (CSB) CSB-
09-001, Revision Level B, Revised on March 18, 2009.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov or in person at 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:
[[Page 20266]]
--Corey Spiegel, Aerospace Engineer, Atlanta Aircraft Certification
Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone:
(404) 474-5574; facsimile: (404) 474-5606; e[dash]mail:
corey.spiegel@faa.gov; or
--Cindy Lorenzen, Aerospace Engineer, Atlanta Aircraft Certification
Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone:
(404) 474-5524; facsimile: (404) 474-5606; e[dash]mail:
cindy.lorenzen@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
On April 3, 2009, we issued AD 2009-08-05, Amendment 39-15878 (74
FR 16117, April 9, 2009), to require repetitively inspecting the
exhaust muffler for cracks, replacing the exhaust muffler when cracks
are found, and reporting the results of the inspections to the FAA.
Since AD 2009-08-05 became effective, the FAA's Atlanta Aircraft
Certification Office (ACO) moved, which has caused the office personnel
problems in receiving fax and mailed copies of the inspection result
reports.
Consequently, the FAA sees a need to correct the mailing address,
telephone number, and fax information of the Atlanta ACO in AD 2009-08-
05 to assure that the inspection results are received and reviewed to
help assure the continued operational safety of the affected airplanes.
Thus, the FAA is revising the AD to incorporate the language discussed
above and to add the amendment to section 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
Since this action only corrects the address, telephone number, and
fax information for the reporting requirement and does not require any
additional actions over that originally required by AD 2009-08-05, it
has no adverse economic impact and imposes no additional burden on any
person than was already required. Therefore, the FAA has determined
that prior notice and opportunity for public comment are unnecessary.
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 removing Airworthiness Directive (AD)
2009-08-05, Amendment 39-15878 (74 FR 16117, April 9, 2009), and adding
the following new AD:
2009-08-05 R1 Liberty Aerospace Incorporated: Amendment 39-16264;
Docket No. FAA-2009-0329; Directorate Identifier 2009-CE-020-AD.
Effective Date
(a) This final rule is effective April 19, 2010. The compliance
date of this AD is April 20, 2009, which is the same as the
effective date of AD 2009-08-05.
Affected ADs
(b) This AD revises AD 2009-08-05.
Applicability
(c) This AD applies to Model XL-2 airplanes, serial numbers
0007, 0009, and subsequent, that are certificated in any category.
Unsafe Condition
(d) This AD is the result of reports that eight cracks have been
found in the exhaust muffler during maintenance and service
inspections. We are issuing this AD to detect and correct cracks in
the exhaust muffler, which could result in carbon monoxide entering
the cabin heating system. This condition could lead to
incapacitation of the pilot.
Compliance
(e) To address this problem, you must do the following, unless
already done:
----------------------------------------------------------------------------------------------------------------
Actions Compliance Procedures
----------------------------------------------------------------------------------------------------------------
(1) Inspect the following: Initially inspect within the next 10 Follow Liberty Aerospace, Inc.
(i) The exhaust muffler for cracks. hours time-in-service (TIS) after Service Document Critical Service
There are two different exhaust April 20, 2009 (the effective date Bulletin (CSB) CSB-09-001, Revision
systems available for the affected of AD 2009-08-05) or at the next Level B, Revised on March 18, 2009.
airplanes. They are: annual inspection, whichever occurs
(A) Standard exhaust system, part first. Repetitively inspect the
number (P/N) DEL200201-002 that exhaust muffler thereafter as
incorporates muffler P/N DEL200201- specified in paragraph (e)(5) of
101; and this AD.
(B) Reduced sound exhaust
system, P/N DEL200201-003
that incorporates muffler P/
N 200201-104.
(ii) The tail pipe and the tail
pipe opening in the lower cowl
for a 0.5-inch minimum
clearance.
(iii) Inspect the propeller for
proper propeller clocking
position.
(2) As a result of the inspections Before further flight after the As specified in Liberty Aerospace,
required in paragraphs (e)(1)(ii) inspection required in paragraph Inc. Service Document Critical
and (e)(1)(iii) of this AD: (e)(1) of this AD. Service Bulletin (CSB) CSB-09-001,
(i) If the clearance between the Revision Level B, Revised on March
tail pipe and the tail pipe opening 18, 2009.
is less than the required 0.5-inch
minimum, trim the lower cowl as
needed to achieve the minimum
clearance.
(ii) If there is a discrepancy
in the propeller clocking
position, remove and reinstall
the propeller at the correct
position.
[[Page 20267]]
(3) As a result of the initial Before further flight after the Follow Liberty Aerospace, Inc.
inspection required in paragraph initial inspection required in Service Document Critical Service
(e)(1)(i) of this AD or any paragraph (e)(1) of this AD and Bulletin (CSB) CSB-09-001, Revision
repetitive inspection required in before further flight after any Level B, Revised on March 18, 2009.
paragraph (e)(5) of this AD, if a repetitive inspection required in
crack is found, replace the exhaust paragraph (e)(5) of this AD.
muffler.
(i) The manufacturer will provide
the replacement exhaust system.
(ii) A reduced sound exhaust
system may be replaced with a
standard exhaust system.
(iii) Installing a reduced sound
exhaust system as a replacement
part also requires installing a
bypass SCAT tube and a ``Do Not
Use'' placard on or near the
heater knob.
(4) If the airplane is equipped with Within the next 10 hours TIS after Follow Liberty Aerospace, Inc.
a reduced sound exhaust system and April 20, 2009 (the effective date Service Document Critical Service
no cracks are found during the of AD 2009-08-05). Bulletin (CSB) CSB-09-001, Revision
initial inspection required in Level B, Revised on March 18, 2009.
paragraph (e)(1) of this AD,
install a bypass SCAT tube and a
``Do Not Use'' placard on or near
the heater knob.
(5) If no cracks are found in the (i) For airplanes equipped with a Follow Liberty Aerospace, Inc.
exhaust muffler during the initial standard exhaust system and the Service Document Critical Service
inspection required in paragraph optional bypass SCAT tube has not Bulletin (CSB) CSB-09-001, Revision
(e)(1) of this AD or if the exhaust been installed, repetitively Level B, Revised on March 18, 2009.
muffler was replaced as required in inspect thereafter every 25 hours
paragraph (e)(3) of this AD, TIS or every 12 months, whichever
repetitively inspect thereafter at occurs first.
the intervals specified in (ii) For airplanes equipped with a
paragraphs (e)(5)(i), (e)(5)(ii), standard exhaust system and the
and (e)(5)(iii) of this AD. optional bypass SCAT tube has been
installed, repetitively inspect
thereafter every 50 hours TIS or
every 12 months, whichever occurs
first.
(iii) For airplanes equipped with a
reduced sound exhaust system and
the required bypass SCAT tube has
been installed, repetitively
inspect thereafter every 50 hours
TIS or every 12 months, whichever
occurs first.
(6) Report the results of the Within 10 days after each inspection Use the form (Figure 1 of this AD)
following inspections required in required by this AD. and submit it to FAA, Atlanta
this AD to the FAA. Aircraft Certification Office, 1701
(i) Initial inspection required in Columbia Avenue, College Park,
paragraph (e)(1) of this AD. Georgia 30337; fax: (404) 474-5606;
(ii) Repetitive inspections required e-mail corey.spiegel@faa.gov.
in paragraph (e)(5) of this AD only
if cracks are found.
(iii) The Office of Management
and Budget (OMB) approved the
information collection
requirements contained in this
regulation under the provisions
of the Paperwork Reduction Act
of 1980 (44 U.S.C. 3501 et
seq.) and assigned OMB Control
Number 2120-0056.
----------------------------------------------------------------------------------------------------------------
[[Page 20268]]
------------------------------------------------------------------------
------------------------------------------------------------------------
AD 2009-08-05 R1 Inspection Report
------------------------------------------------------------------------
Airplane Serial Number
------------------------------------------------------------------------
Airplane Tach Hours at time of
inspection
------------------------------------------------------------------------
Propeller type (circle one) MT Sensenich
------------------------------------------------------------------------
Propeller Tach Hours at time of
inspection
------------------------------------------------------------------------
Exhaust Type (circle one) Standard Reduced Sound
------------------------------------------------------------------------
Is Exhaust Cracked? (circle one) YES NO
------------------------------------------------------------------------
Did lower cowl require trimming at YES NO
the tail pipe opening? (circle
one) Not applicable after initial
inspection
------------------------------------------------------------------------
Did the propeller clocking YES NO
position need to be corrected?
(circle one) Not applicable after
initial inspection.
------------------------------------------------------------------------
Were any other discrepancies
noticed during the inspection?
------------------------------------------------------------------------
Name:
------------------------------------------------------------------------
Telephone and/or e-mail address:
------------------------------------------------------------------------
Date:
------------------------------------------------------------------------
Send report to: Corey Spiegel, Aerospace Engineer, Atlanta ACO,
1701 Columbia Avenue, College Park, Georgia 30337;
facsimile: (404) 474-5606; e-mail: corey.spiegel@faa.gov.
Figure 1
------------------------------------------------------------------------
Special Flight Permit
(f) Under 14 CFR part 39.23, we are limiting the special flight
permits for this AD by the following conditions:
(1) The cabin heat turned off; and
(2) The fresh air vents are open.
Alternative Methods of Compliance (AMOCs)
(g) The Manager, Atlanta Aircraft Certification Office (ACO),
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: Corey Spiegel, Aerospace Engineer, Atlanta ACO, 1701 Columbia
Avenue, College Park, Georgia 30337. 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.
Material Incorporated by Reference
(h) You must use Liberty Aerospace, Inc. Service Document
Critical Service Bulletin (CSB) CSB-09-001, Revision Level B,
Revised on March 18, 2009, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) On April 20, 2009 (74 FR 16117, April 9, 2009), the Director
of the Federal Register previously 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
Liberty Aerospace, 100 Aerospace Drive, Melbourne, Florida 32901;
telephone: (321) 752-0332 or (800) 759-5953; fax: (321) 752-0377;
Internet: https://www.libertyaircraft.com.
(3) You may review copies of the service information
incorporated by reference for this AD at the FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the
Central Region, call (816) 329-3768.
(4) You may also review copies of the service information
incorporated by reference for this AD 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: https://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Kansas City, Missouri, on April 7, 2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-8596 Filed 4-16-10; 8:45 am]
BILLING CODE 4910-13-P
