Airworthiness Directives; Quartz Mountain Aerospace, Inc. Model 11E Airplanes, 30282-30284 [2010-12302]
Download as PDF
30282
Federal Register / Vol. 75, No. 104 / Tuesday, June 1, 2010 / Rules and Regulations
STEMME F & D Service Bulletin A31–10–
083, Am-Index: 01.a, dated February 26,
2008, or STEMME F & D Service Bulletin
A31–10–083, Am-Index: 01.b, dated May 6,
2009.
(4) For sailplanes that had P/Ns M476
replaced with P/Ns 10M–181 in compliance
with AD 2008–11–20: Before further flight
after July 6, 2010 (the effective date of this
AD), do a leak test as specified in STEMME
F & D Service Bulletin A31–10–083, AmIndex: 01.a, dated February 26, 2008, or
STEMME F & D Service Bulletin A31–10–
083, Am-Index: 01.b, dated May 6, 2009.
(5) For sailplanes that had P/Ns M476
replaced with P/Ns 10M–181 in compliance
with AD 2008–11–20: If a leak is found
during the leak test required in paragraph
(f)(4) of this AD, before further flight, repair
the leak following an FAA-approved
procedure. Contact the manufacturer at the
address specified in paragraph (i)(4) of this
AD to obtain an FAA-approved repair
procedure.
(6) For all sailplanes affected by this AD:
If no leak is found during the inspection
required in paragraph (f)(2) of this AD,
within the next 12 months after July 6, 2010
(the effective date of this AD), replace all P/
Ns M476 in the fuel system with P/Ns 10M–
181. Do the replacements following STEMME
F & D Service Bulletin A31–10–083, AmIndex: 01.a, dated February 26, 2008, or
STEMME F & D Service Bulletin A31–10–
083, Am-Index: 01.b, dated May 6, 2009.
(7) For all sailplanes affected by this AD:
Before further flight after doing the
replacement required in paragraph (f)(6) of
this AD, do a leak test as specified in
STEMME F & D Service Bulletin A31–10–
083, Am-Index: 01.a, dated February 26,
2008, or STEMME F & D Service Bulletin
A31–10–083, Am-Index: 01.b, dated May 6,
2009.
(8) For all sailplanes affected by this AD:
If a leak is found during the leak test required
in paragraph (f)(7) of this AD, before further
flight, repair the leak following an FAAapproved procedure. Contact the
manufacturer at the address specified in
paragraph (i)(4) of this AD to obtain an FAAapproved repair procedure.
(9) For all sailplanes affected by this AD:
After June 23, 2008 (the compliance date
retained from AD 2008–11–20), do not install
plastic ‘‘T’’ and ‘‘Y’’ shape connectors and P/
N M476 single-ear clamps in the fuel system.
FAA AD Differences
srobinson on DSKHWCL6B1PROD with RULES
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, Standards Office,
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: Greg Davison, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4130; fax: (816) 329–
4090. Before using any approved AMOC on
VerDate Mar<15>2010
16:55 May 28, 2010
Jkt 220001
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
(44 U.S.C. 3501 et. seq.), 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 European Aviation
Safety Agency (EASA) Emergency AD No.
2008–0053–E, dated March 5, 2008;
STEMME F & D Service Bulletin A31–10–
082, AM.-Index: 01.a, dated November 30,
2007; STEMME F & D Service Bulletin A31–
10–083, Am-Index: 01.a, dated February 26,
2008; and STEMME F & D Service Bulletin
A31–10–083, Am-Index: 01.b, dated May 6,
2009, for related information.
Material Incorporated by Reference
(i) You must use STEMME F & D Service
Bulletin A31–10–082, AM.-Index: 01.a, dated
November 30, 2007; STEMME F & D Service
Bulletin A31–10–083, Am-Index: 01.a, dated
February 26, 2008; and STEMME F & D
Service Bulletin A31–10–083, Am-Index:
01.b, dated May 6, 2009, 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
STEMME F & D Service Bulletin A31–10–
083, Am-Index: 01.b, dated May 6, 2009,
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) On June 23, 2008 (73 FR 31355, June
2, 2008), the Director of the Federal Register
previously approved the incorporation by
reference of STEMME F & D Service Bulletin
A31–10–083, Am-Index: 01.a, dated February
26, 2008, listed in this AD.
(3) On February 20, 2008 (73 FR 5733,
January 31, 2008), the Director of the Federal
Register previously approved the
incorporation by reference of STEMME F &
D Service Bulletin A31–10–082, AM.-Index:
01.a, dated November 30, 2007, listed in this
AD.
(4) For service information identified in
this AD, contact STEMME GmbH & Co. KG,
Flugplatzstra+e F 2, Nr. 7, 15344 Strausberg,
Federal Republic of Germany; Internet:
https://www.stemme.de/man/.
(5) 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.
(6) You may also review copies of the
service information incorporated by reference
PO 00000
Frm 00016
Fmt 4700
Sfmt 4700
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 May
18, 2010.
John Colomy,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2010–12443 Filed 5–28–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0261; Directorate
Identifier 2010–CE–008–AD; Amendment
39–16312; AD 2010–11–07]
RIN 2120–AA64
Airworthiness Directives; Quartz
Mountain Aerospace, Inc. Model 11E
Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new
airworthiness directive (AD) for all
Quartz Mountain Aerospace, Inc. Model
11E airplanes. This AD requires you to
clean and lubricate the aileron pushrod
bearings. This AD results from reports of
the aileron control stick force increasing
and of the controls being very noisy. We
are issuing this AD to detect and correct
insufficient lubrication and residual
metallic paint particles in the pushrod
end ball joints, which could result in
difficulty actuating aileron controls
sometime during flight after takeoff.
This condition could lead to difficulty
controlling the airplane in flight.
DATES: This AD becomes effective on
July 6, 2010.
On July 6, 2010, the Director of the
Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: Quartz Mountain
Aerospace, Inc. is in liquidation. For
service/or continued airworthiness
information identified in this AD,
contact Manager, Fort Worth Aircraft
Certification Office, FAA, ATTN: Garry
D. Sills, Aerospace Engineer, Rotorcraft
Directorate—Airplane Certification
Office, ASW–150, 2601 Meacham Blvd,
Fort Worth, Texas 76193; telephone:
(817) 222–5154; facsimile: (817) 222–
5960.
E:\FR\FM\01JNR1.SGM
01JNR1
30283
Federal Register / Vol. 75, No. 104 / Tuesday, June 1, 2010 / Rules and Regulations
To view the AD docket, go to U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue, SE., Washington,
DC 20590, or on the Internet at https://
www.regulations.gov. The docket
number is FAA–2010–0261; Directorate
Identifier 2010–CE–008–AD.
FOR FURTHER INFORMATION CONTACT:
Garry D. Sills, Aerospace Engineer,
Rotorcraft Directorate—Airplane
Certification Office, ASW–150, 2601
Meacham Blvd, Fort Worth, Texas
76193; telephone: (817) 222–5154;
facsimile: (817) 222–5960.
SUPPLEMENTARY INFORMATION:
Aviation Regulations (14 CFR part 39) to
include an AD that would apply to all
Quartz Mountain Aerospace, Inc. Model
11E airplanes. This proposal was
published in the Federal Register as a
notice of proposed rulemaking (NPRM)
on March 16, 2010 (75 FR 12468). The
NPRM proposed to require you to clean
and lubricate the aileron pushrod
bearings.
Discussion
On March 9, 2010, we issued a
proposal to amend part 39 of the Federal
Conclusion
Comments
We provided the public the
opportunity to participate in developing
this AD. We received no comments on
the proposal or on the determination of
the cost to the public.
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD as proposed except for
minor editorial corrections. We have
determined that these minor
corrections:
• Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Costs of Compliance
We estimate that this proposed AD
would affect 12 airplanes in the U.S.
registry.
We estimate the following costs to do
the proposed cleaning and lubrication:
Labor cost
Parts cost
1 work-hour × $85 per hour = $85 ..........................................................................................................
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 AD.
srobinson on DSKHWCL6B1PROD with RULES
Regulatory Findings
We have 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:
VerDate Mar<15>2010
16:55 May 28, 2010
Jkt 220001
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 summary of the costs
to comply with this AD (and other
information as included in the
Regulatory Evaluation) and placed it in
the AD Docket. You may get a copy of
this summary by sending a request to us
at the address listed under ADDRESSES.
Include ‘‘Docket No. FAA–2010–0261;
Directorate Identifier 2010–CE–008–AD’’
in your request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (14 CFR part 39) as follows:
■
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
PO 00000
Frm 00017
Fmt 4700
Sfmt 4700
Total cost
per airplane
Total cost
on U.S. operators
$95
$1,140
$10
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. FAA amends § 39.13 by adding the
following new AD:
■
2010–11–07 Quartz Mountain Aerospace,
Inc.: Amendment 39–16312; Docket No.
FAA–2010–0261; Directorate Identifier
2010–CE–008–AD.
Effective Date
(a) This AD becomes effective on July 6,
2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model 11E
airplanes, all serial numbers, that are
certificated in any category.
Subject
(d) Air Transport Association of America
(ATA) Code 27: Flight Controls.
Unsafe Condition
(e) This AD results from reports of the
aileron control stick force increasing and of
the controls being very noisy. We are issuing
this AD to detect and correct insufficient
lubrication and residual metallic paint
particles in the rod end ball joints, which
could result in difficulty actuating aileron
controls sometime during flight after takeoff.
This failure could lead to difficulty
controlling the airplane in flight.
Compliance
(f) To address this problem, you must do
the following, unless already done:
E:\FR\FM\01JNR1.SGM
01JNR1
30284
Federal Register / Vol. 75, No. 104 / Tuesday, June 1, 2010 / Rules and Regulations
Actions
Compliance
Procedures
(1) Clean and lubricate the aileron pushrod
bearings.
Within the next 10 hours time-in-service (TIS)
after July 6, 2010 (the effective date of this
AD).
Within 50 hours TIS after the cleaning and lubrication required by paragraph (f)(1) of this
AD. Repetitively thereafter at intervals not
to exceed 50 hours TIS.
Follow Quartz Mountain Aerospace Mandatory Service Bulletin No. SB 09–02, dated
May 5, 2009.
Follow Quartz Mountain Aerospace Mandatory Service Bulletin No. SB 09–02, dated
May 5, 2009.
(2) Lubricate the aileron pushrod bearings ........
Special Flight Permit
Issued in Kansas City, Missouri, on May
14, 2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
(g) Under 14 CFR part 39.23, a special
flight is not permitted for this AD.
Alternative Methods of Compliance
(AMOCs)
[FR Doc. 2010–12302 Filed 5–28–10; 8:45 am]
(h) The Manager, Fort Worth Aircraft
Certification Office, 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: Garry D. Sills,
Aerospace Engineer, Rotorcraft Directorate—
Airplane Certification Office, ASW–150,
2601 Meacham Blvd, Fort Worth, Texas
76193; telephone: (817) 222–5154; facsimile:
(817) 222–5960. 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.
srobinson on DSKHWCL6B1PROD with RULES
Material Incorporated by Reference
(i) You must use Quartz Mountain
Aerospace Mandatory Service Bulletin No.
SB 09–02, dated May 5, 2009, 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) Quartz Mountain Aerospace, Inc. is in
liquidation. For service information
identified in this AD, contact Manager, Fort
Worth Aircraft Certification Office, FAA,
ATTN: Garry D. Sills, Aerospace Engineer,
Rotorcraft Directorate—Airplane Certification
Office, ASW–150, 2601 Meacham Blvd, Fort
Worth, Texas 76193; telephone: (817) 222–
5154; fax: (817) 222–5960.
(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.
VerDate Mar<15>2010
16:55 May 28, 2010
Jkt 220001
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0176; Directorate
Identifier 2009–NM–201–AD; Amendment
39–16318; AD 2010–11–13]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
originated by an aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
During ERJ 170 airplane full scale fatigue
test, cracks were found in some structural
components of the airplane. Analysis of these
cracks resulted in modifications on the
airplane Airworthiness Limitation Items
(ALI), to include new inspections tasks or
modification of existing ones and its
respective thresholds and intervals.
Failure to inspect these components
according to the new tasks, thresholds and
intervals, could prevent a timely detection of
fatigue cracks. Undetected fatigue cracks in
these areas could adversely affect the
structural integrity of these airplanes.
*
*
*
*
*
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
July 6, 2010.
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of July 6, 2010.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at the
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Kenny Kaulia, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–2848; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM was published in the Federal
Register on March 4, 2010 (75 FR 9811).
That NPRM proposed to correct an
unsafe condition for the specified
products. The MCAI states:
During ERJ 170 airplane full scale fatigue
test, cracks were found in some structural
components of the airplane. Analysis of these
cracks resulted in modifications on the
airplane Airworthiness Limitation Items
(ALI), to include new inspections tasks or
modification of existing ones and its
respective thresholds and intervals.
Failure to inspect these components
according to the new tasks, thresholds and
intervals, could prevent a timely detection of
fatigue cracks. Undetected fatigue cracks in
these areas could adversely affect the
structural integrity of these airplanes.
*
*
*
*
*
The corrective action is revising the
Airworthiness Limitations section of the
Instructions for Continued
Airworthiness to incorporate new
structural inspection requirements. You
may obtain further information by
examining the MCAI in the AD docket.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM or
E:\FR\FM\01JNR1.SGM
01JNR1
Agencies
[Federal Register Volume 75, Number 104 (Tuesday, June 1, 2010)]
[Rules and Regulations]
[Pages 30282-30284]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-12302]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0261; Directorate Identifier 2010-CE-008-AD;
Amendment 39-16312; AD 2010-11-07]
RIN 2120-AA64
Airworthiness Directives; Quartz Mountain Aerospace, Inc. Model
11E Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Quartz Mountain Aerospace, Inc. Model 11E airplanes. This AD requires
you to clean and lubricate the aileron pushrod bearings. This AD
results from reports of the aileron control stick force increasing and
of the controls being very noisy. We are issuing this AD to detect and
correct insufficient lubrication and residual metallic paint particles
in the pushrod end ball joints, which could result in difficulty
actuating aileron controls sometime during flight after takeoff. This
condition could lead to difficulty controlling the airplane in flight.
DATES: This AD becomes effective on July 6, 2010.
On July 6, 2010, the Director of the Federal Register approved the
incorporation by reference of certain publications listed in this AD.
ADDRESSES: Quartz Mountain Aerospace, Inc. is in liquidation. For
service/or continued airworthiness information identified in this AD,
contact Manager, Fort Worth Aircraft Certification Office, FAA, ATTN:
Garry D. Sills, Aerospace Engineer, Rotorcraft Directorate--Airplane
Certification Office, ASW-150, 2601 Meacham Blvd, Fort Worth, Texas
76193; telephone: (817) 222-5154; facsimile: (817) 222-5960.
[[Page 30283]]
To view the AD docket, go to U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at
https://www.regulations.gov. The docket number is FAA-2010-0261;
Directorate Identifier 2010-CE-008-AD.
FOR FURTHER INFORMATION CONTACT: Garry D. Sills, Aerospace Engineer,
Rotorcraft Directorate--Airplane Certification Office, ASW-150, 2601
Meacham Blvd, Fort Worth, Texas 76193; telephone: (817) 222-5154;
facsimile: (817) 222-5960.
SUPPLEMENTARY INFORMATION:
Discussion
On March 9, 2010, we issued a proposal to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) to include an AD that
would apply to all Quartz Mountain Aerospace, Inc. Model 11E airplanes.
This proposal was published in the Federal Register as a notice of
proposed rulemaking (NPRM) on March 16, 2010 (75 FR 12468). The NPRM
proposed to require you to clean and lubricate the aileron pushrod
bearings.
Comments
We provided the public the opportunity to participate in developing
this AD. We received no comments on the proposal or on the
determination of the cost to the public.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed
except for minor editorial corrections. We have determined that these
minor corrections:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this proposed AD would affect 12 airplanes in the
U.S. registry.
We estimate the following costs to do the proposed cleaning and
lubrication:
------------------------------------------------------------------------
Total cost Total cost
Labor cost Parts cost per on U.S.
airplane operators
------------------------------------------------------------------------
1 work-hour x $85 per hour = $85. $10 $95 $1,140
------------------------------------------------------------------------
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 AD.
Regulatory Findings
We have 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 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 summary of the costs to comply with this AD (and
other information as included in the Regulatory Evaluation) and placed
it in the AD Docket. You may get a copy of this summary by sending a
request to us at the address listed under ADDRESSES. Include ``Docket
No. FAA-2010-0261; Directorate Identifier 2010-CE-008-AD'' in your
request.
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 Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (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. FAA amends Sec. 39.13 by adding the following new AD:
2010-11-07 Quartz Mountain Aerospace, Inc.: Amendment 39-16312;
Docket No. FAA-2010-0261; Directorate Identifier 2010-CE-008-AD.
Effective Date
(a) This AD becomes effective on July 6, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model 11E airplanes, all serial numbers,
that are certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 27: Flight
Controls.
Unsafe Condition
(e) This AD results from reports of the aileron control stick
force increasing and of the controls being very noisy. We are
issuing this AD to detect and correct insufficient lubrication and
residual metallic paint particles in the rod end ball joints, which
could result in difficulty actuating aileron controls sometime
during flight after takeoff. This failure could lead to difficulty
controlling the airplane in flight.
Compliance
(f) To address this problem, you must do the following, unless
already done:
[[Page 30284]]
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Clean and lubricate the Within the next 10 Follow Quartz
aileron pushrod bearings. hours time-in- Mountain Aerospace
service (TIS) after Mandatory Service
July 6, 2010 (the Bulletin No. SB 09-
effective date of 02, dated May 5,
this AD). 2009.
(2) Lubricate the aileron Within 50 hours TIS Follow Quartz
pushrod bearings. after the cleaning Mountain Aerospace
and lubrication Mandatory Service
required by Bulletin No. SB 09-
paragraph (f)(1) of 02, dated May 5,
this AD. 2009.
Repetitively
thereafter at
intervals not to
exceed 50 hours TIS.
------------------------------------------------------------------------
Special Flight Permit
(g) Under 14 CFR part 39.23, a special flight is not permitted
for this AD.
Alternative Methods of Compliance (AMOCs)
(h) The Manager, Fort Worth Aircraft Certification Office, 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:
Garry D. Sills, Aerospace Engineer, Rotorcraft Directorate--Airplane
Certification Office, ASW-150, 2601 Meacham Blvd, Fort Worth, Texas
76193; telephone: (817) 222-5154; facsimile: (817) 222-5960. 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
(i) You must use Quartz Mountain Aerospace Mandatory Service
Bulletin No. SB 09-02, dated May 5, 2009, 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) Quartz Mountain Aerospace, Inc. is in liquidation. For
service information identified in this AD, contact Manager, Fort
Worth Aircraft Certification Office, FAA, ATTN: Garry D. Sills,
Aerospace Engineer, Rotorcraft Directorate--Airplane Certification
Office, ASW-150, 2601 Meacham Blvd, Fort Worth, Texas 76193;
telephone: (817) 222-5154; fax: (817) 222-5960.
(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 May 14, 2010.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-12302 Filed 5-28-10; 8:45 am]
BILLING CODE 4910-13-P