Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate (TC) No. 3A20 and TC No. A24CE Formerly Held by Raytheon Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and B300C Airplanes, 31988-31990 [E7-10758]
Download as PDF
<![CDATA[
31988
Federal Register / Vol. 72, No. 111 / Monday, June 11, 2007 / Rules and Regulations
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. 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.
(3) AMOCs approved previously in
accordance with AD 96–23–05, are approved
as AMOCs for the corresponding provisions
of this AD.
Material Incorporated by Reference
(x) You must use Boeing Service Bulletin
747–53A2378, Revision 1, dated March 10,
1994; or Boeing Service Bulletin 747–
53A2378, Revision 3, dated August 11, 2005;
as applicable, to perform the actions that are
required by this AD, unless the AD specifies
otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
Boeing Service Bulletin 747–53A2378,
Revision 3, dated August 11, 2005, in
accordance with 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) On December 16, 1996 (61 FR 58318,
November 14, 1996), the Director of the
Federal Register approved the incorporation
by reference of Boeing Service Bulletin 747–
53A2378, Revision 1, dated March 10, 1994.
(3) Contact Boeing Commercial Airplanes,
P.O. Box 3707, Seattle, Washington 98124–
2207, for a copy of this service information.
You may review copies at the FAA,
Transport Airplane Directorate, 1601 Lind
Avenue, SW., Renton, Washington; or at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Renton, Washington, on May 30,
2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–10982 Filed 6–8–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–27071; Directorate
Identifier 2007–CE–004–AD; Amendment
39–15084; AD 2007–12–06]
RIN 2120–AA64
Airworthiness Directives; Hawker
Beechcraft Corporation (Type
Certificate (TC) No. 3A20 and TC No.
A24CE Formerly Held by Raytheon
Aircraft Corporation and Beech)
Models C90A, B200, B200C, B300, and
B300C Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) that
supersedes AD 2006–23–02, which
applies to certain Hawker Beechcraft
Corporation (HBC) (Type Certificate
(TC) No. 3A20 and TC No. A24CE
formerly held by Raytheon Aircraft
Corporation and Beech) Models C90A,
B200, B200C, B300, and B300C
airplanes. AD 2006–23–02 currently
requires you to inspect the flight
controls for improper assembly or
damage, and if any improperly
assembled or damaged flight controls
are found, take corrective action. Since
we issued AD 2006–23–02, we have
determined the need to add airplane
serial numbers that were not previously
included in the applicability.
Consequently, this AD retains the
actions of AD 2006–23–02 and adds
airplane serial numbers to the
applicability. We are issuing this AD to
detect and correct improperly
assembled or damaged flight controls,
which could result in an unsafe
condition by reducing capabilities of the
flight controls and lead to loss of
control.
SUMMARY:
This AD becomes effective on
July 16, 2007.
On July 16, 2007, the Director of the
Federal Register approved the
incorporation by reference of Raytheon
Aircraft Company Mandatory Service
Bulletin Number SB 27–3761, Rev. 1,
December 2006, listed in this AD.
As of December 13, 2006 (71 FR
65390 Nov. 8, 2006), the Director of the
Federal Register approved the
incorporation by reference of Raytheon
Aircraft Company Mandatory Service
Bulletin Number SB 27–3761, Issued:
February 2006, listed in this AD.
rmajette on DSK8KYBLC1PROD with MISCELLANEOUS
DATES:
VerDate Mar<15>2010
12:20 Mar 07, 2011
Jkt 223001
PO 00000
Frm 00020
Fmt 4700
Sfmt 4700
For service information
identified in this AD, contact Hawker
Beechcraft Corporation, P.O. Box 85,
Wichita, Kansas 67201–0085; telephone:
(800) 429–5372 or (316) 676–3140.
To view the AD docket, go to the
Docket Management Facility; U.S.
Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
0001 or on the Internet at https://
dms.dot.gov. The docket number is
FAA–2007–27071; Directorate Identifier
2007–CE–004–AD.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
Chris B. Morgan, Aerospace Engineer,
FAA, Wichita Aircraft Certification
Office, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946–
4154; fax: (316) 946–4107.
SUPPLEMENTARY INFORMATION:
Discussion
On March 6, 2007, 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
certain HBC Models C90A, B200,
B200C, B300, and B300C airplanes. This
proposal was published in the Federal
Register as a notice of proposed
rulemaking (NPRM) on March 12, 2007
(72 FR 10949). The NPRM proposed to
retain the actions of AD 2006–23–02
and add airplane serial numbers to the
applicability.
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 AD affects 138
airplanes in the U.S. registry.
We estimate the following costs to do
the inspection:
E:\ERIC\11JNR1.SGM
11JNR1
Federal Register / Vol. 72, No. 111 / Monday, June 11, 2007 / Rules and Regulations
31989
Total cost per
airplane
Total cost on
U.S. operators
$6,400
$883,200
Labor cost
Parts cost
80 work-hours × $80 per hour = $6,400 ......................
Not Applicable ..............................................................
We have no way of determining the
number of airplanes that may need any
corrective action that would be required
based on the results of the proposed
inspection.
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–2007–27071;
Directorate Identifier 2007–CE–004–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,
■
Model
Unsafe Condition
(d) This AD results from our determination
to add airplane serial numbers that were not
rmajette on DSK8KYBLC1PROD with MISCELLANEOUS
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. FAA amends § 39.13 by adding the
following new AD:
■
2007–12–06 Hawker Beechcraft
Corporation Hawker Beechcraft
Corporation (Type Certificate (TC) No.
3A20 and TC No. A24CE formerly held
by Raytheon Aircraft Corporation and
Beech): Amendment 39–15084; Docket
No. FAA–2007–27071; Directorate
Identifier 2007–CE–004–AD.
Effective Date
(a) This AD becomes effective on July 16,
2007.
Affected ADs
(b) This AD supersedes AD 2006–23–02,
Amendment 39–14814.
Applicability
(c) This AD applies to the following
airplane models and serial numbers that are
certificated in any category:
(1) Group 1 Airplanes (maintains the
actions from AD 2006–23–02):
LJ–1697 through LJ–1726, LJ–1728, LJ–1729, and LJ–1731 through LJ–1739.
BB–1827 through BB–1912.
BL–148 and BL–149.
FL–379 through FL–423, FL–426, FL–428 through FL–450, and FL–452.
FM–11.
(2) Group 2 Airplanes: Model C90A, serial
numbers LJ–1741 through LJ–1743.
12:20 Mar 07, 2011
PART 39—AIRWORTHINESS
DIRECTIVES
Serial No.
(i) C90A ...........................................
(ii) B200 ...........................................
(iii) B200C .......................................
(iv) B300 ..........................................
(v) B300C ........................................
VerDate Mar<15>2010
the Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (14 CFR part 39) as follows:
Jkt 223001
previously included in the applicability. We
are issuing this AD to detect and correct
improperly assembled or damaged flight
controls, which could result in an unsafe
condition by reducing capabilities of the
flight controls and lead to loss of control.
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
Compliance
(e) To address this problem, you must do
the following, unless already done:
E:\ERIC\11JNR1.SGM
11JNR1
31990
Federal Register / Vol. 72, No. 111 / Monday, June 11, 2007 / Rules and Regulations
Actions
Compliance
Procedures
(1) Inspect the entire flight control system for
improper assembly and any damage.
(i) For Group 1 Airplanes: At whichever of the
following occurs first:
(A) Within the next 100 hours time-inservice (TIS) after December 13, 2006
(the effective date of AD 2006–23–02);
or
(B) At the next annual inspection that occurs at least 30 days after December
13, 2006 (the effective date of AD
2006–23–02)
(ii) For Group 2 Airplanes: At whichever of the
following occurs first:
(A) Within the next 100 hours TIS after
July 16, 2007 (the effective date of this
AD); or
(B) At the next annual inspection that occurs at least 30 days after July 16,
2007 (the effective date of this AD).
Before further flight after the inspection required by paragraph (e)(1) of this AD.
Follow Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27–3761,
Issued: February 2006; or Raytheon Aircraft
Company Mandatory Service Bulletin Number SB 27–3761, Rev. 1, Dated December
2006.
(2) If you find any improperly assembled or
damaged flight controls as a result of the inspection required by paragraph (e)(1) of this
AD, take corrective action as specified in the
service information.
Alternative Methods of Compliance
(AMOCs)
(f) The Manager, Wichita 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: Chris
B. Morgan, Aerospace Engineer, FAA,
Wichita ACO, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946–4154;
fax: (316) 946–4107. 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.
(g) AMOCs approved for AD 2006–23–02
are approved for this AD.
rmajette on DSK8KYBLC1PROD with MISCELLANEOUS
Related Information
(h) To get copies of the service information
referenced in this AD, contact Hawker
Beechcraft Corporation, P.O. Box 85, Wichita,
Kansas 67201–0085; telephone: (800) 429–
5372 or (316) 676–3140. To view the AD
docket, go to the Docket Management
Facility; U.S. Department of Transportation,
400 Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC, or on the
Internet at https://dms.dot.gov. The docket
number is Docket No. FAA–2007–27071;
Directorate Identifier 2007–CE–004–AD.
(2) On December 13, 2006 (71 FR 65390
Nov. 8, 2006), the Director of the Federal
Register approved the incorporation by
reference of Raytheon Aircraft Company
Mandatory Service Bulletin Number SB 27–
3761, Issued: February 2006.
(3) For service information identified in
this AD, contact Hawker Beechcraft
Corporation, P.O. Box 85, Wichita, Kansas
67201–0085; telephone: (800) 429–5372 or
(316) 676–3140.
(4) You may review copies at the FAA,
Central Region, Office of the Regional
Counsel, 901 Locust, Kansas City, Missouri
64106; or at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
DEPARTMENT OF HOMELAND
SECURITY
Issued in Kansas City, Missouri, on May
29, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
SUMMARY: This rule amends title 19 of
the Code of Federal Regulations (‘‘CFR’’)
on an interim basis to implement the
preferential tariff treatment and other
customs-related provisions of the U.S.Singapore Free Trade Agreement
entered into by the United States and
the Republic of Singapore.
DATES: Interim rule effective June 11,
2007; comments must be received by
August 10, 2007.
ADDRESSES: You may submit comments,
identified by docket number, by one of
the following methods:
• Federal eRulemaking Portal: https://
www.regulations.gov. Follow the
instructions for submitting comments
via docket number USCBP–2007–0057.
• Mail: Trade and Commercial
Regulations Branch, Regulations and
Rulings, U.S. Customs and Border
Protection, 1300 Pennsylvania Avenue,
[FR Doc. E7–10758 Filed 6–8–07; 8:45 am]
BILLING CODE 4910–13–P
Material Incorporated by Reference
(i) You must use Raytheon Aircraft
Company Mandatory Service Bulletin
Number SB 27–3761, Issued: February 2006;
or Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27–3761, Rev. 1,
Dated December 2006, 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
Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27–3761, Rev. 1,
Dated December 2006, under 5 U.S.C. 552(a)
and 1 CFR part 51.
VerDate Mar<15>2010
12:20 Mar 07, 2011
Jkt 223001
Follow Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27–3761,
Issued: February 2006; or Raytheon Aircraft
Company Mandatory Service Bulletin Number SB 27–3761, Rev. 1, Dated December
2006.
PO 00000
Frm 00022
Fmt 4700
Sfmt 4700
U.S. Customs and Border Protection
DEPARTMENT OF THE TREASURY
19 CFR Parts 10, 24, 162, 163, and 178
[USCBP–2007–0057; CBP Dec. 07–28]
RIN 1505–AB48
United States-Singapore Free Trade
Agreement
U.S. Customs and Border
Protection, Department of Homeland
Security; Department of the Treasury.
ACTION: Interim rule; solicitation of
comments.
AGENCIES:
E:\ERIC\11JNR1.SGM
11JNR1
]]>Agencies
[Federal Register Volume 72, Number 111 (Monday, June 11, 2007)]
[Rules and Regulations]
[Pages 31988-31990]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-10758]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27071; Directorate Identifier 2007-CE-004-AD;
Amendment 39-15084; AD 2007-12-06]
RIN 2120-AA64
Airworthiness Directives; Hawker Beechcraft Corporation (Type
Certificate (TC) No. 3A20 and TC No. A24CE Formerly Held by Raytheon
Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and
B300C Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) that
supersedes AD 2006-23-02, which applies to certain Hawker Beechcraft
Corporation (HBC) (Type Certificate (TC) No. 3A20 and TC No. A24CE
formerly held by Raytheon Aircraft Corporation and Beech) Models C90A,
B200, B200C, B300, and B300C airplanes. AD 2006-23-02 currently
requires you to inspect the flight controls for improper assembly or
damage, and if any improperly assembled or damaged flight controls are
found, take corrective action. Since we issued AD 2006-23-02, we have
determined the need to add airplane serial numbers that were not
previously included in the applicability. Consequently, this AD retains
the actions of AD 2006-23-02 and adds airplane serial numbers to the
applicability. We are issuing this AD to detect and correct improperly
assembled or damaged flight controls, which could result in an unsafe
condition by reducing capabilities of the flight controls and lead to
loss of control.
DATES: This AD becomes effective on July 16, 2007.
On July 16, 2007, the Director of the Federal Register approved the
incorporation by reference of Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27-3761, Rev. 1, December 2006, listed in
this AD.
As of December 13, 2006 (71 FR 65390 Nov. 8, 2006), the Director of
the Federal Register approved the incorporation by reference of
Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761,
Issued: February 2006, listed in this AD.
ADDRESSES: For service information identified in this AD, contact
Hawker Beechcraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085;
telephone: (800) 429-5372 or (316) 676-3140.
To view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC 20590-0001 or on the Internet at https://dms.dot.gov. The docket number is FAA-2007-27071; Directorate
Identifier 2007-CE-004-AD.
FOR FURTHER INFORMATION CONTACT: Chris B. Morgan, Aerospace Engineer,
FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946-4154; fax: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
On March 6, 2007, 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 certain HBC Models C90A, B200, B200C, B300, and B300C
airplanes. This proposal was published in the Federal Register as a
notice of proposed rulemaking (NPRM) on March 12, 2007 (72 FR 10949).
The NPRM proposed to retain the actions of AD 2006-23-02 and add
airplane serial numbers to the applicability.
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 AD affects 138 airplanes in the U.S.
registry.
We estimate the following costs to do the inspection:
[[Page 31989]]
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
80 work-hours x $80 per hour = $6,400......... Not Applicable.................. $6,400 $883,200
----------------------------------------------------------------------------------------------------------------
We have no way of determining the number of airplanes that may need
any corrective action that would be required based on the results of
the proposed inspection.
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-2007-27071; Directorate Identifier 2007-CE-004-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:
2007-12-06 Hawker Beechcraft Corporation Hawker Beechcraft
Corporation (Type Certificate (TC) No. 3A20 and TC No. A24CE
formerly held by Raytheon Aircraft Corporation and Beech): Amendment
39-15084; Docket No. FAA-2007-27071; Directorate Identifier 2007-CE-
004-AD.
Effective Date
(a) This AD becomes effective on July 16, 2007.
Affected ADs
(b) This AD supersedes AD 2006-23-02, Amendment 39-14814.
Applicability
(c) This AD applies to the following airplane models and serial
numbers that are certificated in any category:
(1) Group 1 Airplanes (maintains the actions from AD 2006-23-
02):
------------------------------------------------------------------------
Model Serial No.
------------------------------------------------------------------------
(i) C90A.......................... LJ-1697 through LJ-1726, LJ-1728, LJ-
1729, and LJ-1731 through LJ-1739.
(ii) B200......................... BB-1827 through BB-1912.
(iii) B200C....................... BL-148 and BL-149.
(iv) B300......................... FL-379 through FL-423, FL-426, FL-
428 through FL-450, and FL-452.
(v) B300C......................... FM-11.
------------------------------------------------------------------------
(2) Group 2 Airplanes: Model C90A, serial numbers LJ-1741
through LJ-1743.
Unsafe Condition
(d) This AD results from our determination to add airplane
serial numbers that were not previously included in the
applicability. We are issuing this AD to detect and correct
improperly assembled or damaged flight controls, which could result
in an unsafe condition by reducing capabilities of the flight
controls and lead to loss of control.
Compliance
(e) To address this problem, you must do the following, unless
already done:
[[Page 31990]]
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Inspect the entire (i) For Group 1 Follow Raytheon
flight control system for Airplanes: At Aircraft Company
improper assembly and any whichever of the Mandatory Service
damage. following occurs Bulletin Number SB
first: 27-3761, Issued:
(A) Within the next February 2006; or
100 hours time-in- Raytheon Aircraft
service (TIS) after Company Mandatory
December 13, 2006 Service Bulletin
(the effective date Number SB 27-3761,
of AD 2006-23-02); Rev. 1, Dated
or. December 2006.
(B) At the next
annual inspection
that occurs at
least 30 days after
December 13, 2006
(the effective date
of AD 2006-23-02).
(ii) For Group 2
Airplanes: At
whichever of the
following occurs
first:.
(A) Within the next
100 hours TIS after
July 16, 2007 (the
effective date of
this AD); or.
(B) At the next
annual inspection
that occurs at
least 30 days after
July 16, 2007 (the
effective date of
this AD)..
(2) If you find any Before further Follow Raytheon
improperly assembled or flight after the Aircraft Company
damaged flight controls as inspection required Mandatory Service
a result of the inspection by paragraph (e)(1) Bulletin Number SB
required by paragraph of this AD. 27-3761, Issued:
(e)(1) of this AD, take February 2006; or
corrective action as Raytheon Aircraft
specified in the service Company Mandatory
information. Service Bulletin
Number SB 27-3761,
Rev. 1, Dated
December 2006.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(f) The Manager, Wichita 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: Chris B. Morgan, Aerospace Engineer, FAA, Wichita ACO, 1801
Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4154; fax:
(316) 946-4107. 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.
(g) AMOCs approved for AD 2006-23-02 are approved for this AD.
Related Information
(h) To get copies of the service information referenced in this
AD, contact Hawker Beechcraft Corporation, P.O. Box 85, Wichita,
Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. To
view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif
Building, Room PL-401, Washington, DC, or on the Internet at https://dms.dot.gov. The docket number is Docket No. FAA-2007-27071;
Directorate Identifier 2007-CE-004-AD.
Material Incorporated by Reference
(i) You must use Raytheon Aircraft Company Mandatory Service
Bulletin Number SB 27-3761, Issued: February 2006; or Raytheon
Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Rev.
1, Dated December 2006, 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 Raytheon Aircraft Company Mandatory
Service Bulletin Number SB 27-3761, Rev. 1, Dated December 2006,
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) On December 13, 2006 (71 FR 65390 Nov. 8, 2006), the
Director of the Federal Register approved the incorporation by
reference of Raytheon Aircraft Company Mandatory Service Bulletin
Number SB 27-3761, Issued: February 2006.
(3) For service information identified in this AD, contact
Hawker Beechcraft Corporation, P.O. Box 85, Wichita, Kansas 67201-
0085; telephone: (800) 429-5372 or (316) 676-3140.
(4) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at
the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, call 202-
741-6030, or go to: https://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Kansas City, Missouri, on May 29, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-10758 Filed 6-8-07; 8:45 am]
BILLING CODE 4910-13-P
