Airworthiness Directives; Dowty Aerospace Propellers Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies, 59647-59651 [05-20170]
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Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations
by adding the following new
airworthiness directive (AD):
2005–20–41 Boeing: Amendment 39–14338.
Docket No. FAA–2005–20137;
Directorate Identifier 2004–NM–96–AD.
Effective Date
(a) This AD becomes effective November
17, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Boeing Model 757–
200, –200PF, and –300 series airplanes;
certificated in any category; powered by Pratt
& Whitney PW2000 series engines.
Unsafe Condition
(d) This AD was prompted by reports of
damage and subsequent failure of the support
brackets and associated fasteners for the
hydraulic lines located internal to the upper
fairing cavity of the nacelle struts. We are
issuing this AD to prevent such failure,
which, in conjunction with sparking of
electrical wires, failure of seals that would
allow flammable fluids to migrate to
compartments with ignition sources, or
overheating of the pneumatic ducts beyond
auto-ignition temperatures, could result in an
uncontained fire.
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Repetitive Inspections
(f) Within 6,000 flight hours or 24 months
after the effective date of this AD, whichever
is first: Do a detailed inspection for loose or
damaged components of the support brackets
and associated fasteners for the hydraulic
lines located in the nacelle struts by
accomplishing all of the actions specified in
Part 1, Part 2, and Part 3 of the
Accomplishment Instructions of Boeing
Service Bulletin 757–29–0064 (for Model
757–200 and –200PF series airplanes) or
Boeing Service Bulletin 757–29–0065 (for
Model 757–300 series airplanes), both dated
February 29, 2004; as applicable. Repeat the
inspection thereafter at intervals not to
exceed 6,000 flight hours or 24 months,
whichever is first.
Note 1: For the purposes of this AD, a
detailed inspection is defined as: ‘‘An
intensive visual examination of a specific
structural area, system, installation, or
assembly to detect damage, failure, or
irregularity. Available lighting is normally
supplemented with a direct source of good
lighting at intensity deemed appropriate by
the inspector. Inspection aids such as mirror,
magnifying lenses, etc., may be used. Surface
cleaning and elaborate access procedures
may be required.’’
Concurrent Service Bulletin
(g) Prior to or concurrently with the
accomplishment of paragraph (f) of this AD:
Accomplish all of the actions specified in the
Accomplishment Instructions of Boeing
VerDate Aug<31>2005
14:41 Oct 12, 2005
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Service Bulletin 757–29–0043, dated June 21,
1990.
Note 2: The part numbers identified in
Boeing Service Bulletins 757–29–0064 or
757–29–0065, both dated February 29, 2004;
or Boeing Service Bulletin 757–29–0043,
dated June 21, 1990; are acceptable
configurations and fully comply with the AD
requirements for the actions required by
paragraphs (f) and (g) of this AD.
Related Investigative and Corrective Actions
(h) Except as required by paragraph (i) of
this AD: If any loose or damaged part is
found during any inspection required by
paragraph (f) of this AD, before further flight,
do all of the related investigative and
corrective actions specified in Part 1 and Part
2 of the Accomplishment Instructions of
Boeing Service Bulletin 757–29–0064, or
Boeing Service Bulletin 757–29–0065, both
dated February 29, 2004; as applicable.
Repair Information
(i) If any damage is found during any
inspection required by this AD, and the
service bulletin specifies contacting Boeing
for appropriate action: Before further flight,
repair per a method approved by the
Manager, Seattle Aircraft Certification Office
(ACO), FAA. For a repair method to be
approved, the approval letter must
specifically refer to this AD.
Note 3: There is no terminating action
currently available for the repetitive
inspections required by paragraph (f) of this
AD.
Alternative Methods of Compliance
(AMOCs)
(j)(1) The Manager, Seattle ACO, has the
authority to approve AMOCs for this AD, if
requested in accordance with the procedures
found in 14 CFR 39.19.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Material Incorporated by Reference
(k) You must use Boeing Service Bulletin
757–29–0064, dated February 29, 2004, or
Boeing Service Bulletin 757–29–0065, dated
February 29, 2004; and Boeing Service
Bulletin 757–29–0043, dated June 21, 1990;
as applicable, to perform the actions that are
required by this AD, unless the AD specifies
otherwise. The Director of the Federal
Register approved the incorporation by
reference of these documents in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51.
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 Docket Management
Facility, U.S. Department of Transportation,
400 Seventh Street SW., Room PL–401,
Nassif Building, Washington, DC; on the
Internet at https://dms.dot.gov; or at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at the NARA,
call (202) 741–6030, or go to https://
www.archives.gov/federal_register/
PO 00000
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59647
code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on
September 30, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–20264 Filed 10–12–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001–NE–50–AD; Amendment
39–14306; AD 2005–20–12]
RIN 2120–AA64
Airworthiness Directives; Dowty
Aerospace Propellers Type R321/4–82–
F/8, R324/4–82–F/9, R333/4–82–F/12,
and R334/4–82–F/13 Propeller
Assemblies
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: The FAA is superseding an
existing airworthiness directive (AD) for
Type R321/4–82–F/8, R324/4–82–F/9,
R333/4–82–F/12, and R334/4–82–F/13
propeller assemblies. That AD currently
requires initial and repetitive ultrasonic
inspections of propeller hubs, part
number (P/N) 660709201. This AD
requires the same initial and repetitive
ultrasonic inspections, but reduces the
initial and repetitive compliance times
for Type R334/4–82–F/13 propeller
assemblies when used on
Construcciones Aeronauticas, S.A.
(CASA) 212 airplanes. This AD results
from a report of a hub separation on a
CASA 212 airplane. We are issuing this
AD to prevent propeller hub failure due
to cracks in the hub, which could result
in loss of control of the airplane.
DATES: Effective October 28, 2005. The
Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the
regulations as of October 28, 2005. The
Director of the Federal Register
previously approved the incorporation
by reference of certain publications as
listed in the regulations as of July 27,
2004 (69 FR 34560, June 22, 2004).
We must receive any comments on
this AD by December 12, 2005.
ADDRESSES:
Use one of the following addresses to
comment on this AD:
• By mail: Federal Aviation
Administration (FAA), New England
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59648
Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations
Region, Office of the Regional Counsel,
Attention: Rules Docket No. 2001–NE–
50–AD, 12 New England Executive Park,
Burlington, MA 01803–5299.
• By fax: (781) 238–7055.
• By e-mail: 9–ane–
adcomment@faa.gov.
You can get the service information
referenced in this AD from Dowty
Aerospace Propellers, Anson Business
Park, Cheltenham Road East, Gloucester
GL 29QN, UK; telephone 44 (0) 1452
716000; fax 44 (0) 1452 716001.
You may examine the AD docket at
the FAA, New England Region, Office of
the Regional Counsel, 12 New England
Executive Park, Burlington, MA.
FOR FURTHER INFORMATION CONTACT:
Terry Fahr, Aerospace Engineer, Boston
Aircraft Certification Office, FAA,
Engine and Propeller Directorate, 12
New England Executive Park,
Burlington, MA 01803–5299; telephone
(781) 238–7116; fax (781) 238–7155.
SUPPLEMENTARY INFORMATION: June 10,
2004, the FAA issued AD 2004–13–01,
Amendment 39–13681 (69 FR 34560,
June 22, 2004). That AD requires initial
and repetitive ultrasonic inspections of
propeller hubs, P/N 660709201,
installed on airplanes, and for hubs and
propellers in storage, initial ultrasonic
inspection of propeller hubs before
placing in service. That AD was the
result of the manufacturer’s reevaluation
of potential hub failure on Type R321/
4–82–F/8, R324/4–82–F/9, R333/4–82–
F/12, and R334/4–82–F/13 propeller
assemblies. That condition, if not
corrected, could result in propeller hub
failure due to cracks in the hub, which
could result in loss of control of the
airplane.
Actions Since AD 2004–13–01 Was
Issued
Since we issued AD 2004–13–01, the
Civil Aviation Authority (CAA), which
is the airworthiness authority for the
United Kingdom (U.K.), recently
notified the FAA that an unsafe
condition might exist on Dowty
Aerospace Propellers Type R334/4–82–
F/13 propeller assemblies installed on
CASA 212 airplanes. The CAA advises
that they have received a report of a hub
separation of a Type R334/4–82–F/13
propeller assembly installed on a CASA
212 airplane. This AD requires the same
initial and repetitive inspections as
specified in AD 2004–13–01, but
reduces the compliance intervals for the
initial and repetitive inspections on
Type R334/4–82–F/13 propeller
assemblies installed on CASA 212
airplanes. We intend the actions
specified in this AD to prevent propeller
hub failure due to cracks in the hub,
VerDate Aug<31>2005
14:41 Oct 12, 2005
Jkt 208001
which could result in loss of control of
the airplane.
Relevant Service Information
We have reviewed and approved the
technical contents of Dowty Aerospace
Propellers Alert Mandatory Service
Bulletin (MSB) No. 61–1119, Revision 4,
dated September 14, 2005, that specifies
initial and repetitive ultrasonic
inspections of the rear wall of the rear
half of the propeller hub for cracks on
Type R334/4–82–F/13 propeller
assemblies. The CAA classified this
service bulletin as mandatory and
issued CAA UK AD No. G–2005–0027,
dated September 8, 2005, to assure the
airworthiness of these Dowty Aerospace
Propellers in the U.K.
Differences Between This AD and the
Manufacturer’s Service Information
Although Appendix A of Alert MSB
No. 61–1119, Revision 4, dated
September 14, 2005, requires reporting
the inspection data to Dowty Aerospace
Propellers, this AD requires that you
report the data to the Boston Aircraft
Certification Office of the FAA. Also,
the Accomplishment Instructions
3.A.(1) of Alert MSB No. 61–1119,
Revision 4, dated September 14, 2005,
allows you to use Appendix A or
Appendix D of that MSB, this AD
requires that you use Appendix A of
that MSB.
Bilateral Airworthiness Agreement
This propeller model is manufactured
in the U.K. and is type certificated for
operation in the United States under the
provisions of section 21.29 of the
Federal Aviation Regulations (14 CFR
21.29) and the applicable bilateral
airworthiness agreement. Under this
bilateral airworthiness agreement, the
CAA has kept the FAA informed of the
situation described above. We have
examined the findings of the CAA,
reviewed all available information, and
determined that AD action is necessary
for products of this type design that are
certificated for operation in the United
States.
FAA’s Determination and Requirements
of This AD
The unsafe condition described
previously is likely to exist or develop
on other Dowty Aerospace Propellers
Type R321/4–82–F/8, R324/4–82–F/9,
R333/4–82–F/12, and R334/4–82–F/13
propeller assemblies of the same type
design. We are issuing this AD to
prevent propeller hub failure due to
cracks in the hub, which could result in
loss of control of the airplane. This AD
requires:
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Fmt 4700
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• Within 10 flight hours (FH) time-inservice (TIS) or 20 days after the
effective date of this AD, whichever
occurs earlier, performing an initial
ultrasonic inspection of the rear halves
of propeller hubs P/N 660709201, that
are installed in Type R334/4–82–F/13
propeller assemblies, and;
• Within 50 FH TIS or 60 days after
the effective date of this AD, whichever
occurs earlier, performing an initial
ultrasonic inspection of the rear halves
of propeller hubs P/N 660709201, that
are installed in Type R321/4–82–F/8,
R324/4–82–F/9, and R333/4–82–F/12
propeller assemblies, and;
• Within 300 FH time-since-lastinspection (TSLI) performing a
repetitive ultrasonic inspection of the
rear halves of propeller hubs P/N
660709201, that are installed in Type
R334/4–82–F/13 propeller assemblies,
and;
• Within 1,000 FH TSLI performing a
repetitive ultrasonic inspection of the
rear halves of propeller hubs P/N
660709201, that are installed in Type
R321/4–82–F/8, R324/4–82–F/9, and
R333/4–82–F/12 propeller assemblies,
and;
• If not already done, performing an
ultrasonic inspection of the rear halves
of propeller hubs P/N 660709201, that
are installed in Type R321/4–82–F/8,
R324/4–82–F/9, R333/4–82–F/12, and
R334/4–82–F/13 propeller assemblies
that are in storage before installing the
propeller assembly onto an airplane.
You must use the service information
described previously to perform the
actions required by this AD.
FAA’s Determination of the Effective
Date
Since an unsafe condition exists that
requires the immediate adoption of this
AD, we have found that notice and
opportunity for public comment before
issuing this AD are impracticable and
that good cause exists for making this
amendment effective in less than 30
days.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety. We
did not precede it by notice and an
opportunity for public comment;
however, we invite you to send us any
written relevant data, views, or
arguments regarding this AD. Send your
comments to an address listed under
ADDRESSES. Include ‘‘AD Docket No.
2001–NE–50–AD’’ in the subject line of
your comments. If you want us to
acknowledge receipt of your mailed
comments, send us a self-addressed,
stamped postcard with the docket
number written on it; we will date-
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Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations
stamp your postcard and mail it back to
you. We specifically invite comments
on the overall regulatory, economic,
environmental, and energy aspects of
the rule that might suggest a need to
modify it. If a person contacts us
verbally, and that contact relates to a
substantive part of this AD, we will
summarize the contact and place the
summary in the docket. We will
consider all comments received by the
closing date and may amend the AD in
light of those comments.
Examining the AD Docket
You may examine the AD Docket
(including any comments and service
information), by appointment, between
8 a.m. and 4:30 p.m., Monday through
Friday, except Federal holidays. See
ADDRESSES for the location.
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 rulemaking
action.
Regulatory Findings
§ 39.13
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 the regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a summary of the costs
to comply with this AD 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 ‘‘AD Docket No. 2001–NE–50–
AD’’ in your request.
59649
I
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:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The FAA amends § 39.13 by
removing Amendment 39–13681 (69 FR
34560, June 22, 2004), and by adding a
new airworthiness directive,
Amendment 39–14306, to read as
follows:
2005–20–12 Dowty Aerospace Propellers:
Amendment 39–14306. Docket No.
2001–NE–50–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective October 28, 2005.
Affected ADs
(b) This AD supersedes AD 2004–13–01,
Amendment 39–13681.
Applicability
(c) This AD applies to Dowty Aerospace
Propellers Type R321/4–82–F/8, R324/4–82–
F/9, R333/4–82–F/12, and R334/4–82–F/13
propeller assemblies with propeller hubs part
number (P/N) 660709201. These propeller
assemblies are installed on, but not limited
to, Construcciones Aeronauticas, S.A.
(CASA) 212, British Aerospace Regional
Aircraft Jetstream Models 3101 and 3201,
Fairchild Aircraft, Inc., Merlin IIIC, and
Merlin IVC/Metro III airplanes.
Unsafe Condition
(d) This AD results from a report of a hub
separation on a CASA 212 airplane. We are
issuing this AD to prevent propeller hub
failure due to cracks in the hub, which could
result in loss of control of the airplane.
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified unless the
actions have already been done.
Initial Ultrasonic Inspections
(f) Perform an initial ultrasonic inspection
of the rear wall of the rear half of the
propeller hub for cracks within the
compliance time specified in the following
Table 1. Use Appendix A of the applicable
Dowty Mandatory Service Bulletin (MSB)
listed in Table 1 of this AD.
TABLE 1.—APPLICABLE MSB FOR PROPELLER TYPE
Propeller assembly type
Initial inspection within the earlier
of . . .
Repeat inspection within . . .
Applicable MSB
(1) R334/4–82–F/13 .......................
10 flight hours (FH) time-in-service (TIS) or 20 days after the
effective date of this AD.
50 FH TIS or 60 days after the effective date of this AD.
50 FH TIS or 60 days after the effective date of this AD.
50 FH TIS or 60 days after the effective date of this AD.
300 FH time-since-last-inspection
(TSLI).
Alert MSB No. 61–1119, Revision
4, dated September 14, 2005.
1,000 FH TSLI ..............................
MSB No. 61–1125, Revision 1,
dated October 9, 2002.
MSB No. 61–1126, Revision 1,
dated October 9, 2002.
MSB No. 61–1124, Revision 1,
dated October 8, 2002.
(2) R321/4–82–F/8 .........................
(3) R324/4–82–F/9 .........................
(4) R333/4–82–F/12 .......................
(g) For hubs and propellers in storage,
perform an initial ultrasonic inspection of the
rear wall of the rear half of the propeller hub
for cracks, before placing in service. Use
VerDate Aug<31>2005
14:41 Oct 12, 2005
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1,000 FH TSLI ..............................
1,000 FH TSLI ..............................
Appendix A of the applicable Dowty MSB
listed in Table 1 of this AD.
(h) Propeller hubs, P/N 660709201, already
inspected using a Dowty MSB listed in Table
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1 or earlier issue of those MSBs, comply with
paragraph (f) of this AD.
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Repetitive Ultrasonic Inspections
Alternative Methods of Compliance
(i) Thereafter, perform a repetitive
ultrasonic inspection of the rear wall of the
rear half of the propeller hub for cracks
within the compliance time specified in
Table 1 of this AD. Use Appendix A of the
applicable Dowty Mandatory Service Bulletin
(MSB) listed in Table 1 of this AD.
(k) The Manager, Boston Certification
Office, has the authority to approve
alternative methods of compliance for this
AD if requested using the procedures found
in 14 CFR 39.19.
Inspection Reporting Requirements
(j) Within 10 days after each inspection,
record the inspection data on a copy of
Appendix B of the applicable MSB listed in
Table 1 of this AD. Report the findings to the
Manager, Boston Aircraft Certification Office,
FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington,
MA 01803–5299. The Office of Management
and Budget (OMB) approved the reporting
requirements and assigned OMB control
number 2120–0056.
Special Flight Permits
(l) Special flight permits may be issued in
accordance with §§ 21.197 and 21.199 of the
Federal Aviation Regulations (14 CFR 21.197
and 21.199) to operate the airplane to a
location where the requirements of this AD
can be done.
Documents That Have Been Incorporated by
Reference
(m) You must use the service information
specified in Table 2 to perform the
inspections required by this AD. The Director
of the Federal Register approved the
incorporation by reference of Dowty Alert
Mandatory Service Bulletin (MSB) No. 61–
1119, Revision 4, Dated September 14, 2005,
listed in Table 2 of this AD, in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51. The
Director of the Federal Register previously
approved the incorporation by reference of
MSB No. 61–1124, Revision 1, Dated October
8, 2002, and MSB No. 61–1125, Revision 1,
Dated October 9, 2002, and MSB 61–1126,
Revision 1, Dated October 9, 2002 (69 FR
34560, June 22, 2004). Contact Dowty
Propellers, Anson Business Park, Cheltenham
Road East, Gloucester GL 29QN, UK;
telephone 44 (0) 1452 716000; fax 44 (0) 1452
716001 for a copy of this service information.
You may review copies at the FAA, New
England Region, Office of the Regional
Counsel, 12 New England Executive Park,
Burlington, MA; 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/ibr-locations.html.
TABLE 2.—INCORPORATION BY REFERENCE
Service Bulletin No.
Page
Revision
Date
Alert MSB No. 61–1119 ......................................................
Appendix A .........................................................................
All .........................................
1 ...........................................
2 ...........................................
3–6 .......................................
1 ...........................................
All .........................................
All .........................................
4 ...........................................
1 ...........................................
Original .................................
1 ...........................................
Original .................................
Original .................................
Original .................................
September 14, 2005.
November 27, 2001.
November 1, 2001.
November 27, 2001.
November 1, 2001.
November 27, 2001.
December 6, 2001.
30 .........................................
1 ...........................................
2–3 .......................................
All .........................................
All .........................................
All .........................................
All .........................................
..............................................
1 ...........................................
Original .................................
Original .................................
Original .................................
Original .................................
Original .................................
October 8, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
30 .........................................
1 ...........................................
2–3 .......................................
All .........................................
All .........................................
All .........................................
All .........................................
..............................................
1 ...........................................
Original .................................
Original .................................
Original .................................
Original .................................
Original .................................
October 9, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
.........................................................................
.........................................................................
.........................................................................
.........................................................................
30 .........................................
1 ...........................................
2–3 .......................................
All .........................................
All .........................................
All .........................................
All .........................................
..............................................
1 ...........................................
Original .................................
Original .................................
Original .................................
Original .................................
Original .................................
October 9, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
May 7, 2002.
Total pages ..................................................................
30 .........................................
..............................................
Appendix B .........................................................................
Appendix C .........................................................................
Appendix D .........................................................................
Total pages ..................................................................
MSB No. 61–1124 ..............................................................
Appendix
Appendix
Appendix
Appendix
A
B
C
D
.........................................................................
.........................................................................
.........................................................................
.........................................................................
Total pages ..................................................................
MSB No. 61–1125 ..............................................................
Appendix
Appendix
Appendix
Appendix
A
B
C
D
.........................................................................
.........................................................................
.........................................................................
.........................................................................
Total pages ..................................................................
MSB No. 61–1126 ..............................................................
Appendix
Appendix
Appendix
Appendix
A
B
C
D
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Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Rules and Regulations
Related Information
(n) United Kingdom (U.K.) Civil Aviation
Authority (CAA) airworthiness directives No.
G–2006–0027, dated September 8, 2005; CAA
UK AD No. 009–05–2002, dated April 15,
2003; CAA UK AD No. 010–05–2002, dated
April 15, 2003; and CAA UK AD No. 011–
05–2002, dated April 15, 2003, also addresses
the subject of this AD.
§ 71.1
Issued in Burlington, Massachusetts, on
September 26, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 05–20170 Filed 10–12–05; 8:45 am]
Paragraph 5000
Class D Airspace.
*
*
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Amended]
DEPARTMENT OF TRANSPORTATION
2. The incorporation by reference in
14 CFR 71.1 of Federal Aviation
Administration Order 7400.9N, dated
September 1, 2005, and effective
September 15, 2005, is amended as
follows:
I
*
*
*
ACE KS D Salina, KS
Salina Municipal Airport, KS
(Lat. 38°47′27″ N., long. 97°39′08″ W.)
That airspace extending upward from the
surface to and including 3,800 feet MSL
within a 5.4-mile radius of Salina Municipal
Airport. This Class D airspace area is
effective during the specific dates and times
established in advance by a Notice to
Airmen. The effective date and time will
thereafter be continuously published in the
Airport/Facility Directory.
*
*
*
*
*
[Docket No. FAA–2005–21873; Airspace
Docket No. 05–ACE–27]
Paragraph 6002 Class E Airspace
Designated as Surface Areas.
Modification of Class D and Class E
Airspace; Salina Municipal Airport, KS;
Correction
*
Federal Aviation
Administration (FAA), DOT.
ACTION: Direct final rule; request for
comments; correction.
AGENCY:
History
Federal Register Document 2005–
21873 published on Friday July 29, 2005
(70 FR 43742), modified Class D and
Class E Airspace at Salina Municipal
Airport, KS. The legal descriptions of
these airspace areas used outdated and
incorrect information. This action
corrects those errors.
I Accordingly, pursuant to the authority
delegated to me, the errors in the legal
descriptions of airspace at Salina
Municipal Airport, KS as published in
the Federal Register Friday July 29,
2005 (70 FR 43742), (FR Doc. 2005–
21873), are corrected as follows:
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*
*
*
ACE KS E2 Salina, KS
Salina Municipal Airport, KS
(Lat. 38°47′27″ N., long. 97°39′08″ W.)
Airmen. The effective date and time will
thereafter be continuously published in the
Airport/Facility Directory.
*
SUMMARY: This action corrects errors in
the legal description of Class D airspace
in a direct final rule, request for
comments that was published in the
Federal Register on Friday July 29, 2005
(70 FR 43742).
DATES: This direct final rule is effective
on 0901 UTC, October 27, 2005.
FOR FURTHER INFORMATION CONTACT:
Brenda Mumper, Air Traffic Division,
Airspace Branch, ACE–520A, DOT
Regional Headquarters Building, Federal
Aviation Administration, 901 Locust,
Kansas City, MO 64106; telephone:
(816) 329–2524.
SUPPLEMENTARY INFORMATION:
*
*
*
*
*
Paragraph 6004 Class E Airspace
Designated as an Extension to a Class D or
Class E Surface Area.
*
*
*
*
*
ACE KS E4 Salina, KS
Salina Municipal Airport, KS
(Lat. 38°47′27″ N., long. 97°39′08″ W.)
Salina VORTAC
(Lat. 38°55′31″ N., long. 97°37′17″ W.)
That airspace extending upward surface
within 1.5 miles each side of the Salina
VORTAC 190° radial extending from the 5.4mile radius of Salina Municipal Airport to 2
miles south of the VORTAC.
*
*
*
*
*
Paragraph 6005 Class E airspace areas
extending upward from 700 feet or more
above the surface of the earth.
*
*
*
*
*
ACE KS E5 Salina, KS
Salina Municipal Airport, KS
(Lat. 38°47′27″ N., long. 97°39′08″ W.)
That airspace extending upward from 700
feet above the surface within an 8.4-mile
radius of Salina Municipal Airport.
Issued in Kansas City, MO, on September
20, 2005.
Elizabeth S. Wallis,
Acting Area Director, Western Flight Services
Operations.
[FR Doc. 05–20462 Filed 10–12–05; 8:45 am]
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Federal Aviation Administration
14 CFR Part 71
[Docket FAA 2005–21523; Airspace Docket
No. 05–AWP–07]
Establishment of Class E3 Airspace,
Riverside March Field, CA
Federal Aviation
Administration (FAA), DOT.
AGENCY:
ACTION:
Final rule.
SUMMARY: This action establishes a Class
E3 airspace area at Riverside March
Field, CA.
EFFECTIVE DATE:
0901 UTC December 22,
2005.
FOR FURTHER INFORMATION CONTACT:
Debra Trindle, Western Terminal
Service Area, Airspace Specialist,
AWP–520, Federal Aviation
Administration, 15000 Aviation
Boulevard, Lawndale, California 90261,
telephone (310) 725–6613.
SUPPLEMENTARY INFORMATION:
History
On August 2, 2005, the FAA proposed
to establish Class E3 airspace at
Riverside March Field, CA. Class E3
airspace areas are designated as arrival
extensions to a Class C surface area.
Class E arrival extensions are primarily
designated to provide additional
controlled airspace ancillary to a surface
area to protect instrument operations for
the primary airport, without imposing
additional communications burdens on
airspace users. This action is necessary
at Riverside March Field to provide
controlled airspace for Category E
aircraft conducting circling maneuvers
in conjunction with published Standard
Instrument Approach Procedures.
Generally, Category E aircraft are very
large and/or high performance. These
aircraft require additional airspace
when conducting circling maneuvers.
This action will establish the Class E3
airspace at Riverside March Field.
Interested parties were invited to
participate in this rule making
proceeding by submitting written
comments on the proposal to the FAA.
No comments were received. Class E3
airspace is published in Paragraph 6003
of FAA Order 7400.9N dated September
1, 2005, and effective September 16,
2005, which is incorporated by
reference in 14 CFR 71.1. The Class E
Surface Area airspace designation listed
in this document would be published
subsequently in this Order.
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[Federal Register Volume 70, Number 197 (Thursday, October 13, 2005)]
[Rules and Regulations]
[Pages 59647-59651]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-20170]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NE-50-AD; Amendment 39-14306; AD 2005-20-12]
RIN 2120-AA64
Airworthiness Directives; Dowty Aerospace Propellers Type R321/4-
82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller
Assemblies
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding an existing airworthiness directive
(AD) for Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-
82-F/13 propeller assemblies. That AD currently requires initial and
repetitive ultrasonic inspections of propeller hubs, part number (P/N)
660709201. This AD requires the same initial and repetitive ultrasonic
inspections, but reduces the initial and repetitive compliance times
for Type R334/4-82-F/13 propeller assemblies when used on
Construcciones Aeronauticas, S.A. (CASA) 212 airplanes. This AD results
from a report of a hub separation on a CASA 212 airplane. We are
issuing this AD to prevent propeller hub failure due to cracks in the
hub, which could result in loss of control of the airplane.
DATES: Effective October 28, 2005. The Director of the Federal Register
approved the incorporation by reference of certain publications listed
in the regulations as of October 28, 2005. The Director of the Federal
Register previously approved the incorporation by reference of certain
publications as listed in the regulations as of July 27, 2004 (69 FR
34560, June 22, 2004).
We must receive any comments on this AD by December 12, 2005.
ADDRESSES:
Use one of the following addresses to comment on this AD:
By mail: Federal Aviation Administration (FAA), New
England
[[Page 59648]]
Region, Office of the Regional Counsel, Attention: Rules Docket No.
2001-NE-50-AD, 12 New England Executive Park, Burlington, MA 01803-
5299.
By fax: (781) 238-7055.
By e-mail: 9-ane-adcomment@faa.gov.
You can get the service information referenced in this AD from
Dowty Aerospace Propellers, Anson Business Park, Cheltenham Road East,
Gloucester GL 29QN, UK; telephone 44 (0) 1452 716000; fax 44 (0) 1452
716001.
You may examine the AD docket at the FAA, New England Region,
Office of the Regional Counsel, 12 New England Executive Park,
Burlington, MA.
FOR FURTHER INFORMATION CONTACT: Terry Fahr, Aerospace Engineer, Boston
Aircraft Certification Office, FAA, Engine and Propeller Directorate,
12 New England Executive Park, Burlington, MA 01803-5299; telephone
(781) 238-7116; fax (781) 238-7155.
SUPPLEMENTARY INFORMATION: June 10, 2004, the FAA issued AD 2004-13-01,
Amendment 39-13681 (69 FR 34560, June 22, 2004). That AD requires
initial and repetitive ultrasonic inspections of propeller hubs, P/N
660709201, installed on airplanes, and for hubs and propellers in
storage, initial ultrasonic inspection of propeller hubs before placing
in service. That AD was the result of the manufacturer's reevaluation
of potential hub failure on Type R321/4-82-F/8, R324/4-82-F/9, R333/4-
82-F/12, and R334/4-82-F/13 propeller assemblies. That condition, if
not corrected, could result in propeller hub failure due to cracks in
the hub, which could result in loss of control of the airplane.
Actions Since AD 2004-13-01 Was Issued
Since we issued AD 2004-13-01, the Civil Aviation Authority (CAA),
which is the airworthiness authority for the United Kingdom (U.K.),
recently notified the FAA that an unsafe condition might exist on Dowty
Aerospace Propellers Type R334/4-82-F/13 propeller assemblies installed
on CASA 212 airplanes. The CAA advises that they have received a report
of a hub separation of a Type R334/4-82-F/13 propeller assembly
installed on a CASA 212 airplane. This AD requires the same initial and
repetitive inspections as specified in AD 2004-13-01, but reduces the
compliance intervals for the initial and repetitive inspections on Type
R334/4-82-F/13 propeller assemblies installed on CASA 212 airplanes. We
intend the actions specified in this AD to prevent propeller hub
failure due to cracks in the hub, which could result in loss of control
of the airplane.
Relevant Service Information
We have reviewed and approved the technical contents of Dowty
Aerospace Propellers Alert Mandatory Service Bulletin (MSB) No. 61-
1119, Revision 4, dated September 14, 2005, that specifies initial and
repetitive ultrasonic inspections of the rear wall of the rear half of
the propeller hub for cracks on Type R334/4-82-F/13 propeller
assemblies. The CAA classified this service bulletin as mandatory and
issued CAA UK AD No. G-2005-0027, dated September 8, 2005, to assure
the airworthiness of these Dowty Aerospace Propellers in the U.K.
Differences Between This AD and the Manufacturer's Service Information
Although Appendix A of Alert MSB No. 61-1119, Revision 4, dated
September 14, 2005, requires reporting the inspection data to Dowty
Aerospace Propellers, this AD requires that you report the data to the
Boston Aircraft Certification Office of the FAA. Also, the
Accomplishment Instructions 3.A.(1) of Alert MSB No. 61-1119, Revision
4, dated September 14, 2005, allows you to use Appendix A or Appendix D
of that MSB, this AD requires that you use Appendix A of that MSB.
Bilateral Airworthiness Agreement
This propeller model is manufactured in the U.K. and is type
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement. Under this bilateral
airworthiness agreement, the CAA has kept the FAA informed of the
situation described above. We have examined the findings of the CAA,
reviewed all available information, and determined that AD action is
necessary for products of this type design that are certificated for
operation in the United States.
FAA's Determination and Requirements of This AD
The unsafe condition described previously is likely to exist or
develop on other Dowty Aerospace Propellers Type R321/4-82-F/8, R324/4-
82-F/9, R333/4-82-F/12, and R334/4-82-F/13 propeller assemblies of the
same type design. We are issuing this AD to prevent propeller hub
failure due to cracks in the hub, which could result in loss of control
of the airplane. This AD requires:
Within 10 flight hours (FH) time-in-service (TIS) or 20
days after the effective date of this AD, whichever occurs earlier,
performing an initial ultrasonic inspection of the rear halves of
propeller hubs P/N 660709201, that are installed in Type R334/4-82-F/13
propeller assemblies, and;
Within 50 FH TIS or 60 days after the effective date of
this AD, whichever occurs earlier, performing an initial ultrasonic
inspection of the rear halves of propeller hubs P/N 660709201, that are
installed in Type R321/4-82-F/8, R324/4-82-F/9, and R333/4-82-F/12
propeller assemblies, and;
Within 300 FH time-since-last-inspection (TSLI) performing
a repetitive ultrasonic inspection of the rear halves of propeller hubs
P/N 660709201, that are installed in Type R334/4-82-F/13 propeller
assemblies, and;
Within 1,000 FH TSLI performing a repetitive ultrasonic
inspection of the rear halves of propeller hubs P/N 660709201, that are
installed in Type R321/4-82-F/8, R324/4-82-F/9, and R333/4-82-F/12
propeller assemblies, and;
If not already done, performing an ultrasonic inspection
of the rear halves of propeller hubs P/N 660709201, that are installed
in Type R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/
13 propeller assemblies that are in storage before installing the
propeller assembly onto an airplane.
You must use the service information described previously to
perform the actions required by this AD.
FAA's Determination of the Effective Date
Since an unsafe condition exists that requires the immediate
adoption of this AD, we have found that notice and opportunity for
public comment before issuing this AD are impracticable and that good
cause exists for making this amendment effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety. We did not precede it by notice and an opportunity for public
comment; however, we invite you to send us any written relevant data,
views, or arguments regarding this AD. Send your comments to an address
listed under ADDRESSES. Include ``AD Docket No. 2001-NE-50-AD'' in the
subject line of your comments. If you want us to acknowledge receipt of
your mailed comments, send us a self-addressed, stamped postcard with
the docket number written on it; we will date-
[[Page 59649]]
stamp your postcard and mail it back to you. We specifically invite
comments on the overall regulatory, economic, environmental, and energy
aspects of the rule that might suggest a need to modify it. If a person
contacts us verbally, and that contact relates to a substantive part of
this AD, we will summarize the contact and place the summary in the
docket. We will consider all comments received by the closing date and
may amend the AD in light of those comments.
Examining the AD Docket
You may examine the AD Docket (including any comments and service
information), by appointment, between 8 a.m. and 4:30 p.m., Monday
through Friday, except Federal holidays. See ADDRESSES for the
location.
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
rulemaking action.
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 the regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a summary of the costs to comply with this AD 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
``AD Docket No. 2001-NE-50-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
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 Amendment 39-13681 (69 FR
34560, June 22, 2004), and by adding a new airworthiness directive,
Amendment 39-14306, to read as follows:
2005-20-12 Dowty Aerospace Propellers: Amendment 39-14306. Docket
No. 2001-NE-50-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective October
28, 2005.
Affected ADs
(b) This AD supersedes AD 2004-13-01, Amendment 39-13681.
Applicability
(c) This AD applies to Dowty Aerospace Propellers Type R321/4-
82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 propeller
assemblies with propeller hubs part number (P/N) 660709201. These
propeller assemblies are installed on, but not limited to,
Construcciones Aeronauticas, S.A. (CASA) 212, British Aerospace
Regional Aircraft Jetstream Models 3101 and 3201, Fairchild
Aircraft, Inc., Merlin IIIC, and Merlin IVC/Metro III airplanes.
Unsafe Condition
(d) This AD results from a report of a hub separation on a CASA
212 airplane. We are issuing this AD to prevent propeller hub
failure due to cracks in the hub, which could result in loss of
control of the airplane.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified unless the
actions have already been done.
Initial Ultrasonic Inspections
(f) Perform an initial ultrasonic inspection of the rear wall of
the rear half of the propeller hub for cracks within the compliance
time specified in the following Table 1. Use Appendix A of the
applicable Dowty Mandatory Service Bulletin (MSB) listed in Table 1
of this AD.
Table 1.--Applicable MSB for Propeller Type
----------------------------------------------------------------------------------------------------------------
Initial inspection
Propeller assembly type within the earlier of . Repeat inspection Applicable MSB
. . within . . .
----------------------------------------------------------------------------------------------------------------
(1) R334/4-82-F/13................... 10 flight hours (FH) 300 FH time-since-last- Alert MSB No. 61-1119,
time-in-service (TIS) inspection (TSLI). Revision 4, dated
or 20 days after the September 14, 2005.
effective date of this
AD.
(2) R321/4-82-F/8.................... 50 FH TIS or 60 days 1,000 FH TSLI.......... MSB No. 61-1125,
after the effective Revision 1, dated
date of this AD. October 9, 2002.
(3) R324/4-82-F/9.................... 50 FH TIS or 60 days 1,000 FH TSLI.......... MSB No. 61-1126,
after the effective Revision 1, dated
date of this AD. October 9, 2002.
(4) R333/4-82-F/12................... 50 FH TIS or 60 days 1,000 FH TSLI.......... MSB No. 61-1124,
after the effective Revision 1, dated
date of this AD. October 8, 2002.
----------------------------------------------------------------------------------------------------------------
(g) For hubs and propellers in storage, perform an initial
ultrasonic inspection of the rear wall of the rear half of the
propeller hub for cracks, before placing in service. Use Appendix A
of the applicable Dowty MSB listed in Table 1 of this AD.
(h) Propeller hubs, P/N 660709201, already inspected using a
Dowty MSB listed in Table 1 or earlier issue of those MSBs, comply
with paragraph (f) of this AD.
[[Page 59650]]
Repetitive Ultrasonic Inspections
(i) Thereafter, perform a repetitive ultrasonic inspection of
the rear wall of the rear half of the propeller hub for cracks
within the compliance time specified in Table 1 of this AD. Use
Appendix A of the applicable Dowty Mandatory Service Bulletin (MSB)
listed in Table 1 of this AD.
Inspection Reporting Requirements
(j) Within 10 days after each inspection, record the inspection
data on a copy of Appendix B of the applicable MSB listed in Table 1
of this AD. Report the findings to the Manager, Boston Aircraft
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803-5299. The Office of
Management and Budget (OMB) approved the reporting requirements and
assigned OMB control number 2120-0056.
Alternative Methods of Compliance
(k) The Manager, Boston Certification Office, has the authority
to approve alternative methods of compliance for this AD if
requested using the procedures found in 14 CFR 39.19.
Special Flight Permits
(l) Special flight permits may be issued in accordance with
Sec. Sec. 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be done.
Documents That Have Been Incorporated by Reference
(m) You must use the service information specified in Table 2 to
perform the inspections required by this AD. The Director of the
Federal Register approved the incorporation by reference of Dowty
Alert Mandatory Service Bulletin (MSB) No. 61-1119, Revision 4,
Dated September 14, 2005, listed in Table 2 of this AD, in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. The Director of
the Federal Register previously approved the incorporation by
reference of MSB No. 61-1124, Revision 1, Dated October 8, 2002, and
MSB No. 61-1125, Revision 1, Dated October 9, 2002, and MSB 61-1126,
Revision 1, Dated October 9, 2002 (69 FR 34560, June 22, 2004).
Contact Dowty Propellers, Anson Business Park, Cheltenham Road East,
Gloucester GL 29QN, UK; telephone 44 (0) 1452 716000; fax 44 (0)
1452 716001 for a copy of this service information. You may review
copies at the FAA, New England Region, Office of the Regional
Counsel, 12 New England Executive Park, Burlington, MA; 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/ibr-
locations.html.
Table 2.--Incorporation by Reference
----------------------------------------------------------------------------------------------------------------
Service Bulletin No. Page Revision Date
----------------------------------------------------------------------------------------------------------------
Alert MSB No. 61-1119............. All.................. 4................... September 14, 2005.
Appendix A........................ 1.................... 1................... November 27, 2001.
2.................... Original............ November 1, 2001.
3-6.................. 1................... November 27, 2001.
Appendix B........................ 1.................... Original............ November 1, 2001.
Appendix C........................ All.................. Original............ November 27, 2001.
Appendix D........................ All.................. Original............ December 6, 2001.
========================
Total pages................... 30................... .................... ...............................
MSB No. 61-1124................... 1.................... 1................... October 8, 2002.
2-3.................. Original............ May 7, 2002.
Appendix A........................ All.................. Original............ May 7, 2002.
Appendix B........................ All.................. Original............ May 7, 2002.
Appendix C........................ All.................. Original............ May 7, 2002.
Appendix D........................ All.................. Original............ May 7, 2002.
========================
Total pages................... 30................... .................... ...............................
MSB No. 61-1125................... 1.................... 1................... October 9, 2002.
2-3.................. Original............ May 7, 2002.
Appendix A........................ All.................. Original............ May 7, 2002.
Appendix B........................ All.................. Original............ May 7, 2002.
Appendix C........................ All.................. Original............ May 7, 2002.
Appendix D........................ All.................. Original............ May 7, 2002.
========================
Total pages................... 30................... .................... ...............................
MSB No. 61-1126................... 1.................... 1................... October 9, 2002.
2-3.................. Original............ May 7, 2002.
Appendix A........................ All.................. Original............ May 7, 2002.
Appendix B........................ All.................. Original............ May 7, 2002.
Appendix C........................ All.................. Original............ May 7, 2002.
Appendix D........................ All.................. Original............ May 7, 2002.
------------------------
Total pages................... 30................... .................... ...............................
----------------------------------------------------------------------------------------------------------------
[[Page 59651]]
Related Information
(n) United Kingdom (U.K.) Civil Aviation Authority (CAA)
airworthiness directives No. G-2006-0027, dated September 8, 2005;
CAA UK AD No. 009-05-2002, dated April 15, 2003; CAA UK AD No. 010-
05-2002, dated April 15, 2003; and CAA UK AD No. 011-05-2002, dated
April 15, 2003, also addresses the subject of this AD.
Issued in Burlington, Massachusetts, on September 26, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 05-20170 Filed 10-12-05; 8:45 am]
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