Airworthiness Directives; Pratt & Whitney JT9D-7R4 Turbofan Engines, 76381-76385 [05-24448]
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Federal Register / Vol. 70, No. 247 / Tuesday, December 27, 2005 / Rules and Regulations
(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.
Related Information
(i) French airworthiness directive F–2005–
165, dated September 28, 2005, also
addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use the documents listed in
Table 2 of this AD 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 Airbus, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France, 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/
code_of_federal_regulations/
ibr_locations.html.
TABLE 2.—MATERIAL INCORPORATED
BY REFERENCE
Airbus Temporary
Revision to the A318/
A319/A320/A321 Airplane Flight Manual
4.02.00/28 ................
4.02.00/29 ................
4.02.00/30 ................
Date
February 21, 2005.
February 22, 2005.
February 23, 2005.
Issued in Renton, Washington, on
December 14, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–24344 Filed 12–23–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–23072; Directorate
Identifier 2005–NE–38–AD; Amendment 39–
14430; AD 2005–26–09]
wwhite on PROD1PC61 with RULES
RIN 2120–AA64
Airworthiness Directives; Pratt &
Whitney JT9D–7R4 Turbofan Engines
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
AGENCY:
VerDate Aug<31>2005
17:10 Dec 23, 2005
Jkt 208001
Final rule; request for
comments.
ACTION:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for Pratt &
Whitney (PW) JT9D–7R4 turbofan
engines. This AD requires inspection of
the blade root thickness of 1st stage fan
blades identified by part number (P/N)
and serial number (SN) in this AD, by
a repair station approved by PW to
perform the inspection. This AD results
from a report that a repair station
created their own repair and performed
it on 520 1st stage fan blades, without
approval from PW. We are issuing this
AD to prevent 1st stage fan blade
fracture and uncontained engine failure,
resulting in possible damage to the
airplane.
This AD becomes effective
January 11, 2006.
We must receive any comments on
this AD by February 27, 2006.
ADDRESSES: Use one of the following
addresses to comment on this AD:
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
0001.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street, SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Kevin Donovan, Aerospace Engineer,
Engine Certification Office, FAA, Engine
and Propeller Directorate, 12 New
England Executive Park, Burlington, MA
01803–5299; telephone (781) 238–7743,
fax (781) 238–7199.
SUPPLEMENTARY INFORMATION: In May
2005, we received a report from Airfoil
Technologies International (ATI), of the
United Kingdom, that their repair
station created their own repair and
performed it on 520 1st stage fan blades,
without approval from PW. The repairs
were made to a critical area of the fan
blade root. PW requires source
demonstration by each repair station
before they approve the repair station to
perform blade repairs, including the
repair that should have been performed
to these 1st stage fan blades, known as
Repair-23. This requirement exists due
to PW’s concern with proper blending
DATES:
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76381
in a critical area of the blade root. This
condition, if not corrected, could result
in 1st stage fan blade fracture and
uncontained engine failure, resulting in
possible damage to the airplane.
FAA’s Determination and Requirements
of this AD
The unsafe condition described
previously is likely to exist or develop
on other PW JT9D–7R4 turbofan engines
of the same type design. For that reason,
we are issuing this AD to prevent 1st
stage fan blade fracture and uncontained
engine failure, resulting in possible
damage to the airplane. This AD
requires, before installing the 1st stage
fan blades that are listed by P/N and SN
in Table 1 of this AD, or if already
installed, at the next 1st stage fan blade
exposure:
• Checking the 1st stage fan blade for
a circled, letter I, on the approved
marking area of the outboard side of the
blade platform. If the blade has this
marking, no further action is required.
• Removing 1st stage fan blades
without a circled, letter I, on the
approved marking area of the outboard
side of the blade platform if installed;
and
• Sending 1st stage fan blades to a
source-substantiation-approved repair
station, approved by PW, for inspection
of the blade root thickness; and
• Returning to service 1st stage fan
blades that pass the inspection, after
properly marking the blade.
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 and
was not preceded 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.
FAA–2005–23072; Directorate Identifier
2005–NE–38–AD’’ in the subject line of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of the rule that might suggest a
need to modify it.
We will post all comments we
receive, without change, to https://
E:\FR\FM\27DER1.SGM
27DER1
76382
Federal Register / Vol. 70, No. 247 / Tuesday, December 27, 2005 / Rules and Regulations
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact with FAA
personnel concerning this AD. Using the
search function of the DMS Web site,
anyone can find and read the comments
in any of our dockets, including the
name of the individual who sent the
comment (or signed the comment on
behalf of an association, business, labor
union, etc.). You may review the DOT’s
complete Privacy Act Statement in the
Federal Register published on April 11,
2000 (65 FR 19477–78) or you may visit
https://dms.dot.gov.
Examining the AD Docket
You may examine the docket that
contains the AD, any comments
received, and any final disposition in
person at the Docket Management
Facility Docket Office between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The Docket
Office (telephone (800) 647–5227) is
located on the plaza level of the
Department of Transportation Nassif
Building at the street address stated in
ADDRESSES. Comments will be available
in the AD docket shortly after the DMS
receives them.
Authority for This Rulemaking
wwhite on PROD1PC61 with RULES
Regulatory Findings
We 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.
17:10 Dec 23, 2005
Jkt 208001
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
Adoption of the Amendment
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:
I
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.
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.
VerDate Aug<31>2005
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 at the address listed
under ADDRESSES.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
I
2005–26–09 Pratt & Whitney: Amendment
39–14430. Docket No. FAA–2005–23072;
Directorate Identifier 2005–NE–38–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective January 11, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Pratt & Whitney
(PW) JT9D–7R4 turbofan engines. These
engines are installed on, but not limited to,
Airbus A300 and A310, and Boeing 747and
767 airplanes.
Unsafe Condition
(d) This AD results from a report that a
repair station created their own repair and
performed it on 520 1st stage fan blades,
without approval from PW. We are issuing
this AD to prevent 1st stage fan blade fracture
and uncontained engine failure, resulting in
possible damage to 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.
PO 00000
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(f) Before installing the 1st stage fan blades
that are listed by part number and serial
number in Table 1 of this AD, or if already
installed, at the next 1st stage fan blade
exposure, do the following:
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES
Part number
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
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5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
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5001341–022
5001341–022
5001341–022
5001341–022
5001341–022
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NE0394
NE0153
NN8054
JW4693
ND7304
MG6108
MG5862
MG5619
NE0308
NE0200
MG6797
JW0230
ND5652
ND5775
JW0251
ND5719
JW0248
ND5785
ND5676
ND5661
JW0265
ND5699
ND5767
JW0259
ND5680
ND5749
JW0235
ND5776
ND8580
MG6039
ND9127
JW4287
JW0262
JW0445
JW4665
MG5901
NE0303
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JW4286
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Federal Register / Vol. 70, No. 247 / Tuesday, December 27, 2005 / Rules and Regulations
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
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Part number
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VerDate Aug<31>2005
17:10 Dec 23, 2005
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
Serial no.
JW0644
JW4631
JW4651
JW0234
JW4646
NN9016
VJ3393
PX3694
RK9168
PX5023
VJ3324
VJ3504
NN9115
NN8936
PX3816
VJ3412
RK9163
VJ3447
RK9230
RK9109
PX4627
RK8990
SP9459
RK8656
NN8933
VJ3444
ND5864
NN9020
RK8905
SR1733
NN9047
PX3692
PX3786
NN9025
NN9007
RK9100
VJ3399
PX4970
PX5013
RK8904
NN8986
NN8829
VJ3459
RK9143
VJ3414
NN9028
SP1557
PX5003
PX5042
VJ3475
ND7330
PX3714
NS8913
ND6512
ND6941
ND9576
NS7555
NS8286
NS7447
ND6488
ND8296
ND6956
ND7879
ND6509
ND9814
NN7331
ND6991
ND6894
NS6413
ND7344
ND6947
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TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
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ND6723
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ND6013
ND8937
NS7160
NS6435
NS6591
ND9558
NS8479
NS9382
ND8965
ND9837
ND5959
NS6491
NS9072
ND9625
ND6714
ND6820
ND8972
NE0286
NE0347
ND8010
ND8956
ND9535
ND9831
NE0227
ND8283
ND9730
NN7656
NS7775
ND9815
ND6135
NS8491
NS6395
NS8584
NN7272
MG7159
NS6592
ND7862
ND6684
NN7744
ND7480
ND7873
ND6827
ND6576
ND9261
NS8686
ND9052
ND6897
ND6565
NN8966
PX3707
NS7031
ND6584
ND9883
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ND7852
ND9662
ND7871
JW0106
ND8305
NS6409
NE0442
ND9095
ND9302
ND9023
ND8009
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Part number
831021–003
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ND8187
NN8999
ND6043
ND7880
NN7175
ND9816
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Federal Register / Vol. 70, No. 247 / Tuesday, December 27, 2005 / Rules and Regulations
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
wwhite on PROD1PC61 with RULES
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VerDate Aug<31>2005
17:10 Dec 23, 2005
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
Serial no.
ND8174
ND6045
NS7562
JW0075
ND6848
ND8531
ND6311
ND8144
ND5798
ND8113
ND9642
ND7436
ND9054
ND9683
ND5991
ND6026
ND6616
ND6530
NE0374
ND6364
ND7718
ND6473
ND6436
ND6887
ND6518
ND6479
NS6330
ND7264
ND8151
ND6562
NS8776
ND6519
ND7659
NS9049
NS6861
ND9571
ND9346
ND6501
NS8505
ND9338
ND9775
ND6485
ND7165
ND9371
ND9537
NS7889
ND7877
ND8670
ND9032
ND8781
ND8604
ND9329
ND9110
ND5997
ND6027
ND9589
ND6575
ND6592
ND6463
NS8583
NS8590
NS8567
NS6795
NS7110
NS6587
NS6404
ND6486
JW0942
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JW4812
ND6555
Jkt 208001
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MG5722
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ND6984
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M0938
M1117
M0307
JW3871
M1125
M1149
JW2681
M0270
M1120
M0205
AE9352
JW3492
ND6148
ND8907
M1235
MG5585
ND8436
MG5696
ND8704
JW2284
JW2313
JW2498
JW2541
JW2560
JW2589
JW2639
JW2760
JW2792
M0579
MG2825
MG5477
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JW1976
JW2653
JW2608
JW2727
JW2764
JW2265
JW2474
JW2396
JW3554
JW2667
MG2302
MG3972
JW3930
ND6749
M1172
JW2104
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Federal Register / Vol. 70, No. 247 / Tuesday, December 27, 2005 / Rules and Regulations
TABLE 1.—AFFECTED 1ST STAGE FAN
BLADES—Continued
Part number
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831021–003
831021–003
831021–003
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831021–003
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BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22358; Directorate
Identifier 2005–NE–20–AD; Amendment 39–
14431; AD 2005–26–10]
RIN 2120–AA64
Airworthiness Directives; Engine
Components Inc. (ECi) Reciprocating
Engine Cylinder Assemblies
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
(1) Check the 1st stage fan blade for a
circled, letter I, on the approved marking area
of the outboard side of the blade platform. If
the blade has this marking, no further action
is required.
(2) Remove 1st stage fan blades without a
circled, letter I, on the approved marking area
of the outboard side of the blade platform, if
installed.
(3) Send 1st stage fan blades to a sourcesubstantiation-approved repair station,
approved by PW, for inspection of the blade
root thickness. You can find information on
inspecting the blade root thickness in Engine
Manual Section 72–31–02, Inspect—01, and
Repair—23.
(g) For 1st stage fan blades that pass the
inspection referenced in paragraph (f) of this
AD:
(1) Vibropeen the letter I and a circle
around that letter, on the approved marking
area of the outboard side of the blade
platform. You can find information on
approved blade marking in the JT9D–7R4
Engine Manual, Section 72–31–02, Typical
Repair—13, Mark Repair Codes.
(2) Return the 1st stage fan blades to
service.
wwhite on PROD1PC61 with RULES
Alternative Methods of Compliance
(h) The Manager, Engine 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.
Related Information
(i) None.
VerDate Aug<31>2005
17:10 Dec 23, 2005
Jkt 208001
Issued in Burlington, Massachusetts, on
December 16, 2005.
Peter A. White,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 05–24448 Filed 12–23–05; 8:45 am]
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for
Lycoming Engines (formerly Textron
Lycoming) models 320, 360, and 540
series, ‘‘Parallel Valve’’ reciprocating
engines, with certain Engine
Components Inc. (ECi) cylinder
assemblies, part number (P/N)
AEL65102 series ‘‘Classic Cast’’,
installed. This AD requires replacing
these ECi cylinder assemblies. This AD
results from reports of about 30 failures
of the subject cylinder assemblies
marketed by ECi. We are issuing this AD
to prevent loss of engine power due to
cracks in the cylinder assemblies and
possible engine failure caused by
separation of a cylinder head.
DATES: This AD becomes effective
January 31, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in Room PL–401 on the
plaza level of the Nassif Building, 400
Seventh Street, SW., Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Peter Hakala, Aerospace Engineer,
Special Certification Office, FAA,
Rotorcraft Directorate, 2601 Meacham
Blvd., Fort Worth, TX 76193; telephone
(817) 222–5145; fax (817) 222–5785.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend 14 CFR part 39 with
a proposed AD. The proposed AD
applies to certain ECi cylinder
assemblies, P/N AEL65102 series, with
casting P/N AEL65099, installed on
Lycoming Engines models 320, 360, and
540 series, parallel valve reciprocating
engines. Parallel valve Lycoming
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
76385
reciprocating engines are identified by
the intake and exhaust valves in a
parallel configuration. We published the
proposed AD in the Federal Register on
September 9, 2005 (70 FR 53586). That
action proposed to require replacing
these ECi cylinder assemblies.
Examining the AD Docket
You may examine the docket that
contains the AD, any comments
received, and any final disposition in
person at the Docket Management
Facility Docket Office between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The Docket
Office (telephone (800) 647–5227) is
located on the plaza level of the
Department of Transportation Nassif
Building at the street address stated in
ADDRESSES. Comments will be available
in the AD docket shortly after the DMS
receives them.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comments received.
Request To Extend the Proposed AD
Comment Period
One commenter, a law office
representing ECi, requests we extend the
proposed AD comment period an
additional 90 days. We do not agree. We
have worked with ECi for the past four
years regarding the safety and
airworthiness issues with the affected
ECi cylinder assemblies. ECi is very
familiar with the problems with these
cylinder assemblies. ECi published
Service Bulletin No. 05–08, dated
September 1, 2005, for the identification
and warranty of the affected cylinder
assemblies. Evidence of ECi’s awareness
of the problem is confirmed by the
extensive correspondence with the FAA
regarding the service difficulties with P/
N AEL65102 ‘‘Classic Cast’’ cylinder
assemblies. For these reasons, and
because of the minimal amount of
comments received (two) on the
proposed AD, we find it unnecessary to
extend the proposed AD comment
period.
Request To Allow Cylinder Assembly
Removal at Normal Operating TimeBetween-Overhaul
One commenter, ECi, requests that we
allow affected cylinder assemblies to be
removed at the normal engine operating
time-between-overhaul. We do not
agree. We have carefully reviewed ECi’s
request. Both ECi and the FAA
participated in the Alloytek
Metallurgical Services, Inc. examination
and analysis. The examination and
E:\FR\FM\27DER1.SGM
27DER1
Agencies
[Federal Register Volume 70, Number 247 (Tuesday, December 27, 2005)]
[Rules and Regulations]
[Pages 76381-76385]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-24448]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-23072; Directorate Identifier 2005-NE-38-AD;
Amendment 39-14430; AD 2005-26-09]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney JT9D-7R4 Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Pratt & Whitney (PW) JT9D-7R4 turbofan engines. This AD requires
inspection of the blade root thickness of 1st stage fan blades
identified by part number (P/N) and serial number (SN) in this AD, by a
repair station approved by PW to perform the inspection. This AD
results from a report that a repair station created their own repair
and performed it on 520 1st stage fan blades, without approval from PW.
We are issuing this AD to prevent 1st stage fan blade fracture and
uncontained engine failure, resulting in possible damage to the
airplane.
DATES: This AD becomes effective January 11, 2006.
We must receive any comments on this AD by February 27, 2006.
ADDRESSES: Use one of the following addresses to comment on this AD:
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-0001.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT: Kevin Donovan, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803-5299; telephone (781)
238-7743, fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: In May 2005, we received a report from
Airfoil Technologies International (ATI), of the United Kingdom, that
their repair station created their own repair and performed it on 520
1st stage fan blades, without approval from PW. The repairs were made
to a critical area of the fan blade root. PW requires source
demonstration by each repair station before they approve the repair
station to perform blade repairs, including the repair that should have
been performed to these 1st stage fan blades, known as Repair-23. This
requirement exists due to PW's concern with proper blending in a
critical area of the blade root. This condition, if not corrected,
could result in 1st stage fan blade fracture and uncontained engine
failure, resulting in possible damage to the airplane.
FAA's Determination and Requirements of this AD
The unsafe condition described previously is likely to exist or
develop on other PW JT9D-7R4 turbofan engines of the same type design.
For that reason, we are issuing this AD to prevent 1st stage fan blade
fracture and uncontained engine failure, resulting in possible damage
to the airplane. This AD requires, before installing the 1st stage fan
blades that are listed by P/N and SN in Table 1 of this AD, or if
already installed, at the next 1st stage fan blade exposure:
Checking the 1st stage fan blade for a circled, letter I,
on the approved marking area of the outboard side of the blade
platform. If the blade has this marking, no further action is required.
Removing 1st stage fan blades without a circled, letter I,
on the approved marking area of the outboard side of the blade platform
if installed; and
Sending 1st stage fan blades to a source-substantiation-
approved repair station, approved by PW, for inspection of the blade
root thickness; and
Returning to service 1st stage fan blades that pass the
inspection, after properly marking the blade.
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 and was not preceded 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. FAA-2005-23072;
Directorate Identifier 2005-NE-38-AD'' in the subject line of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify it.
We will post all comments we receive, without change, to https://
[[Page 76382]]
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of the DMS Web
site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You may review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78) or you may visit
https://dms.dot.gov.
Examining the AD Docket
You may examine the docket that contains the AD, any comments
received, and any final disposition in person at the Docket Management
Facility Docket Office between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The Docket Office (telephone (800)
647-5227) is located on the plaza level of the Department of
Transportation Nassif Building at the street address stated in
ADDRESSES. Comments will be available in the AD docket shortly after
the DMS receives them.
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 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 at the
address listed under ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
0
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 adding the following new airworthiness
directive:
2005-26-09 Pratt & Whitney: Amendment 39-14430. Docket No. FAA-2005-
23072; Directorate Identifier 2005-NE-38-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective January
11, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Pratt & Whitney (PW) JT9D-7R4 turbofan
engines. These engines are installed on, but not limited to, Airbus
A300 and A310, and Boeing 747and 767 airplanes.
Unsafe Condition
(d) This AD results from a report that a repair station created
their own repair and performed it on 520 1st stage fan blades,
without approval from PW. We are issuing this AD to prevent 1st
stage fan blade fracture and uncontained engine failure, resulting
in possible damage to 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.
(f) Before installing the 1st stage fan blades that are listed
by part number and serial number in Table 1 of this AD, or if
already installed, at the next 1st stage fan blade exposure, do the
following:
Table 1.--Affected 1st Stage Fan Blades
------------------------------------------------------------------------
Part number Serial no.
------------------------------------------------------------------------
5001341-022............................. JW2804
5001341-022............................. JW0354
5001341-022............................. ND5746
5001341-022............................. ND5770
5001341-022............................. JW3992
5001341-022............................. ND8615
5001341-022............................. JW0442
5001341-022............................. JW2317
5001341-022............................. ND8631
5001341-022............................. ND8635
5001341-022............................. JW4624
5001341-022............................. NE0394
5001341-022............................. NE0153
5001341-022............................. NN8054
5001341-022............................. JW4693
5001341-022............................. ND7304
5001341-022............................. MG6108
5001341-022............................. MG5862
5001341-022............................. MG5619
5001341-022............................. NE0308
5001341-022............................. NE0200
5001341-022............................. MG6797
5001341-022............................. JW0230
5001341-022............................. ND5652
5001341-022............................. ND5775
5001341-022............................. JW0251
5001341-022............................. ND5719
5001341-022............................. JW0248
5001341-022............................. ND5785
5001341-022............................. ND5676
5001341-022............................. ND5661
5001341-022............................. JW0265
5001341-022............................. ND5699
5001341-022............................. ND5767
5001341-022............................. JW0259
5001341-022............................. ND5680
5001341-022............................. ND5749
5001341-022............................. JW0235
5001341-022............................. ND5776
5001341-022............................. ND8580
5001341-022............................. MG6039
5001341-022............................. ND9127
5001341-022............................. JW4287
5001341-022............................. JW0262
5001341-022............................. JW0445
5001341-022............................. JW4665
5001341-022............................. MG5901
5001341-022............................. NE0303
5001341-022............................. ND8703
5001341-022............................. JW4574
5001341-022............................. JW4286
5001341-022............................. JW4491
5001341-022............................. JW4630
5001341-022............................. JW4391
5001341-022............................. MG6550
5001341-022............................. MG6776
5001341-022............................. JW4586
5001341-022............................. JW0352
5001341-022............................. JW4261
5001341-022............................. MG6135
5001341-022............................. JW4685
5001341-022............................. MG6772
5001341-022............................. MG6793
5001341-022............................. MG7111
5001341-022............................. ND8618
[[Page 76383]]
5001341-022............................. JW0644
5001341-022............................. JW4631
5001341-022............................. JW4651
5001341-022............................. JW0234
5001341-022............................. JW4646
804121.................................. NN9016
804121.................................. VJ3393
804121.................................. PX3694
804121.................................. RK9168
804121.................................. PX5023
804121.................................. VJ3324
804121.................................. VJ3504
804121.................................. NN9115
804121.................................. NN8936
804121.................................. PX3816
804121.................................. VJ3412
804121.................................. RK9163
804121.................................. VJ3447
804121.................................. RK9230
804121.................................. RK9109
804121.................................. PX4627
804121.................................. RK8990
804121.................................. SP9459
804121.................................. RK8656
804121.................................. NN8933
804121.................................. VJ3444
804121.................................. ND5864
804121.................................. NN9020
804121.................................. RK8905
804121.................................. SR1733
804121.................................. NN9047
804121.................................. PX3692
804121.................................. PX3786
804121.................................. NN9025
804121.................................. NN9007
804121.................................. RK9100
804121.................................. VJ3399
804121.................................. PX4970
804121.................................. PX5013
804121.................................. RK8904
804121.................................. NN8986
804121.................................. NN8829
804121.................................. VJ3459
804121.................................. RK9143
804121.................................. VJ3414
804121.................................. NN9028
804121.................................. SP1557
804121.................................. PX5003
804121.................................. PX5042
804121.................................. VJ3475
804121.................................. ND7330
804121.................................. PX3714
831021-003.............................. NS8913
831021-003.............................. ND6512
831021-003.............................. ND6941
831021-003.............................. ND9576
831021-003.............................. NS7555
831021-003.............................. NS8286
831021-003.............................. NS7447
831021-003.............................. ND6488
831021-003.............................. ND8296
831021-003.............................. ND6956
831021-003.............................. ND7879
831021-003.............................. ND6509
831021-003.............................. ND9814
831021-003.............................. NN7331
831021-003.............................. ND6991
831021-003.............................. ND6894
831021-003.............................. NS6413
831021-003.............................. ND7344
831021-003.............................. ND6947
831021-003.............................. NN8732
831021-003.............................. ND8536
831021-003.............................. ND6946
831021-003.............................. ND6723
831021-003.............................. ND9294
831021-003.............................. ND9290
831021-003.............................. ND6013
831021-003.............................. ND8937
831021-003.............................. NS7160
831021-003.............................. NS6435
831021-003.............................. NS6591
831021-003.............................. ND9558
831021-003.............................. NS8479
831021-003.............................. NS9382
831021-003.............................. ND8965
831021-003.............................. ND9837
831021-003.............................. ND5959
831021-003.............................. NS6491
831021-003.............................. NS9072
831021-003.............................. ND9625
831021-003.............................. ND6714
831021-003.............................. ND6820
831021-003.............................. ND8972
831021-003.............................. NE0286
831021-003.............................. NE0347
831021-003.............................. ND8010
831021-003.............................. ND8956
831021-003.............................. ND9535
831021-003.............................. ND9831
831021-003.............................. NE0227
831021-003.............................. ND8283
831021-003.............................. ND9730
831021-003.............................. NN7656
831021-003.............................. NS7775
831021-003.............................. ND9815
831021-003.............................. ND6135
831021-003.............................. NS8491
831021-003.............................. NS6395
831021-003.............................. NS8584
831021-003.............................. NN7272
831021-003.............................. MG7159
831021-003.............................. NS6592
831021-003.............................. ND7862
831021-003.............................. ND6684
831021-003.............................. NN7744
831021-003.............................. ND7480
831021-003.............................. ND7873
831021-003.............................. ND6827
831021-003.............................. ND6576
831021-003.............................. ND9261
831021-003.............................. NS8686
831021-003.............................. ND9052
831021-003.............................. ND6897
831021-003.............................. ND6565
831021-003.............................. NN8966
831021-003.............................. PX3707
831021-003.............................. NS7031
831021-003.............................. ND6584
831021-003.............................. ND9883
831021-003.............................. NS6535
831021-003.............................. ND7852
831021-003.............................. ND9662
831021-003.............................. ND7871
831021-003.............................. JW0106
831021-003.............................. ND8305
831021-003.............................. NS6409
831021-003.............................. NE0442
831021-003.............................. ND9095
831021-003.............................. ND9302
831021-003.............................. ND9023
831021-003.............................. ND8009
831021-003.............................. ND8477
831021-003.............................. ND7492
831021-003.............................. ND8776
831021-003.............................. ND6524
831021-003.............................. ND6704
831021-003.............................. ND8911
831021-003.............................. ND8789
831021-003.............................. ND8798
831021-003.............................. ND6407
831021-003.............................. ND7668
831021-003.............................. ND9179
831021-003.............................. NE0421
831021-003.............................. ND6513
831021-003.............................. ND6744
831021-003.............................. ND7654
831021-003.............................. ND7870
831021-003.............................. ND9759
831021-003.............................. ND6561
831021-003.............................. ND5826
831021-003.............................. ND6031
831021-003.............................. ND8714
831021-003.............................. ND8872
831021-003.............................. ND6678
831021-003.............................. ND6629
831021-003.............................. ND8995
831021-003.............................. NE0302
831021-003.............................. ND6405
831021-003.............................. NS8300
831021-003.............................. NS8769
831021-003.............................. NS7147
831021-003.............................. ND6649
831021-003.............................. ND7766
831021-003.............................. NS7864
831021-003.............................. NS8734
831021-003.............................. ND6677
831021-003.............................. NS7911
831021-003.............................. ND8205
831021-003.............................. ND8804
831021-003.............................. ND6639
831021-003.............................. ND8994
831021-003.............................. ND7275
831021-003.............................. ND9195
831021-003.............................. ND6178
831021-003.............................. ND8639
831021-003.............................. ND9760
831021-003.............................. ND9108X
831021-003.............................. ND6427
831021-003.............................. ND6590
831021-003.............................. NS6551
831021-003.............................. JW1158
831021-003.............................. ND6412
831021-003.............................. ND7922
831021-003.............................. NS8678
831021-003.............................. ND8930
831021-003.............................. ND6596
831021-003.............................. ND9570
831021-003.............................. NN9027
831021-003.............................. ND6446
831021-003.............................. NE0275
831021-003.............................. ND9917
831021-003.............................. NS7919
831021-003.............................. NS7907
831021-003.............................. ND6583
831021-003.............................. NN7420
831021-003.............................. ND7746
831021-003.............................. ND8187
831021-003.............................. NN8999
831021-003.............................. ND6043
831021-003.............................. ND7880
831021-003.............................. NN7175
831021-003.............................. ND9816
[[Page 76384]]
831021-003.............................. ND8174
831021-003.............................. ND6045
831021-003.............................. NS7562
831021-003.............................. JW0075
831021-003.............................. ND6848
831021-003.............................. ND8531
831021-003.............................. ND6311
831021-003.............................. ND8144
831021-003.............................. ND5798
831021-003.............................. ND8113
831021-003.............................. ND9642
831021-003.............................. ND7436
831021-003.............................. ND9054
831021-003.............................. ND9683
831021-003.............................. ND5991
831021-003.............................. ND6026
831021-003.............................. ND6616
831021-003.............................. ND6530
831021-003.............................. NE0374
831021-003.............................. ND6364
831021-003.............................. ND7718
831021-003.............................. ND6473
831021-003.............................. ND6436
831021-003.............................. ND6887
831021-003.............................. ND6518
831021-003.............................. ND6479
831021-003.............................. NS6330
831021-003.............................. ND7264
831021-003.............................. ND8151
831021-003.............................. ND6562
831021-003.............................. NS8776
831021-003.............................. ND6519
831021-003.............................. ND7659
831021-003.............................. NS9049
831021-003.............................. NS6861
831021-003.............................. ND9571
831021-003.............................. ND9346
831021-003.............................. ND6501
831021-003.............................. NS8505
831021-003.............................. ND9338
831021-003.............................. ND9775
831021-003.............................. ND6485
831021-003.............................. ND7165
831021-003.............................. ND9371
831021-003.............................. ND9537
831021-003.............................. NS7889
831021-003.............................. ND7877
831021-003.............................. ND8670
831021-003.............................. ND9032
831021-003.............................. ND8781
831021-003.............................. ND8604
831021-003.............................. ND9329
831021-003.............................. ND9110
831021-003.............................. ND5997
831021-003.............................. ND6027
831021-003.............................. ND9589
831021-003.............................. ND6575
831021-003.............................. ND6592
831021-003.............................. ND6463
831021-003.............................. NS8583
831021-003.............................. NS8590
831021-003.............................. NS8567
831021-003.............................. NS6795
831021-003.............................. NS7110
831021-003.............................. NS6587
831021-003.............................. NS6404
831021-003.............................. ND6486
5001341-022............................. JW0942
5001341-022............................. ND9231
5001341-022............................. JW4812
5001341-022............................. ND6555
5001341-022............................. M1375
5001341-022............................. MG6627
5001341-022............................. MG6794
5001341-022............................. ND9399
5001341-022............................. NE0084
5001341-022............................. MG6252
5001341-022............................. ND7422
5001341-022............................. ND7043
5001341-022............................. MG5722
5001341-022............................. MG5918
5001341-022............................. ND6984
5001341-022............................. M0839
5001341-022............................. M0922
5001341-022............................. M0938
5001341-022............................. M1117
5001341-022............................. M0307
5001341-022............................. JW3871
5001341-022............................. M1125
5001341-022............................. M1149
5001341-022............................. JW2681
5001341-022............................. M0270
5001341-022............................. M1120
5001341-022............................. M0205
5001341-022............................. AE9352
5001341-022............................. JW3492
5001341-022............................. ND6148
5001341-022............................. ND8907
5001341-022............................. M1235
5001341-022............................. MG5585
5001341-022............................. ND8436
5001341-022............................. MG5696
5001341-022............................. ND8704
5001341-022............................. JW2284
5001341-023............................. JW2313
5001341-024............................. JW2498
5001341-025............................. JW2541
5001341-026............................. JW2560
5001341-027............................. JW2589
5001341-028............................. JW2639
5001341-029............................. JW2760
5001341-030............................. JW2792
5001341-031............................. M0579
5001341-032............................. MG2825
5001341-033............................. MG5477
5001341-034............................. ND5917
5001341-022............................. JW1976
5001341-022............................. JW2653
5001341-022............................. JW2608
5001341-022............................. JW2727
5001341-022............................. JW2764
5001341-022............................. JW2265
5001341-022............................. JW2474
5001341-022............................. JW2396
5001341-022............................. JW3554
5001341-022............................. JW2667
5001341-022............................. MG2302
5001341-022............................. MG3972
5001341-022............................. JW3930
5001341-022............................. ND6749
5001341-022............................. M1172
5001341-022............................. JW2104
5001341-022............................. JW2519
5001341-022............................. JW2640
5001341-022............................. JW2517
5001341-022............................. JW2663
5001341-022............................. JW2823
5001341-022............................. M0536
5001341-022............................. JW2725
5001341-022............................. MG5917
5001341-022............................. JW0681
5001341-022............................. JW0711
5001341-022............................. JW0740
5001341-022............................. JW0807
5001341-022............................. JW1089
5001341-022............................. JW1362
5001341-022............................. JW2065
5001341-022............................. MG2434
5001341-022............................. MG2846
5001341-022............................. JW0806
804121.................................. NN9854
804121.................................. NN9024
804121.................................. NN9032
804121.................................. PX5029
804121.................................. NN9050
804121.................................. NS8242
804121.................................. NS8260
804121.................................. PX4273
804121.................................. PX4378
804121.................................. RL0857
804121.................................. RX8763
804121.................................. NS8331
804121.................................. NN9824
804121.................................. MG6979
804121.................................. MG7023
804121.................................. MG7055
804121.................................. RK8914
804121.................................. RL0023
804121.................................. PX4328
804121.................................. RK9008
804121.................................. TG1506
804121.................................. KK8226
804121.................................. MG2604
804121.................................. NS6691
804121.................................. RK8968
804121.................................. NN9917
804121.................................. RK7824
804121.................................. M1343
804121.................................. NS6559
804121.................................. NS7767
804121.................................. NE0363
804121.................................. PX3771
804121.................................. NN9972
804121.................................. RL0460
804121.................................. RK8310
804121.................................. SR2115
804121.................................. TG2826
804121.................................. PX5018
804121.................................. PX5002
831021-003.............................. ND7627
831021-003.............................. ND6890
831021-003.............................. ND7461
831021-003.............................. ND9616
831021-003.............................. NE0413
831021-003.............................. NS8825
831021-003.............................. NS6350
831021-003.............................. NS7168
831021-003.............................. NS7705
831021-003.............................. NS7848
831021-003.............................. ND9128
831021-003.............................. ND9541
831021-003.............................. ND9671
831021-003.............................. ND9684
831021-003.............................. NE0277
831021-003.............................. NE0384
831021-003.............................. NE0396
831021-003.............................. ND6421
831021-003.............................. ND6599
831021-003.............................. ND6614
831021-003.............................. ND7847
831021-003.............................. ND8346
831021-003.............................. ND8853
831021-003.............................. ND8915
[[Page 76385]]
831021-003.............................. NS8719
831021-003.............................. NS8838
831021-003.............................. NT0169
831021-003.............................. NS9584
831021-003.............................. ND6445
831021-003.............................. ND6834
831021-003.............................. ND7467
831021-003.............................. ND8887
831021-003.............................. ND6520
831021-003.............................. NS8611
831021-003.............................. NS7640
831021-003.............................. NN7037
831021-003.............................. NN7590
831021-003.............................. NN8120
831021-003.............................. NN8573
831021-003.............................. NN9719
831021-003.............................. NS8784
831021-003.............................. TB6B367
831021-003.............................. NN9557
831021-003.............................. NN9710
831021-003.............................. NS8374
831021-003.............................. NS8770
831021-003.............................. NS9022
831021-003.............................. NS8416
831021-003.............................. NS6474
831021-003.............................. ND8912
831021-003.............................. NT0108
831021-003.............................. NS8836
831021-003.............................. NN8310
------------------------------------------------------------------------
(1) Check the 1st stage fan blade for a circled, letter I, on
the approved marking area of the outboard side of the blade
platform. If the blade has this marking, no further action is
required.
(2) Remove 1st stage fan blades without a circled, letter I, on
the approved marking area of the outboard side of the blade
platform, if installed.
(3) Send 1st stage fan blades to a source-substantiation-
approved repair station, approved by PW, for inspection of the blade
root thickness. You can find information on inspecting the blade
root thickness in Engine Manual Section 72-31-02, Inspect--01, and
Repair--23.
(g) For 1st stage fan blades that pass the inspection referenced
in paragraph (f) of this AD:
(1) Vibropeen the letter I and a circle around that letter, on
the approved marking area of the outboard side of the blade
platform. You can find information on approved blade marking in the
JT9D-7R4 Engine Manual, Section 72-31-02, Typical Repair--13, Mark
Repair Codes.
(2) Return the 1st stage fan blades to service.
Alternative Methods of Compliance
(h) The Manager, Engine 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.
Related Information
(i) None.
Issued in Burlington, Massachusetts, on December 16, 2005.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 05-24448 Filed 12-23-05; 8:45 am]
BILLING CODE 4910-13-P