Airworthiness Directives; Boeing Model 747, 757, 767 and 777 Series Airplanes, 49174-49178 [05-16455]
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49174
Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
further flight, contact the Manager,
International Branch, ANM–116, for further
actions, or the LFV (or its delegated agent).
If any scratches or other damage is detected
on the skin surface or the surface of the front
spar, before further flight, repair in
accordance with a method approved by the
Manager, International Branch, ANM–116, or
the LFV (or its delegated agent).
Actions Accomplished Previously
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
I
2005–17–10 SAAB Aircraft AB:
Amendment 39–14231. Docket No.
FAA–2005–21341; Directorate Identifier
2003–NM–026–AD.
Effective Date
(a) This AD becomes effective September
27, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to certain Saab Model
SAAB 2000 airplanes having serial numbers
004 through 063 inclusive, certificated in any
category.
Unsafe Condition
(d) This AD was prompted by a report of
cracking of certain fastener holes in the lower
spar cap of the rear spar and in the lower
skin at the front spar. We are issuing this AD
to prevent cracking of the front and rear
spars, which could result in fuel leakage and
consequent reduced structural integrity of the
wing structure.
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.
Inspection
(f) Prior to the accumulation of 20,000 total
flight cycles, perform non-destructive tests
for cracking of the fastener holes in the lower
spar cap of the rear spar and in the lower
skin at the left-hand and right-hand sides of
the front spar, between WS20 and WS83
inclusive; by accomplishing all the actions
specified in Parts A, B, and C of the
Accomplishment Instructions of Saab Service
Bulletin 2000–57–038, Revision 01, dated
June 24, 2004. If any cracking is detected,
before further flight, repair the cracking
according to a method approved by the
Manager, International Branch, ANM–116,
Transport Airplane Directorate, FAA; or the
Luftfartsverket (LFV) (or its delegated agent).
16:13 Aug 22, 2005
Jkt 205001
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2004–19865; Directorate
Identifier 2003–NM–242–AD; Amendment
39–14230; AD 2005–17–09]
RIN 2120–AA64
(h) Inspections or modifications
accomplished before the effective date of this
AD in accordance with the Accomplishment
Instructions of Saab Service Bulletin 2000–
57–038, dated December 18, 2002, are
considered acceptable for compliance with
the corresponding actions specified in this
AD.
Airworthiness Directives; Boeing
Model 747, 757, 767 and 777 Series
Airplanes
Alternative Methods of Compliance
(AMOCs)
SUMMARY: The FAA is superseding an
existing airworthiness directive (AD),
which applies to certain Boeing Model
747, 757, 767, and 777 series airplanes.
That AD currently requires modifying
certain drip shields located on the flight
deck, and follow-on actions. This new
AD removes certain airplanes that are
included in the applicability statement
of the existing AD, and requires
modifying additional drip shields on the
flight deck of certain other airplanes.
This AD is prompted by a determination
that certain airplanes have drip shields
that are not adequately resistant to fire.
We are issuing this AD to prevent
potential ignition of the moisture barrier
cover of the drip shield, which could
propagate a small fire that results from
an electrical arc, leading to a larger fire.
DATES: This AD becomes effective
September 27, 2005.
The incorporation by reference of
certain publications listed in the AD is
approved by the Director of the Federal
Register as of September 27, 2005.
On February 2, 2001 (65 FR 82901,
December 29, 2000), the Director of the
Federal Register approved the
incorporation by reference of certain
other publications listed in the AD.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, P.O. Box 3707,
Seattle, Washington 98124–2207.
Docket: The AD docket contains the
proposed AD, comments, and any final
disposition. You can examine the AD
docket on the Internet at https://
dms.dot.gov, or in person at the Docket
Management Facility office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the U.S. Department of Transportation,
400 Seventh Street SW, room PL–401,
Washington, DC. This docket number is
(i) The Manager, International Branch,
ANM–116, has the authority to approve
AMOCs for this AD, if requested in
accordance with the procedures found in 14
CFR 39.19.
Material Incorporated by Reference
(j) You must use Saab Service Bulletin
2000–57–038, Revision 01, dated June 24,
2004, to perform the actions that are required
by this AD, unless the AD specifies
otherwise. The Director of the Federal
Register approves the incorporation by
reference of this document in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51. To
get copies of the service information, contact
Saab Aircraft AB, SAAB Aircraft Product
¨
Support, S–581.88, Linkoping, Sweden. To
view the AD docket, go to the Docket
Management Facility, U.S. Department of
Transportation, 400 Seventh Street SW.,
room PL–401, Nassif Building, Washington,
DC. To review copies of the service
information, go to 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/federalregister/cfr/ibr-locations.html.
Issued in Renton, Washington, on August
11, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–16456 Filed 8–22–05; 8:45 am]
BILLING CODE 4910–13–P
Modification
(g) Prior to the accumulation of 20,000 total
flight cycles, modify the fastener holes of the
front and rear spars and the rear spar web,
including related investigative actions, by
accomplishing all the actions specified in
Part D of the Accomplishment Instructions of
Saab Service Bulletin 2000–57–038, Revision
01, dated June 24, 2004. If 1⁄4-inch fasteners
are needed for holes No. 7 and No. 8, before
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DEPARTMENT OF TRANSPORTATION
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Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
FAA–2004–19865; the directorate
identifier for this docket is 2003–NM–
242–AD.
FOR FURTHER INFORMATION CONTACT:
Patrick Gillespie, Aerospace Engineer,
Cabin Safety and Environmental
Systems Branch, ANM–150S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 917–6429; fax (425) 917–6590.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR
part 39) with an AD to supersede AD
2000–26–04, amendment 39–12054 (65
FR 82901, December 29, 2000). The
existing AD applies to certain Boeing
Model 747, 757, 767, and 777 series
airplanes. The proposed AD was
published in the Federal Register on
December 16, 2004 (69 FR 75267), to
require modifying certain drip shields
located on the flight deck, and followon actions.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comments that have
been submitted on the proposed AD.
Support for the Proposed AD
One commenter concurs with the
contents of the proposed AD and has no
additional comments.
Request To Revise Applicability
Statement
One commenter, the airplane
manufacturer, requests that we revise
Table 1 under Applicability in the
proposed AD to remove the Model 777
series airplane having line number (L/N)
254. The commenter states that the
affected Model 777 L/Ns include line
numbers prior to 254, except L/Ns 1,
120, 219, 230, 235, 242, 245, and 249.
We agree and have revised Table 1 of
this AD to remove L/N 254.
Request To Add Later Service Bulletin
Revision
One commenter requests that we
revise paragraph (f) of the proposed AD
to refer to Boeing Service Bulletin 757–
25–0228, Revision 1, dated March 28,
2002 (for Model 757–300 series
airplanes); and Boeing Service Bulletin
777–25–0164, Revision 1, including
Appendices A, B, C, and D, all dated
March 22, 2001; as acceptable methods
of compliance with that paragraph. The
commenter notes that the procedures in
Revision 1 of these service bulletins are
substantially similar to those in the
original issues of the service bulletin,
which paragraph (f) refers to as
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16:13 Aug 22, 2005
Jkt 205001
acceptable sources of service
information for Model 757–300 and
Model 777 series airplanes. Boeing
Service Bulletin 757–25–0228, Revision
1, clarifies certain procedures and
corrects a part number for a washer used
to attach fire blocks. Boeing Service
Bulletin 777–25–0164, Revision 1,
provides additional installation
instructions and placard and
dimensional information. The
commenter also notes that the effectivity
listing is the same in Revision 1 of the
service bulletins as in the original
issues.
We agree. We note that Revision 1 of
these service bulletins was approved as
an alternative method of compliance
(AMOC) for AD 2000–26–04, and that
AMOC remains valid as specified in
paragraph (k)(2) of this AD. However,
for clarification and for the convenience
of affected operators, we have also
revised paragraph (f) of this AD to
specify both the original issue and
Revision 1 of these service bulletins as
acceptable methods of compliance for
doing the modification required by that
paragraph.
Request To Clarify Requirements for
Certain Model 757 Series Airplanes
One commenter requests that we
revise the proposed AD to allow the
proposed actions to be accomplished in
accordance with previous revisions of
Boeing Service Bulletin 757–25–0226
for Boeing Model 757 series airplanes
identified in Groups 2 and 4 of Boeing
Service Bulletin 757–25–0226, Revision
3, dated September 2, 2004. The
commenter states that, for airplanes in
those groups, Boeing Service Bulletins
757–25–0226, Revision 2, dated October
31, 2002, and Revision 3, do not add
additional work beyond what is
specified for those airplanes in the
original issue, dated July 3, 2000, and
Revision 1, dated February 15, 2001.
The commenter states that we should
make it clear that no additional work is
required by this AD for any airplane in
Group 2 or 4 that was modified in
accordance with a previous issue of the
service bulletin. The commenter adds
that the proposed AD should also be
revised to give credit for using any
revision of Boeing Service Bulletin 757–
25–0226 to modify any airplane in
Group 2 or 4. The commenter also notes
that an AMOC was issued for AD 2000–
26–04 to allow certain required actions
to be accomplished in accordance with
Boeing Service Bulletin 757–25–0226,
Revision 1. The commenter states that
this AMOC should also still be valid for
airplanes in Groups 2 and 4.
We agree with the commenter’s
requests for the reasons stated by the
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49175
commenter, and accordingly have made
the following changes to this AD:
• We revised paragraph (i) of this AD
to specify that paragraph (i) applies only
to airplanes identified as being in Group
1 or 3 by Boeing Service Bulletin 757–
25–0226, Revision 3.
• We revised paragraph (f) to state
that only airplanes in Group 1 or 3 are
required to use Revision 3 after the
effective date of this AD.
• We added a new paragraph (j)(2) to
this AD (and renumbered a subsequent
paragraph) to give credit for modifying
the drip shields on airplanes in Groups
2 and 4 before the effective date of this
AD in accordance with Revision 1 of
Boeing Service Bulletin 757–25–0226.
(Paragraph (j)(1) of this AD already gives
credit for modifying the drip shields in
accordance with Revision 2 of that
service bulletin.)
• We revised paragraph (k)(2) of this
AD to state that, except for Model 757–
200, –200CB, and –200PF series
airplanes listed in Groups 1 and 3 of
Boeing Service Bulletin 757–25–0226,
Revision 3, dated September 2, 2004,
AMOCs approved previously in
accordance with AD 2000–26–04,
amendment 39–12054, are acceptable
for compliance with this AD.
• We revised the Costs of Compliance
section to reduce the estimated number
of Model 757–200, –200CB, and –200PF
series airplanes subject to the new
requirements from 491 U.S.-registered
airplanes to 350. This figure includes
only the airplanes in Groups 1 and 3.
Request To Revise Estimated Number of
Airplanes No Longer Affected
One commenter, the airplane
manufacturer, states that the estimate of
Model 747 series airplanes no longer
affected, as stated in the Actions Since
Existing AD Was Issued section of the
proposed AD, should be increased from
550 to 650 airplanes. The commenter
points out that the effectivity listing of
the original issue of Boeing Service
Bulletin 747–25–3253, dated June 29,
2000, included L/Ns 1 through 1234
inclusive, except 1174 and 1216
(approximately 1230 airplanes).
However, the effectivity listing of
Boeing Service Bulletin 747–25–3253,
Revision 3, dated September 4, 2003,
includes L/Ns 1 through 299 inclusive
and 951 through 1234 inclusive, except
292, 296, 297, 1174, and 1216
(approximately 580 airplanes).
Therefore, approximately 650 airplanes
are no longer affected.
We agree with the intent of the
commenter’s request. However, the
relevant paragraph to which the
commenter refers is not restated in this
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49176
Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
final rule. Thus, we have made no
change in this regard.
Request To Increase Estimate for Costs
of Compliance
One commenter requests that we
increase the number of work hours
necessary to accomplish the required
actions on affected Model 757 series
airplanes. The commenter notes that the
proposed AD estimates that 26 work
hours would be needed, while the
referenced service bulletin for Model
757 series airplanes states total workhour estimates of 107, 94.5, 74, and 66
work hours for airplanes in Groups 1, 2,
3, and 4, respectively. The commenter
states that its experience indicates that
the figures provided by Boeing in the
service bulletin are accurate, but the
FAA’s estimate times are lower than the
service bulletin figures and, as a result,
contribute to an erroneously low cost
estimate.
We partially agree with the
commenter’s request. We note that the
total work hour estimates to which the
commenter refers include time for
gaining access and closing up. The cost
analysis in AD actions, however,
typically does not include costs such as
the time required to gain access and
close up, time necessary for planning, or
time necessitated by other
administrative actions. Costs for those
type of actions may vary significantly
among operators and are almost
impossible to calculate.
However, we do agree that the costs
of compliance estimated in the
proposed AD for Model 757 series
airplanes did not include the work
hours necessary for testing, as specified
in Boeing Service Bulletin 757–25–
0226, Revision 3. Therefore, we have
revised the estimated costs of
compliance in this AD to estimate that
58 work hours are needed to do the
required actions on each affected Model
757 series airplane.
Conclusion
We have carefully reviewed the
available data, including the comments
that have been submitted, and
determined that air safety and the
public interest require adopting the AD
with the changes described previously.
We have determined that these changes
will neither increase the economic
burden on any operator nor increase the
scope of the AD.
Costs of Compliance
There are about 2,222 airplanes of
affected design in the worldwide fleet.
The following table provides the
estimated costs for U.S. operators to
comply with the actions that are
required by AD 2000–26–04 and
retained in this proposed AD. The
average labor rate is $65 per work hour.
ESTIMATED COSTS
U.S.registered
airplanes
Model
747
757
767
777
.................................................................................
.................................................................................
.................................................................................
.................................................................................
For Model 747 series airplanes listed
in Group 1 in Boeing Service Bulletin
747–25–3253, Revision 3, in lieu of
doing the modification of the drip
shields, this proposed AD provides an
option to take samples of the drip
shields to determine if the modification
is necessary. Therefore, the estimated
costs above may be reduced if some
airplanes do not need the modification.
It would take approximately 18 work
hours to do the sampling, at an average
labor rate of $65 per work hour. Based
on these figures, the cost impact of the
sampling is estimated to be $1,170 per
sampled airplane.
As many as 350 U.S.-registered Model
757–200, –200CB, and –200PF series
airplanes may be subject to the new
proposed actions. These new actions
would take about 8 additional work
hours per airplane, at an average labor
rate of $65 per work hour. Required
parts would cost an additional $160 per
airplane (for a total parts cost of $1,860
per airplane). Based on these figures, the
estimated cost of the new actions
specified in this proposed AD for U.S.
operators of affected airplanes is up to
an additional $238,000, or $680 per
airplane.
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16:13 Aug 22, 2005
Jkt 205001
Work
hours
(estimated)
105
491
140
56
Labor cost
(estimated)
39
58
17
3
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,
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$2,535
3,770
1,105
195
Parts cost
(estimated)
Maximum fleet
cost
(estimated)
$2,300 to 3,500
1,700
2,300
1,700
$633,675
2,685,770
476,700
106,120
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
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 regulatory evaluation
of the estimated costs to comply with
this AD. See the ADDRESSES section for
a location to examine the regulatory
evaluation.
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 FAA amends 14 CFR part 39 as
follows:
I
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Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
82901, December 29, 2000), and by
adding the following new airworthiness
directive (AD):
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.
§ 39.13
[Amended]
Affected ADs
2005–17–09 Boeing: Amendment 39–14230.
Docket No. FAA–2004–19865;
Directorate Identifier 2003–NM–242–AD.
Applicability
Effective Date
2. The FAA amends § 39.13 by
removing amendment 39–12054 (65 FR
I
49177
(a) This AD becomes effective September
27, 2005.
(b) This AD supersedes AD 2000–26–04,
amendment 39–12054.
(c) This AD applies to Model 747, 757, 767,
and 777 series airplanes having the line
numbers (L/Ns) listed in Table 1 of this AD;
certificated in any category.
TABLE 1.—APPLICABILITY
Model
747
757
767
777
Affected L/Ns
....................
....................
....................
....................
1 through 299 inclusive and 951 through 1234 inclusive .........................................
2 through 895 inclusive .............................................................................................
470 through 768 inclusive .........................................................................................
2 through 253 inclusive .............................................................................................
Unsafe Condition
(d) This AD was prompted by a
determination that certain airplanes have
drip shields that are not adequately resistant
to fire. We are issuing this AD to prevent
potential ignition of the moisture barrier
cover of the drip shield, which could
propagate a small fire that results from an
electrical arc, leading to a larger 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.
Requirements of AD 2000–26–04
Modification
(f) Within 6 years after February 2, 2001
(the effective date of AD 2000–26–04),
accomplish paragraphs (f)(1), (f)(2), and (f)(3)
of this AD; in accordance with Boeing
Service Bulletin 747–25–3253, dated June 29,
2000, or Revision 3, dated September 4, 2003;
757–25–0226, dated July 3, 2000, or Revision
3, dated September 2, 2004; 757–25–0228,
dated July 3, 2000, or Revision 1, dated
March 28, 2002; 767–25–0290, dated June 29,
2000, or Revision 4, dated October 28, 2004;
or 777–25–0164, dated June 29, 2000, or
Revision 1, including Appendices A, B, C,
and D, all dated March 22, 2001; as
applicable; except as provided by paragraph
(g) of this AD. For Model 757–200, –200CB,
and –200PF series airplanes identified as
being in Groups 1 and 3 in Boeing Service
Bulletin 757–25–0226, Revision 3: As of the
effective date of this AD, only Revision 3 of
the service bulletin may be used. For Model
747 and 767 series airplanes: As of the
effective date of this AD, only Boeing Service
Bulletin 747–25–3253, Revision 3, or 767–
25–0290, Revision 4, as applicable, may be
used.
(1) Modify drip shields located on the
flight deck by installing fire blocks.
(2) Prior to further flight following
accomplishment of paragraph (f)(1) of this
AD, perform a functional test of any system
disturbed by the modification, in accordance
with the applicable service bulletin or
airplane maintenance manual (AMM), as
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16:13 Aug 22, 2005
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applicable. If any functional test fails, prior
to further flight, isolate the fault, correct the
discrepancy in accordance with the
applicable AMM, and repeat the failed test
until it is successfully accomplished.
(3) Prior to further flight following the
accomplishment of paragraphs (f)(1) and
(f)(2) of this AD, install placards on all
modified drip shields.
(g) If any wires or equipment are installed
on the outboard surface of the drip shield
(that is, between the drip shield and the
airplane structure), modify that area in
accordance with a method approved by the
Manager, Seattle Aircraft Certification Office
(ACO), FAA.
Optional Sampling (Certain Model 747 Series
Airplanes)
(h) For Model 747 series airplanes listed in
Group 1 in Boeing Service Bulletin 747–25–
3253, Revision 3, dated September 4, 2003:
In lieu of accomplishing paragraph (f) of this
AD, within 6 years after February 2, 2001,
collect samples of the insulation and
adhesive of the drip shields, and submit the
samples to the manufacturer for testing, in
accordance with the Accomplishment
Instructions of Boeing Service Bulletin 747–
25–3253, dated June 29, 2000, or Revision 3,
dated September 4, 2003. After the effective
date of this AD, only Revision 3 may be used.
(1) If the test on all samples is positive, no
further action is required by this AD.
(2) If the test on any sample is negative,
accomplish paragraph (f) of this AD before
the compliance time specified in that
paragraph.
New Requirements of This AD
Model 757–200/–200CB/–200PF Series
Airplanes Previously Modified
(i) For Model 757–200, –200CB, and
–200PF series airplanes identified as being in
Group 1 or 3 in Boeing Service Bulletin 757–
25–0226, Revision 3, dated September 2,
2004, and that were modified before the
effective date of this AD in accordance with
Boeing Service Bulletin 757–25–0226, dated
July 3, 2000: Within 72 months after the
effective date of this AD, modify drip shields
located above windows number 2 and 3 on
the flight deck by installing fire blocks, in
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292, 296, 297, 1174, 1216.
870, 886, 894.
758.
120, 219, 230, 235, 242, 245, 249.
accordance with the Accomplishment
Instructions of Boeing Service Bulletin 757–
25–0226, Revision 3, dated September 2,
2004; except as provided by paragraph (g) of
this AD. After the modification, do the
actions required by paragraphs (f)(2) and
(f)(3) of this AD because these actions apply
to the drip shields modified in accordance
with this paragraph.
Previously Accomplished Actions
(j) Modifying the drip shields before the
effective date of this AD in accordance with
the applicable service bulletin specified in
paragraph (j)(1), (j)(2), or (j)(3) of this AD is
acceptable for compliance with the
corresponding requirements of paragraphs (f)
and (i) of this AD, as applicable.
(1) For Model 757–200, –200CB, and
–200PF series airplanes: Boeing Service
Bulletin 757–25–0226, Revision 2, dated
October 31, 2002.
(2) For Model 757–200, –200CB, and
–200PF series airplanes identified in Groups
2 and 4 of Boeing Service Bulletin 757–25–
0226, Revision 3, dated September 2, 2004:
Boeing Service Bulletin 757–25–0226,
Revision 1, dated February 15, 2001.
(3) For Model 767 series airplanes: Boeing
Service Bulletin 767–25–0290, Revision 3,
dated June 26, 2003.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Seattle ACO, FAA, has
the authority to approve AMOCs for this AD,
if requested using the procedures found in 14
CFR 39.19.
(2) Except for Model 757–200, –200CB, and
–200PF series airplanes listed in Groups 1
and 3 of Boeing Service Bulletin 757–25–
0226, Revision 3, dated September 2, 2004:
Alternative methods of compliance,
approved previously in accordance with AD
2000–26–04, amendment 39–12054, are
approved as alternative methods of
compliance with this AD.
Material Incorporated by Reference
(l) You must use the applicable documents
listed in Table 2 of this AD to perform the
actions that are required by this AD, unless
the AD specifies otherwise.
E:\FR\FM\23AUR1.SGM
23AUR1
49178
Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
TABLE 2.—MATERIAL INCORPORATED BY REFERENCE
Boeing service bulletin
Revision level
Date
747–25–3253, including Appendices A, B, and C .......................................................................................
747–25–3253 ................................................................................................................................................
757–25–0226, including Appendices A, B, and C .......................................................................................
757–25–0226 ................................................................................................................................................
757–25–0228, including Appendices A, B, and C .......................................................................................
757–25–0228 ................................................................................................................................................
767–25–0290, including Appendices A, B, and C .......................................................................................
767–25–0290 ................................................................................................................................................
777–25–0164, including Appendices A, B, and C .......................................................................................
777–25–0164, including Appendices A, B, C, and D ..................................................................................
Original .............
3 .......................
Original .............
3 .......................
Original .............
1 .......................
Original .............
4 .......................
Original .............
1 .......................
June 29, 2000.
September 4, 2003.
July 3, 2000.
September 2, 2004.
July 3, 2000.
March 28, 2002.
June 29, 2000.
October 28, 2004.
June 29, 2000.
March 22, 2001.
(1) The Director of the Federal Register
approves the incorporation by reference of
the documents listed in Table 3 of this AD
in accordance with 5 U.S.C. 552(a) and 1 CFR
part 51.
TABLE 3.—NEW MATERIAL INCORPORATED BY REFERENCE
Boeing service bulletin
Revision level
747–25–3253 ................................................................................................................................................
757–25–0226 ................................................................................................................................................
757–25–0228 ................................................................................................................................................
767–25–0290 ................................................................................................................................................
777–25–0164, including Appendices A, B, C, and D ..................................................................................
(2) On February 2, 2001 (65 FR 82901,
December 29, 2000), the Director of the
Federal Register approved the incorporation
3
3
1
4
1
.......................
.......................
.......................
.......................
.......................
Date
September 4, 2003.
September 2, 2004.
March 28, 2002.
October 28, 2004.
March 22, 2001.
by reference of the documents listed in Table
4 of this AD.
TABLE 4.—MATERIAL PREVIOUSLY INCORPORATED BY REFERENCE
Boeing service bulletin
747–25–3253,
757–25–0226,
757–25–0228,
767–25–0290,
777–25–0164,
including
including
including
including
including
Appendices
Appendices
Appendices
Appendices
Appendices
A,
A,
A,
A,
A,
B,
B,
B,
B,
B,
and
and
and
and
and
C
C
C
C
C
Revision level
.......................................................................................
.......................................................................................
.......................................................................................
.......................................................................................
.......................................................................................
(3) To get copies of the service information,
contact Boeing Commercial Airplanes, P.O.
Box 3707, Seattle, Washington 98124–2207.
To view the AD docket, go to the Docket
Management Facility, U.S. Department of
Transportation, 400 Seventh Street SW.,
room PL–401, Nassif Building, Washington,
DC. To review copies of the service
information, go to 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/federalregister/cfr/ibr-locations.html.
DEPARTMENT OF TRANSPORTATION
Issued in Renton, Washington, on August
11, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–16455 Filed 8–22–05; 8:45 am]
AGENCY:
BILLING CODE 4910–13–P
VerDate jul<14>2003
16:13 Aug 22, 2005
Jkt 205001
Original
Original
Original
Original
Original
.............
.............
.............
.............
.............
Date
June 29, 2000.
July 3, 2000.
July 3, 2000.
June 29, 2000.
June 29, 2000.
[Docket No. FAA–2004–19144; Directorate
Identifier 2003–NE–18–AD; Amendment 39–
14226; AD 2005–17–05]
circumferential repair cuts, and to repair
or replace the spool shaft if you find
certain circumferential cuts. This AD
results from an updated stress analysis.
We are issuing this AD to prevent
failure of the HPCR stage 11–14 spool
shaft due to low-cycle fatigue that could
result in an uncontained engine failure.
RIN 2120–AA64
DATES:
Federal Aviation Administration
14 CFR Part 39
Airworthiness Directives; General
Electric Company (GE) CF6–80C2 and
CF6–80E1 Turbofan Engines
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
GE CF6–80C2 and CF6–80E1 turbofan
engines. This AD requires you to inspect
the high pressure compressor rotor
(HPCR) stage 11–14 spool shaft for
PO 00000
Frm 00026
Fmt 4700
Sfmt 4700
This AD becomes effective
September 27, 2005. The Director of the
Federal Register approved the
incorporation by reference of certain
publications listed in the regulations as
of September 27, 2005.
You can get the service
information identified in this AD from
General Electric Company via Lockheed
Martin Technology Services, 10525
Chester Road, Suite C, Cincinnati, Ohio
45215, telephone (513) 672–8400, fax
(513) 672–8422.
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
ADDRESSES:
E:\FR\FM\23AUR1.SGM
23AUR1
]]>Agencies
[Federal Register Volume 70, Number 162 (Tuesday, August 23, 2005)]
[Rules and Regulations]
[Pages 49174-49178]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-16455]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2004-19865; Directorate Identifier 2003-NM-242-AD;
Amendment 39-14230; AD 2005-17-09]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747, 757, 767 and 777
Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding an existing airworthiness directive
(AD), which applies to certain Boeing Model 747, 757, 767, and 777
series airplanes. That AD currently requires modifying certain drip
shields located on the flight deck, and follow-on actions. This new AD
removes certain airplanes that are included in the applicability
statement of the existing AD, and requires modifying additional drip
shields on the flight deck of certain other airplanes. This AD is
prompted by a determination that certain airplanes have drip shields
that are not adequately resistant to fire. We are issuing this AD to
prevent potential ignition of the moisture barrier cover of the drip
shield, which could propagate a small fire that results from an
electrical arc, leading to a larger fire.
DATES: This AD becomes effective September 27, 2005.
The incorporation by reference of certain publications listed in
the AD is approved by the Director of the Federal Register as of
September 27, 2005.
On February 2, 2001 (65 FR 82901, December 29, 2000), the Director
of the Federal Register approved the incorporation by reference of
certain other publications listed in the AD.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-
2207.
Docket: The AD docket contains the proposed AD, comments, and any
final disposition. You can examine the AD docket on the Internet at
https://dms.dot.gov, or in person at the Docket Management Facility
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S.
Department of Transportation, 400 Seventh Street SW, room PL-401,
Washington, DC. This docket number is
[[Page 49175]]
FAA-2004-19865; the directorate identifier for this docket is 2003-NM-
242-AD.
FOR FURTHER INFORMATION CONTACT: Patrick Gillespie, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton,
Washington 98055-4056; telephone (425) 917-6429; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) with an AD to supersede
AD 2000-26-04, amendment 39-12054 (65 FR 82901, December 29, 2000). The
existing AD applies to certain Boeing Model 747, 757, 767, and 777
series airplanes. The proposed AD was published in the Federal Register
on December 16, 2004 (69 FR 75267), to require modifying certain drip
shields located on the flight deck, and follow-on actions.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comments that have been
submitted on the proposed AD.
Support for the Proposed AD
One commenter concurs with the contents of the proposed AD and has
no additional comments.
Request To Revise Applicability Statement
One commenter, the airplane manufacturer, requests that we revise
Table 1 under Applicability in the proposed AD to remove the Model 777
series airplane having line number (L/N) 254. The commenter states that
the affected Model 777 L/Ns include line numbers prior to 254, except
L/Ns 1, 120, 219, 230, 235, 242, 245, and 249.
We agree and have revised Table 1 of this AD to remove L/N 254.
Request To Add Later Service Bulletin Revision
One commenter requests that we revise paragraph (f) of the proposed
AD to refer to Boeing Service Bulletin 757-25-0228, Revision 1, dated
March 28, 2002 (for Model 757-300 series airplanes); and Boeing Service
Bulletin 777-25-0164, Revision 1, including Appendices A, B, C, and D,
all dated March 22, 2001; as acceptable methods of compliance with that
paragraph. The commenter notes that the procedures in Revision 1 of
these service bulletins are substantially similar to those in the
original issues of the service bulletin, which paragraph (f) refers to
as acceptable sources of service information for Model 757-300 and
Model 777 series airplanes. Boeing Service Bulletin 757-25-0228,
Revision 1, clarifies certain procedures and corrects a part number for
a washer used to attach fire blocks. Boeing Service Bulletin 777-25-
0164, Revision 1, provides additional installation instructions and
placard and dimensional information. The commenter also notes that the
effectivity listing is the same in Revision 1 of the service bulletins
as in the original issues.
We agree. We note that Revision 1 of these service bulletins was
approved as an alternative method of compliance (AMOC) for AD 2000-26-
04, and that AMOC remains valid as specified in paragraph (k)(2) of
this AD. However, for clarification and for the convenience of affected
operators, we have also revised paragraph (f) of this AD to specify
both the original issue and Revision 1 of these service bulletins as
acceptable methods of compliance for doing the modification required by
that paragraph.
Request To Clarify Requirements for Certain Model 757 Series Airplanes
One commenter requests that we revise the proposed AD to allow the
proposed actions to be accomplished in accordance with previous
revisions of Boeing Service Bulletin 757-25-0226 for Boeing Model 757
series airplanes identified in Groups 2 and 4 of Boeing Service
Bulletin 757-25-0226, Revision 3, dated September 2, 2004. The
commenter states that, for airplanes in those groups, Boeing Service
Bulletins 757-25-0226, Revision 2, dated October 31, 2002, and Revision
3, do not add additional work beyond what is specified for those
airplanes in the original issue, dated July 3, 2000, and Revision 1,
dated February 15, 2001. The commenter states that we should make it
clear that no additional work is required by this AD for any airplane
in Group 2 or 4 that was modified in accordance with a previous issue
of the service bulletin. The commenter adds that the proposed AD should
also be revised to give credit for using any revision of Boeing Service
Bulletin 757-25-0226 to modify any airplane in Group 2 or 4. The
commenter also notes that an AMOC was issued for AD 2000-26-04 to allow
certain required actions to be accomplished in accordance with Boeing
Service Bulletin 757-25-0226, Revision 1. The commenter states that
this AMOC should also still be valid for airplanes in Groups 2 and 4.
We agree with the commenter's requests for the reasons stated by
the commenter, and accordingly have made the following changes to this
AD:
We revised paragraph (i) of this AD to specify that
paragraph (i) applies only to airplanes identified as being in Group 1
or 3 by Boeing Service Bulletin 757-25-0226, Revision 3.
We revised paragraph (f) to state that only airplanes in
Group 1 or 3 are required to use Revision 3 after the effective date of
this AD.
We added a new paragraph (j)(2) to this AD (and renumbered
a subsequent paragraph) to give credit for modifying the drip shields
on airplanes in Groups 2 and 4 before the effective date of this AD in
accordance with Revision 1 of Boeing Service Bulletin 757-25-0226.
(Paragraph (j)(1) of this AD already gives credit for modifying the
drip shields in accordance with Revision 2 of that service bulletin.)
We revised paragraph (k)(2) of this AD to state that,
except for Model 757-200, -200CB, and -200PF series airplanes listed in
Groups 1 and 3 of Boeing Service Bulletin 757-25-0226, Revision 3,
dated September 2, 2004, AMOCs approved previously in accordance with
AD 2000-26-04, amendment 39-12054, are acceptable for compliance with
this AD.
We revised the Costs of Compliance section to reduce the
estimated number of Model 757-200, -200CB, and -200PF series airplanes
subject to the new requirements from 491 U.S.-registered airplanes to
350. This figure includes only the airplanes in Groups 1 and 3.
Request To Revise Estimated Number of Airplanes No Longer Affected
One commenter, the airplane manufacturer, states that the estimate
of Model 747 series airplanes no longer affected, as stated in the
Actions Since Existing AD Was Issued section of the proposed AD, should
be increased from 550 to 650 airplanes. The commenter points out that
the effectivity listing of the original issue of Boeing Service
Bulletin 747-25-3253, dated June 29, 2000, included L/Ns 1 through 1234
inclusive, except 1174 and 1216 (approximately 1230 airplanes).
However, the effectivity listing of Boeing Service Bulletin 747-25-
3253, Revision 3, dated September 4, 2003, includes L/Ns 1 through 299
inclusive and 951 through 1234 inclusive, except 292, 296, 297, 1174,
and 1216 (approximately 580 airplanes). Therefore, approximately 650
airplanes are no longer affected.
We agree with the intent of the commenter's request. However, the
relevant paragraph to which the commenter refers is not restated in
this
[[Page 49176]]
final rule. Thus, we have made no change in this regard.
Request To Increase Estimate for Costs of Compliance
One commenter requests that we increase the number of work hours
necessary to accomplish the required actions on affected Model 757
series airplanes. The commenter notes that the proposed AD estimates
that 26 work hours would be needed, while the referenced service
bulletin for Model 757 series airplanes states total work-hour
estimates of 107, 94.5, 74, and 66 work hours for airplanes in Groups
1, 2, 3, and 4, respectively. The commenter states that its experience
indicates that the figures provided by Boeing in the service bulletin
are accurate, but the FAA's estimate times are lower than the service
bulletin figures and, as a result, contribute to an erroneously low
cost estimate.
We partially agree with the commenter's request. We note that the
total work hour estimates to which the commenter refers include time
for gaining access and closing up. The cost analysis in AD actions,
however, typically does not include costs such as the time required to
gain access and close up, time necessary for planning, or time
necessitated by other administrative actions. Costs for those type of
actions may vary significantly among operators and are almost
impossible to calculate.
However, we do agree that the costs of compliance estimated in the
proposed AD for Model 757 series airplanes did not include the work
hours necessary for testing, as specified in Boeing Service Bulletin
757-25-0226, Revision 3. Therefore, we have revised the estimated costs
of compliance in this AD to estimate that 58 work hours are needed to
do the required actions on each affected Model 757 series airplane.
Conclusion
We have carefully reviewed the available data, including the
comments that have been submitted, and determined that air safety and
the public interest require adopting the AD with the changes described
previously. We have determined that these changes will neither increase
the economic burden on any operator nor increase the scope of the AD.
Costs of Compliance
There are about 2,222 airplanes of affected design in the worldwide
fleet. The following table provides the estimated costs for U.S.
operators to comply with the actions that are required by AD 2000-26-04
and retained in this proposed AD. The average labor rate is $65 per
work hour.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
U.S.- Maximum fleet
Model registered Work hours Labor cost Parts cost cost
airplanes (estimated) (estimated) (estimated) (estimated)
----------------------------------------------------------------------------------------------------------------
747.......................... 105 39 $2,535 $2,300 to 3,500 $633,675
757.......................... 491 58 3,770 1,700 2,685,770
767.......................... 140 17 1,105 2,300 476,700
777.......................... 56 3 195 1,700 106,120
----------------------------------------------------------------------------------------------------------------
For Model 747 series airplanes listed in Group 1 in Boeing Service
Bulletin 747-25-3253, Revision 3, in lieu of doing the modification of
the drip shields, this proposed AD provides an option to take samples
of the drip shields to determine if the modification is necessary.
Therefore, the estimated costs above may be reduced if some airplanes
do not need the modification. It would take approximately 18 work hours
to do the sampling, at an average labor rate of $65 per work hour.
Based on these figures, the cost impact of the sampling is estimated to
be $1,170 per sampled airplane.
As many as 350 U.S.-registered Model 757-200, -200CB, and -200PF
series airplanes may be subject to the new proposed actions. These new
actions would take about 8 additional work hours per airplane, at an
average labor rate of $65 per work hour. Required parts would cost an
additional $160 per airplane (for a total parts cost of $1,860 per
airplane). Based on these figures, the estimated cost of the new
actions specified in this proposed AD for U.S. operators of affected
airplanes is up to an additional $238,000, or $680 per airplane.
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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under 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 regulatory evaluation of the estimated costs to
comply with this AD. See the ADDRESSES section for a location to
examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
[[Page 49177]]
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 39-12054 (65 FR
82901, December 29, 2000), and by adding the following new
airworthiness directive (AD):
2005-17-09 Boeing: Amendment 39-14230. Docket No. FAA-2004-19865;
Directorate Identifier 2003-NM-242-AD.
Effective Date
(a) This AD becomes effective September 27, 2005.
Affected ADs
(b) This AD supersedes AD 2000-26-04, amendment 39-12054.
Applicability
(c) This AD applies to Model 747, 757, 767, and 777 series
airplanes having the line numbers (L/Ns) listed in Table 1 of this
AD; certificated in any category.
Table 1.--Applicability
----------------------------------------------------------------------------------------------------------------
Model Affected L/Ns Except L/Ns
----------------------------------------------------------------------------------------------------------------
747......................... 1 through 299 inclusive 292, 296, 297, 1174, 1216.
and 951 through 1234
inclusive.
757......................... 2 through 895 inclusive 870, 886, 894.
767......................... 470 through 768 758.
inclusive.
777......................... 2 through 253 inclusive 120, 219, 230, 235, 242, 245, 249.
----------------------------------------------------------------------------------------------------------------
Unsafe Condition
(d) This AD was prompted by a determination that certain
airplanes have drip shields that are not adequately resistant to
fire. We are issuing this AD to prevent potential ignition of the
moisture barrier cover of the drip shield, which could propagate a
small fire that results from an electrical arc, leading to a larger
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.
Requirements of AD 2000-26-04
Modification
(f) Within 6 years after February 2, 2001 (the effective date of
AD 2000-26-04), accomplish paragraphs (f)(1), (f)(2), and (f)(3) of
this AD; in accordance with Boeing Service Bulletin 747-25-3253,
dated June 29, 2000, or Revision 3, dated September 4, 2003; 757-25-
0226, dated July 3, 2000, or Revision 3, dated September 2, 2004;
757-25-0228, dated July 3, 2000, or Revision 1, dated March 28,
2002; 767-25-0290, dated June 29, 2000, or Revision 4, dated October
28, 2004; or 777-25-0164, dated June 29, 2000, or Revision 1,
including Appendices A, B, C, and D, all dated March 22, 2001; as
applicable; except as provided by paragraph (g) of this AD. For
Model 757-200, -200CB, and -200PF series airplanes identified as
being in Groups 1 and 3 in Boeing Service Bulletin 757-25-0226,
Revision 3: As of the effective date of this AD, only Revision 3 of
the service bulletin may be used. For Model 747 and 767 series
airplanes: As of the effective date of this AD, only Boeing Service
Bulletin 747-25-3253, Revision 3, or 767-25-0290, Revision 4, as
applicable, may be used.
(1) Modify drip shields located on the flight deck by installing
fire blocks.
(2) Prior to further flight following accomplishment of
paragraph (f)(1) of this AD, perform a functional test of any system
disturbed by the modification, in accordance with the applicable
service bulletin or airplane maintenance manual (AMM), as
applicable. If any functional test fails, prior to further flight,
isolate the fault, correct the discrepancy in accordance with the
applicable AMM, and repeat the failed test until it is successfully
accomplished.
(3) Prior to further flight following the accomplishment of
paragraphs (f)(1) and (f)(2) of this AD, install placards on all
modified drip shields.
(g) If any wires or equipment are installed on the outboard
surface of the drip shield (that is, between the drip shield and the
airplane structure), modify that area in accordance with a method
approved by the Manager, Seattle Aircraft Certification Office
(ACO), FAA.
Optional Sampling (Certain Model 747 Series Airplanes)
(h) For Model 747 series airplanes listed in Group 1 in Boeing
Service Bulletin 747-25-3253, Revision 3, dated September 4, 2003:
In lieu of accomplishing paragraph (f) of this AD, within 6 years
after February 2, 2001, collect samples of the insulation and
adhesive of the drip shields, and submit the samples to the
manufacturer for testing, in accordance with the Accomplishment
Instructions of Boeing Service Bulletin 747-25-3253, dated June 29,
2000, or Revision 3, dated September 4, 2003. After the effective
date of this AD, only Revision 3 may be used.
(1) If the test on all samples is positive, no further action is
required by this AD.
(2) If the test on any sample is negative, accomplish paragraph
(f) of this AD before the compliance time specified in that
paragraph.
New Requirements of This AD
Model 757-200/-200CB/-200PF Series Airplanes Previously Modified
(i) For Model 757-200, -200CB, and -200PF series airplanes
identified as being in Group 1 or 3 in Boeing Service Bulletin 757-
25-0226, Revision 3, dated September 2, 2004, and that were modified
before the effective date of this AD in accordance with Boeing
Service Bulletin 757-25-0226, dated July 3, 2000: Within 72 months
after the effective date of this AD, modify drip shields located
above windows number 2 and 3 on the flight deck by installing fire
blocks, in accordance with the Accomplishment Instructions of Boeing
Service Bulletin 757-25-0226, Revision 3, dated September 2, 2004;
except as provided by paragraph (g) of this AD. After the
modification, do the actions required by paragraphs (f)(2) and
(f)(3) of this AD because these actions apply to the drip shields
modified in accordance with this paragraph.
Previously Accomplished Actions
(j) Modifying the drip shields before the effective date of this
AD in accordance with the applicable service bulletin specified in
paragraph (j)(1), (j)(2), or (j)(3) of this AD is acceptable for
compliance with the corresponding requirements of paragraphs (f) and
(i) of this AD, as applicable.
(1) For Model 757-200, -200CB, and -200PF series airplanes:
Boeing Service Bulletin 757-25-0226, Revision 2, dated October 31,
2002.
(2) For Model 757-200, -200CB, and -200PF series airplanes
identified in Groups 2 and 4 of Boeing Service Bulletin 757-25-0226,
Revision 3, dated September 2, 2004: Boeing Service Bulletin 757-25-
0226, Revision 1, dated February 15, 2001.
(3) For Model 767 series airplanes: Boeing Service Bulletin 767-
25-0290, Revision 3, dated June 26, 2003.
Alternative Methods of Compliance (AMOCs)
(k)(1) The Manager, Seattle ACO, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19.
(2) Except for Model 757-200, -200CB, and -200PF series
airplanes listed in Groups 1 and 3 of Boeing Service Bulletin 757-
25-0226, Revision 3, dated September 2, 2004: Alternative methods of
compliance, approved previously in accordance with AD 2000-26-04,
amendment 39-12054, are approved as alternative methods of
compliance with this AD.
Material Incorporated by Reference
(l) You must use the applicable documents listed in Table 2 of
this AD to perform the actions that are required by this AD, unless
the AD specifies otherwise.
[[Page 49178]]
Table 2.--Material Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Boeing service bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
747-25-3253, including Appendices A, B, Original........................ June 29, 2000.
and C.
747-25-3253............................. 3............................... September 4, 2003.
757-25-0226, including Appendices A, B, Original........................ July 3, 2000.
and C.
757-25-0226............................. 3............................... September 2, 2004.
757-25-0228, including Appendices A, B, Original........................ July 3, 2000.
and C.
757-25-0228............................. 1............................... March 28, 2002.
767-25-0290, including Appendices A, B, Original........................ June 29, 2000.
and C.
767-25-0290............................. 4............................... October 28, 2004.
777-25-0164, including Appendices A, B, Original........................ June 29, 2000.
and C.
777-25-0164, including Appendices A, B, 1............................... March 22, 2001.
C, and D.
----------------------------------------------------------------------------------------------------------------
(1) The Director of the Federal Register approves the
incorporation by reference of the documents listed in Table 3 of
this AD in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Table 3.--New Material Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Boeing service bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
747-25-3253............................. 3............................... September 4, 2003.
757-25-0226............................. 3............................... September 2, 2004.
757-25-0228............................. 1............................... March 28, 2002.
767-25-0290............................. 4............................... October 28, 2004.
777-25-0164, including Appendices A, B, 1............................... March 22, 2001.
C, and D.
----------------------------------------------------------------------------------------------------------------
(2) On February 2, 2001 (65 FR 82901, December 29, 2000), the
Director of the Federal Register approved the incorporation by
reference of the documents listed in Table 4 of this AD.
Table 4.--Material Previously Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Boeing service bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
747-25-3253, including Appendices A, B, Original........................ June 29, 2000.
and C.
757-25-0226, including Appendices A, B, Original........................ July 3, 2000.
and C.
757-25-0228, including Appendices A, B, Original........................ July 3, 2000.
and C.
767-25-0290, including Appendices A, B, Original........................ June 29, 2000.
and C.
777-25-0164, including Appendices A, B, Original........................ June 29, 2000.
and C.
----------------------------------------------------------------------------------------------------------------
(3) To get copies of the service information, contact Boeing
Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207.
To view the AD docket, go to the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., room PL-401,
Nassif Building, Washington, DC. To review copies of the service
information, go to 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/cfr/ibr-locations.html.
Issued in Renton, Washington, on August 11, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-16455 Filed 8-22-05; 8:45 am]
BILLING CODE 4910-13-P
