Airworthiness Directives; Rolls-Royce plc (RR) RB211-524 Series Turbofan Engines, 9050-9053 [E9-4317]
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9050
Proposed Rules
Federal Register
Vol. 74, No. 39
Monday, March 2, 2009
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–0162; Directorate
Identifier 2004–NE–19–AD]
RIN 2120–AA64
Airworthiness Directives; Rolls-Royce
plc (RR) RB211–524 Series Turbofan
Engines
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
The FAA proposes to
supersede an existing airworthiness
directive (AD) for certain RR RB211–524
series turbofan engines. That AD
currently requires initial and repetitive
borescope inspections of the head
section and meterpanel assembly of the
combustion liner, and replacement if
necessary with serviceable parts. This
proposed AD would require those same
inspections, and replacement if
necessary with serviceable parts. This
proposed AD would also add more part
number (P/N) combustion liners to the
applicability of this proposed AD. This
proposed AD results from an inquiry
submitted by an operator, which
resulted in RR performing a complete
review of the affected front combustion
liner part numbers. We are proposing
this AD to prevent deterioration of the
engine combustion liner, which can
result in combustion liner breakup, case
burn-through, engine fire, and damage
to the airplane.
DATES: We must receive any comments
on this proposed AD by May 1, 2009.
ADDRESSES: Use one of the following
addresses to comment on this proposed
AD.
• Federal eRulemaking Portal: Go to
https://www.regulations.gov and follow
the instructions for sending your
comments electronically.
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SUMMARY:
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• Mail: Docket Management Facility,
U.S. Department of Transportation, 1200
New Jersey Avenue, SE., West Building
Ground Floor, Room W12–140,
Washington, DC 20590–0001.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
• Fax: (202) 493–2251.
Contact Rolls-Royce plc, P.O. Box 31,
Derby, DE24 8BJ, United Kingdom;
telephone: 011–44–1332–242424; fax:
011–44–1332–249936, for the service
information identified in this proposed
AD.
FOR FURTHER INFORMATION CONTACT:
Ian
Dargin, Aerospace Engineer, Engine
Certification Office, FAA, Engine and
Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803;
e-mail: ian.dargin@faa.gov; telephone
(781) 238–7178; fax (781) 238–7199.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments
regarding this proposal. Send your
comments to an address listed under
ADDRESSES. Include ‘‘Docket No. FAA–
2009–0162; Directorate Identifier 2004–
NE–19–AD’’ in the subject line of your
comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of the proposed AD. We will
consider all comments received by the
closing date and may amend the
proposed AD in light of those
comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact with FAA
personnel concerning this proposed AD.
Using the search function of the Web
site, anyone can find and read the
comments in any of our dockets,
including, if provided, 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).
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Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Operations office between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket
contains this proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Operations
office (telephone (800) 647–5527) is the
same as the Mail address provided in
the ADDRESSES section. Comments will
be available in the AD docket shortly
after receipt.
Discussion
On December 20, 2004, the FAA
issued AD 2004–26–05, Amendment
39–13917 (70 FR 680, January 5, 1005).
That AD requires initial and repetitive
borescope inspections of the
combustion liner head section and
meterpanel assembly of the combustion
liner and replacement if necessary, with
serviceable parts. That action also
reduces the inspection intervals of
certain RB211–524 engine models that
have not been repaired to RR Field
Repair Scheme FRS5367/B, and requires
a mandatory terminating action to be
completed by a certain date. The Civil
Aviation Authority (CAA), which is the
airworthiness authority for the United
Kingdom, notified the FAA that an
unsafe condition may exist on RR
RB211–524 series turbofan engines. The
CAA advises that in August 2002, an
RB211–524B engine suffered a
combustion case burn-through as a
result of combustor head breakup. The
combustor head was previously
inspected within the inspection interval
specified in RR Service Bulletin (SB)
No. RB.211–72–B482, Revision 8, dated
November 15, 2001, only 228 cycles
before the event. Subsequent to the
original AD, RR has issued several
revisions to SB No. RB.211–72–B482 to
expand the applicability and clarify or
revise the inspection requirements. In
2003, RR issued Alert Service Bulletin
(ASB) No. RB.211–72–AB482, Revision
9, dated July 28, 2003, to reduce the
inspection interval for RB211–524B–02,
–524B2, –524B3, and –524B4 engines
that have not been repaired to RR Field
Repair Scheme FRS5367/B. This
condition, if not corrected, could result
in deterioration of the engine
combustion liner, which can result in
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Federal Register / Vol. 74, No. 39 / Monday, March 2, 2009 / Proposed Rules
combustion liner breakup, case burnthrough, and engine fire.
Actions Since AD 2004–26–05 Was
Issued
Since that AD was issued, an operator
submitted an inquiry which resulted in
RR performing a complete review of the
affected front combustion liner part
numbers. Rolls-Royce identified a
number of P/Ns that must be included
in the inspection requirements of this
proposed AD.
Relevant Service Information
We have reviewed and approved the
technical contents of the following RR
SBs:
• RR ASB No. RB.211–72–AB482,
Revision 9, dated July 28, 2003, which
describes the initial inspection
procedures to detect cracking of the
combustion liner head section and the
meterpanel. This ASB also describes the
compliance intervals to do the initial
and repetitive inspections.
• RR SB No. RB.211–72–9670, dated
August 27, 1993, which describes the
procedures to incorporate the improved
combustion liner head with C263
material, and to incorporate local
thickened diffuser walls around the
struts for engine models –524B–02,
–524B2, –524B3, –524B4, –524C2 and
–524D4.
• RR SB No. RB.211–72–9764,
Revision 3, dated January 16, 1998,
which describes the procedures to
incorporate the improved combustion
liner with strengthened head and
improved heat shields for engine
models –524G and –524H.
The CAA classified ASB No. RB.211–
72–AB482, Revision 9, dated July 28,
2003, as mandatory and issued AD G–
2003–0011 (previously 005–07–95),
dated October 1, 2003, in order to
ensure the airworthiness of these RR
engines in the United Kingdom.
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Bilateral Agreement Information
This engine model is manufactured in
the United Kingdom and is type
certificated for operation in the United
States under the provisions of Section
21.29 of the Federal Aviation
Regulations (14 CFR 21.29) and the
applicable bilateral airworthiness
agreement. Under this bilateral
airworthiness agreement, the CAA kept
us informed of the situation described
above. We have examined the findings
of the CAA, reviewed all available
information, and determined that AD
action is necessary for products of this
type design that are certificated for
operation in the United States.
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FAA’s Determination and Requirements
of the Proposed AD
We have evaluated all pertinent
information and identified an unsafe
condition that is likely to exist or
develop on other products of this same
type design. We are proposing this AD,
which would require:
• Initial and repetitive borescope
inspections of the combustion liner
head section and meterpanel assembly
of the combustion liner and, if
necessary, replacement.
• Reduction of the inspection
intervals of certain RB211–524 engine
models that have not been repaired to
RR Field Repair Scheme FRS5367/B,
and
• A mandatory terminating action to
the repetitive inspections to be
completed no later than December 31,
2012.
The proposed AD would require that
you do these actions using the service
information described previously.
Costs of Compliance
We estimate that this proposed AD
would affect 18 engines installed on
airplanes of U.S. registry. We also
estimate that it would take about 2
work-hours per engine to perform the
proposed actions, and that the average
labor rate is $80 per work-hour. No parts
are required, so parts would cost about
$0. Based on these figures, we estimate
the total cost of the proposed AD to U.S.
operators to be $2,880.
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
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
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9051
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 proposed AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Would 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 proposed 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, Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
proposes to amend 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing Amendment 39–13917 (70 FR
680, January 5, 2005, and by adding a
new airworthiness directive, to read as
follows:
Rolls-Royce plc: Docket No. FAA–2009–
0162; Directorate Identifier 2004–NE–
19–AD.
Comments Due Date
(a) The Federal Aviation Administration
(FAA) must receive comments on this
airworthiness directive (AD) action by May 1,
2009.
Affected ADs
(b) This AD supersedes AD 2004–26–05,
Amendment 39–13917.
Applicability
(c) This AD applies to Rolls-Royce plc (RR)
engine models RB211–524B–02, –524B2,
–524B3, –524B4, –524C2, and –524D4 series
engines that incorporate RR Service Bulletin
(SB) No. RB.211–72–7221 or RR SB No.
RB.211–72–7998 with front combustion liner
assembly, part number (P/N) UL16078,
UL16885, UL21441, UL24898, UL26916,
UL27107, UL27108, UL27109, UL27875,
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Federal Register / Vol. 74, No. 39 / Monday, March 2, 2009 / Proposed Rules
UL27876, UL28971, UL28972, UL28973,
UL28974, UL28975, UL28976, UL28977,
UL28978, UL28979, UL28980, UL28981,
UL28982, or UL28983, installed but not
incorporating RR SB No. RB.211–72–9670 or
RR SB No. RB.211–72–9764, and engine
models RB211–524G and –524H series
engines with front combustion liner assembly
P/N UL27659, UL23992, UL22988, UL37874,
and UL37882, but not incorporating RR SB
No. RB.211–72–9764. These engines are
installed on, but not limited to, Boeing 747
and Lockheed L1011 series airplanes.
RR performing a complete review of the
affected front combustion liner part numbers.
We are issuing this AD to prevent
deterioration of the engine combustion liner,
which can result in combustion liner
breakup, case burn-through, engine fire, and
damage to the airplane.
Unsafe Condition
(d) This AD results from an inquiry
submitted by an operator which resulted in
Credit for Previous Inspections
(f) Engine inspections previously made to
RR Service Bulletin No. RB.211–72–B482,
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.
Revision 8, meet the requirements of this AD
for the initial or repetitive inspections
specified in paragraphs (f) through (f)(3) and
(g) through (g)(3) of this AD.
Inspections of Combustion Liner Head
Sections—Not Previously Repaired
(g) Borescope-inspect combustion liner
head sections that have not been previously
repaired. Use paragraphs 3.A.(1) through
3.A.(5) of the Accomplishment Instructions
of RR Alert Service Bulletin (ASB) No.
RB.211–72–AB482, Revision 9, dated July 28,
2003, and the cycles-since-new (CSN),
cycles-since-last inspection (CSLI), and
cycles-in-service (CIS) compliance thresholds
in Table 1 of this AD.
TABLE 1—COMBUSTION LINER HEAD SECTION—NOT PREVIOUSLY REPAIRED
Initial inspection
Repetitive inspection
Parts exceeding initial inspection
cycles
–524D4,
Within 1,400 to 1,600 CSN ..........
Within 200 CSLI ...........................
–524B2,
Within 3,000 to 3,200 CSN ..........
Within 200 CSLI ...........................
Within 100 CIS after the effective
date of this AD.
Within 200 CIS after the effective
date of this AD.
Engine series
(1)
RB211–524C2,
–524G, and –524H.
(2) RB211–524B–02,
–524B3, and –524B4.
Inspections of Combustion Liner Head
Sections—Previously Repaired Using RR
Field Repair Scheme FRS5367/B
(h) Borescope-inspect combustion liner
head sections previously repaired using RR
Field Repair Scheme FRS5367/B. Use
paragraphs 3.A.(1) through 3.A.(5) of the
Accomplishment Instructions of RR ASB No.
RB.211–72–AB482, Revision 9, dated July 28,
2003, and the cycles-since-last repair (CSLR),
CSLI, and CIS compliance thresholds in
Table 2 of this AD.
TABLE 2—COMBUSTION LINER HEAD SECTION—PREVIOUSLY REPAIRED USING RR FIELD REPAIR SCHEME FRS5367/B
Initial inspection
Repetitive inspection
Parts exceeding initial inspection
cycles
–524D4,
Within 1,800 to 2,200 CSLR ........
Within 400 CSLI ...........................
–524B2,
Within 3,000 to 3,200 CSLR ........
Within 400 CSLI ...........................
Within 200 CIS after the effective
date of this AD.
Within 200 CIS after the effective
date of this AD.
Engine series
(1)
RB211–524C2,
–524G, and –524H.
(2) RB211–524B–02,
–524B3, and –524B4.
Inspections of Combustion Liner Head
Sections That Have Been Repaired But Did
Not Use RR Field Repair Scheme FRS5367/
B
(i) Borescope-inspect combustion liner
head sections that have been repaired using
a method other than RR Field Repair Scheme
FRS5367/B. Use paragraphs 3.A.(1) through
3.A.(5) of the Accomplishment Instructions
of RR ASB No. RB.211–72–AB482, Revision
9, dated July 28, 2003, and the CSLR, CSLI,
and CIS compliance thresholds in Table 3 of
this AD.
TABLE 3—COMBUSTION LINER HEAD SECTION—REPAIRED, BUT DID NOT USE RR FIELD REPAIR SCHEME FRS5367/B
Initial inspection
Repetitive inspection
Parts exceeding initial inspection
cycles
–524D4,
Within 500 to 700 CSLR ..............
Within 200 CSLI ...........................
–524B2,
Within 2,000 to 2,200 CSLR ........
Within 200 CSLI ...........................
Within 100 CIS after the effective
date of this AD.
Within 200 CIS after the effective
date of this AD.
Engine series
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(1)
RB211–524C2,
–524G, and –524H.
(2) RB211–524B–02,
–524B3, and –524B4.
(3) For an installed front combustion liner
that is subject to RR ASB No. RB.211–72–
AB482, Revision 9, dated July 28, 2003, if the
operator can confirm with the relevant
overhaul base or repair vendor that the
nicrobraze repair RR Field Repair Scheme
FRS5367 has been applied to all 18 struts,
then this is equivalent to compliance with RR
Field Repair Scheme FRS5367/B.
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(4) Head sections repaired by replacement
of all 18 struts using RR Field Repair Scheme
FRS6548 are considered as equivalent to
fitting a new head section for inspection
purposes.
Inspections of Meterpanel Assemblies—Not
Repaired
(j) Borescope-inspect meterpanel
assemblies that incorporate SB No. RB.211–
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72–7998, that have not been previously
repaired. Use paragraphs 3.B.(1) through
3.B.(7) of the Accomplishment Instructions of
RR ASB No. RB.211–72–AB482, Revision 9,
dated July 28, 2003, and the CSN, CSLI, and
CIS compliance thresholds in Table 4 of this
AD.
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Federal Register / Vol. 74, No. 39 / Monday, March 2, 2009 / Proposed Rules
9053
TABLE 4—METERPANEL ASSEMBLY—NOT REPAIRED
Engine series
Initial inspection
(1) RB211–524D4, –524G, and Within 1,000 to 1,200 CSN ..........
–524H.
(2) RB211–524D4, –524G, and Within 1,800 to 2,000 CSN ..........
–524H that have not used
RB211–524H ratings at any time.
Inspections of Meterpanel Assemblies—
Repaired
(k) Borescope–inspect meterpanel
assemblies that incorporate SB No. RB.211–
Parts exceeding initial inspection
cycles
Repetitive inspection
Within 400 CSLI ...........................
Within 400 CSLI ...........................
72–7998, that have been previously repaired.
Use paragraphs 3.B.(1) through 3.B.(7) of the
Accomplishment Instructions of RR ASB No.
RB.211–72–AB482, Revision 9, dated July 28,
Within
date
Within
date
50 CIS after the effective
of this AD.
50 CIS after the effective
of this AD.
2003, and the CSLR, CSLI, and CIS
compliance thresholds in Table 5 of this AD.
TABLE 5—METERPANEL ASSEMBLY—REPAIRED
Engine series
Initial inspection
Repetitive inspection
Parts exceeding initial inspection
cycles
(1) RB211–524D4, –524G, and
–524H.
Within 500 to 700 CSLR ..............
Within 400 CSLI ...........................
Within 50 CIS after the effective
date of this AD.
Reject Parts
(l) Replace parts that exceed the acceptance
criteria. Information about the acceptance
criteria can be found in the Aircraft
Maintenance Manual, 72–00–00, Inspection/
Check.
Mandatory Terminating Action
(m) Replace any front combustion liner
assembly that has a P/N listed in paragraph
(c) of this AD at the next shop visit, but no
later than December 31, 2012.
(n) For RB211–524B02, –524B2, –524B3,
–524B4, –524C2 and –524D4 engines,
replacing the front combustion liner
assembly with a front combustion liner
assembly that incorporates the modifications
in RR SB No. RB.211–72–9670, Original
Issue, dated August 27, 1993; or RR SB No.
RB.211–72–9764, Revision 3, dated January
16, 1998, constitutes terminating action to
the repetitive inspections in paragraphs (f),
(g), (h), (i), and (j), of this AD.
(o) For RB211–524G and –524H engines,
replacing the front combustion liner
assembly with a front combustion liner
assembly that incorporates the modifications
in RR SB No. RB.211–72–9764, Revision 3,
dated January 16, 1998, constitutes
terminating action to the repetitive
inspections in paragraphs (f), (g), (h), (i), and
(j) of this AD.
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Definition of Shop Visit
(p) For the purpose of this AD, a shop visit
is any time that the 04 module is removed
for refurbishment or overhaul.
Related Information
(q) Contact Ian Dargin, Aerospace Engineer,
Engine Certification Office, FAA, Engine and
Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803;
e-mail: ian.dargin@faa.gov; telephone (781)
238–7178; fax (781) 238–7199, for more
information about this AD.
(r) Rolls-Royce ASB No. RB.211–72–
AB482, Revision 9, dated July 28, 2003; SB
No. RB.211–72–9764, Revision 3, dated
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Jkt 217001
January 16, 1998; and SB No. RB.211–72–
9670, Original Issue, dated August 27, 1993,
pertain to the subject of this AD. Contact
Rolls-Royce plc, P.O. Box 31, Derby, DE24
8BJ, United Kingdom; telephone: 011–44–
1332–242424; fax: 011–44–1332–249936, for
a copy of this service information.
Issued in Burlington, Massachusetts, on
February 19, 2009.
Colleen M. D’Alessandro,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. E9–4317 Filed 2–27–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2009–0120; Airspace
Docket No. 09–ACE–2]
Proposed Establishment of Class E
Airspace; Rushville, NE
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
This action proposes to
establish Class E airspace at Rushville,
NE. Controlled airspace is necessary to
accommodate new Standard Instrument
Approach Procedures (SIAPs) at
Modisett Airport, Rushville, NE. The
FAA is taking this action to enhance the
safety and management of Instrument
Flight Rules (IFR) aircraft operations at
Modisett Airport.
DATES: 0901 UTC. Comments must be
received on or before April 16, 2009.
SUMMARY:
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ADDRESSES: Send comments on this
proposal to the U.S. Department of
Transportation, Docket Operations, 1200
New Jersey Avenue, SE., West Building
Ground Floor, Room W12–140,
Washington, DC 20590–0001. You must
identify the docket number FAA–2009–
0120/Airspace Docket No. 09–ACE–2, at
the beginning of your comments. You
may also submit comments on the
Internet at https://www.regulations.gov.
You may review the public docket
containing the proposal, any comments
received, and any final disposition in
person in the Dockets Office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Office (telephone 1–800–647–
5527), is on the ground floor of the
building at the above address.
FOR FURTHER INFORMATION CONTACT:
Scott Enander, Central Service Center,
Operations Support Group, Federal
Aviation Administration, Southwest
Region, 2601 Meacham Blvd., Fort
Worth, TX 76193–0530; telephone: (817)
321–7716.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested parties are invited to
participate in this proposed rulemaking
by submitting such written data, views,
or arguments, as they may desire.
Comments that provide the factual basis
supporting the views and suggestions
presented are particularly helpful in
developing reasoned regulatory
decisions on the proposal. Comments
are specifically invited on the overall
regulatory, aeronautical, economic,
environmental, and energy-related
aspects of the proposal.
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Agencies
[Federal Register Volume 74, Number 39 (Monday, March 2, 2009)]
[Proposed Rules]
[Pages 9050-9053]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-4317]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 74, No. 39 / Monday, March 2, 2009 / Proposed
Rules
[[Page 9050]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0162; Directorate Identifier 2004-NE-19-AD]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc (RR) RB211-524 Series
Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to supersede an existing airworthiness
directive (AD) for certain RR RB211-524 series turbofan engines. That
AD currently requires initial and repetitive borescope inspections of
the head section and meterpanel assembly of the combustion liner, and
replacement if necessary with serviceable parts. This proposed AD would
require those same inspections, and replacement if necessary with
serviceable parts. This proposed AD would also add more part number (P/
N) combustion liners to the applicability of this proposed AD. This
proposed AD results from an inquiry submitted by an operator, which
resulted in RR performing a complete review of the affected front
combustion liner part numbers. We are proposing this AD to prevent
deterioration of the engine combustion liner, which can result in
combustion liner breakup, case burn-through, engine fire, and damage to
the airplane.
DATES: We must receive any comments on this proposed AD by May 1, 2009.
ADDRESSES: Use one of the following addresses to comment on this
proposed AD.
Federal eRulemaking Portal: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility, U.S. Department of
Transportation, 1200 New Jersey Avenue, SE., West Building Ground
Floor, Room W12-140, Washington, DC 20590-0001.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Fax: (202) 493-2251.
Contact Rolls-Royce plc, P.O. Box 31, Derby, DE24 8BJ, United
Kingdom; telephone: 011-44-1332-242424; fax: 011-44-1332-249936, for
the service information identified in this proposed AD.
FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803; e-mail:
ian.dargin@faa.gov; telephone (781) 238-7178; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments regarding this proposal. Send your comments to an address
listed under ADDRESSES. Include ``Docket No. FAA-2009-0162; Directorate
Identifier 2004-NE-19-AD'' in the subject line of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of the proposed AD. We will consider
all comments received by the closing date and may amend the proposed AD
in light of those comments.
We will post all comments we receive, without change, to https://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact
with FAA personnel concerning this proposed AD. Using the search
function of the Web site, anyone can find and read the comments in any
of our dockets, including, if provided, 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).
Examining the AD Docket
You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Operations office (telephone (800) 647-5527) is
the same as the Mail address provided in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
Discussion
On December 20, 2004, the FAA issued AD 2004-26-05, Amendment 39-
13917 (70 FR 680, January 5, 1005). That AD requires initial and
repetitive borescope inspections of the combustion liner head section
and meterpanel assembly of the combustion liner and replacement if
necessary, with serviceable parts. That action also reduces the
inspection intervals of certain RB211-524 engine models that have not
been repaired to RR Field Repair Scheme FRS5367/B, and requires a
mandatory terminating action to be completed by a certain date. The
Civil Aviation Authority (CAA), which is the airworthiness authority
for the United Kingdom, notified the FAA that an unsafe condition may
exist on RR RB211-524 series turbofan engines. The CAA advises that in
August 2002, an RB211-524B engine suffered a combustion case burn-
through as a result of combustor head breakup. The combustor head was
previously inspected within the inspection interval specified in RR
Service Bulletin (SB) No. RB.211-72-B482, Revision 8, dated November
15, 2001, only 228 cycles before the event. Subsequent to the original
AD, RR has issued several revisions to SB No. RB.211-72-B482 to expand
the applicability and clarify or revise the inspection requirements. In
2003, RR issued Alert Service Bulletin (ASB) No. RB.211-72-AB482,
Revision 9, dated July 28, 2003, to reduce the inspection interval for
RB211-524B-02, -524B2, -524B3, and -524B4 engines that have not been
repaired to RR Field Repair Scheme FRS5367/B. This condition, if not
corrected, could result in deterioration of the engine combustion
liner, which can result in
[[Page 9051]]
combustion liner breakup, case burn-through, and engine fire.
Actions Since AD 2004-26-05 Was Issued
Since that AD was issued, an operator submitted an inquiry which
resulted in RR performing a complete review of the affected front
combustion liner part numbers. Rolls-Royce identified a number of P/Ns
that must be included in the inspection requirements of this proposed
AD.
Relevant Service Information
We have reviewed and approved the technical contents of the
following RR SBs:
RR ASB No. RB.211-72-AB482, Revision 9, dated July 28,
2003, which describes the initial inspection procedures to detect
cracking of the combustion liner head section and the meterpanel. This
ASB also describes the compliance intervals to do the initial and
repetitive inspections.
RR SB No. RB.211-72-9670, dated August 27, 1993, which
describes the procedures to incorporate the improved combustion liner
head with C263 material, and to incorporate local thickened diffuser
walls around the struts for engine models -524B-02, -524B2, -524B3, -
524B4, -524C2 and -524D4.
RR SB No. RB.211-72-9764, Revision 3, dated January 16,
1998, which describes the procedures to incorporate the improved
combustion liner with strengthened head and improved heat shields for
engine models -524G and -524H.
The CAA classified ASB No. RB.211-72-AB482, Revision 9, dated July
28, 2003, as mandatory and issued AD G-2003-0011 (previously 005-07-
95), dated October 1, 2003, in order to ensure the airworthiness of
these RR engines in the United Kingdom.
Bilateral Agreement Information
This engine model is manufactured in the United Kingdom and is type
certificated for operation in the United States under the provisions of
Section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement. Under this bilateral
airworthiness agreement, the CAA kept us informed of the situation
described above. We have examined the findings of the CAA, reviewed all
available information, and determined that AD action is necessary for
products of this type design that are certificated for operation in the
United States.
FAA's Determination and Requirements of the Proposed AD
We have evaluated all pertinent information and identified an
unsafe condition that is likely to exist or develop on other products
of this same type design. We are proposing this AD, which would
require:
Initial and repetitive borescope inspections of the
combustion liner head section and meterpanel assembly of the combustion
liner and, if necessary, replacement.
Reduction of the inspection intervals of certain RB211-524
engine models that have not been repaired to RR Field Repair Scheme
FRS5367/B, and
A mandatory terminating action to the repetitive
inspections to be completed no later than December 31, 2012.
The proposed AD would require that you do these actions using the
service information described previously.
Costs of Compliance
We estimate that this proposed AD would affect 18 engines installed
on airplanes of U.S. registry. We also estimate that it would take
about 2 work-hours per engine to perform the proposed actions, and that
the average labor rate is $80 per work-hour. No parts are required, so
parts would cost about $0. Based on these figures, we estimate the
total cost of the proposed AD to U.S. operators to be $2,880.
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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 proposed AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Would 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 proposed 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, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend 14
CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. The FAA amends Sec. 39.13 by removing Amendment 39-13917 (70 FR
680, January 5, 2005, and by adding a new airworthiness directive, to
read as follows:
Rolls-Royce plc: Docket No. FAA-2009-0162; Directorate Identifier
2004-NE-19-AD.
Comments Due Date
(a) The Federal Aviation Administration (FAA) must receive
comments on this airworthiness directive (AD) action by May 1, 2009.
Affected ADs
(b) This AD supersedes AD 2004-26-05, Amendment 39-13917.
Applicability
(c) This AD applies to Rolls-Royce plc (RR) engine models RB211-
524B-02, -524B2, -524B3, -524B4, -524C2, and -524D4 series engines
that incorporate RR Service Bulletin (SB) No. RB.211-72-7221 or RR
SB No. RB.211-72-7998 with front combustion liner assembly, part
number (P/N) UL16078, UL16885, UL21441, UL24898, UL26916, UL27107,
UL27108, UL27109, UL27875,
[[Page 9052]]
UL27876, UL28971, UL28972, UL28973, UL28974, UL28975, UL28976,
UL28977, UL28978, UL28979, UL28980, UL28981, UL28982, or UL28983,
installed but not incorporating RR SB No. RB.211-72-9670 or RR SB
No. RB.211-72-9764, and engine models RB211-524G and -524H series
engines with front combustion liner assembly P/N UL27659, UL23992,
UL22988, UL37874, and UL37882, but not incorporating RR SB No.
RB.211-72-9764. These engines are installed on, but not limited to,
Boeing 747 and Lockheed L1011 series airplanes.
Unsafe Condition
(d) This AD results from an inquiry submitted by an operator
which resulted in RR performing a complete review of the affected
front combustion liner part numbers. We are issuing this AD to
prevent deterioration of the engine combustion liner, which can
result in combustion liner breakup, case burn-through, engine fire,
and 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.
Credit for Previous Inspections
(f) Engine inspections previously made to RR Service Bulletin
No. RB.211-72-B482, Revision 8, meet the requirements of this AD for
the initial or repetitive inspections specified in paragraphs (f)
through (f)(3) and (g) through (g)(3) of this AD.
Inspections of Combustion Liner Head Sections--Not Previously Repaired
(g) Borescope-inspect combustion liner head sections that have
not been previously repaired. Use paragraphs 3.A.(1) through 3.A.(5)
of the Accomplishment Instructions of RR Alert Service Bulletin
(ASB) No. RB.211-72-AB482, Revision 9, dated July 28, 2003, and the
cycles-since-new (CSN), cycles-since-last inspection (CSLI), and
cycles-in-service (CIS) compliance thresholds in Table 1 of this AD.
Table 1--Combustion Liner Head Section--Not Previously Repaired
----------------------------------------------------------------------------------------------------------------
Parts exceeding initial
Engine series Initial inspection Repetitive inspection inspection cycles
----------------------------------------------------------------------------------------------------------------
(1) RB211-524C2, -524D4, -524G, and - Within 1,400 to 1,600 Within 200 CSLI........ Within 100 CIS after
524H. CSN. the effective date of
this AD.
(2) RB211-524B-02, -524B2, -524B3, Within 3,000 to 3,200 Within 200 CSLI........ Within 200 CIS after
and -524B4. CSN. the effective date of
this AD.
----------------------------------------------------------------------------------------------------------------
Inspections of Combustion Liner Head Sections--Previously Repaired
Using RR Field Repair Scheme FRS5367/B
(h) Borescope-inspect combustion liner head sections previously
repaired using RR Field Repair Scheme FRS5367/B. Use paragraphs
3.A.(1) through 3.A.(5) of the Accomplishment Instructions of RR ASB
No. RB.211-72-AB482, Revision 9, dated July 28, 2003, and the
cycles-since-last repair (CSLR), CSLI, and CIS compliance thresholds
in Table 2 of this AD.
Table 2--Combustion Liner Head Section--Previously Repaired Using RR Field Repair Scheme FRS5367/B
----------------------------------------------------------------------------------------------------------------
Parts exceeding initial
Engine series Initial inspection Repetitive inspection inspection cycles
----------------------------------------------------------------------------------------------------------------
(1) RB211-524C2, -524D4, -524G, and - Within 1,800 to 2,200 Within 400 CSLI........ Within 200 CIS after
524H. CSLR. the effective date of
this AD.
(2) RB211-524B-02, -524B2, -524B3, Within 3,000 to 3,200 Within 400 CSLI........ Within 200 CIS after
and -524B4. CSLR. the effective date of
this AD.
----------------------------------------------------------------------------------------------------------------
Inspections of Combustion Liner Head Sections That Have Been Repaired
But Did Not Use RR Field Repair Scheme FRS5367/B
(i) Borescope-inspect combustion liner head sections that have
been repaired using a method other than RR Field Repair Scheme
FRS5367/B. Use paragraphs 3.A.(1) through 3.A.(5) of the
Accomplishment Instructions of RR ASB No. RB.211-72-AB482, Revision
9, dated July 28, 2003, and the CSLR, CSLI, and CIS compliance
thresholds in Table 3 of this AD.
Table 3--Combustion Liner Head Section--Repaired, But Did Not Use RR Field Repair Scheme FRS5367/B
----------------------------------------------------------------------------------------------------------------
Parts exceeding initial
Engine series Initial inspection Repetitive inspection inspection cycles
----------------------------------------------------------------------------------------------------------------
(1) RB211-524C2, -524D4, -524G, and - Within 500 to 700 CSLR. Within 200 CSLI........ Within 100 CIS after
524H. the effective date of
this AD.
(2) RB211-524B-02, -524B2, -524B3, Within 2,000 to 2,200 Within 200 CSLI........ Within 200 CIS after
and -524B4. CSLR. the effective date of
this AD.
----------------------------------------------------------------------------------------------------------------
(3) For an installed front combustion liner that is subject to
RR ASB No. RB.211-72-AB482, Revision 9, dated July 28, 2003, if the
operator can confirm with the relevant overhaul base or repair
vendor that the nicrobraze repair RR Field Repair Scheme FRS5367 has
been applied to all 18 struts, then this is equivalent to compliance
with RR Field Repair Scheme FRS5367/B.
(4) Head sections repaired by replacement of all 18 struts using
RR Field Repair Scheme FRS6548 are considered as equivalent to
fitting a new head section for inspection purposes.
Inspections of Meterpanel Assemblies--Not Repaired
(j) Borescope-inspect meterpanel assemblies that incorporate SB
No. RB.211-72-7998, that have not been previously repaired. Use
paragraphs 3.B.(1) through 3.B.(7) of the Accomplishment
Instructions of RR ASB No. RB.211-72-AB482, Revision 9, dated July
28, 2003, and the CSN, CSLI, and CIS compliance thresholds in Table
4 of this AD.
[[Page 9053]]
Table 4--Meterpanel Assembly--Not Repaired
----------------------------------------------------------------------------------------------------------------
Parts exceeding initial
Engine series Initial inspection Repetitive inspection inspection cycles
----------------------------------------------------------------------------------------------------------------
(1) RB211-524D4, -524G, and -524H.... Within 1,000 to 1,200 Within 400 CSLI........ Within 50 CIS after the
CSN. effective date of this
AD.
(2) RB211-524D4, -524G, and -524H Within 1,800 to 2,000 Within 400 CSLI........ Within 50 CIS after the
that have not used RB211-524H CSN. effective date of this
ratings at any time. AD.
----------------------------------------------------------------------------------------------------------------
Inspections of Meterpanel Assemblies--Repaired
(k) Borescope-inspect meterpanel assemblies that incorporate SB
No. RB.211-72-7998, that have been previously repaired. Use
paragraphs 3.B.(1) through 3.B.(7) of the Accomplishment
Instructions of RR ASB No. RB.211-72-AB482, Revision 9, dated July
28, 2003, and the CSLR, CSLI, and CIS compliance thresholds in Table
5 of this AD.
Table 5--Meterpanel Assembly--Repaired
----------------------------------------------------------------------------------------------------------------
Parts exceeding initial
Engine series Initial inspection Repetitive inspection inspection cycles
----------------------------------------------------------------------------------------------------------------
(1) RB211-524D4, -524G, and -524H.... Within 500 to 700 CSLR. Within 400 CSLI........ Within 50 CIS after the
effective date of this
AD.
----------------------------------------------------------------------------------------------------------------
Reject Parts
(l) Replace parts that exceed the acceptance criteria.
Information about the acceptance criteria can be found in the
Aircraft Maintenance Manual, 72-00-00, Inspection/Check.
Mandatory Terminating Action
(m) Replace any front combustion liner assembly that has a P/N
listed in paragraph (c) of this AD at the next shop visit, but no
later than December 31, 2012.
(n) For RB211-524B02, -524B2, -524B3, -524B4, -524C2 and -524D4
engines, replacing the front combustion liner assembly with a front
combustion liner assembly that incorporates the modifications in RR
SB No. RB.211-72-9670, Original Issue, dated August 27, 1993; or RR
SB No. RB.211-72-9764, Revision 3, dated January 16, 1998,
constitutes terminating action to the repetitive inspections in
paragraphs (f), (g), (h), (i), and (j), of this AD.
(o) For RB211-524G and -524H engines, replacing the front
combustion liner assembly with a front combustion liner assembly
that incorporates the modifications in RR SB No. RB.211-72-9764,
Revision 3, dated January 16, 1998, constitutes terminating action
to the repetitive inspections in paragraphs (f), (g), (h), (i), and
(j) of this AD.
Definition of Shop Visit
(p) For the purpose of this AD, a shop visit is any time that
the 04 module is removed for refurbishment or overhaul.
Related Information
(q) Contact Ian Dargin, Aerospace Engineer, Engine Certification
Office, FAA, Engine and Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803; e-mail: ian.dargin@faa.gov;
telephone (781) 238-7178; fax (781) 238-7199, for more information
about this AD.
(r) Rolls-Royce ASB No. RB.211-72-AB482, Revision 9, dated July
28, 2003; SB No. RB.211-72-9764, Revision 3, dated January 16, 1998;
and SB No. RB.211-72-9670, Original Issue, dated August 27, 1993,
pertain to the subject of this AD. Contact Rolls-Royce plc, P.O. Box
31, Derby, DE24 8BJ, United Kingdom; telephone: 011-44-1332-242424;
fax: 011-44-1332-249936, for a copy of this service information.
Issued in Burlington, Massachusetts, on February 19, 2009.
Colleen M. D'Alessandro,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E9-4317 Filed 2-27-09; 8:45 am]
BILLING CODE 4910-13-P