[Federal Register: February 4, 2008 (Volume 73, Number 23)]
[Rules and Regulations]
[Page 6419-6423]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr04fe08-1]
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Rules and Regulations
Federal Register
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[[Page 6419]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27229; Directorate Identifier 2007-NE-03-AD;
Amendment 39-15359; AD 2008-03-09]
RIN 2120-AA64
Airworthiness Directives; CFM International, S.A. CFM56-7B Series
Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for CFM
International, S.A. CFM56-7B series turbofan engines. This AD requires
revising the Airworthiness Limitations Section (ALS) in the Engine Shop
Manual (ESM) and the air carrier's approved continuous airworthiness
maintenance program (CAMP) to add mandatory inspections of certain low
pressure turbine rear frames (TRFs) to the ALS or CAMP. This AD results
from a refined lifing analysis by the engine manufacturer that shows
the need to identify an initial threshold for inspecting certain TRFs.
We are issuing this AD to prevent failure of the TRF from low-cycle
fatigue cracks. Failure of the TRF could result in engine separation
from the airplane, which could lead to loss of control of the airplane.
DATES: This AD becomes effective March 10, 2008.
ADDRESSES: The Docket Operations office is located at Docket Management
Facility, U.S. Department of Transportation, 1200 New Jersey Avenue,
SE., West Building Ground Floor, Room W12-140, Washington, DC 20590-
0001.
FOR FURTHER INFORMATION CONTACT: Antonio Cancelliere, Aerospace
Engineer, Engine Certification Office, FAA, Engine and Propeller
Directorate, 12 New England Executive Park, Burlington, MA 01803;
telephone (781) 238-7751; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with a proposed AD. The proposed AD applies to CFM International, S.A.
CFM56-7B series turbofan engines. We published the proposed AD in the
Federal Register on April 23, 2007 (72 FR 20075). That action proposed
to require revising the ALS in the Engine Shop Manual and the air
carrier's approved continuous airworthiness maintenance program (CAMP)
to add mandatory inspections of certain low pressure turbine rear
frames (TRFs) to the ALS or CAMP.
Examining the AD Docket
You may examine the AD docket on the Internet at http://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 AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone (800) 647-5527) is provided in
the ADDRESSES section. Comments will be available in the AD docket
shortly after receipt.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comments received.
Update Table for Figure 805
Delta Airlines requests that we change the wording in the table for
Figure 805 because CFM International updated CFM56-7B Engine Shop
Manual section 05-21-03, with Temporary Revision 05-0080, dated
December 5, 2006. We agree and have reworded the table for Figure 805
to reflect wording used by the original equipment manufacturer (OEM).
For clarification, we also moved the titles for Figures 806 and 807 to
the beginning of the figures.
Guidance on Future Revisions
Delta Airlines also suggests that we provide guidance on making
future OEM revisions to ESM section 05-21-03 while maintaining
compliance with the AD. We disagree. The information contained within
sections (j) and (k) of the AD is adequate. Any future OEM changes to
the ALS that affect compliance with this AD will require an AD revision
or supersedure, depending on the specific situation. Airlines should
make changes to items outside of this specific area and incorporate
them into their ESM or CAMP per their normal procedures.
Add Part Numbers (P/Ns) to Applicability
Finally, Delta Airlines requests that we add P/Ns 340-166-251-0,
340-166-252-0 and 340-166-253-0 to the Applicability section and
clarify whether these P/Ns will be applicable to the business jet
application as well as the commercial application. We disagree. The
intent of this AD is to make operators aware of the life limit/
mandatory inspections recently introduced by CFM International in the
Airworthiness Limitations Section of the CFM56-7B Engine Shop Manual
that affect P/Ns that were not previously limited. Ignoring these new
limitations could create a potentially unsafe condition. The P/Ns
listed above were subject to a life limit and mandatory inspection when
first introduced to the ESM, therefore, there is no potential unsafe
condition. Business jet and commercial engine model applicability of
the new P/Ns is as listed in the ESM.
Conclusion
We have carefully reviewed the available data, including the
comments received, 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
We estimate that this AD will affect 1,228 engines installed on
airplanes of U.S. registry. While the cost of making the manual change
is negligible, the resulting inspections must be discussed. Since life
extensions are possible on condition, the cost of the AD is limited to
performing TRF inspections. We estimate that it will take about 3.0
work-hours per engine to perform the actions, including the TRF
inspections, and that the average labor rate is $80 per work-
[[Page 6420]]
hour. No parts are required. Based on these figures, we estimate the
total cost of the AD to U.S. operators to be $294,720.
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 summary of the costs to comply with this AD and
placed it in the AD Docket. You may get a copy of this summary at the
address listed under ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2008-03-09 CFM International, S.A.: Amendment 39-15359. Docket No.
FAA-2007-27229; Directorate Identifier 2007-NE-03-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective March
10, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to CFM International, S.A. CFM56-7B18, -
7B20, -7B22, -7B24, -7B26, -7B27, -7B22/B1, -7B24/B1, -7B26/B1, -
7B27/B1, -7B22/B2, -7B26/B2, -7B27/B3 turbofan engines with turbine
rear frame (TRF), part numbers 340-166-205-0, 340-166-206-0, 340-
166-207-0, 340-166-208-0, 340-166-209-0, and 340-166-210-0,
installed. These engines are installed on, but not limited to,
Boeing 737 series airplanes.
Unsafe Condition
(d) This AD results from a refined lifing analysis by the engine
manufacturer that shows the need to identify an initial threshold
for inspecting certain TRFs. We are issuing this AD to prevent
failure of the TRF from low-cycle fatigue cracks. Failure of the TRF
could result in engine separation from the airplane, which could
lead to loss of control of the airplane.
Compliance
(e) You are responsible for having the actions required by this
AD performed within 30 days after the effective date of this AD,
unless the actions have already been done.
Mandatory Inspections
(f) Within the next 30 days after the effective date of this AD,
revise the applicable inspection program for the Business Jet and
Air Carrier engine models by adding the Mandatory Inspection
Intervals as specified in this AD, and revise the Airworthiness
Limitations Section (ALS) (chapter 05-21-03) of the CFM56-7B Engine
Shop Manual, CFMI-TP-SM.10 by adding the following:
TURBINE REAR FRAME WITH TANGENTIAL STRUTS--MANDATORY INSPECTIONS--
LIFE LIMITS
TASK 05-21-03-200-001
1. General
A. This section contains the FAA and EASA mandatory Eddy Current
inspection intervals for the turbine rear frame with tangential
struts. The inspection uses:
--A threshold limit, specified in flight cycles
--Inspection intervals, specified in flight cycles
B. The threshold limit is the timing of the first required
inspection. First inspection must be done before that part has
reached the threshold number of flight cycles.
C. The inspection intervals specify the timing of inspections to
be done after the threshold inspection has been reached. Inspections
are repetitive without any limit.
2. Mandatory Inspection Intervals for the Critical Areas of the
Turbine Rear Frame with Tangential Struts (4 Mount Struts, No. 1, 2,
15, and 16).
C. Turbine Rear Frame Part Numbers 340-166-205-0, 340-166-206-0,
340-166-207-0, 340-166-208-0, 340-166-209-0, 340-166-210-0, for all
CFM56-7B SAC engine models (except -7B27A engine models). Refer to
figure 805.
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Inspection threshold Inspection intervals Inspection
Figure index No. Inspection location (cycles since new) (cycles) reference
----------------------------------------------------------------------------------------------------------------
805...................... Strut/outer ring 25,000 * for -7B SAC Refer to Figure 806 Refer to SB 72-
fillet radius on (except business * for -7B SAC 0579.*
trailing edge (A). jet) engine models. (except business
jet) engine models.
Strut/hub fillet 19,000 * for -7B SAC Refer to Figure 807
radius on leading business jet engine * for -7B SAC
edge (B). models. business jet engine
models.
Strut/outer ring
fillet radius on
trailing edge (C1
below outer ring).
Strut/outer ring
fillet radius on
trailing edge (C2
above outer ring) .
----------------------------------------------------------------------------------------------------------------
Note: * Applicable to all inspection locations. If inspection is not performed, part must be removed.
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(g) After the effective date of this AD, we will not approve any
alternative inspection intervals for these parts except as provided
for in paragraph (j) of this AD.
TRFs With Unknown Cycles
(h) If you cannot establish the number of cycles accumulated
since new, remove or inspect the TRF within 300 cycles-in-service
after the effective date of this AD. The CFM56-7B Engine Shop Manual
(ESM) or air carrier's approved continuous airworthiness maintenance
program (CAMP) contains information for inspecting the TRF.
(i) You may install a TRF removed in paragraph (h) of this AD
after the TRF passes an initial inspection for cracks. The CFM56-7B
ESM or CAMP contains information on inspecting the TRF.
Alternative Methods of Compliance
(j) The Manager, Engine Certification Office, has the authority
to approve alternative methods of compliance for this AD if
requested using the procedures found in 14 CFR 39.19.
Maintaining Records of the Mandatory Inspections
(k) You have met the requirements of this AD by making the
changes to the Engine Shop Manual as specified in paragraph (f) of
this AD, and, for air carriers operating under part 121 of the
Federal Aviation Regulations (14 CFR part 121), by modifying your
continuous airworthiness maintenance plan to reflect those changes.
You must maintain records of the mandatory inspections that result
from those changes to the ALS according to the regulations governing
your operation. You do not need to record each inspection as
compliance to this AD. For air carriers operating under part 121,
you may use the system established to comply with section 121.369.
Related Information
(l) CFM International Service Bulletin CFM56-7B S/B 72-0579,
Revision 1, dated October 27, 2006, contains information about Eddy
Current inspection.
(m) Contact Antonio Cancelliere, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803; telephone (781) 238-
7751; fax (781) 238-7199, for more information about this AD.
Issued in Burlington, Massachusetts, on January 23, 2008.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E8-1830 Filed 2-1-08; 8:45 am]
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