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Federal Aviation Regulations [14 CFR
121.369 (c)]; however, the alternate system
must be accepted by the appropriate PMI and
require the maintenance records be
maintained either indefinitely or until the
work is repeated. Records of the piece-part
inspections are not required under § 121.380
(a) (2) (vi) of the Federal Aviation
Regulations [14 CFR 121.380 (a) (2) (vi)]. All
other Operators must maintain the records of
mandatory inspections required by the
applicable regulations governing their
operations.
Note 3: The requirements of this AD have
been met when the engine manual changes
are made and air carriers have modified their
continuous airworthiness maintenance plans
to reflect the requirements in the engine
manuals.
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50910 Federal Register / Vol. 66, No. 194 / Friday, October 5, 2001 / Proposed Rules
Issued in Burlington, Massachusetts, on
October 1, 2001.
Jay J. Pardee,
Manager, Engine and Propeller Directorate,
Aircraft Certification Service.
[FR Doc. 01–25080 Filed 10–4–01; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98–ANE–38–AD]
RIN 2120–AA64
Airworthiness Directives;
Airworthiness Directives; CFM
International (CFMI) CFM56–2, –2A,
–2B, –3, –3B, –3C, –5, –5B, –5C, and
–7B Series Turbofan Engines
AGENCY: Federal Aviation
Administration, DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
SUMMARY: The Federal Aviation
Administration (FAA) proposes to
supersede an existing airworthiness
directive (AD), that is applicable to
certain CFM International (CFMI)
CFM56 series turbofan engines, that
currently requires revisions to the
Airworthiness Limitations Section of
applicable Engine Shop Manuals
(ESM’s) to include required enhanced
inspection of selected critical lifelimited
parts at each piece-part
exposure. This proposal would modify
the airworthiness limitations section of
the manufacturer’s manual and an air
carrier’s approved continuous
airworthiness maintenance program to
incorporate additional inspection
requirements. The actions specified by
this proposed AD are intended to
prevent critical life-limited rotating
engine part failure, which could result
in an uncontained engine failure and
damage to the airplane.
DATES: Comments must be received by
December 4, 2001.
ADDRESSES: Submit comments in
triplicate to the Federal Aviation
Administration (FAA), New England
Region, Office of the Regional Counsel,
Attention: Rules Docket No. 98–ANE–
38–AD, 12 New England Executive Park,
Burlington, MA 01803–5299. Comments
may also be sent via the Internet using
the following address: ‘‘9-aneadcomment@
faa.gov’’. Comments sent
via the Internet must contain the docket
number in the subject line. Comments
may be inspected at this location by
appointment between 8:00 a.m. and 4:30
p.m., Monday through Friday, except
Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Diane Cook, Aerospace Engineer, Engine
Certification Office, FAA, Engine and
Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803–
5299; telephone (781) 238–7138, fax
(781) 238–7199.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested persons are invited to
participate in the making of the
proposed rule by submitting such
written data, views, or arguments as
they may desire. Communications
should identify the Rules Docket
number and be submitted in triplicate to
the address specified above. All
communications received on or before
the closing date for comments, specified
above, will be considered before taking
action on the proposed rule. The
proposals contained in this action may
be changed in light of the comments
received.
Comments are specifically invited on
the overall regulatory, economic,
environmental, and energy aspects of
the proposed rule. All comments
submitted will be available, both before
and after the closing date for comments,
in the Rules Docket for examination by
interested persons. A report
summarizing each FAA-public contact
　
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