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determined that air safety and the
public interest require adopting the AD
with the change described previously.
We have determined that this change
will neither increase the economic
burden on any operator nor increase the
scope of the AD.
Costs of Compliance
The following tables provide the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Action Work hour Average labor
rate per hour Parts Cost per
airplane
Number of
U.S.-registered
airplanes
Fleet cost
AFM revision (required by AD 2004–03–
02).
1 $65 None ........... $65 29 $1,885
Installation of ELACs having L83 or L91
software (new required action).
1 65 No charge ... 65 29 1,885
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Federal Register / Vol. 70, No. 127 / Tuesday, July 5, 2005 / Rules and Regulations 38581
ESTIMATED CONCURRENT SERVICE BULLETIN COSTS
Action Work hour Average labor
rate per hour Parts Cost per
airplane
Number of
U.S.-registered
airplanes
Fleet cost
Installation or ELACs having L81 software 1 $65 No charge ... $65 29 $1,885
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

Accordingly, under the authority
delegated to me by the Administrator,
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:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13 [Amended]

2. The FAA amends § 39.13 by
removing amendment 39–13446 (69 FR
5007, February 3, 2004) and adding the
following new airworthiness directive
(AD):
2005–13–39 Airbus: Amendment 39–14176.
Docket No. FAA–2005–20755;
Directorate Identifier 2004–NM–244—
AD.
Effective Date
(a) This AD becomes effective August 9,
2005.
Affected ADs
(b) This AD supersedes AD 2004–03–02,
amendment 39–13446.
Applicability: (c) This AD applies to Airbus
Model A321–111, –112, –131, –211, and –231
airplanes; certificated in any category; except
those with Airbus Modification 34043
installed in production.
Unsafe Condition
(d) This AD was prompted by issuance of
mandatory continuing airworthiness
information by a civil airworthiness
　
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