Airworthiness Directives; Airbus Model A320 Series Airplanes, 75432-75433 [E6-21354]

Agencies

• Federal Aviation Administration
• DEPARTMENT OF TRANSPORTATION

[Federal Register Volume 71, Number 241 (Friday, December 15, 2006)]
[Proposed Rules]
[Pages 75432-75433]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-21354]


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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. 71, No. 241 / Friday, December 15, 2006 / 
Proposed Rules

[[Page 75432]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-26595; Directorate Identifier 2006-NM-208-AD]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A320 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Airbus Model A320 series airplanes. This proposed AD would 
require replacing the carbon fiber reinforced plastic (CFRP) actuator 
fittings of the rudder with aluminum actuator fittings and doing 
related investigative and corrective actions. This proposed AD results 
from rupture of a CFRP actuator fitting during maintenance. We are 
proposing this AD to prevent rupture of a rudder actuator fitting, 
which could result in reduced controllability of the airplane.

DATES: We must receive comments on this proposed AD by January 16, 
2007.

ADDRESSES: Use one of the following addresses to submit comments on 
this proposed AD.
     DOT Docket Web site: Go to https://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, 
Washington, DC 20590.
     Fax: (202) 493-2251.
     Hand Delivery: Room PL-401 on the plaza level of the 
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, 
France, for service information identified in this proposed AD.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
227-2125; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to submit any relevant written data, views, or 
arguments regarding this proposed AD. Send your comments to an address 
listed in the ADDRESSES section. Include the docket number ``FAA-2006-
26595; Directorate Identifier 2006-NM-208-AD'' at the beginning 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://
dms.dot.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 
that Web site, anyone can find and read the comments in any of our 
dockets, including 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), or you 
may visit https://dms.dot.gov.

Examining the Docket

    You may 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 DOT 
street address stated in the ADDRESSES section. Comments will be 
available in the AD docket shortly after the Docket Management System 
receives them.

Discussion

    The European Aviation Safety Agency (EASA), which is the 
airworthiness authority for the European Union, notified us that an 
unsafe condition may exist on certain Airbus Model A320 series 
airplanes. The EASA advises that a carbon fiber plastic reinforced 
(CFRP) actuator fitting of the rudder ruptured during incorrect 
accomplishment of airplane maintenance task 27-21-00-710-001. 
Investigation revealed that the CFRP actuator fittings cannot sustain 
limit loads resulting from ground gust conditions due to design of the 
fitting. Rupture of a rudder actuator fitting, if not corrected, could 
result in reduced controllability of the airplane.

Relevant Service Information

    Airbus has issued Service Bulletin A320-55-1030, dated March 6, 
2006. The service bulletin describes procedures for replacing all three 
of the CFRP actuator fittings of the rudder with aluminum actuator 
fittings and doing related investigative and corrective actions. The 
related investigative action is an inspection of the bushings to ensure 
that they are not elongated or out of measurement. The corrective 
action is to replace any damaged bushing with a new bushing. 
Accomplishing the actions specified in the service information is 
intended to adequately address the unsafe condition. The EASA mandated 
the service information and issued airworthiness directive 2006-0262, 
dated August 25, 2006, to ensure the continued airworthiness of these 
airplanes in the European Union.

FAA's Determination and Requirements of the Proposed AD

    This airplane model is manufactured in France 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. As described in FAA 
Order 8100.14A, ``Interim Procedures for Working with the European 
Community on Airworthiness Certification and Continued Airworthiness,'' 
dated August 12, 2005, the EASA has kept the FAA informed of the 
situation described above. We have

[[Page 75433]]

examined the EASA's findings, evaluated all pertinent information, and 
determined that we need to issue an AD for airplanes of this type 
design that are certificated for operation in the United States.
    Therefore, we are proposing this AD, which would require 
accomplishing the actions specified in the service information 
described previously.

Costs of Compliance

    This proposed AD would affect about 38 airplanes of U.S. registry. 
The proposed action would take about 100 work hours per airplane, at an 
average labor rate of $80 per work hour. Required parts would cost 
about $6,310 per airplane. Based on these figures, the estimated cost 
of the proposed AD for U.S. operators is $543,780, or $14,310 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 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 
regulation:
    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. 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 proposed AD and placed it in the AD docket. 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 FAA 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 Federal Aviation Administration (FAA) amends Sec.  39.13 by 
adding the following new airworthiness directive (AD):

Airbus: Docket No. FAA-2006-26595; Directorate Identifier 2006-NM-
208-AD.

Comments Due Date

    (a) The FAA must receive comments on this AD action by January 
16, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Airbus Model A320 series airplanes, 
certificated in any category; except those on which Airbus 
Modification 21733 or 21999 has been incorporated in production.

Unsafe Condition

    (d) This AD results from rupture of a carbon fiber reinforced 
plastic (CFRP) actuator fitting during maintenance. We are issuing 
this AD to prevent rupture of a rudder actuator fitting, which could 
result in reduced controllability of 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.

Replacement of Rudder Actuator Fittings

    (f) Within 9,000 flight cycles or 12,000 flight hours, or 60 
months after the effective date of this AD, whichever occurs first: 
Replace all of the CFRP actuator fittings of the rudder with 
aluminum actuator fittings and do all the related investigative 
actions, by accomplishing all of the actions specified in Airbus 
Service Bulletin A320-55-1030, dated March 6, 2006. Do any 
applicable corrective actions before further flight in accordance 
with the Accomplishment Instructions of the service bulletin.

Alternative Methods of Compliance (AMOCs)

    (g)(1) The Manager, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, has the authority to approve AMOCs for 
this AD, if requested in accordance with the procedures found in 14 
CFR 39.19.
    (2) Before using any AMOC approved in accordance with Sec.  
39.19 on any airplane to which the AMOC applies, notify the 
appropriate principal inspector in the FAA Flight Standards 
Certificate Holding District Office.

Related Information

    (h) European Aviation Safety Agency (EASA) airworthiness 
directive 2006-0262, dated August 25, 2006, also addresses the 
subject of this AD.

    Issued in Renton, Washington, on November 27, 2006.
Ali Bahrami,
Manager Transport Airplane Directorate, Aircraft Certification Service.
 [FR Doc. E6-21354 Filed 12-14-06; 8:45 am]
BILLING CODE 4910-13-P