AD 2005-15-09

The FAA is adopting a new airworthiness directive (AD) for certain Airbus airplane models, as specified above. This AD requires modifying the thermal insulation system of certain fuselage frames, and modifying the fuselage drainage system. This AD also requires revising the FAA-approved maintenance inspection program to include inspections for corrosion or cracking in the subject areas. This AD is prompted by reports of corrosion in the lower part of the pressure bulkhead at certain fuselage frames. We are issuing this AD to prevent accumulation of condensation in the insulation blankets of certain fuselage frames, which could cause corrosion that could result in reduced structural integrity of the fuselage and consequent rapid decompression of the airplane.

Final rule.

2005-15-09 Airbus: Amendment 39-14198. Docket No. FAA-2004-19534; Directorate Identifier 2004-NM-99-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective August 30, 2005.

Affected ADs

(b) None.

Applicability

(c) This AD applies to Airbus Model A300 B2-1A, B2-1C, B2K-3C, B4-2C, B4-103, and B4-203 airplanes; A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes; and A310-203, -204, -221, -222, -304, -322, -324, and - 325 airplanes; certificated in any category; except those on which both Airbus Modifications 5946 and 8057 were done during production.

Unsafe Condition

(d) This AD was prompted by reports of corrosion in the lower part of the pressure bulkhead at fuselage frames (FR) 39 and 54. We are issuing this AD to prevent accumulation of condensation in the insulation blankets of certain fuselage FRs, which could cause corrosion that could result in reduced structural integrityof the fuselage and consequent rapid decompression 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.

Modification of Thermal Insulation and Fuselage Drainage Systems

(f) Within 22 months after the effective date of this AD, modify the thermal insulation system of applicable fuselage frames and modify the fuselage drainage system, by doing all actions in the Accomplishment Instructions of the applicable service bulletins specified in Table 1 of this AD.

Table 1.--Relevant Service Bulletins

For Airbus models
Modify the thermal insulation system according to Airbus Service Bulletin
And modify the fuselage drainage system according to Airbus Service Bulletin
A300 B2 1A, B2 1C, B2K 3C, B4 2C, B4 103, and B4 203.
A300 21 0116, Revision 03, dated January 29, 2004.
A300 53 0201, Revision 05, dated July 15, 2004.
A300 B4 601, B4 603, B4 620, B4 622, B4 605R, B4 622R, F4 605R, F4 622R, and C4 605R Variant F.
A300 21 6025, Revision 02, dated January 29, 2004.
A300 53 6008, Revision 05, dated July 15, 2004.
A310 203, 204, 221, 222, 304, 322, 324, and 325.
A310 21 2041, Revision 03, dated January 29, 2004.
A300 53 2027, Revision 04, dated July 15, 2004.

Modifications Accomplished According to Previous Issues of Service Bulletins

(g) Modifications accomplished before the effective date of this AD according to the service bulletins listed in Table 2 are considered acceptable for compliance with the corresponding action specified in paragraph (f) of this AD.

Table 2.--Additional Service Bulletins

Models
Airbus Service Bulletin
Revision level
Date
A300 B2 1A, B2 1C, B2K 3C, B4 2C, B4 103, and B4 203
A300 21 116
1
March 24, 1992.
A300 B2 1A, B2 1C, B2K 3C, B4 2C, B4 103, and B4 203
A300 21 0116
02
June 13, 2003.
A300 B2 1A, B2 1C, B2K 3C, B4 2C, B4 103, and B4 203
A300 53 0201
04
May 2, 2003.
A300 B4 601, B4 603, B4 620, B4 622, B4 605R, F4 605R, F4 622R, B4 622R, and C4 605R Variant F.
A300 21 6025
01
June 13, 2003.
A300 B4 601, B4 603, B4 620, B4 622, B4 605R, F4 605R, F4 622R, B4 622R, and C4 605R Variant F.
A300 53 6008
02
August 10, 1989.
A300 B4 601, B4 603, B4 620, B4 622, B4 605R, F4 605R, F4 622R, B4 622R, and C4 605R Variant F.
A300 53 6008
03
November 6, 1990.
A300 B4 601, B4 603, B4 620, B4 622, B4 605R, F4 605R, F4 622R, B4 622R, and C4 605R Variant F.
A300 53 6008
04
April 28, 2003.
A310 203, 204, 221, 222, 304, 322, 324, and 325
A310 21 2041
1
December 10, 1990.
A310 203, 204, 221, 222, 304, 322, 324, and 325
A310 21 2041
02
June 13, 2003.
A310 203, 204, 221, 222, 304, 322, 324, and 325
A310 53 2027
2
November 6, 1990.
A310 203, 204, 221, 222, 304, 322, 324, and 325
A310 53 2027
03
May 2, 2003.

Maintenance Program Revision

(h) Within 90 days after doing the actions required by paragraph (f) of this AD, or within 90 days after the effective date of this AD, whichever is later: Incorporate into the FAA-approved maintenance inspection program repetitive detailed inspections for corrosion or cracking of fuselage structure from FR 38.2 to 39, and at FR 54, as applicable, as described in Airbus Maintenance Planning Document Task Numbers 538295-0603-1 (for Airbus Model A300 B2-1A, B2-1C, B2K-3C, B4-2C, B4-103, and B4-203 airplanes), and 531531-01-1 and 531533-01-1 (for Airbus Model A300 B4-601, B4-603, B4-620, B4- 622, B4-605R, F4-605R, F4-622R, B4-622R, and C4-605R Variant F airplanes; and A310-203, -204, -221, -222, -304, -322, -324, and - 325 airplanes). Then, thereafter, comply with the applicable requirements.

Note 1: For the purposes of this AD, a detailed inspection is: "An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required."

Alternative Methods of Compliance (AMOCs)

(i) 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.

Related Information

(j) French airworthiness directive 2003-317(B), dated August 20, 2003, also addresses the subject of this AD.

Material Incorporated by Reference

(k) You must use the service information that is specified in Table 3 of this AD to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approves the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of the service information, contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. To view the AD docket, go to the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW, room PL-401, Nassif Building, Washington, DC. To review copies of the service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Table 3.--Material Incorporated by Reference

Airbus Service Bulletin
Revision level
Date
A300 21 0116
Revision 03
January 29, 2004.
A300 21 6025
Revision 02
January 29, 2004.
A300 53 0201
Revision 05
July 15, 2004.
A300 53 6008
Revision 05
July 15, 2004.
A310 21 2041
Revision 03
January 29, 2004.
A310 53 2027
Revision 04
July 15, 2004.

The FAA proposed to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) with an AD for certain Airbus Model A300 B2 and B4 series airplanes; Model A300 B4-600, B4- 600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called A300-600 series airplanes); and Model A310-200 and -300 series airplanes. That proposed AD was published as a supplemental notice of proposed rulemaking (NPRM) in the Federal Register on May 18, 2005 (70 FR 28491). The supplemental NPRM proposed to require modifying the thermal insulation system of certain fuselage frames, and modifying the fuselage drainage system. The supplemental NPRM also proposed to require revising the FAA-approved maintenance inspection program to include inspections for corrosion or cracking in the subject areas.

Comments

We provided the public the opportunity to participate in the development of this AD. No comments have been submitted on the supplemental NPRM or on the determination of the cost to the public. Comments submitted on the original NPRM were addressed in the supplemental NPRM.

Explanation of Change to Applicability

We have revised the applicability of this AD to identify model designations as published in the most recent type certificate data sheet for the affected models.

Conclusion

We have carefully reviewed the available data, and 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 table provides the estimated costs for U.S. operators to comply with this AD, at an average labor rate of $65 per work hour.

Action
Models
Work hours
Parts
Cost per airplane
Number of U.S.-registered airplanes
Fleet cost
Modifying the Thermal Insulation System
A300 B2/B4 series5
$567
$892
23
$20,516
Modifying the Thermal Insulation System
A300 600 series
4
567
827
116
95,932
Modifying the Thermal Insulation System
A310 200 and 300 series
4
567
827
47
38,869
Modifying the Fuselage Drainage System
A300 B2/B4 series
38
1,857
4,327
23
99,521
Modifying the Fuselage Drainage System
A300 600 series
36
1,378
3,718
116
431,288
Modifying the Fuselage Drainage System
A310 200 and 300 series
27
1,451
3,206
47
150,682
Maintenance Program Revision
All

(1)
65
186
12,090
1 None.

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.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive: