AD 98-24-27

Active

Fire Extinguisher

Key Information
98-24-27
Active
January 29, 1999
Not specified
98-ANE-29-AD
39-10914
Applicability
["Appliance"]
Not specified
328 Support Services GmbH Airbus SAS BAE Systems (Operations) Limited Bombardier Inc. Embraer S.A. First Technology Fire and Safety Ltd Fokker Services
328-100 328-300 A320-111 A320-211 A320-212 A320-214 A320-231 A320-232 A320-233 A330-201 A330-202 A330-203 A330-223 A330-223F A330-243 A330-243F A330-301 A330-302 A330-303 A330-321 A330-322 A330-323 A330-341 A330-342 BAe 146-100A BAe 146-200A BAe 146-300A CL-600-2B19 (Regional Jet Series 100) CL-600-2B19 (Regional Jet Series 440) EMB-145 Fire Extinguisher F.28 Mark 0070 F.28 Mark 0100 F.28 Mark 1000 F.28 Mark 2000 F.28 Mark 3000 F.28 Mark 4000 F27 Mark 050 F27 Mark 100 F27 Mark 200 F27 Mark 300 F27 Mark 400 F27 Mark 500 F27 Mark 600 F27 Mark 700
Summary

This amendment adopts a new airworthiness directive (AD) that is applicable to First Technology Fire and Safety Ltd. toilet compartment fire extinguishers. This amendment requires inspection of suspect fire extinguishers for leakage, and removal from service and replacement with serviceable parts if the extinguisher is found to be leaking. This amendment is prompted by reports of leakage at the fire extinguisher's eutectic tip. The leakage is the result of a design change. The actions specified by this AD are intended to prevent fire extinguisher failure due to leakage, which in the event of a toilet compartment fire could result in an uncontained fire and damage to the aircraft.

Action Required

Final rule.

Regulatory Text

98-24-27 First Technology Fire and Safety Ltd.: Amendment 39-10914. Docket No. 98-ANE-29-AD.

Applicability: First Technology Fire and Safety Ltd. toilet compartment fire extinguisher, identified by serial and model number in First Technology Fire and Safety Ltd. Service Bulletin (SB) No. 26-110, Revision 1, dated January 1998. These fire extinguishers are installed on but not limited to Airbus A320, A330, A340; British Aerospace Bae 146, Bombardier CL-600-2B19 (CRJ), Dornier 328 Embraer EMB 145, and all Fokker Series aircraft.

Note 1: This airworthiness directive (AD) applies to each fire extinguisher identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For fire extinguishers that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative methodof compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To prevent fire extinguisher failure due to leakage, which could result in an uncontained fire and damage to the aircraft, accomplish the following:

(a) Within 3 months after the effective date of this AD, perform a one time inspection of fire extinguishers for leakage, and replace leaking fire extinguishers with serviceable parts, in accordance with First Technology Fire and Safety Ltd. SB No. 26-110, Revision 1, dated January 1998.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by theManager, Boston Aircraft Certification Office. Operators shall submit their request through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Boston Aircraft Certification Office.

Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Boston Aircraft Certification Office.

(c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the requirements of this AD can be accomplished.

(d) The actions required by this AD shall be done in accordance with First Technology Fire and Safety Ltd. SB:

Document No.
Pages
Revision
Date
26-110
1-4
1
January, 1998
Total pages: 4

This incorporation by reference was approved by the director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Percival Aviation Ltd., The Sidings, Knowle, Fareham, Hampshire PO17 5LZ England; telephone 011 44 1329 833814, fax 011 44 1329 834013. Copies may be examined at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA; or at the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on January 29, 1999.

Supplementary Information

A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain First Technology Fire and Safety Ltd. toilet compartment fire extinguishers, approved for installation on Airbus A320, A330, A340; British Aerospace Bae 146, Bombardier CL-600-2B19 (CRJ), Dornier 328, Embraer EMB 145, and all Fokker series airplanes, was published in the Federal Register on July 1, 1998 (63 FR 35884). That action proposed to require, within three months after the effective date of this AD, inspection of suspect fire extinguishers for leakage, and removal from service and replacement with serviceable parts if found leaking.

Interested persons have been afforded an opportunity to participate in the making of this amendment. Due consideration has been given to the comments received.

Two commenters indicate that they do not operate any of the affected airplanes.

One commenter doesnot concur with the 3 month compliance time. The initial compliance deadline, for the First Technology fire and Safety Service Bulletin (SB) No. 26-110, Revision 1, dated January 1998, was April 1998. This allowed a sufficient amount of time since issuance of the UK CAA AD to comply with the FAA AD. The commenter has since withdrawn the request for an extended compliance period. The commenter also requests that reference to Revision 1 of SB 26-110, dated January 1998, be made in the final rule since the SB dated January 1998, referenced in the Notice for Proposed Rulemaking (NPRM) is Revision 1. The FAA concurs. SB No. 26-110, Revision 1, dated January 1998 has been listed in the Applicability section.

One commenter disagrees with the 3 minute inspection compliance time. The 3 minute reference was for weighing the extinguisher. A reasonable time period for inspection, weighing, and replacement of the extinguisher is 20 minutes. The FAA concurs. The economic impact statement has been revised.

After careful review of the available data, including the comments noted above, the FAA has determined that air safety and the public interest require the adoption of the rule with the changes described previously. The FAA has determined that these changes will neither increase the economic burden on any operator nor increase the scope of the AD.

There are approximately 1,500 fire extinguishers of the affected design installed on the worldwide fleet. There are an unknown number of fire extinguishers installed on aircraft of U.S. registry. The FAA estimates that it would take approximately 20 minutes per fire extinguisher to accomplish the actions, and that the average labor rate is $60 per work hour. The manufacturer has advised the CAA that replacement parts would be provided at no charge to the operator. Based on these figures, the total cost impact of the AD on worldwide operators is estimated to be $30,000.

The regulations proposed herein wouldnot have substantial direct effects 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. Therefore, in accordance with Executive Order 12612, it is determined that this proposal would not have sufficient federalism implications to warrant the preparation of a Federalism Assessment.

For the reasons discussed above, I certify that this 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) if promulgated, 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. A copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption "ADDRESSES."

List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend part 39 of the Federal Aviation Regulations (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. Section 39.13 is amended by the following new airworthiness directive:

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
Contact Information

Terry Fahr, Aerospace Engineer, Boston Aircraft Certification Office,
FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone
(781) 238-7155, fax (781) 238-7199.

References
This information is not available.
--- - Part 39 [63 FR 65701]
Page 65701
FAA Documents