AD 2004-10-11

Airworthiness directive · Pacific Scientific engine fire extinguisher bottles · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more

Effective
June 25, 2004
Published
May 21, 2004 · 69 FR 29216–29217
Issued
May 10, 2004
Models
Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A, BAe 146-100A, BAe 146-200A, BAe 146-300A
Data sheet
TCDSA49EU
Registered aircraft
22 matched by model
Product
Aircraft · Large airplane
Amendment
39-13641
Docket
2002-NM-343-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 04-11283. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

This amendment adopts a new airworthiness directive (AD), applicable to certain BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ series airplanes equipped with Pacific Scientific engine fire extinguisher bottles. This amendment would require a one-time inspection to detect discrepancies in the wiring installation of the engine fire extinguisher bottles, and related investigative/corrective actions as necessary. This action is necessary to prevent the inability of the left-hand fire extinguisher on one or more engines to discharge, and consequent inability to control or suppress an engine fire. This action is intended to address the identified unsafe condition.

The airworthiness directive

2004-10-11 Bae Systems (Operations) Limited (Formerly British Aerospace Regional Aircraft): Amendment 39-13641. Docket 2002-NM-343-AD.

2. Section 39.13 is amended by adding the following new airworthiness directive:

Applicability: Model BAe 146 and Avro 146-RJ series airplanes, equipped with Pacific Scientific engine fire extinguisher bottles, and having BAE Systems (Operations) Limited Modification HCM01688A, and either HCM01582A or HCM01582B installed; certificated in any category;

Compliance: Required as indicated, unless accomplished previously.

To prevent the inability of the left-hand fire extinguisher bottle on one or more engines to discharge, and consequent inability to control or suppress an engine fire, accomplish the following:

(a) Inspection, Test, and Related Investigative/Corrective Actions

PDF page 1

(a) Within 6 months after the effective date of this AD: Do a one-time detailed inspection to detect discrepancies in the wiring installation of the fire extinguisher bottles for the engines, a one-time test of the wiring for the indicating system of the engine fire extinguishing system, and all applicable related investigative/corrective actions, per the Accomplishment Instructions of BAE Systems (Operations) Limited Inspection Service Bulletin ISB.26-065, dated September 16, 2002. Do all of the actions per the service bulletin. Any corrective actions must be done before further flight. Although the service bulletin specifies to submit certain information to the manufacturer, this AD does not include such a requirement.

Note 1:

For the purposes of this AD, a detailed inspection is defined as: “An intensive visual examination of a specific structural area, system, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at intensity deemed appropriate by the inspector. Inspection aids such as mirror, magnifying lenses, etc., may be used. Surface cleaning and elaborate access procedures may be required.”

(b) Credit for Actions Done per Other Service Information

PDF page 2

(b) For airplanes with BAE Systems (Operations) Limited Modification HCM01582B installed: Accomplishment of BAE Systems (Operations) Limited Inspections Service Bulletin 26-060 (Inspection for Cross Connection of Wiring on Pacific Scientific Fire Extinguishers) on each engine is considered acceptable for compliance with the requirements of this AD.

(c) Alternative Methods of Compliance

PDF page 2

(c) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD.

(d) Incorporation by Reference

PDF page 2

(d) Unless otherwise specified in this AD, the actions shall be done in accordance with BAE Systems (Operations) Limited Inspection Service Bulletin ISB.26-065, dated September 16, 2002. 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 British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Note 2:

The subject of this AD is addressed in British airworthiness directive 003-09-2002.

(e) Effective Date

PDF page 2

(e) This amendment becomes effective on June 25, 2004.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

Effective June 25, 2004.

The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of June 25, 2004.

AddressesPage 1

The service information referenced in this AD may be obtained from British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171. This information may be examined at the Federal Aviation Administration (FAA), Transport Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

For further information contactPage 1

Todd Thompson, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-1175; fax (425) 227-1149.

Supplementary informationPage 1

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 BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ series airplanes equipped with Pacific Scientific engine fire extinguisher bottles was published in the Federal Register on March 17, 2004 (69 FR 12585). That action proposed to require a one-time inspection to detect discrepancies in the wiring installation of the engine fire extinguisher bottles, and related investigative/corrective actions as necessary.

CommentsPage 1

Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were submitted in response to the proposal or the FAA's determination of the cost to the public.

ConclusionPage 1

The FAA has determined that air safety and the public interest require the adoption of the rule as proposed.

Cost impactPage 1

The FAA estimates that 54 airplanes of U.S. registry will be affected by this AD, that it will take approximately 3 work hours per airplane to accomplish the required actions, and that the average labor rate is $65 per work hour. Based on these figures, the cost impact of the AD on U.S. operators is estimated to be $10,530, or $195 per airplane.

The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. The cost impact figures discussed in AD rulemaking actions represent only the time necessary to perform the specific actions actually required by the AD. These figures typically do not include incidental costs, such as the time required to gain access and close up, planning time, or time necessitated by other administrative actions.

Regulatory impactPage 1

The regulations adopted herein 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.

For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption ADDRESSES.

Adoption of the AmendmentPage 1

Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

1. The authority citation for part 39 continues to read as follows:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 22

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • British Aerospace20 aircraft
  • BAE Systems2 aircraft
By year built
19852000
Registered aircraft by year built: 12 aircraft
19851
19861
19871
19881
19892
19952
19961
19981
19991
20001

10 with no year recorded

By model

Aircraft

See all 22 aircraft