AD 2006-25-10

Airworthiness directive · Lift spoiler jack · BAE Systems Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A and 3 more

Effective
January 16, 2007
Published
December 12, 2006 · 71 FR 74464–74466
Issued
December 1, 2006
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
39-14851
Docket
FAA-2006-25920
Project
2006-NM-137-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document E6-20952. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ airplanes. This AD requires calculating the current life of each lift spoiler jack, and eventually replacing each lift spoiler jack. This AD results from a review of all system components as part of the life-extension program for the affected airplanes that indicated the fatigue life limit of certain lift spoiler jacks cannot be extended from the current life limit. We are issuing this AD to prevent failure of the lift spoiler jack, and consequent increased drag and uncommanded roll inputs, which could reduce the flightcrew's ability to control the airplane.

The airworthiness directive

2006-25-10 BAE Systems (Operations) Limited (Formerly British Aerospace Regional Aircraft): Amendment 39-14851. Docket No. FAA-2006-25920; Directorate Identifier 2006-NM-137-AD.

(a) Effective Date

PDF page 2

(a) This AD becomes effective January 16, 2007.

(b) Affected ADs

PDF page 2

(b) None.

(c) Applicability

PDF page 2

(c) This AD applies to the airplanes specified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, having lift spoiler jacks with part number (P/N) P308-45-0002, P308-45-0102, or P308-45-0202.

(1) All BAE Systems (Operations) Limited Model BAe 146-100A, -200A, and -300A series airplanes.

(2) All Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes.

(d) Unsafe Condition

PDF page 2

(d) This AD results from a review of all system components as part of the life-extension program for the affected airplanes that indicated the fatigue life of certain lift spoiler jacks cannot be extended from the current life limit. We are issuing this AD to prevent failure of the lift spoiler jack, and consequent increased drag and uncommanded roll inputs, which could reduce the flightcrew's ability to control the airplane.

(e) Compliance

PDF page 2

(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.

(f) Calculating the Life Limit

PDF page 2

(f) Within 18 months after the effective date of this AD: Calculate the current life of each lift spoiler jack in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Modification Service Bulletin ISB.27-178, dated January 14, 2005.

Note 1:

BAE Systems (Operations) Limited Modification Service Bulletin ISB.27-178 refers to the service information listed in Table 1 of this AD as additional sources of service information for the actions in paragraphs (f) and (g) of this AD.

Table 1.—Additional Sources of Service Information
This service document—Is an additional source of service information for—
BAE Systems (Operations) Limited Modification Service Bulletin SB.27-179-70675A, dated January 19, 2005Replacing lift spoiler jacks having P/N P308-45-0002 and -0102.
BAE Systems (Operations) Limited Inspection Service Bulletin ISB.05-005, Revision 1, dated June 9, 2005Calculating the theoretical life when complete utilization records do not exist.
Smiths Service Newsletter P308-27-003, dated March 12, 2004Resolving anomalies with the P/Ns.

(g) Replacement

PDF page 2

(g) Within 18 months after the effective date of this AD or before the accumulation of 55,000 total flight cycles on the lift spoiler jack, whichever occurs later: Replace each P/N P308-45-0002, P308-45-0102, or P308-45-0202 lift spoiler jack with a serviceable unit, in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Modification Service Bulletin ISB.27-178, dated January 14, 2005. Thereafter, replace each lift spoiler jack with a serviceable unit at intervals not to exceed 55,000 flight cycles.

(h) Alternative Methods of Compliance (AMOCs)

PDF page 2

(h)(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 § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office.

(i) Related Information

PDF page 2

(i) European Aviation Safety Agency airworthiness directive 2006-0138, dated May 23, 2006, also addresses the subject of this AD.

(j) Material Incorporated by Reference

PDF page 2

(j) You must use BAE Systems (Operations) Limited Modification Service Bulletin ISB.27-178, dated January 14, 2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at 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.

Rule preamble

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

DatesPage 1

This AD becomes effective January 16, 2007.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of January 16, 2007.

AddressesPage 1

You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC.

Contact British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171, for service information identified in this AD.

For further information contactPage 1

Todd Thompson, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149.

Examining the DocketPage 1

You may examine the airworthiness directive (AD) docket on the Internet at http://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 street address stated in the ADDRESSES section.

DiscussionPage 1

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to all BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146-RJ airplanes. That NPRM was published in the Federal Register on September 28, 2006 (71 FR 56903). That NPRM proposed to require calculating the current life of each lift spoiler jack, and eventually replacing each lift spoiler jack.

CommentsPage 1

We provided the public the opportunity to participate in the development of this AD. We received no comments on the NPRM or on the determination of the cost to the public.

ConclusionPage 1

We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed.

Costs of CompliancePage 1

The following table provides the estimated costs for U.S. operators to comply with this AD.

Estimated Costs
ActionWork hoursAverage labor rate per hourPartsCost per airplaneNumber of U.S.-registered airplanesFleet cost
Determine the life of each lift spoiler jack1$80None$8053$4,240
Replace each lift spoiler jack (6 per airplane)680$102,000102,480535,431,440
Authority for This RulemakingPage 2

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 findingsPage 2

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 and placed it in the AD docket. See the ADDRESSES section for a location to examine the regulatory evaluation.

Adoption of the amendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

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

2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD):

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