Published 2005-04-25 · Federal Register document 05-8096
Airworthiness Directives; BAE Systems (Operations) Limited Model Avro 146-RJ Series Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all BAE Systems (Operations) Limited Model Avro 146-RJ series airplanes. This AD requires an inspection of the Thales Avionics distance bearing indicator (DBI) to determine part number (P/N) and serial number (S/N), and replacement of the affected DBI with a new or modified DBI. This AD is prompted by a report of defective electrical insulators in DBIs. We are issuing this AD to prevent a short circuit in the DBI due to defective electrical insulation, which could potentially cause a loss of primary navigation instruments (such as airspeed indicator, altimeter, and global positioning system (GPS) information).
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:17.300228+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2005-5d43d153038ee1c1
- Source row
- results[168]
- Raw source SHA-256
- 5d43d153038ee1c1c214f5c3688e38e25e37b832227fe65d52f7420a65ee20f2
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2005-08-16
- Effective date printed in this edition
- 2005-05-31
Read 11 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective May 31, 2005.
Exact source excerpt. Text positions 7191–7256, end exclusive, in the original decoded publication. SHA-256: 2f318769074f4f10bfa8cbfbdad4bcf60adbf6e8cd3f3ee9d684bda8fa48a0f1
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 7256–7285, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to all BAE Systems (Operations) Limited
Model Avro 146-RJ series airplanes, certificated in any category.
Exact source excerpt. Text positions 7285–7432, end exclusive, in the original decoded publication. SHA-256: 6debced1b50137e188b9ec85fdeecb75e7ebef6767dfe24a7a9035985f43bf08
Unsafe Condition
Unsafe Condition
(d) This AD was prompted by a report of defective electrical
insulators in distance bearing indicators (DBI). We are issuing this
AD to prevent a short circuit in the DBI due to defective electrical
insulation, which could potentially cause a loss of primary
[[Page 21139]]
navigation instruments (such as airspeed indicator, altimeter, and
global positioning system (GPS) information).
Exact source excerpt. Text positions 7432–7848, end exclusive, in the original decoded publication. SHA-256: 0b50d6c590f2d1b7ef7bf6d666843b1fe0f48e98ccbba8104e5c0b297f5be59e
Compliance
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.
Exact source excerpt. Text positions 7848–8026, end exclusive, in the original decoded publication. SHA-256: 64a7a1579f37f56eafecd0aeb3c528e7c89f6292ed0cb53091423917642d5847
Part Number Inspection
Part Number Inspection
(f) Within four months after the effective date of this AD,
inspect the Thales Avionics DBI to determine whether a part number
(P/N) and serial number (S/N) listed in the Effectivity of BAE
Systems (Operations) Limited Modification Service Bulletin SB.34-
371-70671A, dated September 19, 2003, is installed. Instead of an
inspection of the DBI, a review of airplane maintenance records is
acceptable if the P/N and the S/N of the DBI can be positively
determined from that review.
(1) If the DBI P/N and S/N do not match those listed in the
service bulletin, no further action is required by this paragraph.
(2) If the DBI P/N and S/N do match those listed in the service
bulletin, within four months after the effective date of this AD,
replace the DBI in accordance with the Accomplishment Instructions
of the service bulletin. The replacement part must be either a new
DBI having P/N 63543-280-1 and a S/N not listed in the service
bulletin, or a new DBI having P/N 63543-280-2.
Exact source excerpt. Text positions 8026–9057, end exclusive, in the original decoded publication. SHA-256: f113a63750ae0581232687f8fb5816a2adf9ea9a3215522c003698849bc898c4
Parts Installation
Parts Installation
(g) As of the effective date of this AD, no person may install a
DBI with a P/N and S/N listed in the Effectivity of BAE Systems
(Operations) Limited Modification Service Bulletin SB.34-371-70671A,
dated September 19, 2003, on any airplane unless the DBI has been
modified in accordance with paragraph (f)(2) of this AD.
Exact source excerpt. Text positions 9057–9407, end exclusive, in the original decoded publication. SHA-256: edc7f6100f5a69e82ab6c4e319a67dd9ac924222583ba6401d7ab86254d876f5
No Reporting
No Reporting
(h) Although the service bulletin references a reporting
requirement in paragraph 2.C.2, ``Documentation,'' that reporting is
not required by this AD.
Exact source excerpt. Text positions 9407–9579, end exclusive, in the original decoded publication. SHA-256: 539fb8a0d9a31c040665f6552065e53e1c5e5e27c514ce8994cc8fab9ec7daa6
Alternative Methods of Compliance (AMOCs)
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.
Exact source excerpt. Text positions 9579–9833, end exclusive, in the original decoded publication. SHA-256: b6ab6b0f246045bba5ba60b95f93a07e33abbbf0018f2163c3bb312358ce2da4
Related Information
Related Information
(j) British airworthiness directive G-2004-0006, dated March 2,
2004, also addresses the subject of this AD.
Exact source excerpt. Text positions 9833–9969, end exclusive, in the original decoded publication. SHA-256: f092424cde937f445a6f096ad584fb89d0f3158578ada7e194405bc4addd3552
Material Incorporated by Reference
Material Incorporated by Reference
(k) You must use BAE Systems (Operations) Limited Modification
Service Bulletin SB.34-371-70671A, dated September 19, 2003, 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 this document in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. To get copies of the service
information, contact British Aerospace Regional Aircraft American
Support, 13850 Mclearen Road, Herndon, Virginia 20171. To view the
AD docket, contact 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, contact 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.
Exact source excerpt. Text positions 9969–10995, end exclusive, in the original decoded publication. SHA-256: 4322ab5286c533cac98d265698f3d9d5da11c8ac1e7ff22408201c01084694d8
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2005-08-16 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: bc5c54facf62233e91934852fc3ddb9a08fad4fac3ae40160987074b406171e0. Source manifest: 102956ee171cf8acc9bf711ab0a18bd2998c9c3f6cea8bee52a76de2ae26d859.
Official source · 2005-04-25
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 70, Number 78 (Monday, April 25, 2005)]
[Rules and Regulations]
[Pages 21137-21139]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-8096]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20078; Directorate Identifier 2004-NM-210-AD;
Amendment 39-14068; AD 2005-08-16]
RIN 2120-AA64
Airworthiness Directives; BAE Systems (Operations) Limited Model
Avro 146-RJ Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
BAE Systems (Operations) Limited Model Avro 146-RJ series airplanes.
This AD requires an inspection of the Thales Avionics distance bearing
indicator (DBI) to determine part number (P/N)
[[Page 21138]]
and serial number (S/N), and replacement of the affected DBI with a new
or modified DBI. This AD is prompted by a report of defective
electrical insulators in DBIs. We are issuing this AD to prevent a
short circuit in the DBI due to defective electrical insulation, which
could potentially cause a loss of primary navigation instruments (such
as airspeed indicator, altimeter, and global positioning system (GPS)
information).
DATES: This AD becomes effective May 31, 2005.
The incorporation by reference of a certain publication listed in
the AD is approved by the Director of the Federal Register as of May
31, 2005.
ADDRESSES: For service information identified in this AD, contact
British Aerospace Regional Aircraft American Support, 13850 Mclearen
Road, Herndon, Virginia 20171.
Docket: The AD docket contains the proposed AD, comments, and any final
disposition. You can examine the 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 U.S.
Department of Transportation, 400 Seventh Street, SW., room PL-401,
Washington, DC. This docket number is FAA-2005-20078; the directorate
identifier for this docket is 2004-NM-210-AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with an AD for all BAE Systems (Operations) Limited Model Avro 146-RJ
series airplanes. That action, published in the Federal Register on
January 19, 2005 (70 FR 2987), proposed to require an inspection of the
Thales Avionics distance bearing indicator (DBI) to determine part
number (P/N) and serial number (S/N), and replacement of the affected
DBI with a new or modified DBI.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been submitted on the proposed
AD or on the determination of the cost to the public.
Clarification of Changes to Proposed AD
In addition to other minor editorial changes to the AD, additional
clarifications have been made.
The requirements of new paragraph (g) (``Parts Installation'') in
this final rule apply to all affected airplanes. Therefore, we revised
paragraph (f)(1) of the AD to properly limit those provisions (no
further action) to paragraph (f).
We revised paragraphs (f)(2) and (g) to clarify that the DBI
replacement is conditional on a finding of certain part/serial numbers.
We combined paragraph (f)(2) and (g), and redesignated the subsequent
paragraphs accordingly.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
changes described previously. We have determined that these changes
will neither increase the economic burden on any operator nor increase
the scope of the AD.
Costs of Compliance
This AD will affect about 54 airplanes of U.S. registry. The
required actions will take about 1 work hour per airplane, at an
average labor rate of $65 per work hour. Required parts will cost about
$728 per airplane. Based on these figures, the estimated cost of the AD
for U.S. operators is $42,822, or $793 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 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
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2005-08-16 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-14068. Docket No. FAA-
2005-20078; Directorate Identifier 2004-NM-210-AD.
Effective Date
(a) This AD becomes effective May 31, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BAE Systems (Operations) Limited
Model Avro 146-RJ series airplanes, certificated in any category.
Unsafe Condition
(d) This AD was prompted by a report of defective electrical
insulators in distance bearing indicators (DBI). We are issuing this
AD to prevent a short circuit in the DBI due to defective electrical
insulation, which could potentially cause a loss of primary
[[Page 21139]]
navigation instruments (such as airspeed indicator, altimeter, and
global positioning system (GPS) information).
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.
Part Number Inspection
(f) Within four months after the effective date of this AD,
inspect the Thales Avionics DBI to determine whether a part number
(P/N) and serial number (S/N) listed in the Effectivity of BAE
Systems (Operations) Limited Modification Service Bulletin SB.34-
371-70671A, dated September 19, 2003, is installed. Instead of an
inspection of the DBI, a review of airplane maintenance records is
acceptable if the P/N and the S/N of the DBI can be positively
determined from that review.
(1) If the DBI P/N and S/N do not match those listed in the
service bulletin, no further action is required by this paragraph.
(2) If the DBI P/N and S/N do match those listed in the service
bulletin, within four months after the effective date of this AD,
replace the DBI in accordance with the Accomplishment Instructions
of the service bulletin. The replacement part must be either a new
DBI having P/N 63543-280-1 and a S/N not listed in the service
bulletin, or a new DBI having P/N 63543-280-2.
Parts Installation
(g) As of the effective date of this AD, no person may install a
DBI with a P/N and S/N listed in the Effectivity of BAE Systems
(Operations) Limited Modification Service Bulletin SB.34-371-70671A,
dated September 19, 2003, on any airplane unless the DBI has been
modified in accordance with paragraph (f)(2) of this AD.
No Reporting
(h) Although the service bulletin references a reporting
requirement in paragraph 2.C.2, ``Documentation,'' that reporting is
not required by this AD.
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) British airworthiness directive G-2004-0006, dated March 2,
2004, also addresses the subject of this AD.
Material Incorporated by Reference
(k) You must use BAE Systems (Operations) Limited Modification
Service Bulletin SB.34-371-70671A, dated September 19, 2003, 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 this document in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. To get copies of the service
information, contact British Aerospace Regional Aircraft American
Support, 13850 Mclearen Road, Herndon, Virginia 20171. To view the
AD docket, contact 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, contact 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.
Issued in Renton, Washington, on April 14, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-8096 Filed 4-22-05; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:55:48.591493+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 69303be3f20b152a57a18fe0ff4b1ce16d49abe280c76df75486a6f458b4df85
- Text SHA-256
- bc5c54facf62233e91934852fc3ddb9a08fad4fac3ae40160987074b406171e0
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.