Published 2001-08-06 · Federal Register document 01-19252
Airworthiness Directives; BAe Systems (Operations) Limited Model Avro 146-RJ Series Airplanes
Publication summary
This amendment adopts a new airworthiness directive (AD), applicable to certain BAe Systems (Operations) Limited Model Avro 146- RJ series airplanes, that requires modification of the passenger service units. The actions specified by this AD are intended to prevent failure of the passenger service units to deliver oxygen to the passengers in the event of decompression of the airplane, which could result in injury to the passengers. This action is intended to address the identified unsafe condition.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:03.835669+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2001-8d66ddb74aa17366
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- 8d66ddb74aa17366596c5f6ccb4e6d04532df19ae027b6fa003379bdedb52c7e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2001-15-28
- Effective date printed in this edition
- 2001-09-10
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Read 2 complete recorded clauses
Applicability wording · Applicability
Applicability: Model Avro 146-RJ series airplanes, certificated
in any category, as listed in BAe Systems (Operations) Limited
Service Bulletin SB.25-418-36215A, Revision 1, dated October 17,
2000.
Note 1: This AD applies to each airplane 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
[[Page 40870]]
airplanes 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 method of
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.
Exact source excerpt. Text positions 5643–6612, end exclusive, in the original decoded publication. SHA-256: 4a0ff33a9b09c7c1f911adae5c12b8caa6ac72b16dce63fa7671d8168c5776f5
Compliance and requirements
Compliance: Required as indicated, unless accomplished
previously.
To prevent failure of the passenger service units (PSUs) to
deliver oxygen to the passengers in the event of decompression of
the airplane, which could result in injury to the passengers,
accomplish the following:
Modification
(a) Within 90 days after the effective date of this AD, modify
the PSUs by relocating the lanyard, in accordance with Bae Systems
(Operations) Limited Service Bulletin SB.25-418-36215A, dated April
5, 2000; or Revision 1, dated October 17, 2001.
Alternative Methods of Compliance
(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 the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager, International
Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(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 airplane to a location where
the requirements of this AD can be accomplished.
Incorporation by Reference
(d) The modification shall be done in accordance with BAe
Systems (Operations) Limited Service Bulletin SB.25-418-36215A,
dated April 5, 2000; or BAe Systems (Operations) Limited Service
Bulletin SB.25-418-36215A, Revision 1, dated October 17, 2000.
Revision 1 of BAe Systems (Operations) Limited Service Bulletin
SB.25-418-36215A contains the following effective pages:
----------------------------------------------------------------------------------------------------------------
Page No. Revision level shown on page Revision date
----------------------------------------------------------------------------------------------------------------
1, 9.................................... 1.............................. October 17, 2000.
2-8, 10, 11............................. Original....................... April 5, 2000.
----------------------------------------------------------------------------------------------------------------
(The revision date is listed only on the first page of the document;
no other page contains this information.) 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 Office of the Federal
Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Note 3: The subject of this AD is addressed in British
airworthiness directive 004-04-2000.
Effective Date
(e) This amendment becomes effective on September 10, 2001.
Exact source excerpt. Text positions 6612–9892, end exclusive, in the original decoded publication. SHA-256: bd31435763dc9bca2b2b8bec8b2604fde43be6ba1d5e3e531a34983cd5de0b44
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 2001-15-28 · 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: b2dc922fe19c7508ac43a43fb72100be32db4d65d0d42e74f53e7f60cc4fb3cd. Source manifest: 871655d848d7abc94d5b721b9bb9c76b8995709bbd8e35f7cb52bbc50d11d20a.
Official source · 2001-08-06
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 66, Number 151 (Monday, August 6, 2001)]
[Rules and Regulations]
[Pages 40869-40870]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-19252]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NM-211-AD; Amendment 39-12363; AD 2001-15-28]
RIN 2120-AA64
Airworthiness Directives; BAe Systems (Operations) Limited Model
Avro 146-RJ Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to certain BAe Systems (Operations) Limited Model Avro 146-
RJ series airplanes, that requires modification of the passenger
service units. The actions specified by this AD are intended to prevent
failure of the passenger service units to deliver oxygen to the
passengers in the event of decompression of the airplane, which could
result in injury to the passengers. This action is intended to address
the identified unsafe condition.
DATES: Effective September 10, 2001.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of September 10, 2001.
ADDRESSES: 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 Office of the Federal Register, 800 North Capitol
Street, NW., suite 700, Washington, DC.
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: 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 Avro 146-RJ series airplanes was published in the Federal
Register on May 1, 2001 (66 FR 21703). That action proposed to require
modification of the passenger service units.
Comments
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments have been received.
Conclusion
The FAA has determined that air safety and the public interest
require the adoption of the rule as proposed.
Cost Impact
The FAA estimates that 40 Model BAe Systems (Operations) Limited
Model Avro 146-RJ series airplanes of U.S. registry will be affected by
this AD, that it will take approximately 5 work hours per airplane to
accomplish the required actions, and that the average labor rate is $60
per work hour. Required parts will be provided at no cost to the
operators. Based on these figures, the cost impact of the AD on U.S.
operators is estimated to be $12,000, or $300 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 Impact
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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
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:
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. Section 39.13 is amended by adding the following new
airworthiness directive:
2001-15-28 BAE Systems (Operations) Limited (Formerly British
Aerospace Regional Aircraft): Amendment 39-12363. Docket 2000-NM-
211-AD.
Applicability: Model Avro 146-RJ series airplanes, certificated
in any category, as listed in BAe Systems (Operations) Limited
Service Bulletin SB.25-418-36215A, Revision 1, dated October 17,
2000.
Note 1: This AD applies to each airplane 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
[[Page 40870]]
airplanes 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 method of
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 failure of the passenger service units (PSUs) to
deliver oxygen to the passengers in the event of decompression of
the airplane, which could result in injury to the passengers,
accomplish the following:
Modification
(a) Within 90 days after the effective date of this AD, modify
the PSUs by relocating the lanyard, in accordance with Bae Systems
(Operations) Limited Service Bulletin SB.25-418-36215A, dated April
5, 2000; or Revision 1, dated October 17, 2001.
Alternative Methods of Compliance
(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 the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager, International
Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(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 airplane to a location where
the requirements of this AD can be accomplished.
Incorporation by Reference
(d) The modification shall be done in accordance with BAe
Systems (Operations) Limited Service Bulletin SB.25-418-36215A,
dated April 5, 2000; or BAe Systems (Operations) Limited Service
Bulletin SB.25-418-36215A, Revision 1, dated October 17, 2000.
Revision 1 of BAe Systems (Operations) Limited Service Bulletin
SB.25-418-36215A contains the following effective pages:
----------------------------------------------------------------------------------------------------------------
Page No. Revision level shown on page Revision date
----------------------------------------------------------------------------------------------------------------
1, 9.................................... 1.............................. October 17, 2000.
2-8, 10, 11............................. Original....................... April 5, 2000.
----------------------------------------------------------------------------------------------------------------
(The revision date is listed only on the first page of the document;
no other page contains this information.) 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 Office of the Federal
Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
Note 3: The subject of this AD is addressed in British
airworthiness directive 004-04-2000.
Effective Date
(e) This amendment becomes effective on September 10, 2001.
Issued in Renton, Washington, on July 25, 2001.
Vi L. Lipski,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 01-19252 Filed 8-3-01; 8:45 am]
BILLING CODE 4910-13-P
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