[Federal Register Volume 65, Number 204 (Friday, October 20, 2000)]
[Rules and Regulations]
[Pages 62999-63001]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-26710]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000-NM-123-AD; Amendment 39-11937; AD 2000-21-05]
RIN 2120-AA64


Airworthiness Directives; British Aerospace BAe Model ATP 
Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments.

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SUMMARY: This amendment adopts a new airworthiness directive (AD), 
applicable to all British Aerospace BAe Model ATP airplanes. This 
action requires repetitive inspections to detect damage of the torque 
link apex joint of the left-and right-hand main landing gear (MLG); and 
replacement of nuts, pins, and bolts with new parts, if necessary. This 
action is necessary to prevent separation of the top and bottom torque 
links, and consequent loss of directional control of the MLG. This 
action is intended to address the identified unsafe condition.

DATES: Effective November 6, 2000.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of November 6, 2000.
    Comments for inclusion in the Rules Docket must be received on or 
before November 20, 2000.

ADDRESSES: Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Transport Airplane Directorate, ANM-114, 
Attention: Rules Docket No. 2000-NM-123-AD, 1601 Lind Avenue, SW.,

[[Page 63000]]

Renton, Washington 98055-4056. Comments may be inspected at this 
location between 9:00 a.m. and 3:00 p.m., Monday through Friday, except 
Federal holidays. Comments may be submitted via fax to (425) 227-1232. 
Comments may also be sent via the Internet using the following address: 
<a href="/cdn-cgi/l/email-protection#665f4b07084b0f071405090b0b0308122600070748010910"><span class="__cf_email__" data-cfemail="3a03175b5417535b48595557575f544e7a5c5b5b145d554c">[email protected]</span></a>. Comments sent via fax or the Internet must 
contain ``Docket No. 2000-NM-123-AD'' in the subject line and need not 
be submitted in triplicate. Comments sent via the Internet as attached 
electronic files must be formatted in Microsoft Word 97 for Windows or 
ASCII text.
    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 
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.

FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2110; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: The Civil Aviation Authority (CAA), which is 
the airworthiness authority for the United Kingdom, notified the FAA 
that an unsafe condition may exist on all British Aerospace BAe Model 
ATP airplanes. The CAA advises that it received reports of failures of 
the torque links of the main landing gear (MLG). The failures have 
occurred at the bolt assembly (apex joint) that attaches the top link 
to the bottom link. The failures are caused by wear in the threads of 
the pin and nut of the bolt assembly. This wear is caused by lateral 
oscillatory loading of the joint coupled with its normal movement as 
the MLG oleo compresses and extends. Excessive wear in the threads can 
result in loss of the nut and separation of the joint when the 
attachment pin migrates from its bushes in the torque links. Separation 
of the top and bottom torque links could result in loss of directional 
control of the MLG.

Explanation of Relevant Service Information

    British Aerospace has issued Service Bulletin ATP-32-99, dated 
February 21, 2000. The service bulletin references Messier-Dowty 
Service Bulletin 200-32-263, including Appendix A, dated February 1, 
2000, as an additional source of service information for accomplishment 
of the recommended actions. The Messier-Dowty service bulletin 
describes procedures for repetitive inspections to detect damage of the 
torque link apex joint of the left-and right-hand MLG; and replacement 
of nuts, pins, and bolts with new parts, if necessary.
    The CAA classified the British Aerospace service bulletin as 
mandatory and issued British airworthiness directive 008-02-2000 in 
order to assure the continued airworthiness of these airplanes in the 
United Kingdom.

FAA's Conclusions

    This airplane model is manufactured in the United Kingdom and is 
type certificated for operation in the United States under the 
provisions of Sec. 21.29 of the Federal Aviation Regulations (14 CFR 
21.19) and the applicable bilateral airworthiness agreement. Pursuant 
to this bilateral airworthiness agreement, the CAA has kept the FAA 
informed of the situation described above. The FAA has examined the 
findings of the CAA, reviewed all available information, and determined 
that AD action is necessary for products of this type design that are 
certificated for operation in the United States.

Explanation of Requirements of the Rule

    Since an unsafe condition has been identified that is likely to 
exist or develop on other airplanes of the same type design registered 
in the United States, this AD is being issued to prevent separation of 
the top and bottom torque links, and consequent loss of directional 
control of the MLG. This AD requires accomplishment of the actions 
specified in the service bulletins described previously.

Cost Impact

    None of the BAe Model ATP airplanes affected by this action are on 
the U.S. Register. All airplanes included in the applicability of this 
rule currently are operated by non-U.S. operators under foreign 
registry; therefore, they are not directly affected by this AD action. 
However, the FAA considers that this rule is necessary to ensure that 
the unsafe condition is addressed in the event that any of these 
subject airplanes are imported and placed on the U.S. Register in the 
future.
    Should an affected airplane be imported and placed on the U.S. 
Register in the future, it would require approximately 2 work hours to 
accomplish the required actions, at an average labor rate of $60 per 
work hour. Based on these figures, the cost impact of this AD would be 
$120 per airplane.

Determination of Rule's Effective Date

    Since this AD action does not affect any airplane that is currently 
on the U.S. register, it has no adverse economic impact and imposes no 
additional burden on any person. Therefore, prior notice and public 
procedures hereon are unnecessary and the amendment may be made 
effective in less than 30 days after publication in the Federal 
Register. 

Comments Invited

    Although this action is in the form of a final rule and was not 
preceded by notice and opportunity for public comment, comments are 
invited on this rule. Interested persons are invited to comment on this 
rule by submitting such written data, views, or arguments as they may 
desire. Communications shall identify the Rules Docket number and be 
submitted in triplicate to the address specified under the caption 
ADDRESSES. All communications received on or before the closing date 
for comments will be considered, and this rule may be amended in light 
of the comments received. Factual information that supports the 
commenter's ideas and suggestions is extremely helpful in evaluating 
the effectiveness of the AD action and determining whether additional 
rulemaking action would be needed.
    Submit comments using the following format:
    <bullet> Organize comments issue-by-issue. For example, discuss a 
request to change the compliance time and a request to change the 
service bulletin reference as two separate issues.
    <bullet> For each issue, state what specific change to the AD is 
being requested.
    <bullet> Include justification (e.g., reasons or data) for each 
request.
    Comments are specifically invited on the overall regulatory, 
economic, environmental, and energy aspects of the rule that might 
suggest a need to modify the rule. All comments submitted will be 
available, both before and after the closing date for comments, in the 
Rules Docket for examination by interested persons. A report that 
summarizes each FAA-public contact concerned with the substance of this 
AD will be filed in the Rules Docket.
    Commenters wishing the FAA to acknowledge receipt of their comments 
submitted in response to this rule must submit a self-addressed, 
stamped postcard on which the following statement is made: ``Comments 
to Docket Number 2000-NM-123-AD.'' The postcard will be date stamped 
and returned to the commenter.

[[Page 63001]]

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:

2000-21-05  British Aerospace Regional Aircraft [Formerly Jetstream 
Aircraft Limited; British Aerospace (Commercial Aircraft) Limited]: 
Amendment 39-11937. Docket 2000-NM-123-AD.

    Applicability: All BAe Model ATP airplanes, certificated in any 
category.

    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 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 separation of the top and bottom torque links, and 
consequent loss of directional control of the main landing gear 
(MLG), accomplish the following:

Inspection

    (a) Within 800 landings or 4 months after the effective date of 
this AD, whichever occurs first: Perform an inspection to detect 
damage of the torque link apex joint of the left- and right-hand 
MLG, in accordance with British Aerospace Service Bulletin ATP-32-
99, dated February 21, 2000, and Messier-Dowty Service Bulletin 200-
32-263, including Appendix A, dated February 1, 2000. If any damage 
exceeds the limit specified in the Messier-Dowty service bulletin, 
prior to further flight, replace the nut, bolt, and pin with new 
parts, as applicable, in accordance with that service bulletin. 
Repeat the inspection thereafter at intervals not to exceed 1,000 
landings.

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 
Secs. 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 actions shall be done in accordance with British 
Aerospace Service
    Bulletin ATP-32-99, dated February 21, 2000, and Messier-Dowty 
Service Bulletin 200-32-263, including Appendix A, dated February 1, 
2000. 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 008-02-2000.

Effective Date

    (e) This amendment becomes effective on November 6, 2000.

    Issued in Renton, Washington, on October 12, 2000.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 00-26710 Filed 10-19-00; 8:45 am]
BILLING CODE 4910-13-P


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