[Federal Register Volume 65, Number 21 (Tuesday, February 1, 2000)]
[Proposed Rules]
[Pages 4786-4788]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-2006]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NM-266-AD]
RIN 2120-AA64


Airworthiness Directives; McDonnell Douglas Model MD-11 Series 
Airplanes

AGENCY:  Federal Aviation Administration, DOT.

ACTION:  Notice of proposed rulemaking (NPRM).

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SUMMARY:  This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to certain McDonnell Douglas Model 
MD-11 series airplanes. This proposal would require a general visual 
inspection to verify that the circuit breaker panel fully opens, 
follow-on inspections, and corrective actions, if necessary. This 
proposal is prompted by an incident of an operator not being able to 
fully open the observer's upper main circuit breaker panel due to a 
certain cable being too short. The actions specified by the proposed AD 
are intended to ensure that the upper main circuit breaker panel opens 
fully. If the panel does not open fully, maintenance activities may be 
hindered and cause damage to the circuit breaker panel and wiring, 
which could result in electrical arcing and consequent smoke and fire 
in the flight compartment.

DATES:  Comments must be received by March 17, 2000.

ADDRESSES:  Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Transport Airplane Directorate, ANM-114, 
Attention: Rules Docket No. 99-NM-266-AD, 1601 Lind Avenue, SW., 
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.
    The service information referenced in the proposed rule may be 
obtained from Boeing Commercial Aircraft Group, Long Beach Division, 
3855 Lakewood Boulevard, Long Beach, California 90846, Attention: 
Technical Publications Business Administration, Dept. C1-L51 (2-60). 
This information may be examined at the FAA, Transport Airplane 
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, 
Transport Airplane Directorate, Los Angeles Aircraft Certification 
Office, 3960 Paramount Boulevard, Lakewood, California.

FOR FURTHER INFORMATION CONTACT:  Brett Portwood, Aerospace Engineer, 
Systems and Equipment Branch, ANM-130L, FAA, Transport Airplane 
Directorate, Los Angeles Aircraft Certification Office, 3960 Paramount 
Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5350; 
fax (562) 627-5210.

SUPPLEMENTARY INFORMATION:

Comments Invited

    Interested persons are invited to participate in the making of the 
proposed 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 above. All 
communications received on or before the closing date for comments, 
specified above, will be considered before taking action on the 
proposed rule. The proposals contained in this notice may be changed in 
light of the comments received.
    Comments are specifically invited on the overall regulatory, 
economic, environmental, and energy aspects of the proposed 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 summarizing each FAA-public contact concerned with 
the substance of this proposal will be filed in the Rules Docket.
    Commenters wishing the FAA to acknowledge receipt of their comments 
submitted in response to this notice must submit a self-addressed, 
stamped postcard on which the following statement is made: ``Comments 
to Docket Number 99-NM-266-AD.'' The postcard will be date stamped and 
returned to the commenter.

Availability of NPRMs

    Any person may obtain a copy of this NPRM by submitting a request 
to the

[[Page 4787]]

FAA, Transport Airplane Directorate, ANM-114, Attention: Rules Docket 
No. 99-NM-266-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056.

Supplementary Information

    As part of its practice of re-examining all aspects of the service 
experience of a particular aircraft whenever an accident occurs, the 
FAA has become aware of an instance of an operator not being able to 
fully open the observer's upper main circuit breaker panel of a 
McDonnell Douglas Model MD-11 series airplane. Investigation revealed 
that a direct current (DC) power feeder bus cable was found to be too 
short, which prevented the panel from being fully opened. If the panel 
cannot be opened, maintenance activities may be hindered and cause 
damage to the circuit breaker panel and wiring. Such damage could 
result in electrical arcing and consequent smoke and fire in the flight 
compartment.
    This incident is not considered to be related to an accident that 
occurred off the coast of Nova Scotia involving a McDonnell Douglas 
Model MD-11 series airplane. The cause of that accident is still under 
investigation.

Other Relevant Rulemaking

    The FAA, in conjunction with Boeing and operators of Model MD-11 
series airplanes, is continuing to review all aspects of the service 
history of those airplanes to identify potential unsafe conditions and 
to take appropriate corrective actions. This proposed airworthiness 
directive (AD) is one of a series of actions identified during that 
process. The process is continuing and the FAA may consider additional 
rulemaking actions as further results of the review become available.

Explanation of Relevant Service Information

    The FAA has reviewed and approved McDonnell Douglas Alert Service 
Bulletin MD11-24A130, Revision 01, dated September 20, 1999, which 
describes procedures for a general visual inspection to verify that the 
circuit breaker panel fully opens, follow-on inspections, and 
corrective actions, if necessary. The follow-on inspections involve a 
detailed visual inspection of the wires between circuit breakers B1-213 
and B1-300 to terminal strip S3-602 to detect chafing damage; and a 
detailed visual inspection of the route path of the subject area to 
detect chafing damage and to determine if the wire can be adjusted or 
if the wire must be replaced; as applicable. The corrective actions 
include adjusting the wire, replacing the wire with a new wire, and 
repairing chafing damage. Accomplishment of the actions specified in 
the service bulletin is intended to adequately address the identified 
unsafe condition.

Explanation of Requirements of Proposed Rule

    Since an unsafe condition has been identified that is likely to 
exist or develop on other products of this same type design, this 
proposed AD would require accomplishment of the actions specified in 
the service bulletin described previously.

Cost Impact

    There are approximately 161 airplanes of the affected design in the 
worldwide fleet. The FAA estimates that 66 airplanes of U.S. registry 
would be affected by this proposed AD, that it would take approximately 
1 work hour per airplane to accomplish the proposed inspections, and 
that the average labor rate is $60 per work hour. Based on these 
figures, the cost impact of the proposed AD on U.S. operators is 
estimated to be $3,960, or $60 per airplane.
    The cost impact figure discussed above is based on assumptions that 
no operator has yet accomplished any of the proposed requirements of 
this AD action, and that no operator would accomplish those actions in 
the future if this AD were not adopted.

Regulatory Impact

    The regulations proposed herein would 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 proposal would not have federalism implications 
under Executive Order 13132.
    For the reasons discussed above, I certify that this proposed 
regulation (1) is not a ``significant regulatory action'' under 
Executive Order 12866; (2) is not a ``significant rule'' under the DOT 
Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 
and (3) if promulgated, 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 copy of the draft 
regulatory evaluation prepared for this action is contained in the 
Rules Docket. A copy of it may be obtained by contacting the Rules 
Docket at the location provided under the caption ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration proposes to amend 
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:

McDonnell Douglas: Docket 99-NM-266-AD.

    Applicability: Model MD-11 series airplanes, as listed in 
McDonnell Douglas Alert Service Bulletin MD11-24A130, Revision 01, 
dated September 20, 1999; 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 (e) 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 ensure that the upper main circuit breaker panel opens fully, 
accomplish the following:

Inspection and a Follow-On Inspection

    (a) Within 6 months after the effective date of this AD, perform 
a general visual inspection to verify that the circuit breaker panel 
fully opens in accordance with McDonnell Douglas Alert Service 
Bulletin MD11-24A130, Revision 01, dated September 20, 1999.


    Note 2:  For the purposes of this AD, a general visual 
inspection is defined as ``A visual examination of an interior or 
exterior area, installation, or assembly to detect obvious damage, 
failure, or irregularity. This level of inspection is made under 
normally available lighting conditions such as daylight, hangar 
lighting, flashlight, or drop-light, and may require removal or 
opening of access panels or doors. Stands, ladders, or platforms may 
be required to gain proximity to the area being checked.''



[[Page 4788]]


    (1) If the circuit breaker panel fully opens, prior to further 
flight, perform a detailed visual inspection of the wires between 
circuit breakers B1-213 and B1-300 to terminal strip S3-602 to 
detect chafing damage, in accordance with the service bulletin.
    (2) If the circuit breaker panel does not fully open, prior to 
further flight, perform a detailed visual inspection of the route 
path from circuit breakers B1-213 and B1-300 to terminal strip S3-
602 to detect chafing damage and to determine if the wire can be 
adjusted or if the wire must be replaced, in accordance with the 
service bulletin.

    Note 3:  For the purposes of this AD, a detailed visual 
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.''

Corrective Actions

    (b) If any wire is found to need adjusting during the inspection 
required by paragraph (a)(2) of this AD, prior to further flight, 
adjust the wire in accordance with McDonnell Douglas Alert Service 
Bulletin MD11-24A130, Revision 01, dated September 20, 1999.
    (c) If any wire is found to need replacing during the inspection 
required by paragraph (a)(2) of this AD, prior to further flight, 
replace the wire with a new wire in accordance with McDonnell 
Douglas Alert Service Bulletin MD11-24A130, Revision 01, dated 
September 20, 1999.
    (d) If any chafing damage is found during the inspection 
required by paragraph (a)(1) or (a)(2) of this AD, prior to further 
flight, repair in accordance with McDonnell Douglas Alert Service 
Bulletin MD11-24A130, Revision 01, dated September 20, 1999.

Alternative Methods of Compliance

    (e) 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, Los Angeles Aircraft Certification 
Office (ACO), 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, Los Angeles ACO.

    Note 4:  Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Los Angeles ACO.

Special Flight Permits

    (f) 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.

    Issued in Renton, Washington, on January 21, 2000.
Vi L. Lipski,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 00-2006 Filed 1-31-00; 8:45 am]
BILLING CODE 4910-13-U