Airworthiness Directives; Boeing Model 767-300 Series Airplanes Modified by Supplemental Type Certificate ST00118SE

[Federal Register Volume 66, Number 135 (Friday, July 13, 2001)]
[Rules and Regulations]
[Pages 36699-36700]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-17157]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000-NM-236-AD; Amendment 39-12314; AD 2001-14-04]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 767-300 Series Airplanes 
Modified by Supplemental Type Certificate ST00118SE

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: This amendment adopts a new airworthiness directive (AD), 
applicable to all Boeing Model 767-300 series airplanes modified by 
Supplemental Type Certificate ST00118SE, that requires modification of 
the in-flight entertainment (IFE) system and revision of the Airplane 
Flight Manual. This action is necessary to ensure that the flight crew 
is able to remove electrical power from the IFE system when necessary 
and is advised of appropriate procedures for such action. Inability to 
remove power from the IFE system during a non-normal or emergency 
situation could result in inability to control smoke or fumes in the 
airplane flight deck or cabin. This action is intended to address the 
identified unsafe condition.

DATES: Effective August 17, 2001.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of August 17, 2001.

ADDRESSES: The service information referenced in this AD may be 
obtained from Matsushita Avionics System Corporation, 22333 29th Drive 
SE, Bothell, Washington 98021. 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: Stephen S. Oshiro, Aerospace Engineer, 
Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft 
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-
4056; telephone (425) 227-2793; fax (425) 227-1181.

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 all Boeing Model 767-300 series 
airplanes modified by Supplemental Type Certificate (STC) ST00118SE was 
published in the Federal Register on March 29, 2001 (66 FR 17115). That 
action proposed to require modification of the in-flight entertainment 
(IFE) system and revision of the Airplane Flight Manual (AFM).

Comments

    Interested persons have been afforded an opportunity to participate 
in the making of this amendment. No comments were submitted in response 
to the proposal or the FAA's determination of the cost to the public.

Conclusion

    After careful review of the available data, the FAA has determined 
that air safety and the public interest require the adoption of the 
rule as proposed.

Cost Impact

    There are approximately 20 Model 767-300 series airplanes modified 
by STC ST00118SE in the worldwide fleet. The FAA estimates that no 
airplanes of U.S. registry will be affected by this AD. All airplanes 
included in the applicability of this AD currently are operated by non-
U.S. operators under foreign registry; therefore, they are not directly 
affected by this AD. However, the FAA considers that this AD 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 will take approximately 50 work hours per 
airplane to accomplish the required modification, at an average labor 
rate of $60 per work hour. Required parts will be provided at no charge 
to the operator. Based on these figures, the cost impact of the 
required modification will be $3,000 per airplane.
    Should an affected airplane be imported and placed on the U.S. 
Register in the future, it will take approximately 1 work hour per 
airplane to accomplish the required AFM revision, at an average labor 
rate of $60 per work hour. Based on these figures, the cost impact of 
the required AFM revision will be $60 per airplane.
    The cost impact figures discussed above are 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.

[[Page 36700]]

Sec. 39.13  [Amended]

    2. Section 39.13 is amended by adding the following new 
airworthiness directive:

2001-14-04  Boeing: Amendment 39-12314. Docket 2000-NM-236-AD.

    Applicability: Model 767-300 series airplanes modified by 
Supplemental Type Certificate (STC) ST00118SE; certificated in any 
category.

    Note 1: This AD applies to each airplane identified in the 
preceding applicability provision, regardless of whether it has been 
otherwise 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 (c) 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 flight crew is able to remove electrical 
power from the in-flight entertainment (IFE) system when necessary 
and is advised of appropriate procedures for such action; accomplish 
the following:

Modification and Airplane Flight Manual Revision

    (a) Within 18 months after the effective date of this AD, 
accomplish paragraphs (a)(1) and (a)(2) of this AD.
    (1) Modify the IFE system installed on the airplane in 
accordance with Matsushita Avionics Systems Corporation Service 
Bulletin S2GFAB767-23-1, dated February 7, 2001.
    (2) Revise the procedures under ``Electrical Smoke or Fire'' in 
the ``Emergency Procedures'' section of the FAA-approved Airplane 
Flight Manual (AFM) to include the following information. This may 
be accomplished by inserting a copy of this AD into the AFM.

``If Smoke Source Cannot Be Located:

Utility bus switches--Off

    Establish communications with cabin crew.
    Instruct cabin crew to place in-flight entertainment (IFE) 
system Master Power Switch in ``OFF'' position.
    Obtain confirmation from cabin crew that electrical power to the 
IFE system has been removed.''

Spares

    (b) As of the effective date of this AD, no person shall install 
an IFE system in accordance with STC ST00118SE on any airplane, 
unless it is modified and the AFM is revised in accordance with this 
AD.

Alternative Methods of Compliance

    (c) 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, Seattle Aircraft Certification 
Office (ACO), FAA. Operators shall submit their requests through an 
appropriate FAA Principal Maintenance Inspector, who may add 
comments and then send it to the Manager, Seattle ACO.

    Note 2: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Seattle ACO.

Special Flight Permits

    (d) 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

    (e) The modification shall be done in accordance with Matsushita 
Avionics Systems Corporation Service Bulletin S2GFAB767-23-1, dated 
February 7, 2001. 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 Matsushita 
Avionics Systems Corporation, 22333 29th Drive SE, Bothell, 
Washington 98021. 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.

Effective Date

    (f) This amendment becomes effective on August 17, 2001.

    Issued in Renton, Washington, on June 29, 2001.
Vi L. Lipski,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 01-17157 Filed 7-12-01; 8:45 am]
BILLING CODE 4910-13-U

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:28:02.406428+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256

7067fbebb1157d6b48362bc99f5563e6920f69846fc15079853fe7316570e800

Text SHA-256

9d4ef93ee8d19651954683832fca382fee88b002daffe9cb4fb92d1212a8a6e5