[Federal Register: December 2, 2008 (Volume 73, Number 232)]
[Rules and Regulations]
[Page 73168-73169]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr02de08-4]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-1241; Directorate Identifier 2008-NM-121-AD;
Amendment 39-15754; AD 2006-20-51 R1]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 777-200LR Series Airplanes
Powered by General Electric (GE) Model GE90-110B Engines, and Model
777-300ER Series Airplanes Powered by GE Model GE90-115B Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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SUMMARY: We are revising an existing airworthiness directive (AD) that
applies to certain Boeing Model 777-200LR and -300ER series airplanes.
That AD currently requires revising the airplane flight manual to
prohibit takeoffs at less than full-rated thrust. This new AD reduces
the applicability of the existing AD. This AD results from a report of
two occurrences of engine thrust rollback during takeoff. We are
issuing this AD to prevent dual-engine thrust rollback during the
takeoff phase of flight, which could result in the airplane failing to
lift off before reaching the end of the runway or failing to clear
obstacles below the takeoff flight path.
DATES: This AD is effective January 6, 2009.
We must receive comments on this AD by February 2, 2009.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
Examining the AD Docket
You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone 800-647-5527) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Margaret Langsted, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6500; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION:
Discussion
On October 2, 2006, we issued AD 2006-20-51, amendment 39-14786 (71
FR 59651, October 11, 2006), for certain Boeing Model 777-200LR and -
300ER series airplanes. That AD requires revising the airplane flight
manual to prohibit takeoffs at less than full-rated thrust. That AD
resulted from a report of two occurrences of engine thrust rollback
(reduction) during takeoff. We issued that AD to prevent dual-engine
thrust rollback, which could result in the airplane failing to lift off
before reaching the end of the runway or failing to clear obstacles
below the takeoff flight path.
Actions Since Existing AD Was Issued
Since issuance of AD 2006-20-51, Boeing has informed us that no
U.S.-registered airplanes have full authority digital engine control
(FADEC) software version A.0.4.5 installed, and that software version
A.0.4.6 is being installed in production. In addition, we have
determined that the affected airplanes are limited to those subject to
the identified unsafe condition with FADEC electronic engine control
(EEC) software version A.0.4.5 installed. We have also determined that
FADEC software version A.0.4.6 has incorporated software revisions that
prevent the reported roll-back conditions from occurring. Therefore, we
also have determined that the applicability of AD 2006-20-51 can be
revised to apply only to affected airplanes equipped with FADEC
software version A.0.4.5.
FAA's Determination and Requirements of This AD
No airplanes affected by this AD are on the U.S. Register. We are
issuing this AD because the unsafe condition described previously is
likely to exist or develop on other products of the(se) same type
design(s) that could be registered in the United States in the future.
This AD revises AD 2006-20-51. This AD retains the requirements of the
existing AD and reduces the applicability of the existing AD.
Since no U.S. registered airplanes are affected by this AD, notice
and opportunity for public comment before issuing this AD are
unnecessary.
Interim Action
We consider the requirements of this AD ``interim action.'' The
manufacturer is developing a modification to address the unsafe
condition (i.e., decreased takeoff thrust). We might consider further
rulemaking if a modification is developed, approved, and available.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2008-1241; Directorate Identifier 2008-NM-121-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this AD because of those comments.
We will post all comments we receive, without change, to http://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
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
[[Page 73169]]
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
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.
You can find our regulatory evaluation and the estimated costs of
compliance in the AD docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, 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 removing amendment 39-14786 (71 FR
59651, October 11, 2006) and adding the following new AD:
2006-20-51-R1 Boeing: Amendment 39-15754. Docket No. FAA-2008-1241;
Directorate Identifier 2008-NM-121-AD.
Effective Date
(a) This airworthiness directive (AD) is effective January 6,
2009.
Affected ADs
(b) This AD revises AD 2006-20-51.
Applicability
(c) This AD applies to airplanes in Table 1 of this AD,
certificated in any category.
Table 1--Applicability
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Equipped with full
Powered by General authority digital
Boeing model-- Electric (GE) engine control
model-- software version--
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(1) 777-200LR series airplanes.. GE90-110B engines. A.0.4.5
(2) 777-300ER series airplanes.. GE90-115B engines. A.0.4.5
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Unsafe Condition
(d) This AD results from a report of two occurrences of engine
thrust rollback during takeoff. We are issuing this AD to prevent
dual-engine thrust rollback during the takeoff phase of flight,
which could result in the airplane failing to lift off before
reaching the end of the runway or failing to clear obstacles below
the takeoff flight path.
Compliance
(e) Comply with this AD within the compliance times specified,
unless already done.
Restatement of AD 2006-20-51:
Revision of the Airplane Flight Manual (AFM)
(f) Within 24 hours after October 16, 2006 (the effective date
of 2006-20-51), revise the Certificate Limitations Section of the
AFM to include the following statement. This may be done by
inserting a copy of this AD into the AFM.
Use of reduced thrust takeoff ratings determined by either the
assumed temperature method or the fixed de-rate method or a
combination of both, is prohibited. Full-rated thrust must be used
for takeoff.
Note 1: When a statement identical to that in paragraph (f) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
Special Flight Permit
(g) Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, Seattle Aircraft Certification Office (ACO),
FAA, ATTN: Margaret Langsted, Aerospace Engineer, Propulsion Branch,
ANM-140S, FAA, Seattle ACO, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6500; fax (425) 917-6590;
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local
FSDO.
Material Incorporated by Reference
(i) None.
Issued in Renton, Washington, on November 16, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E8-28158 Filed 12-1-08; 8:45 am]
BILLING CODE 4910-13-P